Date:
April 24th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 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
116/04:28:00
598 -5
5 8
2 8
2
N/A 0
4 -0
2 189
7
000/00:12:01
195 -6
1 -0
0 179
4
Coasting Arc #1 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2008/112/06:06:59
969
Vector Time (MET): N/A
Weight (LBS) : 614728
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1938686
34 A = 6720074
05 meter
Y = 5821766
59 meter E =
0016162
Z = 2725385
23 I = 51
39666
XDOT = -5718
370936 Wp = 91
97154
YDOT = 515
576430 meter/sec RA = 309
18755 deg
ZDOT = -5143
424142 TA = 56
73502
MA = 56
58027
Ha = 186
397 n
mi
Hp = 177
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6360519
48 X = -2016881
83
Y = 19100284
08 feet Y = 5799649
86 meter
Z = 8941552
59 Z = 2715777
00
XDOT = -18761
059502 XDOT = -5698
724889
YDOT = 1691
523722 feet/sec YDOT = 451
740211 meter/sec
ZDOT = -16874
751123 ZDOT = -5171
156790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19697344
41 X = -6003750
58
Y = 4235457
57 feet Y = 1290967
47 meter
Z = 8905276
26 Z = 2714328
20
XDOT = -10672
247417 XDOT = -3252
901013
YDOT = -13750
957899 feet/sec YDOT = -4191
291968 meter/sec
ZDOT = -16981
072408 ZDOT = -5175
830870
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 08112
29205406
00020000 00000-0 20000-3 0 9009
2 25544 51
6398 309
6023 0003397 54
2033 305
9447 15
77129976 19552
Satellite: ISS
Catalog Number: 25544
Epoch time: 08112
29205406 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 309
6023 deg
Eccentricity:
0003397
Arg of perigee: 54
2033 deg
Mean anomaly: 305
9447 deg
Mean motion: 15
77129976 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1955
Checksum: 293
Coasting Arc #2 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2008/113/06:06:59
969
Vector Time (MET): N/A
Weight (LBS) : 614728
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4541093
11 A = 6712402
51 meter
Y = 316111
15 meter E =
0007892
Z = 4926873
01 I = 51
35396
XDOT = -2705
828944 Wp = 101
33920
YDOT = 6925
171348 meter/sec RA = 304
04895 deg
ZDOT = 2045
344869 TA = 328
78420
MA = 328
83105
Ha = 186
162 n
mi
Hp = 177
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14898599
44 X = 4513286
48
Y = 1037110
07 feet Y = 366736
64 meter
Z = 16164281
52 Z = 4948866
52
XDOT = -8877
391549 XDOT = -2793
002292
YDOT = 22720
378437 feet/sec YDOT = 6894
425755 meter/sec
ZDOT = 6710
449046 ZDOT = 2031
988140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6892480
91 X = 2100828
18
Y = 13145424
51 feet Y = 4006725
39 meter
Z = 16248673
21 Z = 4952595
59
XDOT = -23058
780675 XDOT = -7028
316350
YDOT = 3840
885599 feet/sec YDOT = 1170
701931 meter/sec
ZDOT = 6659
900937 ZDOT = 2029
937805
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 08113
30585955
00020000 00000-0 20000-3 0 9013
2 25544 51
6398 304
3713 0003284 57
4670 302
6812 15
77183020 19715
Satellite: ISS
Catalog Number: 25544
Epoch time: 08113
30585955 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 304
3713 deg
Eccentricity:
0003284
Arg of perigee: 57
4670 deg
Mean anomaly: 302
6812 deg
Mean motion: 15
77183020 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1971
Checksum: 280
Coasting Arc #3 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2008/114/06:06:59
969
Vector Time (MET): N/A
Weight (LBS) : 614728
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2677889
59 A = 6722909
33 meter
Y = -6113798
14 meter E =
0013815
Z = -755803
90 I = 51
37429
XDOT = 4701
973523 Wp = 43
89810
YDOT = 1332
086360 meter/sec RA = 298
84494 deg
ZDOT = 5958
822936 TA = 307
82112
MA = 307
94609
Ha = 186
340 n
mi
Hp = 177
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8785726
99 X = 2749727
63
Y = -20058392
84 feet Y = -6083450
74 meter
Z = -2479671
60 Z = -742620
27
XDOT = 15426
422321 XDOT = 4657
781070
YDOT = 4370
362073 feet/sec YDOT = 1384
419149 meter/sec
ZDOT = 19549
944017 ZDOT = 5981
558242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21635596
