SHUTTLE Columbia STS-107 TRAJECTORY DATA
17-01-2003
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03017.77182080 .00041100 00000-0 34010-3 0 9016
2 27647 39.0160 221.7493 0012102 358.3911 1.7025 15.97715753 196
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18-01-2003
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03018.77172105 .00041100 00000-0 34010-3 0 9025
2 27647 39.0163 215.0830 0011918 6.9480 353.1660 15.97847721 359
19-01-2003
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03019.77152485 .00041100 00000-0 34010-3 0 9036
2 27647 39.0166 208.4159 0011803 16.0053 344.1295 15.98059388 510
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2003/016/15:38:59.958
Area (sq ft) : 1208.48
Drag Coefficient (Cd) : 2.36
90 day mean solar flux (jansky) : 172.4
12 month mean earth geomagnetic index : 2.35
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
026/17:16:36.000 0.0 0.0 0.0
010/01:37:36.043 0.0 0.0 152.8
000/00:00:00.000 0.0 0.0 139.8
Coasting Arc #1 (begining on orbit 2)
---------------------------------------
Vector Time (GMT): 2003/016/17:16:36.000
Vector Time (MET): 000/01:37:36.042
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1209249.02 A = 6660036.09 meter
Y = -5428668.54 meter E = .0015062
Z = 3647326.62 I = 38.78606
XDOT = 6714.931671 Wp = 35.40516
YDOT = 3067.248480 meter/sec RA = 227.86682 deg
ZDOT = 2348.199160 TA = 25.69197
MA = 25.61722
Ha = 156.025 n.mi
Hp = 146.717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3967352.43 X = 1252123.56
Y = -17810592.32 feet Y = -5414910.27 meter
Z = 11966294.68 Z = 3653306.74
XDOT = 22030.615719 XDOT = 6668.734315
YDOT = 10063.151182 feet/sec YDOT = 3142.058841 meter/sec
ZDOT = 7704.065487 ZDOT = 2380.716018
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03016.77183602 .00041100 00000-0 34010-3 0 9005
2 27647 39.0158 228.4149 0012304 349.9852 10.0878 15.97528178 34
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03016.77183602 = yrday.fracday
Element set: 900
Inclination: 39.0158 deg
RA of node: 228.4149 deg
Eccentricity: .0012304
Arg of perigee: 349.9852 deg
Mean anomaly: 10.0878 deg
Mean motion: 15.97528178 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 3
Checksum: 299
Coasting Arc #2 (begining on orbit 18)
---------------------------------------
Vector Time (GMT): 2003/017/17:19:23.877
Vector Time (MET): 001/01:40:23.920
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1738656.16 A = 6658387.14 meter
Y = -5041801.39 meter E = .0014663
Z = 3972951.25 I = 38.80466
XDOT = 6762.112350 Wp = 37.88184
YDOT = 3481.729540 meter/sec RA = 221.14954 deg
ZDOT = 1469.934425 TA = 34.54005
MA = 34.44487
Ha = 155.947 n.mi
Hp = 146.092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5704252.50 X = 1775584.39
Y = -16541343.15 feet Y = -5022157.93 meter
Z = 13034616.98 Z = 3981489.41
XDOT = 22185.407971 XDOT = 6715.545522
YDOT = 11422.997177 feet/sec YDOT = 3557.065286 meter/sec
ZDOT = 4822.619503 ZDOT = 1502.679645
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03017.77182080 .00041100 00000-0 34010-3 0 9016
2 27647 39.0160 221.7493 0012102 358.3911 1.7025 15.97715753 196
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03017.77182080 = yrday.fracday
Element set: 901
Inclination: 39.0160 deg
RA of node: 221.7493 deg
Eccentricity: .0012102
Arg of perigee: 358.3911 deg
Mean anomaly: 1.7025 deg
Mean motion: 15.97715753 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 19
Checksum: 272
Coasting Arc #3 (begining on orbit 34)
---------------------------------------
