Date:
April 25th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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
112/16:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
4
000/00:00:00
000 0
0 0
0 182
5
113/20:40:24
801 -5
0 8
3 8
3
N/A 6
2 -0
6 191
3
000/00:20:45
602 -2
4 -0
1 187
0
Coasting Arc #1 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2010/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 806739
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5851448
99 A = 6728437
90 meter
Y = -3077781
08 meter E =
0015291
Z = 1201219
56 I = 51
77454
XDOT = 3209
710496 Wp = 134
34972
YDOT = 3787
979541 meter/sec RA = 160
48372 deg
ZDOT = -5894
339234 TA = 32
49739
MA = 32
40334
Ha = 188
521 n
mi
Hp = 182
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19197667
28 X = 5879595
09
Y = -10097706
94 feet Y = -3012189
34 meter
Z = 3941009
06 Z = 1229714
21
XDOT = 10530
546247 XDOT = 3195
747702
YDOT = 12427
754399 feet/sec YDOT = 3823
794464 meter/sec
ZDOT = -19338
383315 ZDOT = -5878
780316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11976039
85 X = 3650296
95
Y = -18060539
29 feet Y = -5504852
37 meter
Z = 4054264
05 Z = 1235739
68
XDOT = 13985
296929 XDOT = 4262
718504
YDOT = 4921
207848 feet/sec YDOT = 1499
984152 meter/sec
ZDOT = -19276
358756 ZDOT = -5875
434149
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 10111
53414611
00016717 00000-0 10270-3 0 9006
2 25544 51
6458 161
3441 0003454 194
7544 165
3520 15
75082439 14552
Satellite: ISS
Catalog Number: 25544
Epoch time: 10111
53414611 = yrday
fracday
Element set: 900
Inclination: 51
6458 deg
RA of node: 161
3441 deg
Eccentricity:
0003454
Arg of perigee: 194
7544 deg
Mean anomaly: 165
3520 deg
Mean motion: 15
75082439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 282
Coasting Arc #2 (Orbit 1470)
---------------------------------------
Vector Time (GMT): 2010/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 806739
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2687194
79 A = 6717293
74 meter
Y = -3281927
57 meter E =
0005646
Z = 5207696
53 I = 51
76477
XDOT = 6596
535561 Wp = 159
65509
YDOT = -3860
909440 meter/sec RA = 155
36990 deg
ZDOT = 965
165409 TA = 281
13554
MA = 281
19901
Ha = 188
543 n
mi
Hp = 182
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8816255
86 X = -2675593
98
Y = -10767478
90 feet Y = -3311912
49 meter
Z = 17085618
55 Z = 5194670
36
XDOT = 21642
177038 XDOT = 6634
530080
YDOT = -12667
025721 feet/sec YDOT = -3786
930610 meter/sec
ZDOT = 3166
553180 ZDOT = 997
303645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13076916
36 X = -3985844
11
Y = -4942801
84 feet Y = -1506566
00 meter
Z = 17033681
31 Z = 5191866
06
XDOT = 12159
599152 XDOT = 3706
245822
YDOT = -20754
958917 feet/sec YDOT = -6326
111478 meter/sec
ZDOT = 3294
290452 ZDOT = 1004
099730
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 10112
54928459
00016717 00000-0 10270-3 0 9019
2 25544 51
6454 156
1234 0003477 197
4752 162
6292 15
75100061 14712
Satellite: ISS
Catalog Number: 25544
Epoch time: 10112
54928459 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 156
1234 deg
Eccentricity:
0003477
Arg of perigee: 197
4752 deg
Mean anomaly: 162
6292 deg
Mean motion: 15
75100061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1471
Checksum: 295
Coasting Arc #3 (Orbit 1473)
---------------------------------------
Vector Time (GMT): 2010/112/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 794336
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4214838
95 A = 6719201
12 meter
Y = -2147726
92 meter E =
0008627
Z = 4770024
93 I = 51
77428
XDOT = 5403
