Date:
October 10th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
293/19:22:31
780 1
5 2
2 2
2
N/A -1
5 -0
0 195
3
000/00:04:59
559 0
4 0
1 185
1
Coasting Arc #1 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2010/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2354208
92 A = 6728788
41 meter
Y = 4198309
75 meter E =
0013724
Z = 4691025
89 I = 51
69823
XDOT = -7136
470501 Wp = 97
00700
YDOT = 908
093844 meter/sec RA = 10
38832 deg
ZDOT = 2760
242270 TA = 325
78888
MA = 325
87723
Ha = 195
948 n
mi
Hp = 184
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7723782
56 X = 2284298
98
Y = 13773982
11 feet Y = 4224245
43 meter
Z = 15390504
90 Z = 4702292
75
XDOT = -23413
617128 XDOT = -7159
503643
YDOT = 2979
310513 feet/sec YDOT = 828
160986 meter/sec
ZDOT = 9055
912959 ZDOT = 2725
516464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11178606
18 X = -3407239
16
Y = -11091757
64 feet Y = -3380767
73 meter
Z = 15435631
43 Z = 4704780
46
XDOT = 20889
632530 XDOT = 6367
159995
YDOT = -8605
719734 feet/sec YDOT = -2623
023375 meter/sec
ZDOT = 8916
692094 ZDOT = 2717
807750
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 10281
55243457
00016717 00000-0 10270-3 0 9004
2 25544 51
6478 10
6132 0007021 74
8588 285
3350 15
71809542 1308
Satellite: ISS
Catalog Number: 25544
Epoch time: 10281
55243457 = yrday
fracday
Element set: 900
Inclination: 51
6478 deg
RA of node: 10
6132 deg
Eccentricity:
0007021
Arg of perigee: 74
8588 deg
Mean anomaly: 285
3350 deg
Mean motion: 15
71809542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 286
Coasting Arc #2 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2010/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5714611
70 A = 6734518
30 meter
Y = -1882032
72 meter E =
0011542
Z = -3031264
39 I = 51
68688
XDOT = 4028
533754 Wp = 73
82246
YDOT = 4294
053842 meter/sec RA = 5
22967 deg
ZDOT = 4947
303509 TA = 251
18700
MA = 251
31224
Ha = 196
042 n
mi
Hp = 184
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18748726
06 X = 5749957
91
Y = -6174648
02 feet Y = -1817931
03 meter
Z = -9945093
13 Z = -3003416
15
XDOT = 13216
974259 XDOT = 3956
183730
YDOT = 14088
103156 feet/sec YDOT = 4338
699073 meter/sec
ZDOT = 16231
310724 ZDOT = 4966
698628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16136604
53 X = -4918437
06
Y = 11465575
61 feet Y = 3494707
45 meter
Z = -9833435
53 Z = -2997231
15
XDOT = -15866
794372 XDOT = -4836
198925
YDOT = -8396
621813 feet/sec YDOT = -2559
290328 meter/sec
ZDOT = 16309
013117 ZDOT = 4970
987198
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 10282
50611184
00016717 00000-0 10270-3 0 9017
2 25544 51
6475 5
7334 0007031 76
9298 283
2648 15
71809389 1458
Satellite: ISS
Catalog Number: 25544
Epoch time: 10282
50611184 = yrday
fracday
Element set: 901
Inclination: 51
6475 deg
RA of node: 5
7334 deg
Eccentricity:
0007031
Arg of perigee: 76
9298 deg
Mean anomaly: 283
2648 deg
Mean motion: 15
71809389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 309
Coasting Arc #3 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2010/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4528142
75 A = 6731611
02 meter
Y = -3105530
77 meter E =
0013853
Z = -3908475
97 I = 51
64647
XDOT = 5689
182946 Wp = 76
53651
YDOT = -3196
555934 meter/sec RA =
16268 deg
ZDOT = -4060
174477 TA = 151
15213
MA = 151
07547
Ha = 195
972 n
mi
Hp = 184
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14856111
37 X = -4474092
46
Y = -10188749
25 feet Y = -3155865
10 meter
Z = -12823083
88 Z = -3930342
81
XDOT = 18665
298379 XDOT = 5744
228646
YDOT = -10487
388234 feet/sec YDOT = -3132
628424 meter/sec
ZDOT = -13320
782405 ZDOT = -4032
401968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17223148
59 X = 5249615
69