Vector Time (GMT): 2003/018/17:21:37.877
Vector Time (MET): 002/01:42:37.919
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2135601.59 A = 6657444.17 meter
Y = -4755416.78 meter E = .0015095
Z = 4128660.45 I = 38.82891
XDOT = 6805.128415 Wp = 40.93343
YDOT = 3637.861705 meter/sec RA = 214.43636 deg
ZDOT = 682.427078 TA = 41.04644
MA = 40.93295
Ha = 155.936 n.mi
Hp = 145.554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7006566.90 X = 2168542.27
Y = -15601761.09 feet Y = -4731358.02 meter
Z = 13545473.93 Z = 4139117.76
XDOT = 22326.536795 XDOT = 6760.639501
YDOT = 11935.241813 feet/sec YDOT = 3713.689960 meter/sec
ZDOT = 2238.933984 ZDOT = 715.386370
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03018.77172105 .00041100 00000-0 34010-3 0 9025
2 27647 39.0163 215.0830 0011918 6.9480 353.1660 15.97847721 359
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03018.77172105 = yrday.fracday
Element set: 902
Inclination: 39.0163 deg
RA of node: 215.0830 deg
Eccentricity: .0011918
Arg of perigee: 6.9480 deg
Mean anomaly: 353.1660 deg
Mean motion: 15.97847721 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 35
Checksum: 284
Coasting Arc #4 (begining on orbit 50)
---------------------------------------
Vector Time (GMT): 2003/019/17:23:44.690
Vector Time (MET): 003/01:44:44.733
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2572233.95 A = 6656692.44 meter
Y = -4495240.79 meter E = .0016111
Z = 4170053.41 I = 38.85768
XDOT = 6779.876908 Wp = 45.25732
YDOT = 3745.605868 meter/sec RA = 207.72533 deg
ZDOT = -129.988129 TA = 46.34195
MA = 46.20850
Ha = 155.813 n.mi
Hp = 144.878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8439087.76 X = 2602032.57
Y = -14748165.31 feet Y = -4466318.32 meter
Z = 13681277.59 Z = 4182624.76
XDOT = 22243.690642 XDOT = 6738.132933
YDOT = 12288.733163 feet/sec YDOT = 3821.167173 meter/sec
ZDOT = -426.470240 ZDOT = -97.144870
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03019.77152485 .00041100 00000-0 34010-3 0 9036
2 27647 39.0166 208.4159 0011803 16.0053 344.1295 15.98059388 510
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03019.77152485 = yrday.fracday
Element set: 903
Inclination: 39.0166 deg
RA of node: 208.4159 deg
Eccentricity: .0011803
Arg of perigee: 16.0053 deg
Mean anomaly: 344.1295 deg
Mean motion: 15.98059388 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 51
Checksum: 296
Coasting Arc #5 (begining on orbit 66)
---------------------------------------
Vector Time (GMT): 2003/020/17:25:56.442
Vector Time (MET): 004/01:46:56.484
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3172002.01 A = 6656028.54 meter
Y = -4190203.63 meter E = .0017492
Z = 4072720.58 I = 38.89104
XDOT = 6586.391077 Wp = 51.01248
YDOT = 3938.395318 meter/sec RA = 201.01401 deg
ZDOT = -1060.415974 TA = 51.65870
MA = 51.50162
Ha = 155.407 n.mi
Hp = 144.035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10406830.75 X = 3198819.02
Y = -13747387.25 feet Y = -4154592.81 meter
Z = 13361944.14 Z = 4088199.06
XDOT = 21608.894611 XDOT = 6547.027249
YDOT = 12921.244482 feet/sec YDOT = 4011.806883 meter/sec
ZDOT = -3479.055034 ZDOT = -1028.507115
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03020.77112902 .00041100 00000-0 34010-3 0 9049
2 27647 39.0169 201.7472 0011658 24.4296 335.7231 15.98424843 672
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03020.77112902 = yrday.fracday
Element set: 904
Inclination: 39.0169 deg
RA of node: 201.7472 deg
Eccentricity: .0011658
Arg of perigee: 24.4296 deg