34 X = 6594529
77
Y = -3416782
28 feet Y = -1041435
24 meter
Z = -2429704
34 Z = -740573
88
XDOT = 4336
704797 XDOT = 1321
827622
YDOT = 13674
253194 feet/sec YDOT = 4167
912374 meter/sec
ZDOT = 19637
283784 ZDOT = 5985
444097
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 08114
25628615
00020000 00000-0 20000-3 0 9020
2 25544 51
6401 299
4671 0003381 58
4024 301
7470 15
77176503 19863
Satellite: ISS
Catalog Number: 25544
Epoch time: 08114
25628615 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 299
4671 deg
Eccentricity:
0003381
Arg of perigee: 58
4024 deg
Mean anomaly: 301
7470 deg
Mean motion: 15
77176503 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1986
Checksum: 285
Coasting Arc #4 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2008/115/06:06:59
969
Vector Time (MET): N/A
Weight (LBS) : 614728
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3669367
69 A = 6710975
28 meter
Y = -2073259
12 meter E =
0017980
Z = -5237903
20 I = 51
32230
XDOT = 3361
811839 Wp = 87
30376
YDOT = -6909
125815 meter/sec RA = 293
66773 deg
ZDOT = 381
632172 TA = 186
32813
MA = 186
35087
Ha = 186
284 n
mi
Hp = 177
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12038607
90 X = -3620466
30
Y = -6802031
23 feet Y = -2114018
35 meter
Z = -17184721
78 Z = -5255610
60
XDOT = 11029
566400 XDOT = 3436
966977
YDOT = -22667
735615 feet/sec YDOT = -6871
111923 meter/sec
ZDOT = 1252
074055 ZDOT = 398
146238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -953618
16 X = -290662
81
Y = -13709124
39 feet Y = -4178541
11 meter
Z = -17252851
72 Z = -5258669
21
XDOT = 23977
613480 XDOT = 7308
376589
YDOT = -3314
434063 feet/sec YDOT = -1010
239502 meter/sec
ZDOT = 1314
740634 ZDOT = 400
732945
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 08115
27005408
00020000 00000-0 20000-3 0 9033
2 25544 51
6409 294
2358 0003389 61
8010 298
3497 15
77226915 20020
Satellite: ISS
Catalog Number: 25544
Epoch time: 08115
27005408 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 294
2358 deg
Eccentricity:
0003389
Arg of perigee: 61
8010 deg
Mean anomaly: 298
3497 deg
Mean motion: 15
77226915 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2002
Checksum: 285
Coasting Arc #5 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2008/116/04:34:01
195
Vector Time (MET): N/A
Weight (LBS) : 614216
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2752976
20 A = 6727280
15 meter
Y = 6076849
55 meter E =
0017205
Z = -805435
15 I = 51
35106
XDOT = -4123
603711 Wp = 139
01890
YDOT = -2645
305400 meter/sec RA = 288
83145 deg
ZDOT = -5948
239623 TA = 49
80931
MA = 49
65883
Ha = 189
746 n
mi
Hp = 179
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9032074
16 X = -2816811
17
Y = 19937170
43 feet Y = 6045707
33 meter
Z = -2642503
77 Z = -818963
92
XDOT = -13528
883565 XDOT = -4064
821199
YDOT = -8678
823490 feet/sec YDOT = -2691
088823 meter/sec
ZDOT = -19515
221861 ZDOT = -5968
129724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21319588
38 X = -6498210
54
Y = -4926513
74 feet Y = -1501601
39 meter
Z = -2693801
82 Z = -821070
79
XDOT = 5515
921069 XDOT = 1681
252742
YDOT = -13306
067114 feet/sec YDOT = -4055
689256 meter/sec
ZDOT = -19591
785780 ZDOT = -5971
576306
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 08116
22048255
00020000 00000-0 20000-3 0 9047
2 25544 51
6400 289
3315 0006872 136
6595 223
5111 15
75619929 20176
Satellite: ISS
Catalog Number: 25544
Epoch time: 08116
22048255 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 289
3315 deg
Eccentricity:
0006872
Arg of perigee: 136
6595 deg
Mean anomaly: 223
5111 deg
Mean motion: 15
75619929 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2017
Checksum: 285
Coasting Arc #6 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2008/117/04:34:01
195
Vector Time (MET): N/A
Weight (LBS) : 614216
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3534893
65 A = 6716100
89 meter
Y = 2627930
09 meter E =
0008537
