Date:
January 1st 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12755 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 95 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3712)
---------------------------------------
Vector Time (GMT): 2010/001/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -612286
17 A = 6711720
27 meter
Y = -4247471
26 meter E =
0019742
Z = -5176790
05 I = 51
67849
XDOT = 7596
640447 Wp = 98
31254
YDOT = 317
400992 meter/sec RA = 9
35115 deg
ZDOT = -1165
484348 TA = 160
58972
MA = 160
51443
Ha = 187
720 n
mi
Hp = 176
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2008812
90 X = -539597
09
Y = -13935273
17 feet Y = -4253910
92 meter
Z = -16984219
31 Z = -5179588
65
XDOT = 24923
361047 XDOT = 7598
188258
YDOT = 1041
341838 feet/sec YDOT = 402
359961 meter/sec
ZDOT = -3823
767546 ZDOT = -1128
576489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13409394
39 X = -4087183
41
Y = 4247035
78 feet Y = 1294496
51 meter
Z = -16995343
55 Z = -5180180
71
XDOT = -2898
504505 XDOT = -883
464173
YDOT = -23782
257669 feet/sec YDOT = -7248
832138 meter/sec
ZDOT = -3677
646369 ZDOT = -1120
946613
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 10001
17517343
00016717 00000-0 10270-3 0 9000
2 25544 51
6423 9
7566 0007358 134
5770 225
5996 15
77091010 37139
Satellite: ISS
Catalog Number: 25544
Epoch time: 10001
17517343 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 9
7566 deg
Eccentricity:
0007358
Arg of perigee: 134
5770 deg
Mean anomaly: 225
5996 deg
Mean motion: 15
77091010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3713
Checksum: 293
Coasting Arc #2 (Orbit 3728)
---------------------------------------
Vector Time (GMT): 2010/002/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6693833
72 A = 6723203
65 meter
Y = -518377
98 meter E =
0019282
Z = -35958
27 I = 51
68844
XDOT = 390
965230 Wp = 135
72261
YDOT = -4764
067155 meter/sec RA = 4
18576 deg
ZDOT = -6049
889115 TA = 44
66847
MA = 44
51330
Ha = 187
477 n
mi
Hp = 176
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21961396
73 X = -6687364
95
Y = -1700715
17 feet Y = -593196
21 meter
Z = -117973
34 Z = -68460
72
XDOT = 1282
694324 XDOT = 473
597567
YDOT = -15630
141585 feet/sec YDOT = -4759
232273 meter/sec
ZDOT = -19848
717569 ZDOT = -6047
789802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2428535
82 X = 740217
72
Y = 21891794
53 feet Y = 6672618
97 meter
Z = -246661
74 Z = -75182
50
XDOT = -14020
681388 XDOT = -4273
503687
YDOT = 1366
271011 feet/sec YDOT = 416
439404 meter/sec
ZDOT = -19840
458805 ZDOT = -6047
371844
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 10002
18900223
00016717 00000-0 10270-3 0 9016
2 25544 51
6429 4
5259 0007146 137
5644 222
6074 15
77159149 37295
Satellite: ISS
Catalog Number: 25544
Epoch time: 10002
18900223 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 4
5259 deg
Eccentricity:
0007146
Arg of perigee: 137
5644 deg
Mean anomaly: 222
6074 deg
Mean motion: 15
77159149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 295
Coasting Arc #3 (Orbit 3744)
---------------------------------------
Vector Time (GMT): 2010/003/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1291269
61 A = 6711777
04 meter
Y = 4099802
03 meter E =
0008723
Z = 5147346
19 I = 51
61859
XDOT = -7567
666537 Wp = 113
07172
YDOT = -843
222142 meter/sec RA = 359
01583 deg
ZDOT = -1228
542221 TA = 348
64224
MA = 348
66191
Ha = 187
648 n
mi
Hp = 177
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4236448
86 X = -1362022
74
Y = 13450794
07 feet Y = 4084966
13 meter
Z = 16887618
72 Z = 5140901
91
XDOT = -24828
302287 XDOT = -7551
707114
YDOT = -2766
476845 feet/sec YDOT = -927
758893 meter/sec