Mean anomaly: 335.7231 deg
Mean motion: 15.98424843 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 67
Checksum: 291
Coasting Arc #6 (begining on orbit 82)
---------------------------------------
Vector Time (GMT): 2003/021/17:27:46.369
Vector Time (MET): 005/01:48:46.412
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3753821.12 A = 6655858.03 meter
Y = -3932484.12 meter E = .0019134
Z = 3827128.96 I = 38.92853
XDOT = 6286.873078 Wp = 58.85414
YDOT = 4088.154080 meter/sec RA = 194.30763 deg
ZDOT = -1944.740034 TA = 54.78199
MA = 54.60302
Ha = 154.994 n.mi
Hp = 143.186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12315686.09 X = 3778907.20
Y = -12901850.80 feet Y = -3890378.62 meter
Z = 12556197.37 Z = 3845430.41
XDOT = 20626.224010 XDOT = 6250.154291
YDOT = 13412.579001 feet/sec YDOT = 4158.232014 meter/sec
ZDOT = -6380.380690 ZDOT = -1914.280161
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03021.77049829 .00041100 00000-0 34010-3 0 9058
2 27647 39.0171 195.0764 0011585 32.9566 327.2131 15.98798581 833
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03021.77049829 = yrday.fracday
Element set: 905
Inclination: 39.0171 deg
RA of node: 195.0764 deg
Eccentricity: .0011585
Arg of perigee: 32.9566 deg
Mean anomaly: 327.2131 deg
Mean motion: 15.98798581 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 83
Checksum: 321
Coasting Arc #7 (begining on orbit 98)
---------------------------------------
Vector Time (GMT): 2003/022/17:29:57.335
Vector Time (MET): 006/01:50:57.377
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4535531.54 A = 6656718.38 meter
Y = -3544927.93 meter E = .0020861
Z = 3327895.65 I = 38.97081
XDOT = 5637.360927 Wp = 69.73184
YDOT = 4423.708080 meter/sec RA = 187.60358 deg
ZDOT = -2943.642998 TA = 57.53814
MA = 57.33661
Ha = 154.721 n.mi
Hp = 142.525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14880352.81 X = 4558652.86
Y = -11630340.98 feet Y = -3494094.39 meter
Z = 10918292.82 Z = 3349990.80
XDOT = 18495.278632 XDOT = 5601.792930
YDOT = 14513.477954 feet/sec YDOT = 4486.531324 meter/sec
ZDOT = -9657.621386 ZDOT = -2916.336428
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03022.76965046 .00041100 00000-0 34010-3 0 9067
2 27647 39.0172 188.4039 0011514 41.5523 318.6328 15.99067546 996
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03022.76965046 = yrday.fracday
Element set: 906
Inclination: 39.0172 deg
RA of node: 188.4039 deg
Eccentricity: .0011514
Arg of perigee: 41.5523 deg
Mean anomaly: 318.6328 deg
Mean motion: 15.99067546 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 99
Checksum: 313
Coasting Arc #8 (begining on orbit 114)
---------------------------------------
Vector Time (GMT): 2003/023/17:31:18.422
Vector Time (MET): 007/01:52:18.465
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5036605.81 A = 6657243.99 meter
Y = -3341471.22 meter E = .0021994
Z = 2771747.38 I = 39.01300
XDOT = 5068.286179 Wp = 80.51006
YDOT = 4584.451713 meter/sec RA = 180.91224 deg
ZDOT = -3648.294867 TA = 58.02391
MA = 57.81031
Ha = 154.286 n.mi
Hp = 141.767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16524297.28 X = 5060117.80
Y = -10962832.07 feet Y = -3285033.80 meter
Z = 9093659.39 Z = 2796278.29
XDOT = 16628.235494 XDOT = 5034.387422
YDOT = 15040.852076 feet/sec YDOT = 4640.922400 meter/sec
ZDOT = -11969.471348 ZDOT = -3623.749479
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03023.76863154 .00041100 00000-0 34010-3 0 9076
2 27647 39.0171 181.7297 0011444 50.1504 310.0479 15.99430566 1152
