Date:
January 24th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 2288)
---------------------------------------
Vector Time (GMT): 2009/021/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4052005
36 A = 6732028
62 meter
Y = 2435882
38 meter E =
0001652
Z = 4794020
11 I = 51
49956
XDOT = -5685
946502 Wp = 256
68714
YDOT = 4540
265998 meter/sec RA = 337
24860 deg
ZDOT = 2499
279423 TA = 168
78940
MA = 168
78572
Ha = 194
445 n
mi
Hp = 192
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13293980
83 X = 4001177
60
Y = 7991740
10 feet Y = 2480909
55 meter
Z = 15728412
43 Z = 4813581
29
XDOT = -18654
680126 XDOT = -5748
434795
YDOT = 14895
885820 feet/sec YDOT = 4476
332789 meter/sec
ZDOT = 8199
735640 ZDOT = 2471
506175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1762930
89 X = 537341
34
Y = 15332453
34 feet Y = 4673331
78 meter
Z = 15804706
36 Z = 4817274
50
XDOT = -22109
097080 XDOT = -6738
852790
YDOT = -5797
839042 feet/sec YDOT = -1767
181340 meter/sec
ZDOT = 8091
882002 ZDOT = 2466
405634
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 09021
57283020
00010596 00000-0 82463-4 0 9009
2 25544 51
6410 337
4783 0008375 292
8803 67
1474 15
70526653 22899
Satellite: ISS
Catalog Number: 25544
Epoch time: 09021
57283020 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 337
4783 deg
Eccentricity:
0008375
Arg of perigee: 292
8803 deg
Mean anomaly: 67
1474 deg
Mean motion: 15
70526653 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2289
Checksum: 308
Coasting Arc #2 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2009/022/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3576792
40 A = 6737868
32 meter
Y = -4746281
37 meter E =
0005676
Z = -3166528
41 I = 51
49179
XDOT = 5879
269902 Wp = 327
89325
YDOT = 1219
607281 meter/sec RA = 332
08508 deg
ZDOT = 4813
726931 TA = 355
17143
MA = 355
17690
Ha = 194
834 n
mi
Hp = 191
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11734883
20 X = 3644982
42
Y = -15571789
27 feet Y = -4705901
98 meter
Z = -10388872
72 Z = -3148987
54
XDOT = 19288
943249 XDOT = 5841
811287
YDOT = 4001
336224 feet/sec YDOT = 1285
142715 meter/sec
ZDOT = 15793
067358 ZDOT = 4842
197080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19526972
60 X = 5951821
25
Y = -542102
81 feet Y = -165232
93 meter
Z = -10320864
64 Z = -3145799
54
XDOT = 8850
315394 XDOT = 2697
576132
YDOT = 16055
463221 feet/sec YDOT = 4893
705190 meter/sec
ZDOT = 15903
976589 ZDOT = 4847
532064
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 09022
52729661
00010596 00000-0 82463-4 0 9012
2 25544 51
6407 332
6017 0008384 297
5831 62
4478 15
70499144 23049
Satellite: ISS
Catalog Number: 25544
Epoch time: 09022
52729661 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 332
6017 deg
Eccentricity:
0008384
Arg of perigee: 297
5831 deg
Mean anomaly: 62
4478 deg
Mean motion: 15
70499144 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2304
Checksum: 311
Coasting Arc #3 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2009/023/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5772741
03 A = 6736790
11 meter
Y = 477992
63 meter E =
0005125
Z = -3442595
84 I = 51
46441
XDOT = 2241
143581 Wp = 336
45860
YDOT = -5778
017255 meter/sec RA = 327
01487 deg
ZDOT = -4553
381379 TA = 244
32025
MA = 244
37319
Ha = 194
896 n
mi
Hp = 191
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18939439
08 X = -5760933
83
Y = 1568217
30 feet Y = 413504
88 meter
Z = -11294605
76 Z = -3470610
49
XDOT = 7352
833272 XDOT = 2327