Y = 5061920
26 feet Y = 1542873
30 meter
Z = -12910703
02 Z = -3935182
28
XDOT = -14160
298399 XDOT = -4316
058952
YDOT = 14562
707118 feet/sec YDOT = 4438
713130 meter/sec
ZDOT = -13209
411482 ZDOT = -4026
228620
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 10283
52334202
00016717 00000-0 10270-3 0 9024
2 25544 51
6466
5268 0007098 80
9972 279
1993 15
71846009 1619
Satellite: ISS
Catalog Number: 25544
Epoch time: 10283
52334202 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node:
5268 deg
Eccentricity:
0007098
Arg of perigee: 80
9972 deg
Mean anomaly: 279
1993 deg
Mean motion: 15
71846009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 161
Checksum: 307
Coasting Arc #4 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2010/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4054618
74 A = 6731143
40 meter
Y = 3551292
37 meter E =
0017993
Z = 4019124
32 I = 51
61543
XDOT = -6129
333910 Wp = 79
57426
YDOT = -2564
038801 meter/sec RA = 354
99158 deg
ZDOT = -3899
950710 TA = 50
73138
MA = 50
57189
Ha = 195
950 n
mi
Hp = 184
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13302554
91 X = -4113553
17
Y = 11651221
67 feet Y = 3505621
72 meter
Z = 13186103
40 Z = 3999283
37
XDOT = -20109
363223 XDOT = -6081
261163
YDOT = -8412
200792 feet/sec YDOT = -2632
311964 meter/sec
ZDOT = -12795
113877 ZDOT = -3929
610806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8807195
09 X = 2684433
06
Y = -15402425
10 feet Y = -4694659
17 meter
Z = 13106520
21 Z = 3994867
36
XDOT = 20561
976654 XDOT = 6267
290484
YDOT = 718
083419 feet/sec YDOT = 218
871826 meter/sec
ZDOT = -12913
978178 ZDOT = -3936
180549
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 10284
54054505
00016717 00000-0 10270-3 0 9033
2 25544 51
6470 355
3198 0007123 82
8737 277
3235 15
71928909 1772
Satellite: ISS
Catalog Number: 25544
Epoch time: 10284
54054505 = yrday
fracday
Element set: 903
Inclination: 51
6470 deg
RA of node: 355
3198 deg
Eccentricity:
0007123
Arg of perigee: 82
8737 deg
Mean anomaly: 277
3235 deg
Mean motion: 15
71928909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 177
Checksum: 319
Coasting Arc #5 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2010/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5965637
05 A = 6734424
80 meter
Y = 1233901
13 meter E =
0020609
Z = 2849833
23 I = 51
59617
XDOT = -3407
325867 Wp = 83
01857
YDOT = 4690
266201 meter/sec RA = 349
91918 deg
ZDOT = 5073
109320 TA = 309
71381
MA = 309
89530
Ha = 195
825 n
mi
Hp = 184
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19572300
04 X = 5937551
76
Y = 4048232
06 feet Y = 1300455
46 meter
Z = 9349846
56 Z = 2878746
53
XDOT = -11178
890640 XDOT = -3484
164698
YDOT = 15388
012472 feet/sec YDOT = 4651
733848 meter/sec
ZDOT = 16644
059450 ZDOT = 5056
369581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19715264
85 X = -6009212
73
Y = 2931028
79 feet Y = 893377
57 meter
Z = 9465735
27 Z = 2885156
11
XDOT = 5491
786508 XDOT = 1673
896528
YDOT = -16896
246167 feet/sec YDOT = -5149
975832 meter/sec
ZDOT = 16576
890295 ZDOT = 5052
636162
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 10285
55772367
00016717 00000-0 10270-3 0 9049
2 25544 51
6464 350
1130 0007219 87
1318 273
0670 15
71944536 1931
Satellite: ISS
Catalog Number: 25544
Epoch time: 10285
55772367 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 350
1130 deg
Eccentricity:
0007219
Arg of perigee: 87
1318 deg
Mean anomaly: 273
0670 deg
Mean motion: 15
71944536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 304
Coasting Arc #6 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2010/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1825217
56 A = 6728197
48 meter
Y = -4412882
52 meter E =
0018407
Z = -4756548
23 I = 51