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03023.76863154 = yrday.fracday
Element set: 907
Inclination: 39.0171 deg
RA of node: 181.7297 deg
Eccentricity: .0011444
Arg of perigee: 50.1504 deg
Mean anomaly: 310.0479 deg
Mean motion: 15.99430566 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 115
Checksum: 288
Coasting Arc #9 (begining on orbit 130)
---------------------------------------
Vector Time (GMT): 2003/024/17:33:27.469
Vector Time (MET): 008/01:54:27.511
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5739846.17 A = 6658248.12 meter
Y = -2827720.28 meter E = .0022232
Z = 1814351.46 I = 39.05759
XDOT = 3894.856826 Wp = 94.25364
YDOT = 5050.625281 meter/sec RA = 174.22620 deg
ZDOT = -4395.484657 TA = 60.09165
MA = 59.87100
Ha = 153.859 n.mi
Hp = 141.052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18831516.30 X = 5762214.71
Y = -9277297.51 feet Y = -2763427.48 meter
Z = 5952596.66 Z = 1842296.77
XDOT = 12778.401659 XDOT = 3859.464518
YDOT = 16570.292917 feet/sec YDOT = 5093.969441 meter/sec
ZDOT = -14420.881419 ZDOT = -4376.644806
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03024.76737801 .00041100 00000-0 34010-3 0 9087
2 27647 39.0169 175.0532 0011412 58.6823 301.5270 15.99786928 1317
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03024.76737801 = yrday.fracday
Element set: 908
Inclination: 39.0169 deg
RA of node: 175.0532 deg
Eccentricity: .0011412
Arg of perigee: 58.6823 deg
Mean anomaly: 301.5270 deg
Mean motion: 15.99786928 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 131
Checksum: 304
Coasting Arc #10 (begining on orbit 146)
---------------------------------------
Vector Time (GMT): 2003/025/17:35:04.564
Vector Time (MET): 009/01:56:04.606
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6177817.79 A = 6658466.09 meter
Y = -2341444.86 meter E = .0021172
Z = 775707.24 I = 39.09779
XDOT = 2685.295989 Wp = 106.39536
YDOT = 5453.993948 meter/sec RA = 167.55051 deg
ZDOT = -4798.196461 TA = 62.94882
MA = 62.73290
Ha = 153.405 n.mi
Hp = 140.366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20268431.06 X = 6199764.53
Y = -7681905.70 feet Y = -2272258.17 meter
Z = 2544971.25 Z = 805779.71
XDOT = 8810.026211 XDOT = 2647.441087
YDOT = 17893.680931 feet/sec YDOT = 5483.802235 meter/sec
ZDOT = -15742.114372 ZDOT = -4785.240072
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03025.76589299 .00041100 00000-0 34010-3 0 9095
2 27647 39.0167 168.3745 0011407 67.2924 292.9258 16.00153514 1476
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03025.76589299 = yrday.fracday
Element set: 909
Inclination: 39.0167 deg
RA of node: 168.3745 deg
Eccentricity: .0011407
Arg of perigee: 67.2924 deg
Mean anomaly: 292.9258 deg
Mean motion: 16.00153514 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 147
Checksum: 321
Coasting Arc #11 (begining on orbit 162)
---------------------------------------
Vector Time (GMT): 2003/026/17:21:50.943
Vector Time (MET): 010/01:42:50.986
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2341728.22 A = 6652482.38 meter
Y = -5213393.19 meter E = .0022781
Z = 3382006.70 I = 39.10392
XDOT = 7081.620160 Wp = 86.09831
YDOT = 1298.411923 meter/sec RA = 160.91231 deg
ZDOT = -2879.573362 TA = 40.05574
MA = 39.88796
Ha = 152.790 n.mi
Hp = 139.744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7682835.38 X = 2383401.27
Y = -17104308.36 feet Y = -5186981.25 meter
Z = 11095822.52 Z = 3393486.83
XDOT = 23233.661942 XDOT = 7080.571043
YDOT = 4259.881637 feet/sec YDOT = 1377.574000 meter/sec
