Date:
July 26th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7750 02 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
205/16:28:18
127 -10
4 11
2 11
2
N/A -3
4 0
0 193
9
000/00:20:36
255 2
5 0
3 185
5
Coasting Arc #1 (Orbit 3424)
---------------------------------------
Vector Time (GMT): 2008/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4584305
09 A = 6721298
24 meter
Y = 2639750
23 meter E =
0015165
Z = -4155839
60 I = 51
58210
XDOT = -5551
814824 Wp = 73
36651
YDOT = -3819
103805 meter/sec RA = 188
60564 deg
ZDOT = 3713
753634 TA = 234
59056
MA = 234
73229
Ha = 191
568 n
mi
Hp = 179
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15040371
05 X = -4593294
35
Y = 8660597
88 feet Y = 2588435
93 meter
Z = -13634644
36 Z = -4178131
61
XDOT = -18214
615565 XDOT = -5526
736957
YDOT = -12529
868126 feet/sec YDOT = -3881
047427 meter/sec
ZDOT = 12184
231083 ZDOT = 3686
843805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15106809
15 X = 4604555
43
Y = 8405812
29 feet Y = 2562091
59 meter
Z = -13720381
95 Z = -4181972
42
XDOT = -770
534111 XDOT = -234
858797
YDOT = 21020
421535 feet/sec YDOT = 6407
024484 meter/sec
ZDOT = 12080
030785 ZDOT = 3681
993383
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 08205
50925000
00020000 00000-0 20000-3 0 9005
2 25544 51
6374 189
5898 0010000 43
7935 316
4020 15
75149493 34256
Satellite: ISS
Catalog Number: 25544
Epoch time: 08205
50925000 = yrday
fracday
Element set: 900
Inclination: 51
6374 deg
RA of node: 189
5898 deg
Eccentricity:
0010000
Arg of perigee: 43
7935 deg
Mean anomaly: 316
4020 deg
Mean motion: 15
75149493 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3425
Checksum: 273
Coasting Arc #2 (Orbit 3427)
---------------------------------------
Vector Time (GMT): 2008/205/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5825892
65 A = 6732094
12 meter
Y = 1590097
06 meter E =
0011467
Z = -2962421
30 I = 51
60298
XDOT = -3760
231692 Wp = 9
06988
YDOT = -4496
349106 meter/sec RA = 187
61127 deg
ZDOT = 4995
153457 TA = 316
73954
MA = 316
82954
Ha = 193
897 n
mi
Hp = 185
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19113821
03 X = -5828849
59
Y = 5216853
88 feet Y = 1524932
26 meter
Z = -9719229
98 Z = -2990730
33
XDOT = -12336
718148 XDOT = -3733
938690
YDOT = -14751
801528 feet/sec YDOT = -4538
251513 meter/sec
ZDOT = 16388
298744 ZDOT = 4976
949947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17760196
97 X = 5413308
04
Y = -8660099
09 feet Y = -2639598
20 meter
Z = -9828287
62 Z = -2995662
07
XDOT = 14318
368110 XDOT = 4364
238600
YDOT = 10896
019167 feet/sec YDOT = 3321
106642 meter/sec
ZDOT = 16317
618396 ZDOT = 4973
610087
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 08205
69957900
00020000 00000-0 20000-3 0 9010
2 25544 51
6402 188
6113 0010128 345
5083 14
5787 15
72658063 34280
Satellite: ISS
Catalog Number: 25544
Epoch time: 08205
69957900 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 188
6113 deg
Eccentricity:
0010128
Arg of perigee: 345
5083 deg
Mean anomaly: 14
5787 deg
Mean motion: 15
72658063 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3428
Checksum: 292
Coasting Arc #3 (Orbit 3443)
---------------------------------------
Vector Time (GMT): 2008/206/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4066679
75 A = 6728658
55 meter
Y = 3445882
78 meter E =
0013613
Z = -4119682
93 I = 51
62120
XDOT = -6125
951734 Wp = 23
33852
YDOT = 2715
714551 meter/sec RA = 182
53369 deg
ZDOT = -3767
569068 TA = 207
92950
MA = 208
00263
Ha = 194
120 n
mi
Hp = 185
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13342125
17 X = 4047857
70
Y = 11305389
68 feet Y = 3491253
81 meter
Z = -13516020
12 Z = -4099972
51
XDOT = -20098
266845 XDOT = -6137
561886
YDOT = 8909
824644 feet/sec YDOT = 2647
146022 meter/sec
ZDOT = -12360
790907 ZDOT = -3797