54498
XDOT = 7223
939520 Wp = 100
64384
YDOT = 179
546951 meter/sec RA = 344
75064 deg
ZDOT = 2610
659454 TA = 195
04390
MA = 195
09872
Ha = 195
870 n
mi
Hp = 184
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5988246
60 X = 1897534
32
Y = -14477961
02 feet Y = -4392067
54 meter
Z = -15605473
21 Z = -4747505
51
XDOT = 23700
588977 XDOT = 7208
712620
YDOT = 589
064800 feet/sec YDOT = 260
244270 meter/sec
ZDOT = 8565
155690 ZDOT = 2645
716797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -444143
68 X = -135374
99
Y = 15697297
54 feet Y = 4784536
29 meter
Z = -15569162
89 Z = -4745480
85
XDOT = -21122
713859 XDOT = -6438
203184
YDOT = 8019
978515 feet/sec YDOT = 2444
489451 meter/sec
ZDOT = 8705
689789 ZDOT = 2653
494248
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 10286
51130515
00016717 00000-0 10270-3 0 9050
2 25544 51
6458 345
2313 0007305 89
2240 270
9760 15
71979625 2085
Satellite: ISS
Catalog Number: 25544
Epoch time: 10286
51130515 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 345
2313 deg
Eccentricity:
0007305
Arg of perigee: 89
2240 deg
Mean anomaly: 270
9760 deg
Mean motion: 15
71979625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 299
Coasting Arc #7 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2010/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6445846
24 A = 6736468
89 meter
Y = 939633
57 meter E =
0013566
Z = -1711867
24 I = 51
54498
XDOT = 758
452696 Wp = 117
11854
YDOT = -5110
048381 meter/sec RA = 339
65984 deg
ZDOT = -5701
383463 TA = 81
82092
MA = 81
66707
Ha = 195
791 n
mi
Hp = 184
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21147789
50 X = -6447558
30
Y = 3082787
31 feet Y = 867542
64 meter
Z = -5616362
33 Z = -1743185
63
XDOT = 2488
361864 XDOT = 843
234384
YDOT = -16765
250594 feet/sec YDOT = -5101
092981 meter/sec
ZDOT = -18705
326322 ZDOT = -5697
492827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18394232
98 X = 5606562
21
Y = -10814740
62 feet Y = -3296332
94 meter
Z = -5741923
23 Z = -1750138
20
XDOT = 3124
174236 XDOT = 952
248307
YDOT = 15167
498037 feet/sec YDOT = 4623
053402 meter/sec
ZDOT = -18689
661893 ZDOT = -5696
608945
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 10287
52843352
00016717 00000-0 10270-3 0 9063
2 25544 51
6463 340
0235 0007394 92
5728 267
6281 15
72024803 2242
Satellite: ISS
Catalog Number: 25544
Epoch time: 10287
52843352 = yrday
fracday
Element set: 906
Inclination: 51
6463 deg
RA of node: 340
0235 deg
Eccentricity:
0007394
Arg of perigee: 92
5728 deg
Mean anomaly: 267
6281 deg
Mean motion: 15
72024803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 299
Coasting Arc #8 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2010/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 504453
26 A = 6726111
93 meter
Y = 4294658
25 meter E =
0010813
Z = 5143039
81 I = 51
48217
XDOT = -7232
428599 Wp = 80
73257
YDOT = 2348
627329 meter/sec RA = 334
50430 deg
ZDOT = -1247
875231 TA = 21
23476
MA = 21
18991
Ha = 195
677 n
mi
Hp = 184
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1655030
37 X = 431407
95
Y = 14090086
12 feet Y = 4299891
11 meter
Z = 16873490
18 Z = 5145312
88
XDOT = -23728
440286 XDOT = -7252
091851
YDOT = 7705
470238 feet/sec YDOT = 2267
639980 meter/sec
ZDOT = -4094
078841 ZDOT = -1283
058482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6965406
86 X = -2123056
01
Y = -12346942
40 feet Y = -3763348
04 meter
Z = 16882548
51 Z = 5145800
79
XDOT = 17870
496054 XDOT = 5446
927197
YDOT = -15890
042610 feet/sec YDOT = -4843
284988 meter/sec
ZDOT = -4235
149341 ZDOT = -1290
873519
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 10288
54553431
00016717 00000-0 10270-3 0 9073
2 25544 51
6460 334
8163 0007271 96
1655 264
0336 15
72081616 2408
