Date:
May 12th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9256 96 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 2242)
---------------------------------------
Vector Time (GMT): 2008/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 213473
80 A = 6715477
05 meter
Y = -4599788
86 meter E =
0010581
Z = 4887941
70 I = 51
43921
XDOT = 6887
627628 Wp = 157
41052
YDOT = 2664
431997 meter/sec RA = 214
85672 deg
ZDOT = 2195
354167 TA = 271
15777
MA = 271
27900
Ha = 187
506 n
mi
Hp = 180
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 700373
36 X = 241148
65
Y = -15091170
79 feet Y = -4597247
58 meter
Z = 16036554
15 Z = 4889045
38
XDOT = 22597
203505 XDOT = 6846
656947
YDOT = 8741
574793 feet/sec YDOT = 2741
224018 meter/sec
ZDOT = 7202
605534 ZDOT = 2228
715248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10607075
96 X = -3233036
75
Y = -10751900
35 feet Y = -3277179
23 meter
Z = 16040311
91 Z = 4889087
07
XDOT = 21006
359462 XDOT = 6402
738364
YDOT = -9731
818552 feet/sec YDOT = -2966
258295 meter/sec
ZDOT = 7330
989741 ZDOT = 2234
485673
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 08130
55138401
00020000 00000-0 20000-3 0 9008
2 25544 51
6409 215
5337 0006386 192
6751 167
4254 15
76207648 22433
Satellite: ISS
Catalog Number: 25544
Epoch time: 08130
55138401 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 215
5337 deg
Eccentricity:
0006386
Arg of perigee: 192
6751 deg
Mean anomaly: 167
4254 deg
Mean motion: 15
76207648 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2243
Checksum: 283
Coasting Arc #2 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2008/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6162633
98 A = 6725319
13 meter
Y = -2408145
20 meter E =
0004049
Z = -1203364
35 I = 51
49652
XDOT = 782
369713 Wp = 69
57242
YDOT = -4924
759337 meter/sec RA = 209
66306 deg
ZDOT = 5865
947790 TA = 277
20961
MA = 277
25564
Ha = 187
335 n
mi
Hp = 180
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20218615
42 X = -6129401
97
Y = -7900738
86 feet Y = -2476873
36 meter
Z = -3948045
78 Z = -1233222
01
XDOT = 2566
829767 XDOT = 808
885264
YDOT = -16157
346907 feet/sec YDOT = -4915
862835 meter/sec
ZDOT = 19245
235531 ZDOT = 5869
812398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19400529
75 X = -5913281
47
Y = 9690866
66 feet Y = 2953776
16 meter
Z = -4062966
71 Z = -1238392
25
XDOT = -9636
110057 XDOT = -2937
086346
YDOT = -11239
297033 feet/sec YDOT = -3425
737736 meter/sec
ZDOT = 19259
559056 ZDOT = 5870
313600
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 08131
50239849
00020000 00000-0 20000-3 0 9013
2 25544 51
6403 210
6345 0006099 196
9589 163
1372 15
76174627 22589
Satellite: ISS
Catalog Number: 25544
Epoch time: 08131
50239849 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 210
6345 deg
Eccentricity:
0006099
Arg of perigee: 196
9589 deg
Mean anomaly: 163
1372 deg
Mean motion: 15
76174627 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2258
Checksum: 304
Coasting Arc #3 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2008/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1216464
82 A = 6713884
76 meter
Y = 4029818
22 meter E =
0013511
Z = -5240915
63 I = 51
48350
XDOT = -7145
192114 Wp = 110
46711
YDOT = -2812
644158 meter/sec RA = 204
51633 deg
ZDOT = -509
923934 TA = 154
70807
MA = 154
64186
Ha = 187
136 n
mi
Hp = 180
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3991026