ZDOT = -9447.419167 ZDOT = -2845.165010
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03026.76417395 .00041100 00000-0 34010-3 0 9105
2 27647 39.0160 161.6940 0011280 75.8488 284.3743 16.00543419 1630
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03026.76417395 = yrday.fracday
Element set: 910
Inclination: 39.0160 deg
RA of node: 161.6940 deg
Eccentricity: .0011280
Arg of perigee: 75.8488 deg
Mean anomaly: 284.3743 deg
Mean motion: 16.00543419 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 163
Checksum: 295
Coasting Arc #12 (begining on orbit 178)
---------------------------------------
Vector Time (GMT): 2003/027/17:22:33.023
Vector Time (MET): 011/01:43:33.066
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3164600.93 A = 6653566.73 meter
Y = -5186881.47 meter E = .0024385
Z = 2682134.09 I = 39.14578
XDOT = 6482.463786 Wp = 97.09890
YDOT = 1995.677881 meter/sec RA = 154.22770 deg
ZDOT = -3757.217322 TA = 43.13258
MA = 42.94179
Ha = 152.373 n.mi
Hp = 139.232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10382548.99 X = 3209317.15
Y = -17017327.67 feet Y = -5151253.34 meter
Z = 8799652.53 Z = 2697620.10
XDOT = 21267.925808 XDOT = 6477.928965
YDOT = 6547.499608 feet/sec YDOT = 2068.122295 meter/sec
ZDOT = -12326.828485 ZDOT = -3725.728849
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03027.76221530 .00041100 00000-0 34010-3 0 9111
2 27647 39.0160 155.0107 0011285 84.4216 275.8049 16.00843826 1798
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03027.76221530 = yrday.fracday
Element set: 911
Inclination: 39.0160 deg
RA of node: 155.0107 deg
Eccentricity: .0011285
Arg of perigee: 84.4216 deg
Mean anomaly: 275.8049 deg
Mean motion: 16.00843826 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 179
Checksum: 279
Coasting Arc #13 (begining on orbit 194)
---------------------------------------
Vector Time (GMT): 2003/028/17:22:56.479
Vector Time (MET): 012/01:43:56.522
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3806320.55 A = 6654843.62 meter
Y = -5118182.25 meter E = .0025111
Z = 1856216.59 I = 39.18498
XDOT = 5793.058092 Wp = 108.79798
YDOT = 2698.391539 meter/sec RA = 147.55450 deg
ZDOT = -4389.659932 TA = 44.95454
MA = 44.75150
Ha = 152.171 n.mi
Hp = 138.982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12487928.33 X = 3854234.25
Y = -16791936.52 feet Y = -5075362.23 meter
Z = 6089949.45 Z = 1874828.60
XDOT = 19006.096101 XDOT = 5783.791936
YDOT = 8852.990615 feet/sec YDOT = 2763.102399 meter/sec
ZDOT = -14401.771430 ZDOT = -4361.532901
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03028.76013840 .00041100 00000-0 34010-3 0 9126
2 27647 39.0161 148.3265 0011316 93.3117 266.9155 16.00996565 1959
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03028.76013840 = yrday.fracday
Element set: 912
Inclination: 39.0161 deg
RA of node: 148.3265 deg
Eccentricity: .0011316
Arg of perigee: 93.3117 deg
Mean anomaly: 266.9155 deg
Mean motion: 16.00996565 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 195
Checksum: 295
Coasting Arc #14 (begining on orbit 210)
---------------------------------------
Vector Time (GMT): 2003/029/17:24:02.969
Vector Time (MET): 013/01:45:03.011
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4576436.82 A = 6655620.37 meter
Y = -4771630.57 meter E = .0024222
Z = 665680.72 I = 39.22042
XDOT = 4702.777047 Wp = 122.22184
YDOT = 3815.883988 meter/sec RA = 140.88998 deg
ZDOT = -4837.828250 TA = 48.66217
MA = 48.45401
Ha = 151.856 n.mi
