Date:
April 6th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8342 03 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
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
There are no maneuvers
Coasting Arc #1 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2009/093/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6035123
01 A = 6734672
32 meter
Y = -996665
84 meter E =
0012818
Z = 2817239
43 I = 51
48135
XDOT = -1460
839267 Wp = 120
95581
YDOT = 5587
730055 meter/sec RA = 329
11661 deg
ZDOT = 5082
654629 TA = 271
36602
MA = 271
51286
Ha = 194
818 n
mi
Hp = 186
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19800272
34 X = 6032133
82
Y = -3269901
06 feet Y = -929194
25 meter
Z = 9242911
51 Z = 2846550
57
XDOT = -4792
779747 XDOT = -1547
904041
YDOT = 18332
447687 feet/sec YDOT = 5570
907371 meter/sec
ZDOT = 16675
376080 ZDOT = 5075
346368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17930794
96 X = 5465306
30
Y = -8893928
67 feet Y = -2710869
46 meter
Z = 9357300
68 Z = 2852105
25
XDOT = 29
193407 XDOT = 8
898150
YDOT = 17653
716668 feet/sec YDOT = 5380
852840 meter/sec
ZDOT = 16647
196901 ZDOT = 5074
065615
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
ISS
1 25544U 98067A 09093
57383674
00010596 00000-0 82463-4 0 9004
2 25544 51
6431 329
3306 0009077 195
1863 164
9028 15
71887744 34216
Satellite: ISS
Catalog Number: 25544
Epoch time: 09093
57383674 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 329
3306 deg
Eccentricity:
0009077
Arg of perigee: 195
1863 deg
Mean anomaly: 164
9028 deg
Mean motion: 15
71887744 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3421
Checksum: 330
Coasting Arc #2 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2009/094/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 83536
69 A = 6728251
72 meter
Y = -4760822
72 meter E =
0014578
Z = -4765426
43 I = 51
43461
XDOT = 6824
194110 Wp = 146
89981
YDOT = -2447
587618 meter/sec RA = 323
93994 deg
ZDOT = 2556
518225 TA = 148
31529
MA = 148
22747
Ha = 194
638 n
mi
Hp = 187
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 274070
50 X = 159916
15
Y = -15619497
12 feet Y = -4759461
70 meter
Z = -15634601
15 Z = -4764834
89
XDOT = 22389
088288 XDOT = 6838
637271
YDOT = -8030
143105 feet/sec YDOT = -2371
194639 meter/sec
ZDOT = 8387
526984 ZDOT = 2589
705020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4471052
13 X = -1362776
69
Y = -14970504
78 feet Y = -4563009
86 meter
Z = -15632601
75 Z = -4764817
01
XDOT = 17682
476786 XDOT = 5389
618924
YDOT = -14203
181160 feet/sec YDOT = -4329
129618 meter/sec
ZDOT = 8516
955234 ZDOT = 2595
967955
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
ISS
1 25544U 98067A 09094
52744734
00010596 00000-0 82463-4 0 9019
2 25544 51
6425 324
4480 0009146 199
3490 160
7326 15
71929604 34360
Satellite: ISS
Catalog Number: 25544
Epoch time: 09094
52744734 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 324
4480 deg
Eccentricity:
0009146
Arg of perigee: 199
3490 deg
Mean anomaly: 160
7326 deg
Mean motion: 15
71929604 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3436
Checksum: 319
Coasting Arc #3 (Orbit 3451)
---------------------------------------
Vector Time (GMT): 2009/095/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5670199
26 A = 6736946
57 meter
Y = 3235782
21 meter E =
0014751
Z = -1625239
39 I = 51
44023
XDOT = -1217
379806 Wp = 175
43869
YDOT = -5001
943562 meter/sec RA = 318
84214 deg
ZDOT = -5729
430016 TA = 22
55618
MA = 22
49141
Ha = 194
465 n
mi
Hp = 187
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18603015
93 X = -5698065
84
Y = 10616083