ZDOT = -4030
650330 ZDOT = -1265
266569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14052067
32 X = 4283070
12
Y = 1506722
60 feet Y = 459249
05 meter
Z = 16862153
40 Z = 5139584
35
XDOT = 2449
926991 XDOT = 746
737747
YDOT = 23823
421351 feet/sec YDOT = 7261
378828 meter/sec
ZDOT = -4176
061513 ZDOT = -1272
863549
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 10003
20281812
00016717 00000-0 10270-3 0 9027
2 25544 51
6423 359
2949 0007459 142
2301 217
9389 15
77107320 37453
Satellite: ISS
Catalog Number: 25544
Epoch time: 10003
20281812 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 359
2949 deg
Eccentricity:
0007459
Arg of perigee: 142
2301 deg
Mean anomaly: 217
9389 deg
Mean motion: 15
77107320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3745
Checksum: 294
Coasting Arc #4 (Orbit 3760)
---------------------------------------
Vector Time (GMT): 2010/004/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6315260
21 A = 6721231
81 meter
Y = 973636
33 meter E =
0017492
Z = 2071897
18 I = 51
62136
XDOT = -2557
859022 Wp = 94
15580
YDOT = 4694
177356 meter/sec RA = 353
88423 deg
ZDOT = 5549
298322 TA = 289
01377
MA = 289
20319
Ha = 187
449 n
mi
Hp = 177
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20719357
64 X = 6293838
75
Y = 3194344
91 feet Y = 1044137
36 meter
Z = 6797562
93 Z = 2102524
22
XDOT = -8391
925926 XDOT = -2637
117039
YDOT = 15400
844344 feet/sec YDOT = 4665
130263 meter/sec
ZDOT = 18206
359323 ZDOT = 5536
680327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1440731
75 X = -439135
04
Y = -20874781
20 feet Y = -6362633
31 meter
Z = 6918835
46 Z = 2108861
05
XDOT = 15373
202799 XDOT = 4685
752213
YDOT = 5000
950459 feet/sec YDOT = 1524
289700 meter/sec
ZDOT = 18156
462324 ZDOT = 5534
089716
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 10004
21661475
00016717 00000-0 10270-3 0 9037
2 25544 51
6426 354
0638 0007506 146
3511 213
8132 15
77171383 37614
Satellite: ISS
Catalog Number: 25544
Epoch time: 10004
21661475 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 354
0638 deg
Eccentricity:
0007506
Arg of perigee: 146
3511 deg
Mean anomaly: 213
8132 deg
Mean motion: 15
77171383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3761
Checksum: 285
Coasting Arc #5 (Orbit 3775)
---------------------------------------
Vector Time (GMT): 2010/005/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3112789
05 A = 6715074
07 meter
Y = -4114270
94 meter E =
0015411
Z = -4314442
71 I = 51
57158
XDOT = 6715
953466 Wp = 128
16825
YDOT = 1453
561434 meter/sec RA = 348
67766 deg
ZDOT = 3458
296627 TA = 176
85695
MA = 176
84726
Ha = 187
417 n
mi
Hp = 177
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10212562
51 X = 3179522
69
Y = -13498264
23 feet Y = -4079088
49 meter
Z = -14154995
78 Z = -4299159
16
XDOT = 22033
968064 XDOT = 6682
400802
YDOT = 4768
902344 feet/sec YDOT = 1528
475379 meter/sec
ZDOT = 11346
117542 ZDOT = 3490
840858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15554736
59 X = -4741083
71
Y = -6801288
52 feet Y = -2073032
74 meter
Z = -14094542
20 Z = -4296016
46
XDOT = -1071
147050 XDOT = -326
485621
YDOT = -21337
188934 feet/sec YDOT = -6503
575187 meter/sec
ZDOT = 11474
985121 ZDOT = 3497
575465
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 10005
16703541
00016717 00000-0 10270-3 0 9044
2 25544 51
6436 349
1601 0007608 149
2888 210
8724 15
77192061 37768
Satellite: ISS
Catalog Number: 25544
Epoch time: 10005
16703541 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 349
1601 deg
Eccentricity:
0007608
Arg of perigee: 149
2888 deg
Mean anomaly: 210
8724 deg
Mean motion: 15
77192061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3776
