Date:
May 17th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 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
There are no maneuvers
Coasting Arc #1 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2008/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6018553
53 A = 6724443
35 meter
Y = -2397170
89 meter E =
0009828
Z = 1791992
14 I = 51
60197
XDOT = 3301
560771 Wp = 84
98763
YDOT = -4027
947038 meter/sec RA = 189
05379 deg
ZDOT = 5674
582748 TA = 294
89988
MA = 295
00201
Ha = 186
719 n
mi
Hp = 181
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19745910
53 X = -6000005
92
Y = -7864733
89 feet Y = -2464370
18 meter
Z = 5879239
32 Z = 1762798
72
XDOT = 10831
892294 XDOT = 3318
790213
YDOT = -13215
049337 feet/sec YDOT = -3990
931032 meter/sec
ZDOT = 18617
397466 ZDOT = 5690
663515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18402542
96 X = -5609095
10
Y = 10696288
59 feet Y = 3260228
76 meter
Z = 5766827
53 Z = 1757729
03
XDOT = -2986
991420 XDOT = -910
434985
YDOT = -15255
938166 feet/sec YDOT = -4650
009953 meter/sec
ZDOT = 18678
742208 ZDOT = 5693
280625
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 08135
55996770
00020000 00000-0 20000-3 0 9004
2 25544 51
6383 189
7309 0005866 211
5317 148
5497 15
76249809 23228
Satellite: ISS
Catalog Number: 25544
Epoch time: 08135
55996770 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 189
7309 deg
Eccentricity:
0005866
Arg of perigee: 211
5317 deg
Mean anomaly: 148
5497 deg
Mean motion: 15
76249809 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2322
Checksum: 324
Coasting Arc #2 (Orbit 2336)
---------------------------------------
Vector Time (GMT): 2008/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3443649
52 A = 6716253
74 meter
Y = 3446945
66 meter E =
0010809
Z = -4632269
07 I = 51
60420
XDOT = -6599
001277 Wp = 141
13191
YDOT = -2726
540296 meter/sec RA = 183
85982 deg
ZDOT = 2872
206386 TA = 157
32824
MA = 157
28046
Ha = 186
479 n
mi
Hp = 181
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11298062
73 X = -3459434
86
Y = 11308876
85 feet Y = 3408348
78 meter
Z = -15197733
19 Z = -4649036
70
XDOT = -21650
266658 XDOT = -6581
975054
YDOT = -8945
342179 feet/sec YDOT = -2800
239055 meter/sec
ZDOT = 9423
249297 ZDOT = 2840
189253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2239513
27 X = 682603
64
Y = 15766119
89 feet Y = 4805513
34 meter
Z = -15261784
13 Z = -4651791
80
XDOT = -19089
856883 XDOT = -5818
588378
YDOT = 11728
823995 feet/sec YDOT = 3574
945554 meter/sec
ZDOT = 9299
947315 ZDOT = 2834
623941
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 08136
51092923
00020000 00000-0 20000-3 0 9019
2 25544 51
6384 184
8304 0005833 215
6321 144
4454 15
76287898 23378
Satellite: ISS
Catalog Number: 25544
Epoch time: 08136
51092923 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 184
8304 deg
Eccentricity:
0005833
Arg of perigee: 215
6321 deg
Mean anomaly: 144
4454 deg
Mean motion: 15
76287898 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2337
Checksum: 299
Coasting Arc #3 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2008/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5418191
48 A = 6721282
06 meter
Y = 2392147
47 meter E =
0005490
Z = -3172002
85 I = 51
65097
XDOT = -4551
155722 Wp = 171
65134
YDOT = 3917
825758 meter/sec RA = 178
75286 deg
ZDOT = -4825
730169 TA = 45
36198
MA = 45
31722
Ha = 186
391 n
mi
Hp = 181
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17776218
77 X = 5406448
69
Y = 7848252
86 feet Y = 2452671
34 meter
Z = -10406833