36 feet Y = 3172218
82 meter
Z = -5332150
24 Z = -1652852
89
XDOT = -3994
028234 XDOT = -1133
524447
YDOT = -16410
575991 feet/sec YDOT = -5015
088533 meter/sec
ZDOT = -18797
342573 ZDOT = -5735
139984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14117542
07 X = -4303026
82
Y = 16072002
83 feet Y = 4898746
46 meter
Z = -5439759
65 Z = -1658038
74
XDOT = -7832
215322 XDOT = -2387
259230
YDOT = -13229
997984 feet/sec YDOT = -4032
503386 meter/sec
ZDOT = -18819
970918 ZDOT = -5736
327136
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
ISS
1 25544U 98067A 09095
54462028
00010596 00000-0 82463-4 0 9026
2 25544 51
6420 319
2413 0009266 203
5598 156
5141 15
71907275 34529
Satellite: ISS
Catalog Number: 25544
Epoch time: 09095
54462028 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 319
2413 deg
Eccentricity:
0009266
Arg of perigee: 203
5598 deg
Mean anomaly: 156
5141 deg
Mean motion: 15
71907275 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3452
Checksum: 305
Coasting Arc #4 (Orbit 3467)
---------------------------------------
Vector Time (GMT): 2009/096/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2121567
04 A = 6726354
18 meter
Y = 3751238
60 meter E =
0006004
Z = 5164254
80 I = 51
38310
XDOT = -5870
332096 Wp = 189
16814
YDOT = 4852
622004 meter/sec RA = 313
68058 deg
ZDOT = -1119
254616 TA = 271
52170
MA = 271
59047
Ha = 194
207 n
mi
Hp = 187
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6960521
79 X = 2054375
47
Y = 12307213
25 feet Y = 3774587
94 meter
Z = 16943093
17 Z = 5174397
81
XDOT = -19259
619736 XDOT = -5918
721516
YDOT = 15920
675865 feet/sec YDOT = 4786
705873 meter/sec
ZDOT = -3672
095197 ZDOT = -1147
890508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10647725
00 X = 3245426
58
Y = 9229846
97 feet Y = 2813257
36 meter
Z = 16982951
60 Z = 5176403
65
XDOT = -11983
441292 XDOT = -3652
552906
YDOT = 20749
885291 feet/sec YDOT = 6324
565037 meter/sec
ZDOT = -3783
581384 ZDOT = -1153
235606
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
ISS
1 25544U 98067A 09096
56177844
00010596 00000-0 82463-4 0 9039
2 25544 51
6416 314
0331 0009155 207
6441 152
4235 15
71958841 34686
Satellite: ISS
Catalog Number: 25544
Epoch time: 09096
56177844 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 314
0331 deg
Eccentricity:
0009155
Arg of perigee: 207
6441 deg
Mean anomaly: 152
4235 deg
Mean motion: 15
71958841 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3468
Checksum: 315
Coasting Arc #5 (Orbit 3483)
---------------------------------------
Vector Time (GMT): 2009/097/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4399311
68 A = 6737861
51 meter
Y = -5091526
88 meter E =
0004958
Z = 334445
65 I = 51
40114
XDOT = 3438
274421 Wp = 81
70111
YDOT = 3369
844124 meter/sec RA = 308
55466 deg
ZDOT = 5999
409633 TA = 281
94069
MA = 281
99627
Ha = 194
080 n
mi
Hp = 187
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14433437
27 X = 4454294
34
Y = -16704484
52 feet Y = -5042023
76 meter
Z = 1097262
64 Z = 355951
54
XDOT = 11280
427891 XDOT = 3371
192632
YDOT = 11055
919043 feet/sec YDOT = 3407
918379 meter/sec
ZDOT = 19683
102472 ZDOT = 6015
949545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7510444
61 X = 2289183
52
Y = -20754918
23 feet Y = -6326099
08 meter
Z = 1180885
54 Z = 359933
91
XDOT = 12864
819312 XDOT = 3921
196926
YDOT = 5791
932491 feet/sec YDOT = 1765
381023 meter/sec
ZDOT = 19747
913373 ZDOT = 6019
163996
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
ISS
1 25544U 98067A 09097
57892332
00010596 00000-0 82463-4 0 9048
2 25544 51
6401 308
8240 0009151 211
8113 148
2497 15