Satellite: ISS
Catalog Number: 25544
Epoch time: 10288
54553431 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 334
8163 deg
Eccentricity:
0007271
Arg of perigee: 96
1655 deg
Mean anomaly: 264
0336 deg
Mean motion: 15
72081616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 295
Coasting Arc #9 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2010/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5958708
67 A = 6737615
75 meter
Y = -3097125
66 meter E =
0018989
Z = 463523
15 I = 51
49366
XDOT = 1836
891674 Wp = 66
64860
YDOT = 4460
007536 meter/sec RA = 329
38818 deg
ZDOT = 6000
161827 TA = 298
39961
MA = 298
59090
Ha = 195
805 n
mi
Hp = 184
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19549569
13 X = 5990646
71
Y = -10161173
43 feet Y = -3030313
20 meter
Z = 1520745
26 Z = 492548
52
XDOT = 6026
547487 XDOT = 1757
734589
YDOT = 14632
570657 feet/sec YDOT = 4480
106477 meter/sec
ZDOT = 19685
570297 ZDOT = 6008
893014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13682459
52 X = -4170413
66
Y = 17258558
89 feet Y = 5260408
75 meter
Z = 1637135
12 Z = 498998
78
XDOT = -10114
550123 XDOT = -3082
914878
YDOT = -9943
357458 feet/sec YDOT = -3030
735353 meter/sec
ZDOT = 19720
518764 ZDOT = 6010
814119
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 10289
56261320
00016717 00000-0 10270-3 0 9080
2 25544 51
6459 329
6085 0007466 97
7053 262
4957 15
72054370 2561
Satellite: ISS
Catalog Number: 25544
Epoch time: 10289
56261320 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 329
6085 deg
Eccentricity:
0007466
Arg of perigee: 97
7053 deg
Mean anomaly: 262
4957 deg
Mean motion: 15
72054370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 325
Coasting Arc #10 (Orbit 270)
---------------------------------------
Vector Time (GMT): 2010/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2578248
55 A = 6725484
46 meter
Y = -3320921
60 meter E =
0022304
Z = -5268549
48 I = 51
42867
XDOT = 6168
777023 Wp = 93
26235
YDOT = -4575
122313 meter/sec RA = 324
25052 deg
ZDOT = -136
700340 TA = 175
44354
MA = 175
42320
Ha = 195
667 n
mi
Hp = 183
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8458820
69 X = -2515327
86
Y = -10895412
08 feet Y = -3349401
67 meter
Z = -17285267
33 Z = -5280921
68
XDOT = 20238
769762 XDOT = 6220
142480
YDOT = -15010
243810 feet/sec YDOT = -4505
852150 meter/sec
ZDOT = -448
491930 ZDOT = -106
607069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12189429
53 X = 3715338
12
Y = 6321685
86 feet Y = 1926849
85 meter
Z = -17334826
63 Z = -5283655
16
XDOT = -11499
984910 XDOT = -3505
195401
YDOT = 21290
945961 feet/sec YDOT = 6489
480329 meter/sec
ZDOT = -327
811401 ZDOT = -99
916915
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 10290
51609636
00016717 00000-0 10270-3 0 9094
2 25544 51
6467 324
7258 0007404 102
6260 257
5731 15
72116663 2712
Satellite: ISS
Catalog Number: 25544
Epoch time: 10290
51609636 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 324
7258 deg
Eccentricity:
0007404
Arg of perigee: 102
6260 deg
Mean anomaly: 257
5731 deg
Mean motion: 15
72116663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 271
Checksum: 300
Coasting Arc #11 (Orbit 286)
---------------------------------------
Vector Time (GMT): 2010/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4682610
45 A = 6737166
16 meter
Y = 4782675
65 meter E =
0020497
Z = 689964
65 I = 51
44391
XDOT = -3887
371666 Wp = 119
61168
YDOT = -2927
224342 meter/sec RA = 319
10705 deg
ZDOT = -5969
178321 TA = 52
85377
MA = 52
66672
Ha = 195
585 n
mi
Hp = 183
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15362895
17 X = -4739094
96
Y = 15691193
08 feet Y = 4729996
12 meter
Z = 2263663
55 Z = 667078
67
XDOT = -12753
844050 XDOT = -3825
352422
YDOT = -9603