Checksum: 306
Coasting Arc #6 (Orbit 3791)
---------------------------------------
Vector Time (GMT): 2010/006/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5262113
46 A = 6716440
11 meter
Y = -1631908
03 meter E =
0010927
Z = -3846177
10 I = 51
54780
XDOT = 4467
928553 Wp = 115
82260
YDOT = -4729
040041 meter/sec RA = 343
56344 deg
ZDOT = -4119
971519 TA = 111
14342
MA = 111
02660
Ha = 187
212 n
mi
Hp = 177
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17264151
78 X = -5224790
24
Y = -5354028
97 feet Y = -1690543
19 meter
Z = -12618691
27 Z = -3871649
63
XDOT = 14658
558244 XDOT = 4540
491323
YDOT = -15515
223232 feet/sec YDOT = -4678
671065 meter/sec
ZDOT = -13516
966927 ZDOT = -4098
090554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -816693
08 X = -248928
05
Y = 17985931
01 feet Y = 5482111
77 meter
Z = -12719560
94 Z = -3876922
17
XDOT = -17436
101671 XDOT = -5314
523789
YDOT = -10258
073477 feet/sec YDOT = -3126
660796 meter/sec
ZDOT = -13430
406272 ZDOT = -4093
587832
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 10006
18080081
00016717 00000-0 10270-3 0 9055
2 25544 51
6439 343
9299 0007535 152
6146 207
5417 15
77229127 37924
Satellite: ISS
Catalog Number: 25544
Epoch time: 10006
18080081 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 343
9299 deg
Eccentricity:
0007535
Arg of perigee: 152
6146 deg
Mean anomaly: 207
5417 deg
Mean motion: 15
77229127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3792
Checksum: 313
Coasting Arc #7 (Orbit 3807)
---------------------------------------
Vector Time (GMT): 2010/007/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4535259
39 A = 6719841
83 meter
Y = 4126952
42 meter E =
0019034
Z = 2721202
52 I = 51
52961
XDOT = -5234
289519 Wp = 120
29781
YDOT = -2336
207168 meter/sec RA = 338
34651 deg
ZDOT = -5163
350728 TA = 28
49787
MA = 28
39393
Ha = 187
254 n
mi
Hp = 177
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14879459
95 X = -4594289
66
Y = 13539870
15 feet Y = 4075906
24 meter
Z = 8927829
78 Z = 2699027
24
XDOT = -17172
865876 XDOT = -5182
694140
YDOT = -7664
721681 feet/sec YDOT = -2394
451272 meter/sec
ZDOT = -16940
127061 ZDOT = -5188
653582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17072920
97 X = 5203826
31
Y = 10714503
46 feet Y = 3265780
66 meter
Z = 8840098
51 Z = 2694462
03
XDOT = -1982
143504 XDOT = -604
157340
YDOT = 17264
846482 feet/sec YDOT = 5262
325208 meter/sec
ZDOT = -17040
332194 ZDOT = -5193
893253
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 10007
19455022
00016717 00000-0 10270-3 0 9069
2 25544 51
6432 338
6987 0007622 157
2986 202
8518 15
77225817 38082
Satellite: ISS
Catalog Number: 25544
Epoch time: 10007
19455022 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 338
6987 deg
Eccentricity:
0007622
Arg of perigee: 157
2986 deg
Mean anomaly: 202
8518 deg
Mean motion: 15
77225817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3808
Checksum: 325
Coasting Arc #8 (Orbit 3823)
---------------------------------------
Vector Time (GMT): 2010/008/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3769138
47 A = 6712011
51 meter
Y = 2511804
39 meter E =
0012711
Z = 4950214
64 I = 51
47727
XDOT = -5774
880529 Wp = 144
97352
YDOT = 4698
646117 meter/sec RA = 333
21629 deg
ZDOT = 2000
102507 TA = 285
58863
MA = 285
72890
Ha = 186
903 n
mi
Hp = 177
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12365939
88 X = 3716723
74
Y = 8240828
06 feet Y = 2553659
67 meter
Z = 16240861
68 Z = 4968397
94
XDOT = -18946
458428 XDOT = -5836
708517
YDOT = 15415
505634 feet/sec YDOT = 4633
722133 meter/sec
ZDOT = 6562
016100 ZDOT = 1971
898420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4374420
33 X = 1333323