71983463 34848
Satellite: ISS
Catalog Number: 25544
Epoch time: 09097
57892332 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 308
8240 deg
Eccentricity:
0009151
Arg of perigee: 211
8113 deg
Mean anomaly: 148
2497 deg
Mean motion: 15
71983463 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3484
Checksum: 316
Coasting Arc #6 (Orbit 3498)
---------------------------------------
Vector Time (GMT): 2009/098/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3712675
77 A = 6725824
54 meter
Y = -1996983
77 meter E =
0011869
Z = -5248755
45 I = 51
34201
XDOT = 4000
653215 Wp = 124
77312
YDOT = -6559
865040 meter/sec RA = 303
41362 deg
ZDOT = -341
232341 TA = 142
01170
MA = 141
92793
Ha = 193
825 n
mi
Hp = 187
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12180694
79 X = -3664571
55
Y = -6551784
03 feet Y = -2038232
56 meter
Z = -17220326
29 Z = -5266674
74
XDOT = 13125
502673 XDOT = 4075
367042
YDOT = -21521
866928 feet/sec YDOT = -6514
709683 meter/sec
ZDOT = -1119
528677 ZDOT = -321
614999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13653100
56 X = -4161465
05
Y = -1571237
68 feet Y = -478913
24 meter
Z = -17290427
82 Z = -5270122
40
XDOT = 4038
732109 XDOT = 1231
005547
YDOT = -23871
734099 feet/sec YDOT = -7276
104553 meter/sec
ZDOT = -1043
385329 ZDOT = -318
023848
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
ISS
1 25544U 98067A 09098
53248458
00010596 00000-0 82463-4 0 9050
2 25544 51
6388 303
9405 0009115 215
2465 144
8095 15
72005032 34999
Satellite: ISS
Catalog Number: 25544
Epoch time: 09098
53248458 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 303
9405 deg
Eccentricity:
0009115
Arg of perigee: 215
2465 deg
Mean anomaly: 144
8095 deg
Mean motion: 15
72005032 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3499
Checksum: 319
Coasting Arc #7 (Orbit 3514)
---------------------------------------
Vector Time (GMT): 2009/099/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2480064
31 A = 6737351
21 meter
Y = 6183527
35 meter E =
0015653
Z = 930178
90 I = 51
36665
XDOT = -4815
841395 Wp = 160
03902
YDOT = -1038
396284 meter/sec RA = 298
26142 deg
ZDOT = -5922
417812 TA = 9
76506
MA = 9
73468
Ha = 193
524 n
mi
Hp = 188
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8136693
94 X = -2553543
92
Y = 20287163
22 feet Y = 6155383
04 meter
Z = 3051768
03 Z = 917951
68
XDOT = -15800
004577 XDOT = -4775
101578
YDOT = -3406
811957 feet/sec YDOT = -1092
022465 meter/sec
ZDOT = -19430
504633 ZDOT = -5945
714404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 380207
30 X = 115887
18
Y = 21861307
42 feet Y = 6663326
50 meter
Z = 3004454
71 Z = 915757
79
XDOT = -14182
894154 XDOT = -4322
946138
YDOT = 2936
323057 feet/sec YDOT = 894
991268 meter/sec
ZDOT = -19521
533359 ZDOT = -5950
163368
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
ISS
1 25544U 98067A 09099
54960208
00010596 00000-0 82463-4 0 9067
2 25544 51
6393 298
7326 0009019 220
4889 139
5603 15
72057657 35154
Satellite: ISS
Catalog Number: 25544
Epoch time: 09099
54960208 = yrday
fracday
Element set: 906
Inclination: 51
6393 deg
RA of node: 298
7326 deg
Eccentricity:
0009019
Arg of perigee: 220
4889 deg
Mean anomaly: 139
5603 deg
Mean motion: 15
72057657 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3515
Checksum: 341
Coasting Arc #8 (Orbit 3530)
---------------------------------------
Vector Time (GMT): 2009/100/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4475663
93 A = 6726839
52 meter
Y = -244778
74 meter E =
0009822
Z = 5019951
59 I = 51
31675
XDOT = -1590
283424 Wp = 190
38466
YDOT = 7318
117494 meter/sec RA = 293
14176 deg