49 Z = -3145709
21
XDOT = -14931
613262 XDOT = -4571
184302
YDOT = 12853
759048 feet/sec YDOT = 3866
820460 meter/sec
ZDOT = -15832
448062 ZDOT = -4847
888442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16862945
32 X = 5139825
73
Y = -9763599
92 feet Y = -2975945
25 meter
Z = -10305551
99 Z = -3141132
25
XDOT = 902
729995 XDOT = 275
152102
YDOT = 18337
529762 feet/sec YDOT = 5589
279071 meter/sec
ZDOT = -15917
167342 ZDOT = -4851
552606
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 08137
52527809
00020000 00000-0 20000-3 0 9028
2 25544 51
6389 179
6033 0005758 218
9328 141
1422 15
76318461 23531
Satellite: ISS
Catalog Number: 25544
Epoch time: 08137
52527809 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 179
6033 deg
Eccentricity:
0005758
Arg of perigee: 218
9328 deg
Mean anomaly: 141
1422 deg
Mean motion: 15
76318461 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2353
Checksum: 301
Coasting Arc #4 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2008/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4434684
32 A = 6719472
45 meter
Y = -3436196
30 meter E =
0008237
Z = 3689180
49 I = 51
67351
XDOT = 5749
147188 Wp = 110
51572
YDOT = 2782
399897 meter/sec RA = 173
55046 deg
ZDOT = -4314
443080 TA = 25
02704
MA = 24
98713
Ha = 186
007 n
mi
Hp = 181
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14549489
23 X = 4454857
09
Y = -11273609
89 feet Y = -3386492
64 meter
Z = 12103610
53 Z = 3710773
31
XDOT = 18862
031456 XDOT = 5738
565848
YDOT = 9128
608586 feet/sec YDOT = 2846
631353 meter/sec
ZDOT = -14154
996981 ZDOT = -4286
538651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -867710
85 X = -264478
27
Y = -18330915
67 feet Y = -5587263
10 meter
Z = 12186218
17 Z = 3714359
30
XDOT = 17040
175813 XDOT = 5193
845588
YDOT = -10155
825231 feet/sec YDOT = -3095
495530 meter/sec
ZDOT = -14047
479475 ZDOT = -4281
671744
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 08138
53961455
00020000 00000-0 20000-3 0 9030
2 25544 51
6377 174
3763 0005694 223
9090 136
1623 15
76351552 23693
Satellite: ISS
Catalog Number: 25544
Epoch time: 08138
53961455 = yrday
fracday
Element set: 903
Inclination: 51
6377 deg
RA of node: 174
3763 deg
Eccentricity:
0005694
Arg of perigee: 223
9090 deg
Mean anomaly: 136
1623 deg
Mean motion: 15
76351552 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2369
Checksum: 305
Coasting Arc #5 (Orbit 2384)
---------------------------------------
Vector Time (GMT): 2008/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4535718
82 A = 6717682
37 meter
Y = -2514953
72 meter E =
0008751
Z = 4269145
12 I = 51
69541
XDOT = 5556
253136 Wp = 141
29036
YDOT = -3990
713266 meter/sec RA = 168
45085 deg
ZDOT = 3541
672973 TA = 272
79407
MA = 272
89422
Ha = 186
038 n
mi
Hp = 181
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14880967
25 X = -4527998
26
Y = -8251160
49 feet Y = -2565632
01 meter
Z = 14006381
64 Z = 4247128
63
XDOT = 18229
176957 XDOT = 5583
259805
YDOT = -13092
891292 feet/sec YDOT = -3928
429440 meter/sec
ZDOT = 11619
661984 ZDOT = 3568
730981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15234218
86 X = -4643389
91
Y = 7733926
99 feet Y = 2357300
95 meter
Z = 13921512
54 Z = 4243277
02
XDOT = -53
358014 XDOT = -16
263523
YDOT = -21270
527433 feet/sec YDOT = -6483
256761 meter/sec
ZDOT = 11723
224800 ZDOT = 3573
238919
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 08139
55394143
00020000 00000-0 20000-3 0 9048
2 25544 51
6371 169
1484 0005552 226
5399 133
5304 15
76339108 23851
Satellite: ISS
Catalog Number: 25544