32 X = -1235977
07
Y = 13221188
39 feet Y = 4016106
39 meter
Z = -17194605
10 Z = -5246872
25
XDOT = -23442
231344 XDOT = -7110
732522
YDOT = -9227
835164 feet/sec YDOT = -2892
353064 meter/sec
ZDOT = -1672
978787 ZDOT = -544
551813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7402543
75 X = 2256295
34
Y = 11625742
48 feet Y = 3543526
31 meter
Z = -17217055
96 Z = -5247758
66
XDOT = -21511
003366 XDOT = -6556
553826
YDOT = 11049
544541 feet/sec YDOT = 3367
901176 meter/sec
ZDOT = -1806
279139 ZDOT = -550
553882
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 08132
51679482
00020000 00000-0 20000-3 0 9027
2 25544 51
6395 205
4079 0006152 200
8933 159
1980 15
76218254 22746
Satellite: ISS
Catalog Number: 25544
Epoch time: 08132
51679482 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 205
4079 deg
Eccentricity:
0006152
Arg of perigee: 200
8933 deg
Mean anomaly: 159
1980 deg
Mean motion: 15
76218254 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2274
Checksum: 295
Coasting Arc #4 (Orbit 2289)
---------------------------------------
Vector Time (GMT): 2008/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6239207
20 A = 6725696
31 meter
Y = 2465221
07 meter E =
0015115
Z = -325264
52 I = 51
55110
XDOT = -2030
777869 Wp = 158
83513
YDOT = 4357
843401 meter/sec RA = 199
35365 deg
ZDOT = -6026
068256 TA = 24
71009
MA = 24
63776
Ha = 186
970 n
mi
Hp = 180
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20469839
89 X = 6212757
07
Y = 8087995
64 feet Y = 2534843
59 meter
Z = -1067140
82 Z = -295018
51
XDOT = -6662
657049 XDOT = -2050
083458
YDOT = 14297
386487 feet/sec YDOT = 4335
026551 meter/sec
ZDOT = -19770
565144 ZDOT = -6035
980376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19379159
86 X = 5906767
92
Y = -10445723
99 feet Y = -3183856
67 meter
Z = -950695
36 Z = -289771
95
XDOT = 5950
567328 XDOT = 1813
732922
YDOT = 12808
770434 feet/sec YDOT = 3904
113228 meter/sec
ZDOT = -19808
173628 ZDOT = -6037
531322
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 08133
53117264
00020000 00000-0 20000-3 0 9036
2 25544 51
6396 200
1812 0005982 203
4523 156
6370 15
76269579 22907
Satellite: ISS
Catalog Number: 25544
Epoch time: 08133
53117264 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 200
1812 deg
Eccentricity:
0005982
Arg of perigee: 203
4523 deg
Mean anomaly: 156
6370 deg
Mean motion: 15
76269579 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2290
Checksum: 285
Coasting Arc #5 (Orbit 2305)
---------------------------------------
Vector Time (GMT): 2008/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2342842
94 A = 6713950
27 meter
Y = -3622114
48 meter E =
0002976
Z = 5143893
03 I = 51
54057
XDOT = 7067
728678 Wp = 172
61509
YDOT = 2806
434975 meter/sec RA = 194
18073 deg
ZDOT = -1245
725566 TA = 289
28310
MA = 289
31529
Ha = 186
653 n
mi
Hp = 181
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7686492
59 X = 2358183
68
Y = -11883577
69 feet Y = -3595829
97 meter
Z = 16876289
46 Z = 5155311
67
XDOT = 23188
086215 XDOT = 7041
872923
YDOT = 9207
463829 feet/sec YDOT = 2885
325861 meter/sec
ZDOT = -4087
026136 ZDOT = -1211
453067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4427053
80 X = -1349366
00
Y = -13387810
97 feet Y = -4080604
78 meter
Z = 16919764
92 Z = 5157144
35
XDOT = 20815
105478 XDOT = 6344
444150
YDOT = -11869
901092 feet/sec YDOT = -3617
945853 meter/sec
ZDOT = -3955