Z = 5062365
87 I = 51
30539
XDOT = -2958
475232 Wp = 105
57575
YDOT = 6951
174552 meter/sec RA = 283
64065 deg
ZDOT = -1542
729643 TA = 359
27752
MA = 359
27875
Ha = 189
458 n
mi
Hp = 179
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11597420
12 X = 3480652
74
Y = 8621817
87 feet Y = 2667155
67 meter
Z = 16608811
93 Z = 5079406
96
XDOT = -9706
283570 XDOT = -3028
490106
YDOT = 22805
690787 feet/sec YDOT = 6917
699822 meter/sec
ZDOT = -5061
448959 ZDOT = -1557
271638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5971234
92 X = -1820032
40
Y = 13076528
03 feet Y = 3985725
74 meter
Z = 16674450
48 Z = 5082372
50
XDOT = -23390
996200 XDOT = -7129
575642
YDOT = -4157
335909 feet/sec YDOT = -1267
155985 meter/sec
ZDOT = -5116
546637 ZDOT = -1559
523415
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 08117
23525087
00020000 00000-0 20000-3 0 9053
2 25544 51
6396 284
1080 0006686 140
2546 219
9109 15
75683307 20337
Satellite: ISS
Catalog Number: 25544
Epoch time: 08117
23525087 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 284
1080 deg
Eccentricity:
0006686
Arg of perigee: 140
2546 deg
Mean anomaly: 219
9109 deg
Mean motion: 15
75683307 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2033
Checksum: 292
Coasting Arc #7 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2008/118/04:34:01
195
Vector Time (MET): N/A
Weight (LBS) : 614216
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2415940
07 A = 6725838
67 meter
Y = -5983801
23 meter E =
0017001
Z = 1880742
22 I = 51
33280
XDOT = 4031
511991 Wp = 89
30289
YDOT = 3405
147637 meter/sec RA = 278
49954 deg
ZDOT = 5611
666328 TA = 291
69684
MA = 291
87776
Ha = 189
510 n
mi
Hp = 179
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7926312
55 X = 2473535
95
Y = -19631893
80 feet Y = -5956462
89 meter
Z = 6170414
09 Z = 1892618
46
XDOT = 13226
745376 XDOT = 3965
874855
YDOT = 11171
744217 feet/sec YDOT = 3449
862975 meter/sec
ZDOT = 18410
978766 ZDOT = 5631
092294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20920434
13 X = 6376548
32
Y = 3164838
35 feet Y = 964642
73 meter
Z = 6215378
42 Z = 1894447
34
XDOT = -7623
881770 XDOT = -2323
759163
YDOT = 13813
829260 feet/sec YDOT = 4210
455159 meter/sec
ZDOT = 18485
851809 ZDOT = 5634
487631
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 08118
25000229
00020000 00000-0 20000-3 0 9063
2 25544 51
6398 278
8833 0006661 143
4827 216
6793 15
75683062 20493
Satellite: ISS
Catalog Number: 25544
Epoch time: 08118
25000229 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 278
8833 deg
Eccentricity:
0006661
Arg of perigee: 143
4827 deg
Mean anomaly: 216
6793 deg
Mean motion: 15
75683062 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2049
Checksum: 308
Coasting Arc #8 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2008/119/04:34:01
195
Vector Time (MET): N/A
Weight (LBS) : 614216
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3544359
50 A = 6717795
88 meter
Y = -3323219
97 meter E =
0016651
Z = -4655338
32 I = 51
30349
XDOT = 2611
996459 Wp = 123
27281
YDOT = -6678
634828 meter/sec RA = 273
28866 deg
ZDOT = 2777
057612 TA = 174
29775
MA = 174
27876
Ha = 189
361 n
mi
Hp = 179
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11628476
04 X = -3484320
43
Y = -10902952
67 feet Y = -3362519
11 meter
Z = -15273419
70 Z = -4672411
21
XDOT = 8569
542188 XDOT = 2672
993376
YDOT = -21911
531589 feet/sec YDOT = -6649
085072 meter/sec
ZDOT = 9111
081405 ZDOT = 2789
894581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7719010
62 X = 2352754
44
Y = -13874329
93 feet Y = -4228895
76 meter
Z = -15339264
17 Z = -4675407
72
XDOT = 22323
780504 XDOT = 6804
288298
YDOT = 2286
437902 feet/sec YDOT = 696
906273 meter/sec
ZDOT = 9159
657061 ZDOT = 2791
863472
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 08119
20131320
00020000 00000-0 20000-3 0 9077
2 25544 51
6402 273
9853 0006557 147
2004 212
9568 15
75718636 20642
Satellite: ISS
Catalog Number: 25544