32
Y = -14119051
98 feet Y = -4303487
04 meter
Z = 16312882
10 Z = 4972166
46
XDOT = 19184
661187 XDOT = 5847
484730
YDOT = 13444
830799 feet/sec YDOT = 4097
984428 meter/sec
ZDOT = 6450
426951 ZDOT = 1966
090135
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 10008
20828161
00016717 00000-0 10270-3 0 9071
2 25544 51
6441 333
4680 0007546 161
6744 198
4694 15
77292610 38249
Satellite: ISS
Catalog Number: 25544
Epoch time: 10008
20828161 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 333
4680 deg
Eccentricity:
0007546
Arg of perigee: 161
6744 deg
Mean anomaly: 198
4694 deg
Mean motion: 15
77292610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3824
Checksum: 314
Coasting Arc #9 (Orbit 3838)
---------------------------------------
Vector Time (GMT): 2010/009/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5372357
40 A = 6722626
32 meter
Y = -3985048
82 meter E =
0009109
Z = -672509
90 I = 51
48760
XDOT = 3347
812628 Wp = 83
68359
YDOT = 3516
555954 meter/sec RA = 328
02216 deg
ZDOT = 5976
331883 TA = 268
97133
MA = 269
07569
Ha = 186
956 n
mi
Hp = 177
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17625844
49 X = 5419786
55
Y = -13074307
15 feet Y = -3924706
69 meter
Z = -2206397
32 Z = -646296
24
XDOT = 10983
637232 XDOT = 3279
209203
YDOT = 11537
257066 feet/sec YDOT = 3553
609016 meter/sec
ZDOT = 19607
388069 ZDOT = 5992
429217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17808683
36 X = -5428086
69
Y = -12841558
92 feet Y = -3914107
16 meter
Z = -2102677
43 Z = -640896
08
XDOT = 6760
965527 XDOT = 2060
742293
YDOT = -12557
553052 feet/sec YDOT = -3827
542170 meter/sec
ZDOT = 19671
163936 ZDOT = 5995
770768
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 10009
15864131
00016717 00000-0 10270-3 0 9084
2 25544 51
6451 328
5644 0007614 164
2495 195
8908 15
77295267 38399
Satellite: ISS
Catalog Number: 25544
Epoch time: 10009
15864131 = yrday
fracday
Element set: 908
Inclination: 51
6451 deg
RA of node: 328
5644 deg
Eccentricity:
0007614
Arg of perigee: 164
2495 deg
Mean anomaly: 195
8908 deg
Mean motion: 15
77295267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3839
Checksum: 337
Coasting Arc #10 (Orbit 3854)
---------------------------------------
Vector Time (GMT): 2010/010/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2053806
96 A = 6710702
51 meter
Y = -3682862
94 meter E =
0018553
Z = -5235164
31 I = 51
42281
XDOT = 6360
377151 Wp = 117
01395
YDOT = -4297
430462 meter/sec RA = 322
85104 deg
ZDOT = 521
062246 TA = 157
99577
MA = 157
91601
Ha = 186
772 n
mi
Hp = 177
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6738211
82 X = -1987040
52
Y = -12082883
66 feet Y = -3705455
92 meter
Z = -17175735
94 Z = -5244979
91
XDOT = 20867
379105 XDOT = 6405
427841
YDOT = -14099
181307 feet/sec YDOT = -4226
053133 meter/sec
ZDOT = 1709
521806 ZDOT = 552
069777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9327434
88 X = -2843002
15
Y = 10151866
55 feet Y = 3094288
93 meter
Z = -17214646
24 Z = -5247024
17
XDOT = -19286
545837 XDOT = -5878
539171
YDOT = -14575
188555 feet/sec YDOT = -4442
517471 meter/sec
ZDOT = 1832
217694 ZDOT = 558
459953
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 10010
17234124
00016717 00000-0 10270-3 0 9092
2 25544 51
6451 323
3343 0007565 167
8520 192
2829 15
77340264 38550
Satellite: ISS
Catalog Number: 25544
Epoch time: 10010
17234124 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 323
3343 deg
Eccentricity:
0007565
Arg of perigee: 167
8520 deg
Mean anomaly: 192
2829 deg
Mean motion: 15
77340264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3855
Checksum: 296
Coasting Arc #11 (Orbit 3870)
---------------------------------------