066487 ZDOT = -1205
504265
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 08134
54552997
00020000 00000-0 20000-3 0 9045
2 25544 51
6400 194
9542 0005994 209
1928 150
8902 15
76327109 23067
Satellite: ISS
Catalog Number: 25544
Epoch time: 08134
54552997 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 194
9542 deg
Eccentricity:
0005994
Arg of perigee: 209
1928 deg
Mean anomaly: 150
8902 deg
Mean motion: 15
76327109 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2306
Checksum: 304
Coasting Arc #6 (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 = -5991732
27 A = 6724224
00 meter
Y = -2428862
29 meter E =
0009999
Z = 1837399
76 I = 51
60299
XDOT = 3364
710745 Wp = 84
96355
YDOT = -4002
707185 meter/sec RA = 189
05000 deg
ZDOT = 5655
654648 TA = 295
45077
MA = 295
55420
Ha = 186
605 n
mi
Hp = 181
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19657914
28 X = -5973052
86
Y = -7968708
30 feet Y = -2495760
91 meter
Z = 6028214
43 Z = 1808336
95
XDOT = 11039
077246 XDOT = 3381
745207
YDOT = -13132
241419 feet/sec YDOT = -3964
986089 meter/sec
ZDOT = 18555
297402 ZDOT = 5672
041728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18430477
45 X = -5617609
53
Y = 10563529
63 feet Y = 3219763
83 meter
Z = 5916301
03 Z = 1803288
55
XDOT = -2803
355763 XDOT = -854
462837
YDOT = -15365
957174 feet/sec YDOT = -4683
543747 meter/sec
ZDOT = 18617
821637 ZDOT = 5674
712035
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
55987296
00020000 00000-0 20000-3 0 9052
2 25544 51
6395 189
7270 0005679 211
4440 148
6385 15
76302181 23226
Satellite: ISS
Catalog Number: 25544
Epoch time: 08135
55987296 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 189
7270 deg
Eccentricity:
0005679
Arg of perigee: 211
4440 deg
Mean anomaly: 148
6385 deg
Mean motion: 15
76302181 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2322
Checksum: 310
Coasting Arc #7 (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 = -3516258
05 A = 6716202
96 meter
Y = 3416476
50 meter E =
0010622
Z = -4600007
59 I = 51
60589
XDOT = -6548
635874 Wp = 140
87911
YDOT = -2775
983071 meter/sec RA = 183
85502 deg
ZDOT = 2939
621288 TA = 158
30924
MA = 158
26422
Ha = 186
351 n
mi
Hp = 181
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11536279
68 X = -3531854
00
Y = 11208912
39 feet Y = 3377068
72 meter
Z = -15091888
42 Z = -4617127
49
XDOT = -21485
025834 XDOT = -6531
388010
YDOT = -9107
556007 feet/sec YDOT = -2849
117380 meter/sec
ZDOT = 9644
426798 ZDOT = 2907
849369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2015584
40 X = 614350
13
Y = 15896048
47 feet Y = 4845115
57 meter
Z = -15157296
08 Z = -4619943
85
XDOT = -19110
594464 XDOT = -5824
909192
YDOT = 11516
483492 feet/sec YDOT = 3510
224168 meter/sec
ZDOT = 9522
061610 ZDOT = 2902
324379
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
51080025
00020000 00000-0 20000-3 0 9064
2 25544 51
6396 184
8264 0005636 215
5282 144
5508 15
76350772 23375
Satellite: ISS
Catalog Number: 25544
Epoch time: 08136
51080025 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 184
8264 deg
Eccentricity:
0005636
Arg of perigee: 215
5282 deg
Mean anomaly: 144
5508 deg
Mean motion: 15
76350772 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2337
Checksum: 291
Coasting Arc #8 (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 = 5350320
38 A = 6720882
57 meter
Y = 2449195
66 meter E =
0005111
Z = -3242828
78 I = 51
65154
XDOT = -4655