767891 Wp = 142
16437
YDOT = -4843
920473 meter/sec RA = 154
41902 deg
ZDOT = 2584
685535 TA = 282
50394
MA = 282
60043
Ha = 188
439 n
mi
Hp = 182
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13828211
78 X = -4213681
32
Y = -7046348
16 feet Y = -2194853
24 meter
Z = 15649688
09 Z = 4749552
10
XDOT = 17728
897281 XDOT = 5444
975938
YDOT = -15892
127535 feet/sec YDOT = -4783
261892 meter/sec
ZDOT = 8479
939418 ZDOT = 2611
037148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5207401
63 X = -1587216
02
Y = 14707092
41 feet Y = 4482721
77 meter
Z = 15568159
87 Z = 4745175
13
XDOT = -16950
325426 XDOT = -5166
459190
YDOT = -15120
799958 feet/sec YDOT = -4608
819827 meter/sec
ZDOT = 8584
622416 ZDOT = 2616
592912
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 10112
73962060
00016717 00000-0 10270-3 0 9027
2 25544 51
6433 155
1443 0003364 201
4227 158
6796 15
75111947 14740
Satellite: ISS
Catalog Number: 25544
Epoch time: 10112
73962060 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 155
1443 deg
Eccentricity:
0003364
Arg of perigee: 201
4227 deg
Mean anomaly: 158
6796 deg
Mean motion: 15
75111947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1474
Checksum: 291
Coasting Arc #4 (Orbit 1488)
---------------------------------------
Vector Time (GMT): 2010/113/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 794336
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4628464
44 A = 6727349
26 meter
Y = 4494706
20 meter E =
0003998
Z = -1903245
41 I = 51
82877
XDOT = -4648
643810 Wp = 53
18332
YDOT = -2400
059884 meter/sec RA = 149
24892 deg
ZDOT = 5647
428759 TA = 285
72257
MA = 285
76666
Ha = 188
280 n
mi
Hp = 182
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15185250
80 X = -4669135
42
Y = 14746411
40 feet Y = 4442720
49 meter
Z = -6244243
48 Z = -1925829
44
XDOT = -15251
456071 XDOT = -4648
894625
YDOT = -7874
212219 feet/sec YDOT = -2452
045014 meter/sec
ZDOT = 18528
309578 ZDOT = 5624
845095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16786378
20 X = 5116488
08
Y = 12850586
63 feet Y = 3916858
80 meter
Z = -6333955
95 Z = -1930589
77
XDOT = -4626
848588 XDOT = -1410
263450
YDOT = 15115
370153 feet/sec YDOT = 4607
164823 meter/sec
ZDOT = 18438
367391 ZDOT = 5620
014381
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 10113
69129042
00016717 00000-0 10270-3 0 9039
2 25544 51
6432 150
2493 0003237 202
0885 158
0139 15
75124685 14890
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
69129042 = yrday
fracday
Element set: 903
Inclination: 51
6432 deg
RA of node: 150
2493 deg
Eccentricity:
0003237
Arg of perigee: 202
0885 deg
Mean anomaly: 158
0139 deg
Mean motion: 15
75124685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1489
Checksum: 293
Coasting Arc #5 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2010/113/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 454304
12 A = 6723110
00 meter
Y = 4403791
18 meter E =
0010397
Z = -5066460
53 I = 51
80444
XDOT = -6988
567442 Wp = 149
75532
YDOT = 2715
950713 meter/sec RA = 148
32252 deg
ZDOT = 1726
792689 TA = 136
87848
MA = 136
79699
Ha = 191
299 n
mi
Hp = 186
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1490499
08 X = 429638
36
Y = 14448133
79 feet Y = 4408733
39 meter
Z = -16622245
83 Z = -5064313
58
XDOT = -22928
370873 XDOT = -7026
806742
YDOT = 8910
599451 feet/sec YDOT = 2637
586643 meter/sec
ZDOT = 5665
330346 ZDOT = 1692
749203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2527505
65 X = 770383
72
Y = -14313305
03 feet Y = -4362695
37 meter
Z = -16613555
56 Z = -5063811
73
XDOT = 23495
186739 XDOT = 7161
332918
YDOT = -2297