Vector Time (GMT): 2010/011/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5578935
35 A = 6721539
84 meter
Y = 3392267
03 meter E =
0015076
Z = -1563302
02 I = 51
43642
XDOT = -1396
514451 Wp = 156
54955
YDOT = -4934
558229 meter/sec RA = 317
69397 deg
ZDOT = -5756
521848 TA = 40
77536
MA = 40
66263
Ha = 186
572 n
mi
Hp = 177
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18303593
68 X = -5608859
46
Y = 11129485
01 feet Y = 3329712
96 meter
Z = -5128943
63 Z = -1590476
55
XDOT = -4581
740324 XDOT = -1313
267619
YDOT = -16189
495501 feet/sec YDOT = -4949
708691 meter/sec
ZDOT = -18886
226535 ZDOT = -5763
104488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16621106
28 X = 5066113
19
Y = 13472606
95 feet Y = 4106450
60 meter
Z = -5236480
59 Z = -1596079
28
XDOT = -12764
781856 XDOT = -3890
705510
YDOT = 8437
755482 feet/sec YDOT = 2571
827871 meter/sec
ZDOT = -18912
356906 ZDOT = -5764
486385
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 10011
18602452
00016717 00000-0 10270-3 0 9109
2 25544 51
6453 318
1022 0007538 172
1425 187
9859 15
77352440 38712
Satellite: ISS
Catalog Number: 25544
Epoch time: 10011
18602452 = yrday
fracday
Element set: 910
Inclination: 51
6453 deg
RA of node: 318
1022 deg
Eccentricity:
0007538
Arg of perigee: 172
1425 deg
Mean anomaly: 187
9859 deg
Mean motion: 15
77352440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3871
Checksum: 295
Coasting Arc #12 (Orbit 3886)
---------------------------------------
Vector Time (GMT): 2010/012/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 451726
67 A = 6713566
34 meter
Y = 4898545
99 meter E =
0009258
Z = 4559496
69 I = 51
38852
XDOT = -6281
493941 Wp = 114
98927
YDOT = 3345
887924 meter/sec RA = 312
47985 deg
ZDOT = -2971
526479 TA = 4
55803
MA = 4
54961
Ha = 186
547 n
mi
Hp = 177
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1482042
87 X = 374767
73
Y = 16071345
10 feet Y = 4903166
55 meter
Z = 14958978
65 Z = 4561504
88
XDOT = -20608
575921 XDOT = -6304
006419
YDOT = 10977
322586 feet/sec YDOT = 3275
519068 meter/sec
ZDOT = -9749
102622 ZDOT = -3002
095875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14551740
74 X = 4435370
58
Y = -6963573
10 feet Y = -2122497
08 meter
Z = 14967000
96 Z = 4561941
89
XDOT = 17002
058636 XDOT = 5182
227472
YDOT = 14309
185499 feet/sec YDOT = 4361
439740 meter/sec
ZDOT = -9870
084312 ZDOT = -3008
401698
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 10012
19969239
00016717 00000-0 10270-3 0 9111
2 25544 51
6460 312
8719 0007547 175
1717 184
9522 15
77343216 38873
Satellite: ISS
Catalog Number: 25544
Epoch time: 10012
19969239 = yrday
fracday
Element set: 911
Inclination: 51
6460 deg
RA of node: 312
8719 deg
Eccentricity:
0007547
Arg of perigee: 175
1717 deg
Mean anomaly: 184
9522 deg
Mean motion: 15
77343216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3887
Checksum: 328
Coasting Arc #13 (Orbit 3902)
---------------------------------------
Vector Time (GMT): 2010/013/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5257678
56 A = 6716987
59 meter
Y = -2278291
86 meter E =
0014689
Z = 3502061
21 I = 51
38223
XDOT = -281
915126 Wp = 123
40805
YDOT = 6264
464776 meter/sec RA = 307
34913 deg
ZDOT = 4477
173950 TA = 278
46161
MA = 278
62808
Ha = 186
277 n
mi
Hp = 177
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17249601
58 X = 5265751
95
Y = -7474710
84 feet Y = -2219452
71 meter
Z = 11489702
12 Z = 3527621
93
XDOT = -924
918391 XDOT = -373
693482
YDOT = 20552
705957 feet/sec YDOT = 6260
798484 meter/sec
ZDOT = 14688
890913 ZDOT = 4475
582327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13274692
41 X = -4046126
25
Y = -13223748
76 feet Y = -4030598
62 meter