343320 Wp = 168
22624
YDOT = 3871
050036 meter/sec RA = 178
74828 deg
ZDOT = -4763
373448 TA = 49
75764
MA = 49
71295
Ha = 186
251 n
mi
Hp = 181
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17553544
56 X = 5338288
78
Y = 8035418
82 feet Y = 2508958
94 meter
Z = -10639202
03 Z = -3216865
56
XDOT = -15273
436088 XDOT = -4675
144025
YDOT = 12700
295394 feet/sec YDOT = 3818
880923 meter/sec
ZDOT = -15627
865644 ZDOT = -4786
037322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16883363
15 X = 5146049
09
Y = -9474447
30 feet Y = -2887811
54 meter
Z = -10539183
99 Z = -3212343
28
XDOT = 597
482437 XDOT = 182
112647
YDOT = 18522
303816 feet/sec YDOT = 5645
598203 meter/sec
ZDOT = -15714
532555 ZDOT = -4789
789523
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
52510631
00020000 00000-0 20000-3 0 9078
2 25544 51
6400 179
5991 0005562 218
8350 141
2415 15
76389579 23535
Satellite: ISS
Catalog Number: 25544
Epoch time: 08137
52510631 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 179
5991 deg
Eccentricity:
0005562
Arg of perigee: 218
8350 deg
Mean anomaly: 141
2415 deg
Mean motion: 15
76389579 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2353
Checksum: 295
Coasting Arc #9 (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 = 4542347
80 A = 6719506
80 meter
Y = -3382714
65 meter E =
0008665
Z = 3606366
16 I = 51
67565
XDOT = 5637
445300 Wp = 110
62773
YDOT = 2867
011623 meter/sec RA = 173
54523 deg
ZDOT = -4405
874775 TA = 26
16397
MA = 26
12022
Ha = 185
856 n
mi
Hp = 181
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14902715
88 X = 4562316
84
Y = -11098145
17 feet Y = -3331808
17 meter
Z = 11831909
99 Z = 3628481
53
XDOT = 18495
555446 XDOT = 5626
370288
YDOT = 9406
206111 feet/sec YDOT = 2929
991212 meter/sec
ZDOT = -14454
969733 ZDOT = -4378
514196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -519858
34 X = -158452
82
Y = -18519716
32 feet Y = -5644809
53 meter
Z = 11916531
18 Z = 3632158
70
XDOT = 17043
046804 XDOT = 5194
720666
YDOT = -9723
112974 feet/sec YDOT = -2963
604834 meter/sec
ZDOT = -14349
533032 ZDOT = -4373
737668
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
53939355
00020000 00000-0 20000-3 0 9089
2 25544 51
6389 174
3719 0005492 223
8315 136
2414 15
76432258 23694
Satellite: ISS
Catalog Number: 25544
Epoch time: 08138
53939355 = yrday
fracday
Element set: 908
Inclination: 51
6389 deg
RA of node: 174
3719 deg
Eccentricity:
0005492
Arg of perigee: 223
8315 deg
Mean anomaly: 136
2414 deg
Mean motion: 15
76432258 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2369
Checksum: 315
Coasting Arc #10 (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 = -4402505
92 A = 6717109
57 meter
Y = -2607875
93 meter E =
0008636
Z = 4351189
41 I = 51
69559
XDOT = 5695
060121 Wp = 143
01536
YDOT = -3911
627592 meter/sec RA = 168
44463 deg
ZDOT = 3407
541362 TA = 272
62511
MA = 272
72396
Ha = 185
882 n
mi
Hp = 181
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14443917
07 X = -4394154
76
Y = -8556023
41 feet Y = -2657061
04 meter
Z = 14275555
80 Z = 4329821
60
XDOT = 18684
580450 XDOT = 5721
823725
YDOT = -12833
423858 feet/sec YDOT = -3847
792892 meter/sec
ZDOT = 11179
597645 ZDOT = 3435
273126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15241510
44 X = -4645612
38
Y = 7202365
00 feet Y = 2195280
85 meter
Z = 14193169
78 Z = 4326078
15
XDOT = 379
883597 XDOT = 115
788520
YDOT = -21502