356831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15428704
46 X = -4702669
12
Y = -8356940
16 feet Y = -2547195
36 meter
Z = -13439626
84 Z = -4096398
26
XDOT = 17201
428674 XDOT = 5242
995460
YDOT = -11651
935418 feet/sec YDOT = -3551
509916 meter/sec
ZDOT = -12475
448943 ZDOT = -3802
516838
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 08206
71627875
00020000 00000-0 20000-3 0 9020
2 25544 51
6408 183
4006 0010195 349
6142 10
4808 15
72684831 34444
Satellite: ISS
Catalog Number: 25544
Epoch time: 08206
71627875 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 183
4006 deg
Eccentricity:
0010195
Arg of perigee: 349
6142 deg
Mean anomaly: 10
4808 deg
Mean motion: 15
72684831 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3444
Checksum: 286
Coasting Arc #4 (Orbit 3459)
---------------------------------------
Vector Time (GMT): 2008/207/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4779618
30 A = 6730222
11 meter
Y = -3075490
60 meter E =
0015418
Z = 3605249
52 I = 51
65527
XDOT = 5419
329966 Wp = 44
64944
YDOT = 3235
767584 meter/sec RA = 177
35711 deg
ZDOT = -4402
179665 TA = 92
27429
MA = 92
09774
Ha = 194
213 n
mi
Hp = 185
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15681162
39 X = 4796140
05
Y = -10090192
26 feet Y = -3021950
14 meter
Z = 11828246
45 Z = 3628508
72
XDOT = 17779
953956 XDOT = 5404
129302
YDOT = 10616
035381 feet/sec YDOT = 3296
285089 meter/sec
ZDOT = -14442
846669 ZDOT = -4375
889171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13023045
46 X = -3969424
26
Y = 13266018
01 feet Y = 4043482
29 meter
Z = 11917688
57 Z = 3632511
47
XDOT = -18786
837754 XDOT = -5726
228147
YDOT = -5494
516734 feet/sec YDOT = -1674
728701 meter/sec
ZDOT = -14341
080143 ZDOT = -4371
161228
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 08207
73296902
00020000 00000-0 20000-3 0 9037
2 25544 51
6401 178
1896 0010171 353
5211 6
5818 15
72678585 34604
Satellite: ISS
Catalog Number: 25544
Epoch time: 08207
73296902 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 178
1896 deg
Eccentricity:
0010171
Arg of perigee: 353
5211 deg
Mean anomaly: 6
5818 deg
Mean motion: 15
72678585 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3460
Checksum: 293
Coasting Arc #5 (Orbit 3475)
---------------------------------------
Vector Time (GMT): 2008/208/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5303974
93 A = 6730528
32 meter
Y = -2109704
05 meter E =
0015203
Z = 3546952
96 I = 51
68573
XDOT = 4664
157476 Wp = 50
74244
YDOT = -4199
110144 meter/sec RA = 172
28492 deg
ZDOT = 4473
731421 TA = 351
53071
MA = 351
55634
Ha = 194
465 n
mi
Hp = 184
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17401492
55 X = -5297220
13
Y = -6921601
22 feet Y = -2168978
82 meter
Z = 11636984
79 Z = 3521202
39
XDOT = 15302
353923 XDOT = 4689
033368
YDOT = -13776
608084 feet/sec YDOT = -4146
814332 meter/sec
ZDOT = 14677
596524 ZDOT = 4496
449794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18607405
41 X = 5671537
17
Y = 2606273
83 feet Y = 794392
26 meter
Z = 11537405
34 Z = 3516601
15
XDOT = -11349
447685 XDOT = -3459
311655
YDOT = 15620
401838 feet/sec YDOT = 4761
098480 meter/sec
ZDOT = 14764
852382 ZDOT = 4500
327006
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 08208
74964816
00020000 00000-0 20000-3 0 9046
2 25544 51
6406 172
9780 0010248 357
2768 2
8337 15
72691049 34768
Satellite: ISS
Catalog Number: 25544
Epoch time: 08208
74964816 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 172
9780 deg
Eccentricity:
0010248
Arg of perigee: 357
2768 deg
Mean anomaly: 2
8337 deg
Mean motion: 15
72691049 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3476
Checksum: 316
Coasting Arc #6 (Orbit 3490)
---------------------------------------
Vector Time (GMT): 2008/209/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3275006