706788
YDOT = -18956
749524 feet/sec YDOT = -5752
471005 meter/sec
ZDOT = -14938
915284 ZDOT = -4542
284489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13266629
39 X = -4043668
64
Y = -13516034
50 feet Y = -4119687
32 meter
Z = -11403645
61 Z = -3475831
18
XDOT = 18349
628064 XDOT = 5592
966634
YDOT = -5423
977885 feet/sec YDOT = -1653
228459 meter/sec
ZDOT = -14896
057521 ZDOT = -4540
318332
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 09023
54537858
00010596 00000-0 82463-4 0 9021
2 25544 51
6416 327
4003 0008329 301
7671 58
2678 15
70548313 23201
Satellite: ISS
Catalog Number: 25544
Epoch time: 09023
54537858 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 327
4003 deg
Eccentricity:
0008329
Arg of perigee: 301
7671 deg
Mean anomaly: 58
2678 deg
Mean motion: 15
70548313 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2320
Checksum: 302
Coasting Arc #4 (Orbit 2335)
---------------------------------------
Vector Time (GMT): 2009/024/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -265602
19 A = 6732774
03 meter
Y = 4893930
64 meter E =
0008394
Z = 4619584
01 I = 51
42681
XDOT = -6728
414517 Wp = 4
26003
YDOT = 2363
279598 meter/sec RA = 321
84517 deg
ZDOT = -2881
904969 TA = 114
41974
MA = 114
33213
Ha = 195
070 n
mi
Hp = 191
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -871398
27 X = -342747
74
Y = 16056202
90 feet Y = 4890528
74 meter
Z = 15156115
51 Z = 4618106
83
XDOT = -22074
850778 XDOT = -6740
341608
YDOT = 7753
541988 feet/sec YDOT = 2287
972152 meter/sec
ZDOT = -9455
068795 ZDOT = -2914
619540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12797641
95 X = -3900721
27
Y = 9744055
84 feet Y = 2969988
22 meter
Z = 15150662
04 Z = 4617921
79
XDOT = -19527
334425 XDOT = -5951
931533
YDOT = -10703
898262 feet/sec YDOT = -3262
548190 meter/sec
ZDOT = -9582
296547 ZDOT = -2920
683988
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 09024
56344629
00010596 00000-0 82463-4 0 9037
2 25544 51
6417 322
1994 0008314 305
3354 54
7030 15
70553638 23361
Satellite: ISS
Catalog Number: 25544
Epoch time: 09024
56344629 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 322
1994 deg
Eccentricity:
0008314
Arg of perigee: 305
3354 deg
Mean anomaly: 54
7030 deg
Mean motion: 15
70553638 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2336
Checksum: 298
Coasting Arc #5 (Orbit 2351)
---------------------------------------
Vector Time (GMT): 2009/025/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5518317
96 A = 6740944
58 meter
Y = -3555211
22 meter E =
0013250
Z = 1493438
95 I = 51
43234
XDOT = 1560
761760 Wp = 26
21594
YDOT = 4850
668385 meter/sec RA = 316
75646 deg
ZDOT = 5772
431665 TA = 350
26674
MA = 350
29239
Ha = 195
156 n
mi
Hp = 191
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18104717
73 X = 5550408
14
Y = -11664078
81 feet Y = -3493322
88 meter
Z = 4899734
10 Z = 1520323
86
XDOT = 5120
609450 XDOT = 1478
364133
YDOT = 15914
266356 feet/sec YDOT = 4867
660557 meter/sec
ZDOT = 18938
424099 ZDOT = 5779
813888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20732448
91 X = 6319250
43
Y = 5741303
79 feet Y = 1749949
40 meter
Z = 5004190
83 Z = 1525277
37
XDOT = -8132
931578 XDOT = -2478
917545
YDOT = 12814
846739 feet/sec YDOT = 3905
965286 meter/sec
ZDOT = 18967
468961 ZDOT = 5781
284539
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 09025
58149910
00010596 00000-0 82463-4 0 9047
2 25544 51
6418 316
9975 0008378 309
4231 50
6188 15
70572686 23522
Satellite: ISS