Epoch time: 08139
55394143 = yrday
fracday
Element set: 904
Inclination: 51
6371 deg
RA of node: 169
1484 deg
Eccentricity:
0005552
Arg of perigee: 226
5399 deg
Mean anomaly: 133
5304 deg
Mean motion: 15
76339108 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2385
Checksum: 301
Coasting Arc #6 (Orbit 2399)
---------------------------------------
Vector Time (GMT): 2008/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5180583
91 A = 6722765
42 meter
Y = 3542568
02 meter E =
0000258
Z = -2409494
22 I = 51
74274
XDOT = -4587
902579 Wp = 288
81150
YDOT = -3049
866323 meter/sec RA = 163
25719 deg
ZDOT = 5379
854477 TA = 44
03083
MA = 44
02877
Ha = 185
758 n
mi
Hp = 181
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16996666
37 X = -5208107
31
Y = 11622598
49 feet Y = 3484482
18 meter
Z = -7905164
78 Z = -2434728
41
XDOT = -15052
173817 XDOT = -4579
592392
YDOT = -10006
123106 feet/sec YDOT = -3101
125094 meter/sec
ZDOT = 17650
441197 ZDOT = 5357
585793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 435900
30 X = 132862
41
Y = 20548591
22 feet Y = 6263210
60 meter
Z = -8001780
02 Z = -2438942
55
XDOT = -15173
790251 XDOT = -4624
971269
YDOT = 7162
137778 feet/sec YDOT = 2183
019595 meter/sec
ZDOT = 17564
542137 ZDOT = 5353
672443
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 08140
50486132
00020000 00000-0 20000-3 0 9056
2 25544 51
6380 164
2480 0005587 229
9918 130
0757 15
76397426 24004
Satellite: ISS
Catalog Number: 25544
Epoch time: 08140
50486132 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 164
2480 deg
Eccentricity:
0005587
Arg of perigee: 229
9918 deg
Mean anomaly: 130
0757 deg
Mean motion: 15
76397426 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2400
Checksum: 292
Coasting Arc #7 (Orbit 2415)
---------------------------------------
Vector Time (GMT): 2008/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3432776
54 A = 6714587
88 meter
Y = 2878616
29 meter E =
0008081
Z = -5008447
99 I = 51
74177
XDOT = -6223
226631 Wp = 89
84875
YDOT = 4113
272018 meter/sec RA = 158
14771 deg
ZDOT = -1903
878441 TA = 161
80898
MA = 161
78005
Ha = 185
630 n
mi
Hp = 181
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11262390
23 X = 3424662
84
Y = 9444279
16 feet Y = 2916958
92 meter
Z = -16431915
99 Z = -4991790
55
XDOT = -20417
410208 XDOT = -6259
510494
YDOT = 13494
986936 feet/sec YDOT = 4043
477742 meter/sec
ZDOT = -6246
320344 ZDOT = -1934
198967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14045639
72 X = 4281110
99
Y = -4567877
26 feet Y = -1392288
99 meter
Z = -16367596
27 Z = -4988843
34
XDOT = 210
377115 XDOT = 64
122945
YDOT = 23413
979248 feet/sec YDOT = 7136
580875 meter/sec
ZDOT = -6362
442868 ZDOT = -1939
272586
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 08141
51916514
00020000 00000-0 20000-3 0 9061
2 25544 51
6374 159
0202 0005611 235
3284 124
7352 15
76372623 24166
Satellite: ISS
Catalog Number: 25544
Epoch time: 08141
51916514 = yrday
fracday
Element set: 906
Inclination: 51
6374 deg
RA of node: 159
0202 deg
Eccentricity:
0005611
Arg of perigee: 235
3284 deg
Mean anomaly: 124
7352 deg
Mean motion: 15
76372623 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2416
Checksum: 269
Coasting Arc #8 (Orbit 2431)
---------------------------------------
Vector Time (GMT): 2008/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5589089
37 A = 6725017
44 meter
Y = -3622061
38 meter E =
0012492
Z = 873646
51 I = 51
80278
XDOT = 3274
796209 Wp = 149
33999
YDOT = 3605
999674 meter/sec RA = 152
97869 deg
ZDOT = -5973