467988 feet/sec YDOT = -700
268243 meter/sec
ZDOT = 5529
958559 ZDOT = 1685
531369
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 10113
88163286
00016717 00000-0 10270-3 0 9049
2 25544 51
6463 149
2698 0009922 233
1303 126
8951 15
73274948 14921
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
88163286 = yrday
fracday
Element set: 904
Inclination: 51
6463 deg
RA of node: 149
2698 deg
Eccentricity:
0009922
Arg of perigee: 233
1303 deg
Mean anomaly: 126
8951 deg
Mean motion: 15
73274948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 324
Coasting Arc #6 (Orbit 1507)
---------------------------------------
Vector Time (GMT): 2010/114/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5832052
21 A = 6733578
97 meter
Y = -3086796
84 meter E =
0013053
Z = -1296790
25 I = 51
86460
XDOT = 1247
809493 Wp = 193
11082
YDOT = 4825
138802 meter/sec RA = 143
23282 deg
ZDOT = -5874
664147 TA = 1
08091
MA = 1
07809
Ha = 191
221 n
mi
Hp = 187
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19134029
56 X = 5872435
49
Y = -10127286
23 feet Y = -3021353
62 meter
Z = -4254561
18 Z = -1268359
74
XDOT = 4093
863165 XDOT = 1222
299419
YDOT = 15830
507879 feet/sec YDOT = 4838
949660 meter/sec
ZDOT = -19273
832504 ZDOT = -5868
664426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21152277
58 X = -6447214
21
Y = 4712027
52 feet Y = 1436225
99 meter
Z = -4141527
99 Z = -1262337
73
XDOT = 463
258211 XDOT = 141
201103
YDOT = -14836
691974 feet/sec YDOT = -4522
223714 meter/sec
ZDOT = -19249
798897 ZDOT = -5867
338704
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 10114
89792901
00016717 00000-0 10270-3 0 9054
2 25544 51
6463 144
0569 0010050 236
7298 123
2902 15
73265240 15087
Satellite: ISS
Catalog Number: 25544
Epoch time: 10114
89792901 = yrday
fracday
Element set: 905
Inclination: 51
6463 deg
RA of node: 144
0569 deg
Eccentricity:
0010050
Arg of perigee: 236
7298 deg
Mean anomaly: 123
2902 deg
Mean motion: 15
73265240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1508
Checksum: 295
Coasting Arc #7 (Orbit 1523)
---------------------------------------
Vector Time (GMT): 2010/115/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1688008
42 A = 6722386
31 meter
Y = -3948344
45 meter E =
0005993
Z = 5176455
72 I = 51
85109
XDOT = 6258
768362 Wp = 246
18853
YDOT = -4302
963926 meter/sec RA = 138
09562 deg
ZDOT = -1244
640127 TA = 215
65820
MA = 215
69825
Ha = 190
778 n
mi
Hp = 187
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5538085
36 X = -1668878
45
Y = -12953885
99 feet Y = -3967113
60 meter
Z = 16983122
44 Z = 5168301
90
XDOT = 20534
016936 XDOT = 6312
466017
YDOT = -14117
335714 feet/sec YDOT = -4232
674461 meter/sec
ZDOT = -4083
464982 ZDOT = -1214
104068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2259714
29 X = 688760
92
Y = 13945343
02 feet Y = 4250540
55 meter
Z = 16950548
63 Z = 5166527
22
XDOT = -22393
373155 XDOT = -6825
500138
YDOT = 8430
579928 feet/sec YDOT = 2569
640762 meter/sec
ZDOT = -3962
082419 ZDOT = -1207
642721
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 10115
91420366
00016717 00000-0 10270-3 0 9062
2 25544 51
6460 138
8436 0009988 241
8061 118
2094 15
73365321 15246
Satellite: ISS
Catalog Number: 25544
Epoch time: 10115
91420366 = yrday
fracday
Element set: 906
Inclination: 51
6460 deg
RA of node: 138
8436 deg
Eccentricity:
0009988
Arg of perigee: 241
8061 deg
Mean anomaly: 118
2094 deg
Mean motion: 15
73365321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1524
Checksum: 302
Coasting Arc #8 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2010/116/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5036884