Epoch time: 08119
20131320 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 273
9853 deg
Eccentricity:
0006557
Arg of perigee: 147
2004 deg
Mean anomaly: 212
9568 deg
Mean motion: 15
75718636 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2064
Checksum: 281
Coasting Arc #9 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2008/120/04:34:01
195
Vector Time (MET): N/A
Weight (LBS) : 614216
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2182694
24 A = 6723406
36 meter
Y = 5631551
62 meter E =
0010362
Z = -2950854
35 I = 51
32248
XDOT = -4119
205253 Wp = 135
31358
YDOT = -4194
056804 meter/sec RA = 268
16216 deg
ZDOT = -4975
071057 TA = 78
90203
MA = 78
78553
Ha = 189
183 n
mi
Hp = 179
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7161070
33 X = -2231170
14
Y = 18476219
23 feet Y = 5606872
54 meter
Z = -9681280
67 Z = -2961575
48
XDOT = -13514
452930 XDOT = -4047
832428
YDOT = -13760
028883 feet/sec YDOT = -4239
720886 meter/sec
ZDOT = -16322
411605 ZDOT = -4994
908994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19695274
91 X = -6003119
79
Y = -1990172
93 feet Y = -606604
71 meter
Z = -9721839
28 Z = -2963216
61
XDOT = 9595
318729 XDOT = 2924
653149
YDOT = -15134
788055 feet/sec YDOT = -4613
083399 meter/sec
ZDOT = -16398
962779 ZDOT = -4998
403855
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 08120
21602698
00020000 00000-0 20000-3 0 9082
2 25544 51
6405 268
7607 0006481 151
9196 208
2318 15
75737810 20808
Satellite: ISS
Catalog Number: 25544
Epoch time: 08120
21602698 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 268
7607 deg
Eccentricity:
0006481
Arg of perigee: 151
9196 deg
Mean anomaly: 208
2318 deg
Mean motion: 15
75737810 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2080
Checksum: 292
Coasting Arc #10 (Orbit 2095)
---------------------------------------
Vector Time (GMT): 2008/121/04:34:01
195
Vector Time (MET): N/A
Weight (LBS) : 614216
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3693060
03 A = 6720142
01 meter
Y = 3956041
51 meter E =
0013865
Z = 3969748
56 I = 51
31363
XDOT = -2400
795104 Wp = 104
66357
YDOT = 6187
982041 meter/sec RA = 262
93988 deg
ZDOT = -3925
219336 TA = 26
07279
MA = 26
00302
Ha = 188
963 n
mi
Hp = 179
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12116338
67 X = 3629264
06
Y = 12979138
82 feet Y = 3996982
66 meter
Z = 13024109
46 Z = 3987534
64
XDOT = -7876
624358 XDOT = -2450
743555
YDOT = 20301
778349 feet/sec YDOT = 6160
855765 meter/sec
ZDOT = -12878
016193 ZDOT = -3937
003680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9090304
81 X = -2770724
91
Y = 15193315
99 feet Y = 4630922
71 meter
Z = 13092770
62 Z = 3990676
48
XDOT = -20566
458055 XDOT = -6268
656415
YDOT = -1146
806499 feet/sec YDOT = -349
546621 meter/sec
ZDOT = -12922
591048 ZDOT = -3938
805751
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 08121
23072207
00020000 00000-0 20000-3 0 9093
2 25544 51
6399 263
5360 0006361 154
4775 205
6704 15
75787001 20961
Satellite: ISS
Catalog Number: 25544
Epoch time: 08121
23072207 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 263
5360 deg
Eccentricity:
0006361
Arg of perigee: 154
4775 deg
Mean anomaly: 205
6704 deg
Mean motion: 15
75787001 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2096
Checksum: 286
Coasting Arc #11 (Orbit 2111)
---------------------------------------
Vector Time (GMT): 2008/122/04:34:01
195
Vector Time (MET): N/A
Weight (LBS) : 614216
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2051881
44 A = 6720571
52 meter
Y = -5106884
01 meter E =
0015516
Z = 3851332
05 I = 51
32038
XDOT = 4385
040596 Wp = 119
54223
YDOT = 4850
476627 meter/sec RA = 257
81889 deg
ZDOT = 4075
674219 TA = 287
71720
MA = 287
88651
Ha = 188
927 n
mi
Hp = 179
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6731894
48 X = 2090125
68
Y = -16754868
81 feet Y = -5083724
88 meter
Z = 12635603
84 Z = 3861393
05
XDOT = 14386
616130 XDOT = 4310
676845
YDOT = 15913
637227 feet/sec YDOT = 4899