56 A = 6728173
61 meter
Y = 4134181
68 meter E =
0010684
Z = -4179125
46 I = 51
70732
XDOT = -6582
557522 Wp = 46
01374
YDOT = -1489
329785 meter/sec RA = 167
11272 deg
ZDOT = 3698
265130 TA = 261
68069
MA = 261
80184
Ha = 194
394 n
mi
Hp = 184
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10744772
18 X = -3300690
85
Y = 13563588
17 feet Y = 4097415
70 meter
Z = -13711041
52 Z = -4195097
16
XDOT = -21596
317331 XDOT = -6583
379824
YDOT = -4886
252574 feet/sec YDOT = -1562
944879 meter/sec
ZDOT = 12133
415781 ZDOT = 3666
284920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6895118
23 X = 2101632
04
Y = -15817565
20 feet Y = -4821193
87 meter
Z = -13772279
71 Z = -4197790
86
XDOT = 21043
565323 XDOT = 6414
078710
YDOT = -1246
441792 feet/sec YDOT = -379
915458 meter/sec
ZDOT = 12009
843274 ZDOT = 3660
600230
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 08209
70277446
00020000 00000-0 20000-3 0 9050
2 25544 51
6407 168
0928 0010285 359
9616
1544 15
72717573 34910
Satellite: ISS
Catalog Number: 25544
Epoch time: 08209
70277446 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 168
0928 deg
Eccentricity:
0010285
Arg of perigee: 359
9616 deg
Mean anomaly:
1544 deg
Mean motion: 15
72717573 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3491
Checksum: 302
Coasting Arc #7 (Orbit 3506)
---------------------------------------
Vector Time (GMT): 2008/210/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6056766
70 A = 6732238
53 meter
Y = 455439
27 meter E =
0009432
Z = -2918319
26 I = 51
74898
XDOT = -2809
133560 Wp = 30
22883
YDOT = 5083
865700 meter/sec RA = 162
04170 deg
ZDOT = -5035
813304 TA = 183
23942
MA = 183
24553
Ha = 194
507 n
mi
Hp = 184
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19871281
84 X = 6065400
32
Y = 1494223
34 feet Y = 523218
28 meter
Z = -9574538
25 Z = -2888874
66
XDOT = -9216
317455 XDOT = -2841
310494
YDOT = 16679
349410 feet/sec YDOT = 5052
273290 meter/sec
ZDOT = -16521
697192 ZDOT = -5049
537278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19592532
22 X = -5971803
82
Y = 3923974
12 feet Y = 1196027
31 meter
Z = -9460836
98 Z = -2883663
11
XDOT = 4582
046908 XDOT = 1396
607898
YDOT = -17090
185286 feet/sec YDOT = -5209
088475 meter/sec
ZDOT = -16574
178388 ZDOT = -5051
809573
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 08210
71943300
00020000 00000-0 20000-3 0 9063
2 25544 51
6407 162
8814 0010186 3
1630 356
9595 15
72712526 35079
Satellite: ISS
Catalog Number: 25544
Epoch time: 08210
71943300 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 162
8814 deg
Eccentricity:
0010186
Arg of perigee: 3
1630 deg
Mean anomaly: 356
9595 deg
Mean motion: 15
72712526 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3507
Checksum: 274
Coasting Arc #8 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2008/211/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1600637
31 A = 6726353
67 meter
Y = -4631396
19 meter E =
0016369
Z = 4606940
97 I = 51
75787
XDOT = 7093
483640 Wp = 32
31823
YDOT = -500
995033 meter/sec RA = 156
87780 deg
ZDOT = -2949
846070 TA = 86
97502
MA = 86
78772
Ha = 194
521 n
mi
Hp = 184
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5251434
74 X = 1629927
99
Y = -15194869
40 feet Y = -4613333
96 meter
Z = 15114635
74 Z = 4614787
12
XDOT = 23272
584121 XDOT = 7112
888259
YDOT = -1643
684492 feet/sec YDOT = -421
562632 meter/sec
ZDOT = -9677
972669 ZDOT = -2915
339357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -608911
26 X = -185596
15
Y = 16037077
03 feet Y = 4888101
08 meter
Z = 15144478
33 Z = 4616037
00
XDOT = -20716
337831 XDOT = -6314
339771
YDOT = 8283
782514 feet/sec YDOT = 2524
896910 meter/sec
ZDOT = -9544
803734 ZDOT = -2909
256178
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 08211
73607928
00020000 00000-0 20000-3 0 9070
2 25544 51