450095 TA = 21
13394
MA = 21
08237
Ha = 185
389 n
mi
Hp = 181
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18336907
40 X = 5624932
36
Y = -11883403
46 feet Y = -3559360
71 meter
Z = 2866294
33 Z = 900885
21
XDOT = 10744
082052 XDOT = 3263
248336
YDOT = 11830
707593 feet/sec YDOT = 3642
556700 meter/sec
ZDOT = -19597
933384 ZDOT = -5957
568371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -655307
26 X = -199737
65
Y = -21827023
96 feet Y = -6652876
90 meter
Z = 2970638
23 Z = 905450
53
XDOT = 14153
990268 XDOT = 4314
136234
YDOT = -3095
330764 feet/sec YDOT = -943
456817 meter/sec
ZDOT = -19536
517374 ZDOT = -5954
730496
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 08142
53345797
00020000 00000-0 20000-3 0 9074
2 25544 51
6362 153
7922 0005466 239
2867 120
7760 15
76395421 24329
Satellite: ISS
Catalog Number: 25544
Epoch time: 08142
53345797 = yrday
fracday
Element set: 907
Inclination: 51
6362 deg
RA of node: 153
7922 deg
Eccentricity:
0005466
Arg of perigee: 239
2867 deg
Mean anomaly: 120
7760 deg
Mean motion: 15
76395421 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2432
Checksum: 305
Coasting Arc #9 (Orbit 2447)
---------------------------------------
Vector Time (GMT): 2008/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2282170
18 A = 6713237
94 meter
Y = -3471209
40 meter E =
0003686
Z = 5275756
57 I = 51
78825
XDOT = 6490
057909 Wp = 224
63576
YDOT = -4149
426941 meter/sec RA = 147
84497 deg
ZDOT = 74
772895 TA = 224
64159
MA = 224
67128
Ha = 185
246 n
mi
Hp = 181
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7487434
97 X = -2268813
91
Y = -11388482
30 feet Y = -3496656
14 meter
Z = 17308912
64 Z = 5264701
53
XDOT = 21292
840908 XDOT = 6535
611858
YDOT = -13613
605449 feet/sec YDOT = -4076
596709 meter/sec
ZDOT = 245
317896 ZDOT = 106
411916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13659458
88 X = -4163403
07
Y = 812366
16 feet Y = 247609
20 meter
Z = 17266062
45 Z = 5262695
83
XDOT = -968
589306 XDOT = -295
226021
YDOT = -24254
376602 feet/sec YDOT = -7392
733988 meter/sec
ZDOT = 366
543216 ZDOT = 111
722372
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 08143
54773898
00020000 00000-0 20000-3 0 9084
2 25544 51
6358 148
5639 0005506 244
2746 115
7850 15
76412216 24481
Satellite: ISS
Catalog Number: 25544
Epoch time: 08143
54773898 = yrday
fracday
Element set: 908
Inclination: 51
6358 deg
RA of node: 148
5639 deg
Eccentricity:
0005506
Arg of perigee: 244
2746 deg
Mean anomaly: 115
7850 deg
Mean motion: 15
76412216 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2448
Checksum: 317
Coasting Arc #10 (Orbit 2463)
---------------------------------------
Vector Time (GMT): 2008/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5650547
67 A = 6724916
33 meter
Y = 3559213
82 meter E =
0008130
Z = 753254
18 I = 51
85269
XDOT = -1976
966501 Wp = 42
95146
YDOT = -4414
376502 meter/sec RA = 142
71098 deg
ZDOT = 5996
361672 TA = 325
24246
MA = 325
29555
Ha = 184
941 n
mi
Hp = 181
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18538542
22 X = -5693586
59
Y = 11677210
70 feet Y = 3495785
40 meter
Z = 2471306
36 Z = 725699
66
XDOT = -6486
110569 XDOT = -1956
586767
YDOT = -14482
862541 feet/sec YDOT = -4436
371122 meter/sec
ZDOT = 19673
102598 ZDOT = 5986
806264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1112416
11 X = 339064
43
Y = 21893106
23 feet Y = 6673018
78 meter
Z = 2365709
70 Z = 721068
32
XDOT = -14262
960136 XDOT = -4347
350249
YDOT = -1408
876509 feet/sec YDOT = -429
425560 meter/sec
ZDOT = 19635