Hp = 138.698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15014556.50 X = 4626204.05
Y = -15654955.93 feet Y = -4720190.78 meter
Z = 2183991.87 Z = 688039.38
XDOT = 15429.058553 XDOT = 4683.277163
YDOT = 12519.304423 feet/sec YDOT = 3868.349008 meter/sec
ZDOT = -15872.139929 ZDOT = -4815.023958
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03029.75793059 .00041100 00000-0 34010-3 0 9134
2 27647 39.0164 141.6413 0011333 102.0898 258.1351 16.01211471 2113
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03029.75793059 = yrday.fracday
Element set: 913
Inclination: 39.0164 deg
RA of node: 141.6413 deg
Eccentricity: .0011333
Arg of perigee: 102.0898 deg
Mean anomaly: 258.1351 deg
Mean motion: 16.01211471 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 211
Checksum: 267
Coasting Arc #15 (begining on orbit 226)
---------------------------------------
Vector Time (GMT): 2003/030/17:25:23.886
Vector Time (MET): 014/01:46:23.928
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5187835.49 A = 6655163.36 meter
Y = -4096236.98 meter E = .0021092
Z = -702373.77 I = 39.24604
XDOT = 3346.938476 Wp = 133.75863
YDOT = 5045.901776 meter/sec RA = 134.23215 deg
ZDOT = -4834.528288 TA = 55.85580
MA = 55.65594
Ha = 151.583 n.mi
Hp = 138.562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17020457.66 X = 5236654.50
Y = -13439097.71 feet Y = -4037967.45 meter
Z = -2304375.88 Z = -677046.52
XDOT = 10980.769277 XDOT = 3313.772992
YDOT = 16554.795854 feet/sec YDOT = 5083.133011 meter/sec
ZDOT = -15861.313282 ZDOT = -4818.345464
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03030.75561078 .00041100 00000-0 34010-3 0 9141
2 27647 39.0166 134.9555 0011321 111.0202 249.1989 16.01377942 2273
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03030.75561078 = yrday.fracday
Element set: 914
Inclination: 39.0166 deg
RA of node: 134.9555 deg
Eccentricity: .0011321
Arg of perigee: 111.0202 deg
Mean anomaly: 249.1989 deg
Mean motion: 16.01377942 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 227
Checksum: 284
Coasting Arc #16 (begining on orbit 242)
---------------------------------------
Vector Time (GMT): 2003/031/17:25:42.493
Vector Time (MET): 015/01:46:42.536
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5396198.59 A = 6653160.48 meter
Y = -3454513.42 meter E = .0017771
Z = -1774025.93 I = 39.26220
XDOT = 2328.799728 Wp = 139.15990
YDOT = 5898.064239 meter/sec RA = 127.57378 deg
ZDOT = -4448.453956 TA = 65.77787
MA = 65.59226
Ha = 151.074 n.mi
Hp = 138.280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17704063.62 X = 5443035.49
Y = -11333705.45 feet Y = -3393925.60 meter
Z = -5820295.05 Z = -1747691.02
XDOT = 7640.419055 XDOT = 2284.307676
YDOT = 19350.604460 feet/sec YDOT = 5923.850029 meter/sec
ZDOT = -14594.665211 ZDOT = -4437.245973
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03031.75315599 .00041100 00000-0 34010-3 0 9158
2 27647 39.0165 128.2687 0011309 119.8371 240.3733 16.01678641 2431
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03031.75315599 = yrday.fracday
Element set: 915
Inclination: 39.0165 deg
RA of node: 128.2687 deg
Eccentricity: .0011309
Arg of perigee: 119.8371 deg
Mean anomaly: 240.3733 deg
Mean motion: 16.01678641 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 243
Checksum: 299
Coasting Arc #17 (begining on orbit 258)
---------------------------------------
Vector Time (GMT): 2003/032/17:25:47.852
Vector Time (MET): 016/01:46:47.894
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5463675.34 A = 6650473.47 meter
Y = -2630021.46 meter E = .0014799