6410 157
6697 0010379 6
8912 353
2391 15
72796565 35238
Satellite: ISS
Catalog Number: 25544
Epoch time: 08211
73607928 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 157
6697 deg
Eccentricity:
0010379
Arg of perigee: 6
8912 deg
Mean anomaly: 353
2391 deg
Mean motion: 15
72796565 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3523
Checksum: 310
Coasting Arc #9 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2008/212/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6200349
48 A = 6733647
63 meter
Y = 1347892
55 meter E =
0021194
Z = 2214029
95 I = 51
80821
XDOT = 808
693113 Wp = 46
09297
YDOT = -5342
026779 meter/sec RA = 151
80302 deg
ZDOT = 5498
946645 TA = 338
68978
MA = 338
77791
Ha = 194
783 n
mi
Hp = 184
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20342353
93 X = -6225716
14
Y = 4422219
66 feet Y = 1278414
51 meter
Z = 7263877
78 Z = 2183847
85
XDOT = 2653
192628 XDOT = 841
656063
YDOT = -17526
334576 feet/sec YDOT = -5332
800051 meter/sec
ZDOT = 18041
163534 ZDOT = 5502
954438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18094964
32 X = 5515345
13
Y = -10373873
90 feet Y = -3161956
76 meter
Z = 7147469
28 Z = 2178548
64
XDOT = 2107
680216 XDOT = 642
420930
YDOT = 16158
152983 feet/sec YDOT = 4925
005029 meter/sec
ZDOT = 18056
120336 ZDOT = 5503
505478
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 08212
75271748
00020000 00000-0 20000-3 0 9081
2 25544 51
6409 152
4579 0010386 10
8017 349
3367 15
72763282 35393
Satellite: ISS
Catalog Number: 25544
Epoch time: 08212
75271748 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 152
4579 deg
Eccentricity:
0010386
Arg of perigee: 10
8017 deg
Mean anomaly: 349
3367 deg
Mean motion: 15
72763282 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3539
Checksum: 306
Coasting Arc #10 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2008/213/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 174597
95 A = 6724962
89 meter
Y = 4553432
85 meter E =
0016237
Z = -4956418
20 I = 51
80458
XDOT = -6932
533928 Wp = 66
27100
YDOT = 2563
138307 meter/sec RA = 146
65194 deg
ZDOT = 2122
373887 TA = 224
22365
MA = 224
35353
Ha = 194
741 n
mi
Hp = 183
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 572827
91 X = 147744
54
Y = 14939084
14 feet Y = 4555235
79 meter
Z = -16261214
55 Z = -4955634
66
XDOT = -22744
533884 XDOT = -6970
989964
YDOT = 8409
246415 feet/sec YDOT = 2485
399442 meter/sec
ZDOT = 6963
168921 ZDOT = 2088
603386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5388768
34 X = -1642496
59
Y = -13949135
08 feet Y = -4251696
37 meter
Z = -16257744
98 Z = -4955360
67
XDOT = 17902
338045 XDOT = 5456
632636
YDOT = -14834
538477 feet/sec YDOT = -4521
567328 meter/sec
ZDOT = 6833
006452 ZDOT = 2082
700367
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 08213
70580422
00020000 00000-0 20000-3 0 9090
2 25544 51
6408 147
5720 0010319 14
0339 346
1108 15
72795371 35543
Satellite: ISS
Catalog Number: 25544
Epoch time: 08213
70580422 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 147
5720 deg
Eccentricity:
0010319
Arg of perigee: 14
0339 deg
Mean anomaly: 346
1108 deg
Mean motion: 15
72795371 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3554
Checksum: 275
Coasting Arc #11 (Orbit 3569)
---------------------------------------
Vector Time (GMT): 2008/214/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5796993
21 A = 6734715
69 meter
Y = -3084387
57 meter E =
0008712
Z = -1511553
09 I = 51
86088
XDOT = 1115
553133 Wp = 70
07209
YDOT = 4926
132478 meter/sec RA = 141
57071 deg
ZDOT = -5797
712854 TA = 126
49964
MA = 126
41936
Ha = 194
817 n
mi
Hp = 183
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19019006
60 X = 5838395
14
Y = -10119381
81 feet Y = -3019330
63 meter
Z = -4959163
67 Z = -1483291
76
XDOT = 3659
951223 XDOT = 1088
548930
YDOT = 16161