096857 meter/sec
ZDOT = 13371
634578 ZDOT = 4096
796310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17975887
84 X = 5479050
61
Y = 1395693
22 feet Y = 425407
29 meter
Z = 12673674
03 Z = 3862935
85
XDOT = -10856
353259 XDOT = -3309
016473
YDOT = 17072
596207 feet/sec YDOT = 5203
727324 meter/sec
ZDOT = 13453
197258 ZDOT = 4100
534524
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 08122
24539837
00020000 00000-0 20000-3 0 9104
2 25544 51
6403 258
3106 0006276 158
3630 201
7800 15
75796422 21125
Satellite: ISS
Catalog Number: 25544
Epoch time: 08122
24539837 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 258
3106 deg
Eccentricity:
0006276
Arg of perigee: 158
3630 deg
Mean anomaly: 201
7800 deg
Mean motion: 15
75796422 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2112
Checksum: 271
Coasting Arc #12 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2008/123/04:34:01
195
Vector Time (MET): N/A
Weight (LBS) : 614216
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3979041
87 A = 6722782
45 meter
Y = -4469677
60 meter E =
0007741
Z = -3074430
22 I = 51
33594
XDOT = 2373
423596 Wp = 127
66421
YDOT = -5461
726173 meter/sec RA = 252
59551 deg
ZDOT = 4872
318593 TA = 196
51517
MA = 196
54040
Ha = 188
730 n
mi
Hp = 179
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13054599
30 X = -3913830
27
Y = -14664296
59 feet Y = -4513808
91 meter
Z = -10086713
33 Z = -3093602
26
XDOT = 7786
822821 XDOT = 2410
651911
YDOT = -17919
049123 feet/sec YDOT = -5434
977028 meter/sec
ZDOT = 15985
297220 ZDOT = 4883
939280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9864315
76 X = 3006643
44
Y = -16931043
12 feet Y = -5160581
94 meter
Z = -10160757
68 Z = -3096998
94
XDOT = 18192
333331 XDOT = 5545
023199
YDOT = 986
807199 feet/sec YDOT = 300
778834 meter/sec
ZDOT = 16029
312159 ZDOT = 4885
734346
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 08123
19663927
00020000 00000-0 20000-3 0 9118
2 25544 51
6404 253
4118 0006109 163
3141 196
8225 15
75834628 21275
Satellite: ISS
Catalog Number: 25544
Epoch time: 08123
19663927 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 253
4118 deg
Eccentricity:
0006109
Arg of perigee: 163
3141 deg
Mean anomaly: 196
8225 deg
Mean motion: 15
75834628 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2127
Checksum: 285
Coasting Arc #13 (Orbit 2142)
---------------------------------------
Vector Time (GMT): 2008/124/04:34:01
195
Vector Time (MET): N/A
Weight (LBS) : 614216
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2163156
28 A = 6717594
50 meter
Y = 4398306
31 meter E =
0011470
Z = -4602246
37 I = 51
32853
XDOT = -4723
773149 Wp = 101
54911
YDOT = -5342
658192 meter/sec RA = 247
47026 deg
ZDOT = -2893
979985 TA = 139
70208
MA = 139
61702
Ha = 188
506 n
mi
Hp = 180
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7096969
43 X = -2189820
75
Y = 14430138
82 feet Y = 4373967
60 meter
Z = -15099233
49 Z = -4612819
93
XDOT = -15497
943402 XDOT = -4649
620921
YDOT = -17528
406143 feet/sec YDOT = -5395
067504 meter/sec
ZDOT = -9494
684989 ZDOT = -2916
748428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15933460
39 X = -4856518
73
Y = -1872931
08 feet Y = -570869
39 meter
Z = -15139342
88 Z = -4614471
71
XDOT = 11334
700020 XDOT = 3454
816566
YDOT = -19189
119007 feet/sec YDOT = -5848
843473 meter/sec
ZDOT = -9582
625858 ZDOT = -2920
784362
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 08124
21127868
00020000 00000-0 20000-3 0 9122
2 25544 51
6403 248
1862 0006001 168
0370 192
0938 15
75868822 21438
Satellite: ISS
Catalog Number: 25544
Epoch time: 08124
21127868 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 248
1862 deg
Eccentricity:
0006001
Arg of perigee: 168
0370 deg
Mean anomaly: 192
0938 deg
Mean motion: 15
75868822 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2143
Checksum: 282
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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