14 A = 6733668
50 meter
Y = 4374527
19 meter E =
0004323
Z = 893449
82 I = 51
91040
XDOT = -2536
794356 Wp = 27
37066
YDOT = -4141
960067 meter/sec RA = 133
00027 deg
ZDOT = 5970
996507 TA = 342
33891
MA = 342
35394
Ha = 190
490 n
mi
Hp = 187
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16525210
42 X = -5089766
82
Y = 14352123
34 feet Y = 4317906
10 meter
Z = 2931265
81 Z = 868851
66
XDOT = -8322
816128 XDOT = -2519
296185
YDOT = -13589
107830 feet/sec YDOT = -4170
230030 meter/sec
ZDOT = 19589
883553 ZDOT = 5958
715156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19405783
12 X = 5914882
70
Y = -10151117
21 feet Y = -3094060
52 meter
Z = 2833503
79 Z = 863651
96
XDOT = 4337
157587 XDOT = 1321
965632
YDOT = 13752
989773 feet/sec YDOT = 4191
911283 meter/sec
ZDOT = 19540
882142 ZDOT = 5956
060877
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 10116
93046166
00016717 00000-0 10270-3 0 9078
2 25544 51
6457 133
6295 0009931 245
8691 114
1434 15
73362149 15405
Satellite: ISS
Catalog Number: 25544
Epoch time: 10116
93046166 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 133
6295 deg
Eccentricity:
0009931
Arg of perigee: 245
8691 deg
Mean anomaly: 114
1434 deg
Mean motion: 15
73362149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 307
Coasting Arc #9 (Orbit 1554)
---------------------------------------
Vector Time (GMT): 2010/117/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2694995
54 A = 6721989
89 meter
Y = 3235576
86 meter E =
0007301
Z = -5244685
26 I = 51
89084
XDOT = -5182
301544 Wp = 133
45765
YDOT = 5632
024969 meter/sec RA = 127
87240 deg
ZDOT = 807
382122 TA = 144
22895
MA = 144
18002
Ha = 190
201 n
mi
Hp = 187
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8841848
89 X = 2684092
69
Y = 10615409
63 feet Y = 3265652
94 meter
Z = -17206972
62 Z = -5231619
19
XDOT = -17002
301654 XDOT = -5248
816890
YDOT = 18477
772207 feet/sec YDOT = 5573
701482 meter/sec
ZDOT = 2648
891477 ZDOT = 782
044422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6466656
23 X = -1971036
82
Y = -12281595
95 feet Y = -3743430
45 meter
Z = -17154879
14 Z = -5228807
16
XDOT = 19679
241147 XDOT = 5998
232702
YDOT = -13940
452685 feet/sec YDOT = -4249
049978 meter/sec
ZDOT = 2548
207049 ZDOT = 776
693508
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 10117
88318493
00016717 00000-0 10270-3 0 9089
2 25544 51
6454 128
7414 0009954 249
7527 110
2566 15
73405860 15553
Satellite: ISS
Catalog Number: 25544
Epoch time: 10117
88318493 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 128
7414 deg
Eccentricity:
0009954
Arg of perigee: 249
7527 deg
Mean anomaly: 110
2566 deg
Mean motion: 15
73405860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1555
Checksum: 326
Coasting Arc #10 (Orbit 1570)
---------------------------------------
Vector Time (GMT): 2010/118/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3967153
47 A = 6733853
68 meter
Y = -5406341
34 meter E =
0011617
Z = -522651
58 I = 51
94803
XDOT = 3560
514627 Wp = 191
29502
YDOT = 3197
285870 meter/sec RA = 122
77340 deg
ZDOT = -6035
782226 TA = 354
36812
MA = 354
38117
Ha = 190
082 n
mi
Hp = 187
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13015595
38 X = 4029852
30
Y = -17737340
36 feet Y = -5361627
69 meter
Z = -1714736
16 Z = -503226
59
XDOT = 11681
478436 XDOT = 3553
818724
YDOT = 10489
783037 feet/sec YDOT = 3237
064379 meter/sec
ZDOT = -19802
435125 ZDOT = -6018
501068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16264101
14 X = -4957298
03
Y = 14824192
96 feet Y = 4518414
01 meter
Z = -1637560
24 Z = -499128
36
XDOT = -8419
663372 XDOT = -2566