820751 feet/sec YDOT = -6554
059765 meter/sec
ZDOT = 11285
757883 ZDOT = 3439
899003
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
55366473
00020000 00000-0 20000-3 0 9098
2 25544 51
6383 169
1438 0005356 226
3990 133
6731 15
76431267 23854
Satellite: ISS
Catalog Number: 25544
Epoch time: 08139
55366473 = yrday
fracday
Element set: 909
Inclination: 51
6383 deg
RA of node: 169
1438 deg
Eccentricity:
0005356
Arg of perigee: 226
3990 deg
Mean anomaly: 133
6731 deg
Mean motion: 15
76431267 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2385
Checksum: 314
Coasting Arc #11 (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 = -5309715
75 A = 6722797
10 meter
Y = 3452787
75 meter E =
0000755
Z = -2252759
75 I = 51
74503
XDOT = -4389
238832 Wp = 358
37021
YDOT = -3182
164942 meter/sec RA = 163
25188 deg
ZDOT = 5468
775077 TA = 336
36793
MA = 336
37139
Ha = 185
588 n
mi
Hp = 181
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17420327
26 X = -5336987
01
Y = 11328043
81 feet Y = 3393259
28 meter
Z = -7390944
08 Z = -2278620
68
XDOT = -14400
389869 XDOT = -4379
895995
YDOT = -10440
173694 feet/sec YDOT = -3231
196379 meter/sec
ZDOT = 17942
175449 ZDOT = 5447
474013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -44221
90 X = -13478
84
Y = 20744076
68 feet Y = 6322794
57 meter
Z = -7489977
29 Z = -2282945
08
XDOT = -15166
469553 XDOT = -4622
739920
YDOT = 6415
484854 feet/sec YDOT = 1955
439783 meter/sec
ZDOT = 17859
981515 ZDOT = 5443
722366
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
50452668
00020000 00000-0 20000-3 0 9109
2 25544 51
6391 164
2431 0005395 229
8014 130
2679 15
76499141 24007
Satellite: ISS
Catalog Number: 25544
Epoch time: 08140
50452668 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 164
2431 deg
Eccentricity:
0005395
Arg of perigee: 229
8014 deg
Mean anomaly: 130
2679 deg
Mean motion: 15
76499141 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2400
Checksum: 278
Coasting Arc #12 (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 = 3214303
74 A = 6714002
10 meter
Y = 3018585
74 meter E =
0008760
Z = -5070482
78 I = 51
74207
XDOT = -6374
060232 Wp = 90
85950
YDOT = 3979
701126 meter/sec RA = 158
13899 deg
ZDOT = -1674
060955 TA = 163
07846
MA = 163
04923
Ha = 185
445 n
mi
Hp = 181
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10545615
95 X = 3204942
48
Y = 9903496
54 feet Y = 3054478
32 meter
Z = -16635442
21 Z = -5054889
71
XDOT = -20912
271101 XDOT = -6409
955705
YDOT = 13056
762223 feet/sec YDOT = 3908
222280 meter/sec
ZDOT = -5492
325967 ZDOT = -1705
113320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14052373
83 X = 4283163
54
Y = -3717627
58 feet Y = -1133132
89 meter
Z = -16575199
30 Z = -5052120
75
XDOT = -364
540034 XDOT = -111
111802
YDOT = 23601
949669 feet/sec YDOT = 7193
874259 meter/sec
ZDOT = -5611
275091 ZDOT = -1710
316648
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
51876241
00020000 00000-0 20000-3 0 9119
2 25544 51
6386 159
0150 0005417 235
2106 124
8549 15
76481403 24163
Satellite: ISS
Catalog Number: 25544
Epoch time: 08141
51876241 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 159
0150 deg
Eccentricity:
0005417
Arg of perigee: 235
2106 deg
Mean anomaly: 124
8549 deg
Mean motion: 15
76481403 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2416
Checksum: 274
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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