851961 feet/sec YDOT = 4938
456804 meter/sec
ZDOT = -19021
367632 ZDOT = -5792
358755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14561010
30 X = -4438195
94
Y = 15911291
87 feet Y = 4849761
76 meter
Z = -4850316
98 Z = -1478376
61
XDOT = -7800
806119 XDOT = -2377
685705
YDOT = -12906
172611 feet/sec YDOT = -3933
801412 meter/sec
ZDOT = -19000
206098 ZDOT = -5791
262819
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 08214
72242073
00020000 00000-0 20000-3 0 9102
2 25544 51
6409 142
3611 0010187 17
7396 342
4120 15
72773057 35700
Satellite: ISS
Catalog Number: 25544
Epoch time: 08214
72242073 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 142
3611 deg
Eccentricity:
0010187
Arg of perigee: 17
7396 deg
Mean anomaly: 342
4120 deg
Mean motion: 15
72773057 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3570
Checksum: 264
Coasting Arc #12 (Orbit 3585)
---------------------------------------
Vector Time (GMT): 2008/215/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1737730
05 A = 6723987
54 meter
Y = -3941020
02 meter E =
0013942
Z = 5159488
23 I = 51
84737
XDOT = 6156
886984 Wp = 31
11361
YDOT = -4440
979917 meter/sec RA = 136
43401 deg
ZDOT = -1305
285397 TA = 71
40644
MA = 71
25507
Ha = 194
885 n
mi
Hp = 183
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5701214
08 X = -1718595
04
Y = -12929855
70 feet Y = -3960345
67 meter
Z = 16927454
84 Z = 5151092
76
XDOT = 20199
760446 XDOT = 6212
429825
YDOT = -14570
144086 feet/sec YDOT = -4371
819425 meter/sec
ZDOT = -4282
432405 ZDOT = -1275
241352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9966181
66 X = 3037692
17
Y = 10073238
27 feet Y = 3070323
02 meter
Z = 16894639
13 Z = 5149486
01
XDOT = -13090
916417 XDOT = -3990
111324
YDOT = 20013
375687 feet/sec YDOT = 6100
076909 meter/sec
ZDOT = -4166
826485 ZDOT = -1270
048713
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 08215
73902490
00020000 00000-0 20000-3 0 9111
2 25544 51
6408 137
1490 0010268 21
3572 338
8017 15
72825063 35869
Satellite: ISS
Catalog Number: 25544
Epoch time: 08215
73902490 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 137
1490 deg
Eccentricity:
0010268
Arg of perigee: 21
3572 deg
Mean anomaly: 338
8017 deg
Mean motion: 15
72825063 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3586
Checksum: 282
Coasting Arc #13 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2008/216/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4838923
27 A = 6735263
88 meter
Y = 4604814
76 meter E =
0022994
Z = 754246
55 I = 51
90456
XDOT = -2801
128333 Wp = 40
96333
YDOT = -3940
758628 meter/sec RA = 131
34148 deg
ZDOT = 6002
893598 TA = 327
23337
MA = 327
37577
Ha = 194
919 n
mi
Hp = 183
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15875732
51 X = -4893719
32
Y = 15107659
98 feet Y = 4550396
73 meter
Z = 2474562
18 Z = 730606
65
XDOT = -9190
053587 XDOT = -2786
014335
YDOT = -12928
998122 feet/sec YDOT = -3971
998220 meter/sec
ZDOT = 19694
532801 ZDOT = 5989
322526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9237487
91 X = 2815586
32
Y = -19884428
69 feet Y = -6060773
87 meter
Z = 2383703
70 Z = 726552
89
XDOT = 11947
797969 XDOT = 3641
688821
YDOT = 7939
902018 feet/sec YDOT = 2420
082135 meter/sec
ZDOT = 19641
722742 ZDOT = 5986
797092
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 08216
75561895
00020000 00000-0 20000-3 0 9125
2 25544 51
6397 131
9367 0010248 25
1321 335
0338 15
72841324 36025
Satellite: ISS
Catalog Number: 25544
Epoch time: 08216
75561895 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 131
9367 deg
Eccentricity:
0010248
Arg of perigee: 25
1321 deg
Mean anomaly: 335
0338 deg
Mean motion: 15
72841324 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3602
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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