313396
YDOT = -11421
644911 feet/sec YDOT = -3481
317369 meter/sec
ZDOT = -19733
568803 ZDOT = -6014
791771
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 10118
89940576
00016717 00000-0 10270-3 0 9095
2 25544 51
6454 123
5281 0010040 252
6796 107
3269 15
73373881 15719
Satellite: ISS
Catalog Number: 25544
Epoch time: 10118
89940576 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 123
5281 deg
Eccentricity:
0010040
Arg of perigee: 252
6796 deg
Mean anomaly: 107
3269 deg
Mean motion: 15
73373881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1571
Checksum: 318
Coasting Arc #11 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2010/119/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3460444
55 A = 6721708
42 meter
Y = -2314383
19 meter E =
0007407
Z = 5283477
30 I = 51
92318
XDOT = 3841
937864 Wp = 259
27231
YDOT = -6655
399416 meter/sec RA = 117
65421 deg
ZDOT = -400
861971 TA = 194
51142
MA = 194
53270
Ha = 189
641 n
mi
Hp = 187
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11353164
53 X = -3459974
18
Y = -7593120
72 feet Y = -2353077
58 meter
Z = 17334243
10 Z = 5266667
16
XDOT = 12604
783020 XDOT = 3918
021544
YDOT = -21835
299920 feet/sec YDOT = -6612
011154 meter/sec
ZDOT = -1315
163948 ZDOT = -382
013005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9900511
10 X = 3017675
78
Y = 9531366
36 feet Y = 2905160
47 meter
Z = 17267273
85 Z = 5263065
07
XDOT = -15643
221225 XDOT = -4768
053829
YDOT = 18485
164086 feet/sec YDOT = 5634
278014 meter/sec
ZDOT = -1240
292173 ZDOT = -378
041054
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 10119
91560491
00016717 00000-0 10270-3 0 9105
2 25544 51
6453 118
3135 0009979 257
6271 102
3775 15
73451643 15877
Satellite: ISS
Catalog Number: 25544
Epoch time: 10119
91560491 = yrday
fracday
Element set: 910
Inclination: 51
6453 deg
RA of node: 118
3135 deg
Eccentricity:
0009979
Arg of perigee: 257
6271 deg
Mean anomaly: 102
3775 deg
Mean motion: 15
73451643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 316
Coasting Arc #12 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2010/120/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2716340
26 A = 6733611
78 meter
Y = 6153257
97 meter E =
0007136
Z = 190659
14 I = 51
97605
XDOT = -4271
410490 Wp = 354
25088
YDOT = -2072
595976 meter/sec RA = 112
54885 deg
ZDOT = 6061
256055 TA = 7
81043
MA = 7
79932
Ha = 189
045 n
mi
Hp = 187
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8911877
48 X = -2785871
41
Y = 20187854
25 feet Y = 6122493
46 meter
Z = 625522
13 Z = 177294
49
XDOT = -14013
813945 XDOT = -4277
361831
YDOT = -6799
855563 feet/sec YDOT = -2120
395129 meter/sec
ZDOT = 19886
010678 ZDOT = 6040
490616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12089316
41 X = 3684823
64
Y = -18463017
76 feet Y = -5627527
81 meter
Z = 572451
85 Z = 174483
32
XDOT = 11485
874315 XDOT = 3500
894491
YDOT = 8131
864799 feet/sec YDOT = 2478
592391 meter/sec
ZDOT = 19803
298893 ZDOT = 6036
045503
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 10120
93178506
00016717 00000-0 10270-3 0 9112
2 25544 51
6448 113
0986 0010045 261
6970 98
3054 15
73491881 16035
Satellite: ISS
Catalog Number: 25544
Epoch time: 10120
93178506 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 113
0986 deg
Eccentricity:
0010045
Arg of perigee: 261
6970 deg
Mean anomaly: 98
3054 deg
Mean motion: 15
73491881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1603
Checksum: 301
Coasting Arc #13 (Orbit 1617)
---------------------------------------
Vector Time (GMT): 2010/121/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3940468
78 A = 6721456