Catalog Number: 25544
Epoch time: 09025
58149910 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 316
9975 deg
Eccentricity:
0008378
Arg of perigee: 309
4231 deg
Mean anomaly: 50
6188 deg
Mean motion: 15
70572686 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2352
Checksum: 329
Coasting Arc #6 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2009/026/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2791238
58 A = 6729860
31 meter
Y = -3169955
64 meter E =
0009933
Z = -5246607
73 I = 51
37535
XDOT = 5368
393713 Wp = 61
44380
YDOT = -5485
912863 meter/sec RA = 311
61210 deg
ZDOT = 463
850332 TA = 212
95352
MA = 213
01548
Ha = 195
271 n
mi
Hp = 190
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9157606
89 X = -2730097
83
Y = -10400116
92 feet Y = -3200826
72 meter
Z = -17213279
97 Z = -5260018
86
XDOT = 17612
840265 XDOT = 5427
085872
YDOT = -17998
401783 feet/sec YDOT = -5425
552232 meter/sec
ZDOT = 1521
818676 ZDOT = 490
071469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1506671
79 X = 459233
56
Y = -13709366
33 feet Y = -4178614
86 meter
Z = -17265700
63 Z = -5262585
55
XDOT = 24165
404789 XDOT = 7365
615380
YDOT = 633
058135 feet/sec YDOT = 192
956119 meter/sec
ZDOT = 1623
564768 ZDOT = 494
862541
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 09026
53590980
00010596 00000-0 82463-4 0 9051
2 25544 51
6424 312
1212 0008363 313
0015 47
0445 15
70609316 23679
Satellite: ISS
Catalog Number: 25544
Epoch time: 09026
53590980 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 312
1212 deg
Eccentricity:
0008363
Arg of perigee: 313
0015 deg
Mean anomaly: 47
0445 deg
Mean motion: 15
70609316 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2367
Checksum: 280
Coasting Arc #7 (Orbit 2382)
---------------------------------------
Vector Time (GMT): 2009/027/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3535565
95 A = 6741646
56 meter
Y = 5697284
21 meter E =
0005219
Z = 682242
76 I = 51
39640
XDOT = -4420
150040 Wp = 114
43805
YDOT = -2025
315577 meter/sec RA = 306
48210 deg
ZDOT = -5959
707459 TA = 58
11945
MA = 58
06868
Ha = 195
479 n
mi
Hp = 190
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11599625
81 X = -3602325
27
Y = 18691877
32 feet Y = 5657374
16 meter
Z = 2238329
27 Z = 664905
53
XDOT = -14501
804592 XDOT = -4368
223756
YDOT = -6644
736145 feet/sec YDOT = -2074
453707 meter/sec
ZDOT = -19552
845993 ZDOT = -5981
053886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21539575
80 X = -6565262
70
Y = 4503364
96 feet Y = 1372625
64 meter
Z = 2171196
16 Z = 661780
59
XDOT = -4797
916972 XDOT = -1462
405093
YDOT = -13426
421171 feet/sec YDOT = -4092
373173 meter/sec
ZDOT = -19636
095560 ZDOT = -5985
081927
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 09027
55393461
00010596 00000-0 82463-4 0 9060
2 25544 51
6424 306
9197 0008326 316
4703 43
5800 15
70610427 23831
Satellite: ISS
Catalog Number: 25544
Epoch time: 09027
55393461 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 306
9197 deg
Eccentricity:
0008326
Arg of perigee: 316
4703 deg
Mean anomaly: 43
5800 deg
Mean motion: 15
70610427 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2383
Checksum: 301
Coasting Arc #8 (Orbit 2398)
---------------------------------------
Vector Time (GMT): 2009/028/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4546140
58 A = 6730923
87 meter
Y = 165937
41 meter E =
0003195
Z = 4960411
28 I = 51
34415
XDOT = -2422
901168 Wp = 350
07355
YDOT = 7028
514606 meter/sec RA = 301
37553 deg
ZDOT = 1988