Z = -2728260.23 I = 39.27098
XDOT = 1347.334993 Wp = 137.62288
YDOT = 6646.706200 meter/sec RA = 120.90945 deg
ZDOT = -3736.871540 TA = 82.78424
MA = 82.61602
Ha = 150.544 n.mi
Hp = 138.088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17925444.04 X = 5505926.91
Y = -8628679.33 feet Y = -2568704.92 meter
Z = -8950985.01 Z = -2701608.58
XDOT = 4420.390398 XDOT = 1291.089253
YDOT = 21806.778871 feet/sec YDOT = 6661.454147 meter/sec
ZDOT = -12260.077231 ZDOT = -3730.461230
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03032.75052226 .00041100 00000-0 34010-3 0 9165
2 27647 39.0160 121.5801 0011228 128.0586 232.1407 16.01959627 2590
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03032.75052226 = yrday.fracday
Element set: 916
Inclination: 39.0160 deg
RA of node: 121.5801 deg
Eccentricity: .0011228
Arg of perigee: 128.0586 deg
Mean anomaly: 232.1407 deg
Mean motion: 16.01959627 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 259
Checksum: 275
Coasting Arc #18 (begining on orbit 274)
---------------------------------------
Vector Time (GMT): 2003/033/17:30:54.088
Vector Time (MET): 017/01:51:54.131
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5178360.94 A = 6644920.15 meter
Y = 741304.54 meter E = .0015098
Z = -4109535.03 I = 39.26403
XDOT = -1900.985366 Wp = 119.94121
YDOT = 7422.631317 meter/sec RA = 114.19437 deg
ZDOT = -1069.246803 TA = 137.50362
MA = 137.38665
Ha = 149.660 n.mi
Hp = 137.642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16989373.15 X = 5189657.48
Y = 2432101.51 feet Y = 799258.42 meter
Z = -13482726.46 Z = -4084344.97
XDOT = -6236.828629 XDOT = -1978.625800
YDOT = 24352.464950 feet/sec YDOT = 7400.945547 meter/sec
ZDOT = -3508.027570 ZDOT = -1078.672659
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03033.74762928 .00041100 00000-0 34010-3 0 9173
2 27647 39.0154 114.8892 0011143 135.8102 224.3768 16.02447316 2753
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03033.74762928 = yrday.fracday
Element set: 917
Inclination: 39.0154 deg
RA of node: 114.8892 deg
Eccentricity: .0011143
Arg of perigee: 135.8102 deg
Mean anomaly: 224.3768 deg
Mean motion: 16.02447316 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 275
Checksum: 296
Coasting Arc #19 (begining on orbit 290)
---------------------------------------
Vector Time (GMT): 2003/034/17:36:02.924
Vector Time (MET): 018/01:57:02.966
Weight (LBS) : 255099.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3514297.40 A = 6644770.83 meter
Y = 4204366.37 meter E = .0013486
Z = -3773725.85 I = 39.28190
XDOT = -4615.122229 Wp = 131.53460
YDOT = 5813.966431 meter/sec RA = 107.45428 deg
ZDOT = 2174.765931 TA = 164.84948
MA = 164.80905
Ha = 148.747 n.mi
Hp = 137.214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11529847.12 X = 3485372.51
Y = 13793852.92 feet Y = 4243492.27 meter
Z = -12380990.31 Z = -3756719.49
XDOT = -15141.477128 XDOT = -4690.340529
YDOT = 19074.693016 feet/sec YDOT = 5761.951898 meter/sec
ZDOT = 7135.058829 ZDOT = 2152.157465
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 27647U 03003A 03034.74443609 .00041100 00000-0 34010-3 0 9187
2 27647 39.0147 108.1954 0010980 143.9339 216.2382 16.02919538 2910
Satellite: SHUTTLE
Catalog Number: 27647
Epoch time: 03034.74443609 = yrday.fracday
Element set: 918
Inclination: 39.0147 deg
RA of node: 108.1954 deg
Eccentricity: .0010980
Arg of perigee: 143.9339 deg
Mean anomaly: 216.2382 deg
Mean motion: 16.02919538 rev/day
Decay rate: 4.11000E-04 rev/day^2
Epoch rev: 291
Checksum: 307