85 meter
Y = 1287545
41 meter E =
0005135
Z = -5295160
00 I = 51
94507
XDOT = -2338
048992 Wp = 99
64710
YDOT = 7333
100711 meter/sec RA = 107
43712 deg
ZDOT = 42
382194 TA = 170
75829
MA = 170
74884
Ha = 188
573 n
mi
Hp = 187
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12928047
18 X = 3951501
57
Y = 4224230
34 feet Y = 1331672
19 meter
Z = -17372572
19 Z = -5275990
09
XDOT = -7670
764410 XDOT = -2420
081159
YDOT = 24058
729366 feet/sec YDOT = 7306
496586 meter/sec
ZDOT = 139
049194 ZDOT = 30
825156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12273022
84 X = -3740817
36
Y = -6082625
59 feet Y = -1853984
28 meter
Z = -17296224
06 Z = -5271889
09
XDOT = 10661
471310 XDOT = 3249
616455
YDOT = -21784
371088 feet/sec YDOT = -6639
876308 meter/sec
ZDOT = 93
183573 ZDOT = 28
402353
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 10121
88443724
00016717 00000-0 10270-3 0 9125
2 25544 51
6440 108
2097 0010024 265
5324 94
4694 15
73522120 16183
Satellite: ISS
Catalog Number: 25544
Epoch time: 10121
88443724 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 108
2097 deg
Eccentricity:
0010024
Arg of perigee: 265
5324 deg
Mean anomaly: 94
4694 deg
Mean motion: 15
73522120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1618
Checksum: 282
Coasting Arc #14 (Orbit 1633)
---------------------------------------
Vector Time (GMT): 2010/122/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1353909
75 A = 6733516
93 meter
Y = -6589099
93 meter E =
0008832
Z = 107790
15 I = 51
99424
XDOT = 4664
552980 Wp = 186
61187
YDOT = 860
157321 meter/sec RA = 102
32884 deg
ZDOT = -6066
487864 TA = 352
22301
MA = 352
23669
Ha = 188
186 n
mi
Hp = 187
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4441961
13 X = 1426966
00
Y = -21617781
92 feet Y = -6573551
23 meter
Z = 353642
23 Z = 114544
41
XDOT = 15303
651509 XDOT = 4684
057973
YDOT = 2822
038455 feet/sec YDOT = 912
428678 meter/sec
ZDOT = -19903
175408 ZDOT = -6043
779855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7193528
63 X = -2192587
53
Y = 20863676
77 feet Y = 6359248
68 meter
Z = 380413
00 Z = 115949
88
XDOT = -13405
942549 XDOT = -4086
131289
YDOT = -4264
138002 feet/sec YDOT = -1299
709263 meter/sec
ZDOT = -19812
742225 ZDOT = -6038
923830
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 10122
90058057
00016717 00000-0 10270-3 0 9131
2 25544 51
6446 102
9964 0010039 269
1594 90
8419 15
73527345 16345
Satellite: ISS
Catalog Number: 25544
Epoch time: 10122
90058057 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 102
9964 deg
Eccentricity:
0010039
Arg of perigee: 269
1594 deg
Mean anomaly: 90
8419 deg
Mean motion: 15
73527345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1634
Checksum: 310
Coasting Arc #15 (Orbit 1649)
---------------------------------------
Vector Time (GMT): 2010/123/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4146120
71 A = 6721445
41 meter
Y = -220281
26 meter E =
0007570
Z = 5292198
99 I = 51
95837
XDOT = 754
658142 Wp = 269
40850
YDOT = -7653
048489 meter/sec RA = 97
22302 deg
ZDOT = 272
937782 TA = 178
01170
MA = 178
00869
Ha = 188
331 n
mi
Hp = 187
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13602758
25 X = -4169057
98
Y = -722707
55 feet Y = -266774
28 meter
Z = 17362857
58 Z = 5272001
33
XDOT = 2475
912539 XDOT = 838
853930
YDOT = -25108
426802 feet/sec YDOT = -7644
138709 meter/sec
ZDOT = 895
465164 ZDOT = 276
807887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13537655
01 X = 4126277
25
Y = 2252958
28 feet Y = 686701
68 meter
Z = 17282425
68 Z = 5267683
35
XDOT = -5103
518503 XDOT = -1555
552440
YDOT = 23686