921726 ZDOT = 5985
028942
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 08144
56200698
00020000 00000-0 20000-3 0 9091
2 25544 51
6362 143
3367 0005616 247
3204 112
7367 15
76477708 24647
Satellite: ISS
Catalog Number: 25544
Epoch time: 08144
56200698 = yrday
fracday
Element set: 909
Inclination: 51
6362 deg
RA of node: 143
3367 deg
Eccentricity:
0005616
Arg of perigee: 247
3204 deg
Mean anomaly: 112
7367 deg
Mean motion: 15
76477708 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2464
Checksum: 300
Coasting Arc #11 (Orbit 2478)
---------------------------------------
Vector Time (GMT): 2008/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1206184
94 A = 6714225
89 meter
Y = 4270985
50 meter E =
0009079
Z = -5046197
44 I = 51
83837
XDOT = -6376
386088 Wp = 121
19790
YDOT = 3922
591783 meter/sec RA = 137
54910 deg
ZDOT = 1793
607912 TA = 166
05161
MA = 166
02651
Ha = 184
765 n
mi
Hp = 182
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3957299
66 X = 1182850
07
Y = 14012419
63 feet Y = 4284344
08 meter
Z = -16555765
89 Z = -5040393
78
XDOT = -20919
901864 XDOT = -6428
488274
YDOT = 12869
395615 feet/sec YDOT = 3850
995785 meter/sec
ZDOT = 5884
540393 ZDOT = 1762
505363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14258705
03 X = 4346053
29
Y = 3074075
78 feet Y = 936978
30 meter
Z = -16533024
46 Z = -5039265
86
XDOT = 1624
878905 XDOT = 495
263090
YDOT = 23509
994925 feet/sec YDOT = 7165
846453 meter/sec
ZDOT = 5765
321225 ZDOT = 1757
269909
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 08145
51287660
00020000 00000-0 20000-3 0 9103
2 25544 51
6358 138
4351 0005537 253
4109 106
6447 15
76423229 24790
Satellite: ISS
Catalog Number: 25544
Epoch time: 08145
51287660 = yrday
fracday
Element set: 910
Inclination: 51
6358 deg
RA of node: 138
4351 deg
Eccentricity:
0005537
Arg of perigee: 253
4109 deg
Mean anomaly: 106
6447 deg
Mean motion: 15
76423229 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2479
Checksum: 295
Coasting Arc #12 (Orbit 2494)
---------------------------------------
Vector Time (GMT): 2008/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5421579
73 A = 6722845
51 meter
Y = -3202933
31 meter E =
0005438
Z = -2344441
85 I = 51
88834
XDOT = 839
934259 Wp = 193
60405
YDOT = 5396
874140 meter/sec RA = 132
44568 deg
ZDOT = -5433
383770 TA = 12
72033
MA = 12
70662
Ha = 184
648 n
mi
Hp = 182
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17787335
06 X = 5468381
38
Y = -10508311
37 feet Y = -3142044
08 meter
Z = -7691738
36 Z = -2317990
54
XDOT = 2755
689825 XDOT = 805
917579
YDOT = 17706
279987 feet/sec YDOT = 5406
077350 meter/sec
ZDOT = -17826
062239 ZDOT = -5429
385213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1157192
52 X = -352712
28
Y = -20664574
49 feet Y = -6298562
30 meter
Z = -7590322
91 Z = -2313530
42
XDOT = 15536
878729 XDOT = 4735
640637
YDOT = 5668
587768 feet/sec YDOT = 1727
785552 meter/sec
ZDOT = -17810
150792 ZDOT = -5428
533961
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 08146
52712459
00020000 00000-0 20000-3 0 9115
2 25544 51
6357 133
2068 0005452 257
7410 102
3144 15
76461938 24959
Satellite: ISS
Catalog Number: 25544
Epoch time: 08146
52712459 = yrday
fracday
Element set: 911
Inclination: 51
6357 deg
RA of node: 133
2068 deg
Eccentricity:
0005452
Arg of perigee: 257
7410 deg
Mean anomaly: 102
3144 deg
Mean motion: 15
76461938 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2495
Checksum: 286
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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