ZDOT = 1765
708732 TA = 242
46908
MA = 242
56892
Ha = 193
463 n
mi
Hp = 188
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14683936
77 X = 4453682
07
Y = -803079
85 feet Y = -194851
90 meter
Z = 16469657
45 Z = 5041641
30
XDOT = -5217
465302 XDOT = -1680
575264
YDOT = 24009
571831 feet/sec YDOT = 7299
829259 meter/sec
ZDOT = 5793
007650 ZDOT = 1757
763331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13014659
08 X = 3966868
09
Y = -6639696
87 feet Y = -2023779
61 meter
Z = 16554323
52 Z = 5045757
81
XDOT = 4433
696980 XDOT = 1351
390840
YDOT = 23131
003393 feet/sec YDOT = 7050
329834 meter/sec
ZDOT = 5762
489402 ZDOT = 1756
406770
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
ISS
1 25544U 98067A 09100
56670920
00010596 00000-0 82463-4 0 9072
2 25544 51
6382 293
5230 0009017 223
2737 136
7718 15
71998303 35315
Satellite: ISS
Catalog Number: 25544
Epoch time: 09100
56670920 = yrday
fracday
Element set: 907
Inclination: 51
6382 deg
RA of node: 293
5230 deg
Eccentricity:
0009017
Arg of perigee: 223
2737 deg
Mean anomaly: 136
7718 deg
Mean motion: 15
71998303 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3531
Checksum: 307
Coasting Arc #9 (Orbit 3545)
---------------------------------------
Vector Time (GMT): 2009/101/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 284959
92 A = 6735735
35 meter
Y = -6386376
50 meter E =
0002853
Z = -2122958
89 I = 51
33666
XDOT = 5140
208010 Wp = 237
66931
YDOT = -1599
486757 meter/sec RA = 287
96370 deg
ZDOT = 5494
716725 TA = 98
52550
MA = 98
49317
Ha = 193
311 n
mi
Hp = 188
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 934907
87 X = 366665
38
Y = -20952678
81 feet Y = -6382733
13 meter
Z = -6965088
22 Z = -2121375
90
XDOT = 16864
199509 XDOT = 5131
018951
YDOT = -5247
659964 feet/sec YDOT = -1542
057184 meter/sec
ZDOT = 18027
285843 ZDOT = 5519
665961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7925366
17 X = -2415651
61
Y = -19420539
07 feet Y = -5919380
31 meter
Z = -6959345
48 Z = -2121208
50
XDOT = 11583
467954 XDOT = 3530
641032
YDOT = -11230
164764 feet/sec YDOT = -3422
954220 meter/sec
ZDOT = 18124
586375 ZDOT = 5524
373927
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
ISS
1 25544U 98067A 09101
52023065
00010596 00000-0 82463-4 0 9082
2 25544 51
6380 288
6389 0009149 226
3842 133
6561 15
72064424 35467
Satellite: ISS
Catalog Number: 25544
Epoch time: 09101
52023065 = yrday
fracday
Element set: 908
Inclination: 51
6380 deg
RA of node: 288
6389 deg
Eccentricity:
0009149
Arg of perigee: 226
3842 deg
Mean anomaly: 133
6561 deg
Mean motion: 15
72064424 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3546
Checksum: 309
Coasting Arc #10 (Orbit 3561)
---------------------------------------
Vector Time (GMT): 2009/102/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4294953
86 A = 6728594
33 meter
Y = 2517239
21 meter E =
0003502
Z = -4527881
20 I = 51
30529
XDOT = -901
660952 Wp = 129
52650
YDOT = -7009
804817 meter/sec RA = 282
86221 deg
ZDOT = -3045
531182 TA = 110
02551
MA = 109
98781
Ha = 192
930 n
mi
Hp = 188
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14091055
98 X = -4300786
89
Y = 8258658
82 feet Y = 2469177
90 meter
Z = -14855253
28 Z = -4548760
56
XDOT = -2958
205224 XDOT = -808
414272
YDOT = -22998
047299 feet/sec YDOT = -7019
366358 meter/sec
ZDOT = -9991
900205 ZDOT = -3049
684988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9002622
58 X = -2743999
36
Y = 13538556
51 feet Y = 4126552
02 meter
Z = -14936603
65 Z = -4552676
79
XDOT = -11650
581946 XDOT = -3551
097377
YDOT = -18775
771485 feet/sec YDOT = -5722
855149 meter/sec
ZDOT = -10008