404834 feet/sec YDOT = 7219
616193 meter/sec
ZDOT = 910
742228 ZDOT = 277
594231
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 10123
91670395
00016717 00000-0 10270-3 0 9149
2 25544 51
6440 97
7810 0010007 272
9349 87
0668 15
73536612 16504
Satellite: ISS
Catalog Number: 25544
Epoch time: 10123
91670395 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 97
7810 deg
Eccentricity:
0010007
Arg of perigee: 272
9349 deg
Mean anomaly: 87
0668 deg
Mean motion: 15
73536612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1650
Checksum: 307
Coasting Arc #16 (Orbit 1664)
---------------------------------------
Vector Time (GMT): 2010/124/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 34312
86 A = 6733306
29 meter
Y = 6716984
66 meter E =
0009921
Z = -360100
41 I = 52
00044
XDOT = -4746
600469 Wp = 346
61056
YDOT = 350
112716 meter/sec RA = 92
10778 deg
ZDOT = 6054
875817 TA = 9
49413
MA = 9
47539
Ha = 188
732 n
mi
Hp = 187
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 112574
99 X = -39050
92
Y = 22037351
24 feet Y = 6716958
19 meter
Z = -1181431
78 Z = -360111
53
XDOT = -15572
836185 XDOT = -4779
576266
YDOT = 1148
663765 feet/sec YDOT = 296
848681 meter/sec
ZDOT = 19865
078141 ZDOT = 6031
736704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1972681
88 X = 601273
44
Y = -21949173
26 feet Y = -6690108
01 meter
Z = -1181365
11 Z = -360080
08
XDOT = 14127
308679 XDOT = 4306
003685
YDOT = 201
304520 feet/sec YDOT = 61
357618 meter/sec
ZDOT = 19772
936850 ZDOT = 6026
791152
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 10124
86929981
00016717 00000-0 10270-3 0 9153
2 25544 51
6431 92
8914 0010092 276
5342 83
4672 15
73582987 16659
Satellite: ISS
Catalog Number: 25544
Epoch time: 10124
86929981 = yrday
fracday
Element set: 915
Inclination: 51
6431 deg
RA of node: 92
8914 deg
Eccentricity:
0010092
Arg of perigee: 276
5342 deg
Mean anomaly: 83
4672 deg
Mean motion: 15
73582987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1665
Checksum: 336
Coasting Arc #17 (Orbit 1680)
---------------------------------------
Vector Time (GMT): 2010/125/20:50:47
602
Vector Time (MET): N/A
Weight (LBS) : 793448
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4090107
86 A = 6721244
60 meter
Y = -818040
64 meter E =
0005789
Z = -5274927
62 I = 51
95945
XDOT = 824
131418 Wp = 61
16114
YDOT = 7633
365330 meter/sec RA = 87
00712 deg
ZDOT = -542
485209 TA = 203
69117
MA = 203
71783
Ha = 189
035 n
mi
Hp = 187
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13418989
04 X = 4124576
05
Y = -2683860
37 feet Y = -772109
68 meter
Z = -17306192
99 Z = -5254974
15
XDOT = 2703
843236 XDOT = 741
347803
YDOT = 25043
849507 feet/sec YDOT = 7642
118412 meter/sec
ZDOT = -1779
807115 ZDOT = -538
682338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13688562
59 X = -4172273
88
Y = 1624601
00 feet Y = 495178
38 meter
Z = -17226741
28 Z = -5250710
74
XDOT = -639
750092 XDOT = -194
995828
YDOT = -24180
860578 feet/sec YDOT = -7370
326304 meter/sec
ZDOT = -1764
542900 ZDOT = -537
832676
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 10125
88538379
00016717 00000-0 10270-3 0 9164
2 25544 51
6424 87
6763 0009941 279
9350 80
0691 15
73630534 16816
Satellite: ISS
Catalog Number: 25544
Epoch time: 10125
88538379 = yrday
fracday
Element set: 916
Inclination: 51
6424 deg
RA of node: 87
6763 deg
Eccentricity:
0009941
Arg of perigee: 279
9350 deg
Mean anomaly: 80
0691 deg
Mean motion: 15
73630534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1681
Checksum: 334
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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