Z = 11590872
34 Z = 3532897
89
XDOT = 18517
640313 XDOT = 5644
176768
YDOT = -5658
139574 feet/sec YDOT = -1724
600942 meter/sec
ZDOT = 14682
685790 ZDOT = 4475
282629
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 10013
21333991
00016717 00000-0 10270-3 0 9126
2 25544 51
6467 307
6406 0007539 180
1414 179
9750 15
77430386 39037
Satellite: ISS
Catalog Number: 25544
Epoch time: 10013
21333991 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 307
6406 deg
Eccentricity:
0007539
Arg of perigee: 180
1414 deg
Mean anomaly: 179
9750 deg
Mean motion: 15
77430386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3903
Checksum: 307
Coasting Arc #14 (Orbit 3917)
---------------------------------------
Vector Time (GMT): 2010/014/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 849610
06 A = 6718484
33 meter
Y = -5932772
70 meter E =
0007034
Z = -3046611
05 I = 51
36959
XDOT = 5689
035364 Wp = 147
52538
YDOT = -1700
724074 meter/sec RA = 302
11865 deg
ZDOT = 4897
762237 TA = 177
01876
MA = 177
01457
Ha = 186
172 n
mi
Hp = 178
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2787434
58 X = 930687
82
Y = -19464477
35 feet Y = -5922818
15 meter
Z = -9995443
07 Z = -3042287
52
XDOT = 18664
814185 XDOT = 5683
838364
YDOT = -5579
803392 feet/sec YDOT = -1637
135579 meter/sec
ZDOT = 16068
773743 ZDOT = 4925
386200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19064942
36 X = -5810994
43
Y = 4848052
16 feet Y = 1477686
30 meter
Z = -9978422
48 Z = -3041423
17
XDOT = -11930
196002 XDOT = -3636
323741
YDOT = -13612
875863 feet/sec YDOT = -4149
204563 meter/sec
ZDOT = 16178
125878 ZDOT = 4931
092768
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 10014
16362293
00016717 00000-0 10270-3 0 9139
2 25544 51
6468 302
7371 0007318 184
4255 175
6847 15
77398627 39187
Satellite: ISS
Catalog Number: 25544
Epoch time: 10014
16362293 = yrday
fracday
Element set: 913
Inclination: 51
6468 deg
RA of node: 302
7371 deg
Eccentricity:
0007318
Arg of perigee: 184
4255 deg
Mean anomaly: 175
6847 deg
Mean motion: 15
77398627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3918
Checksum: 330
Coasting Arc #15 (Orbit 3933)
---------------------------------------
Vector Time (GMT): 2010/015/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4626633
67 A = 6712095
34 meter
Y = 552999
08 meter E =
0011352
Z = -4839080
14 I = 51
33348
XDOT = 1564
694760 Wp = 109
28269
YDOT = -7171
986728 meter/sec RA = 296
98034 deg
ZDOT = -2323
721980 TA = 138
02265
MA = 137
93559
Ha = 185
962 n
mi
Hp = 178
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15179244
32 X = -4608966
70
Y = 1814301
45 feet Y = 501360
64 meter
Z = -15876247
18 Z = -4861512
85
XDOT = 5133
512993 XDOT = 1656
064853
YDOT = -23530
140183 feet/sec YDOT = -7153
978254 meter/sec
ZDOT = -7623
759776 ZDOT = -2315
899716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7695285
63 X = 2345523
06
Y = 13101740
14 feet Y = 3993410
39 meter
Z = -15965066
77 Z = -4866152
35
XDOT = -22682
311799 XDOT = -6913
568636
YDOT = 4102
397344 feet/sec YDOT = 1250
410711 meter/sec
ZDOT = -7592
915521 ZDOT = -2314
320651
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 10015
17724093
00016717 00000-0 10270-3 0 9142
2 25544 51
6468 297
5062 0007422 188
3347 171
7696 15
77431976 39348
Satellite: ISS
Catalog Number: 25544
Epoch time: 10015
17724093 = yrday
fracday
Element set: 914
Inclination: 51
6468 deg
RA of node: 297
5062 deg
Eccentricity:
0007422
Arg of perigee: 188
3347 deg
Mean anomaly: 171
7696 deg
Mean motion: 15
77431976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3934
Checksum: 334
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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