598480 ZDOT = -3050
620817
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
ISS
1 25544U 98067A 09102
53730829
00010596 00000-0 82463-4 0 9098
2 25544 51
6382 283
4307 0008963 230
1273 129
9101 15
72099423 35629
Satellite: ISS
Catalog Number: 25544
Epoch time: 09102
53730829 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 283
4307 deg
Eccentricity:
0008963
Arg of perigee: 230
1273 deg
Mean anomaly: 129
9101 deg
Mean motion: 15
72099423 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3562
Checksum: 307
Coasting Arc #11 (Orbit 3577)
---------------------------------------
Vector Time (GMT): 2009/103/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1799130
05 A = 6733206
68 meter
Y = 5655111
11 meter E =
0008219
Z = 3169334
25 I = 51
31518
XDOT = -4423
460426 Wp = 138
14274
YDOT = 4093
884559 meter/sec RA = 277
66927 deg
ZDOT = -4792
640081 TA = 4
73644
MA = 4
72867
Ha = 192
813 n
mi
Hp = 188
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5902657
63 X = 1720363
69
Y = 18553514
14 feet Y = 5674789
58 meter
Z = 10398078
24 Z = 3177883
28
XDOT = -14512
665441 XDOT = -4445
628107
YDOT = 13431
379788 feet/sec YDOT = 4044
294969 meter/sec
ZDOT = -15723
884779 ZDOT = -4814
183296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13588995
28 X = 4141925
76
Y = 13917976
10 feet Y = 4242199
11 meter
Z = 10431847
09 Z = 3179626
99
XDOT = -5790
050717 XDOT = -1764
807458
YDOT = 17504
163843 feet/sec YDOT = 5335
269139 meter/sec
ZDOT = -15807
722778 ZDOT = -4818
193903
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
ISS
1 25544U 98067A 09103
55437114
00010596 00000-0 82463-4 0 9104
2 25544 51
6380 278
2214 0009147 234
5607 125
4702 15
72097154 35784
Satellite: ISS
Catalog Number: 25544
Epoch time: 09103
55437114 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 278
2214 deg
Eccentricity:
0009147
Arg of perigee: 234
5607 deg
Mean anomaly: 125
4702 deg
Mean motion: 15
72097154 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3578
Checksum: 298
Coasting Arc #12 (Orbit 3593)
---------------------------------------
Vector Time (GMT): 2009/104/12:23:05
892
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3248954
33 A = 6731138
53 meter
Y = -4509458
21 meter E =
0007431
Z = 3799231
30 I = 51
30620
XDOT = 3066
814025 Wp = 150
83649
YDOT = 5710
233026 meter/sec RA = 272
57492 deg
ZDOT = 4145
273340 TA = 255
46849
MA = 255
55093
Ha = 192
630 n
mi
Hp = 188
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10659298
99 X = 3280682
24
Y = -14794810
40 feet Y = -4472949
20 meter
Z = 12464669
63 Z = 3815091
82
XDOT = 10061
725804 XDOT = 2982
596142
YDOT = 18734
360321 feet/sec YDOT = 5744
056939 meter/sec
ZDOT = 13599
978150 ZDOT = 4159
967628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2458252
59 X = 749275
39
Y = -18025649
93 feet Y = -5494218
10 meter
Z = 12526292
24 Z = 3818013
88
XDOT = 16258
218815 XDOT = 4955
505095
YDOT = 11730
446736 feet/sec YDOT = 3575
440165 meter/sec
ZDOT = 13657
751550 ZDOT = 4162
882672
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
ISS
1 25544U 98067A 09104
57141971
00010596 00000-0 82463-4 0 9111
2 25544 51
6382 273
0122 0009135 237
9508 122
0767 15
72146477 35946
Satellite: ISS
Catalog Number: 25544
Epoch time: 09104
57141971 = yrday
fracday
Element set: 911
Inclination: 51
6382 deg
RA of node: 273
0122 deg
Eccentricity:
0009135
Arg of perigee: 237
9508 deg
Mean anomaly: 122
0767 deg
Mean motion: 15
72146477 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3594
Checksum: 307
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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