722497 TA = 80
62013
MA = 80
58401
Ha = 195
473 n
mi
Hp = 190
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14915159
37 X = 4519851
01
Y = 544414
06 feet Y = 216627
92 meter
Z = 16274315
23 Z = 4982432
00
XDOT = -7949
150813 XDOT = -2510
975705
YDOT = 23059
431122 feet/sec YDOT = 7000
927838 meter/sec
ZDOT = 6524
680108 ZDOT = 1976
738530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10027506
34 X = 3056383
93
Y = 10927440
42 feet Y = 3330683
84 meter
Z = 16360069
21 Z = 4986549
09
XDOT = -21221
681980 XDOT = -6468
368668
YDOT = 9790
740958 feet/sec YDOT = 2984
217844 meter/sec
ZDOT = 6478
489727 ZDOT = 1974
643669
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 09028
57194366
00010596 00000-0 82463-4 0 9077
2 25544 51
6421 301
7178 0008388 320
3518 39
7030 15
70658163 23994
Satellite: ISS
Catalog Number: 25544
Epoch time: 09028
57194366 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 301
7178 deg
Eccentricity:
0008388
Arg of perigee: 320
3518 deg
Mean anomaly: 39
7030 deg
Mean motion: 15
70658163 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2399
Checksum: 321
Coasting Arc #9 (Orbit 2413)
---------------------------------------
Vector Time (GMT): 2009/029/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 588068
38 A = 6738425
67 meter
Y = -6128453
97 meter E =
0009501
Z = -2724848
25 I = 51
35553
XDOT = 5449
967548 Wp = 354
36116
YDOT = -1760
405950 meter/sec RA = 296
20581 deg
ZDOT = 5143
316094 TA = 334
42822
MA = 334
47518
Ha = 195
697 n
mi
Hp = 190
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1929358
20 X = 669790
57
Y = -20106476
28 feet Y = -6121420
92 meter
Z = -8939790
84 Z = -2721792
97
XDOT = 17880
470958 XDOT = 5444
262917
YDOT = -5775
610073 feet/sec YDOT = -1699
493135 meter/sec
ZDOT = 16874
396634 ZDOT = 5169
777577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15476140
19 X = 4717127
53
Y = -12987953
86 feet Y = -3958728
34 meter
Z = -8928315
13 Z = -2721350
45
XDOT = 15803
589670 XDOT = 4816
934132
YDOT = 7178
065044 feet/sec YDOT = 2187
874226 meter/sec
ZDOT = 16977
309350 ZDOT = 5174
683890
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 09029
52631494
00010596 00000-0 82463-4 0 9082
2 25544 51
6424 296
8410 0008459 324
0807 35
9784 15
70680968 24141
Satellite: ISS
Catalog Number: 25544
Epoch time: 09029
52631494 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 296
8410 deg
Eccentricity:
0008459
Arg of perigee: 324
0807 deg
Mean anomaly: 35
9784 deg
Mean motion: 15
70680968 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2414
Checksum: 333
Coasting Arc #10 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2009/030/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4531133
18 A = 6735088
39 meter
Y = 3167311
46 meter E =
0009183
Z = -3855516
47 I = 51
33257
XDOT = -1016
901133 Wp = 10
21105
YDOT = -6433
709047 meter/sec RA = 291
12324 deg
ZDOT = -4082
788738 TA = 216
89685
MA = 216
96006
Ha = 195
861 n
mi
Hp = 189
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14865922
51 X = -4547484
76
Y = 10391441
81 feet Y = 3116550
24 meter
Z = -12649332
26 Z = -3877568
06
XDOT = -3336
289808 XDOT = -925
049673
YDOT = -21107
969314 feet/sec YDOT = -6444
567097 meter/sec
ZDOT = -13394
976175 ZDOT = -4087
505588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17888501
48 X = -5452415
25
Y = -2608696
08 feet Y = -795130
57 meter
Z = -12734973
16 Z = -3881619
82
XDOT = 11939
964497 XDOT = 3639
301179
YDOT = -16274
832678 feet/sec YDOT = -4960
569000 meter/sec
ZDOT = -13413
791554 ZDOT = -4088
523666
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 09030
54429653
00010596 00000-0 82463-4 0 9099
2 25544 51
6423 291
6391 0008575 327
3894 32
6737 15
70693710 24301
Satellite: ISS
Catalog Number: 25544
Epoch time: 09030
54429653 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 291
6391 deg
Eccentricity:
0008575
Arg of perigee: 327
3894 deg
Mean anomaly: 32
6737 deg
Mean motion: 15
70693710 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2430
Checksum: 320
Coasting Arc #11 (Orbit 2445)
---------------------------------------
Vector Time (GMT): 2009/031/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2212161
01 A = 6733505
18 meter
Y = 4712207
12 meter E =
0011842
Z = 4273082
61 I = 51
31784
XDOT = -4407
253036 Wp = 26
08101
YDOT = 5248
952887 meter/sec RA = 285
93973 deg
ZDOT = -3492
580983 TA = 99
55057
MA = 99
41673
Ha = 195
962 n
mi
Hp = 189
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7257746
09 X = 2138546
34
Y = 15459997
11 feet Y = 4736533
22 meter
Z = 14019299
90 Z = 4283650
29
XDOT = -14459
491589 XDOT = -4448
654048
YDOT = 17220
974039 feet/sec YDOT = 5199
436912 meter/sec
ZDOT = -11458
599024 ZDOT = -3514
091720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5124517
26 X = -1561952
86
Y = 16256104
47 feet Y = 4954860
64 meter
Z = 14060780
52 Z = 4285725
90
XDOT = -21055
249281 XDOT = -6417
639981
YDOT = 3385
968983 feet/sec YDOT = 1032
043346 meter/sec
ZDOT = -11541
983716 ZDOT = -3517
996637
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 09031
56226377
00010596 00000-0 82463-4 0 9102
2 25544 51
6419 286
4365 0008657 331
6770 28
3920 15
70745573 24469
Satellite: ISS
Catalog Number: 25544
Epoch time: 09031
56226377 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 286
4365 deg
Eccentricity:
0008657
Arg of perigee: 331
6770 deg
Mean anomaly: 28
3920 deg
Mean motion: 15
70745573 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2446
Checksum: 321
Coasting Arc #12 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2009/032/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2833580
03 A = 6739518
50 meter
Y = -5718835
06 meter E =
0015822
Z = 2132383
33 I = 51
33089
XDOT = 3730
158913 Wp = 37
21505
YDOT = 3900
535407 meter/sec RA = 280
84949 deg
ZDOT = 5495
269135 TA = 346
73044
MA = 346
77201
Ha = 196
092 n
mi
Hp = 189
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9296522
39 X = 2886959
76
Y = -18762582
21 feet Y = -5686849
87 meter
Z = 6996008
32 Z = 2146278
36
XDOT = 12238
054177 XDOT = 3659
570498
YDOT = 12797
032175 feet/sec YDOT = 3941
853506 meter/sec
ZDOT = 18029
098211 ZDOT = 5513
218620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19352624
94 X = 5898680
08
Y = -7948681
36 feet Y = -2422758
08 meter
Z = 7049703
87 Z = 2148749
74
XDOT = 55
357199 XDOT = 16
872874
YDOT = 16212
510505 feet/sec YDOT = 4941
573202 meter/sec
ZDOT = 18099
266691 ZDOT = 5516
656487
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 09032
58021828
00010596 00000-0 82463-4 0 9110
2 25544 51
6418 281
2334 0008697 335
4820 24
5927 15
70724106 24621
Satellite: ISS
Catalog Number: 25544
Epoch time: 09032
58021828 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 281
2334 deg
Eccentricity:
0008697
Arg of perigee: 335
4820 deg
Mean anomaly: 24
5927 deg
Mean motion: 15
70724106 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2462
Checksum: 301
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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