754403 feet/sec YDOT = -2970
348962 meter/sec
ZDOT = -19583
918377 ZDOT = -5987
912536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6908871
90 X = 2105824
16
Y = -20854416
57 feet Y = -6356426
17 meter
Z = 2171879
27 Z = 661988
80
XDOT = 14052
720414 XDOT = 4283
269182
YDOT = 2564
507218 feet/sec YDOT = 781
661800 meter/sec
ZDOT = -19658
984488 ZDOT = -5992
058472
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 10291
53312092
00016717 00000-0 10270-3 0 9106
2 25544 51
6459 319
5176 0007530 105
6516 254
5478 15
72183430 2879
Satellite: ISS
Catalog Number: 25544
Epoch time: 10291
53312092 = yrday
fracday
Element set: 910
Inclination: 51
6459 deg
RA of node: 319
5176 deg
Eccentricity:
0007530
Arg of perigee: 105
6516 deg
Mean anomaly: 254
5478 deg
Mean motion: 15
72183430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 287
Checksum: 299
Coasting Arc #12 (Orbit 302)
---------------------------------------
Vector Time (GMT): 2010/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4059723
54 A = 6725840
32 meter
Y = 1652165
01 meter E =
0012011
Z = 5093262
20 I = 51
38317
XDOT = -4355
322061 Wp = 114
83548
YDOT = 6187
407162 meter/sec RA = 313
98819 deg
ZDOT = 1456
784496 TA = 321
11875
MA = 321
20508
Ha = 195
422 n
mi
Hp = 183
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13319302
95 X = 4016204
43
Y = 5420488
89 feet Y = 1697320
38 meter
Z = 16710177
84 Z = 5112878
82
XDOT = -14289
114373 XDOT = -4431
264008
YDOT = 20299
892264 feet/sec YDOT = 6138
278840 meter/sec
ZDOT = 4779
476693 ZDOT = 1435
441010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14238530
63 X = -4339904
14
Y = 1190079
56 feet Y = 362736
25 meter
Z = 16788791
81 Z = 5117223
74
XDOT = 3595
416380 XDOT = 1095
882913
YDOT = -23553
677860 feet/sec YDOT = -7179
161012 meter/sec
ZDOT = 4693
869611 ZDOT = 1430
691457
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 10292
55011911
00016717 00000-0 10270-3 0 9116
2 25544 51
6450 314
3094 0007585 109
1157 251
0827 15
72222278 3035
Satellite: ISS
Catalog Number: 25544
Epoch time: 10292
55011911 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 314
3094 deg
Eccentricity:
0007585
Arg of perigee: 109
1157 deg
Mean anomaly: 251
0827 deg
Mean motion: 15
72222278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 303
Checksum: 275
Coasting Arc #13 (Orbit 317)
---------------------------------------
Vector Time (GMT): 2010/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2830522
78 A = 6735603
74 meter
Y = -5835749
38 meter E =
0011926
Z = -1819959
57 I = 51
39727
XDOT = 5171
533603 Wp = 76
06333
YDOT = 759
077943 meter/sec RA = 308
82019 deg
ZDOT = 5642
863655 TA = 263
71185
MA = 263
84770
Ha = 195
420 n
mi
Hp = 183
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9286492
05 X = 2904410
05
Y = -19146159
39 feet Y = -5803683
80 meter
Z = -5970995
98 Z = -1806028
64
XDOT = 16966
973763 XDOT = 5135
248499
YDOT = 2490
413199 feet/sec YDOT = 816
706733 meter/sec
ZDOT = 18513
332202 ZDOT = 5667
899287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 780454
42 X = 237882
51
Y = 21280731
19 feet Y = 6486366
87 meter
Z = -5915109
27 Z = -1802925
31
XDOT = -14495
243396 XDOT = -4418
150187
YDOT = 5674
314681 feet/sec YDOT = 1729
531115 meter/sec
ZDOT = 18613
671695 ZDOT = 5673
447133
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 10293
50353056
00016717 00000-0 10270-3 0 9122
2 25544 51
6458 309
4270 0007625 113
0406 247
1561 15
72298603 3182
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
50353056 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 309
4270 deg
Eccentricity:
0007625
Arg of perigee: 113
0406 deg
Mean anomaly: 247
1561 deg
Mean motion: 15
72298603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 318
Checksum: 288
Coasting Arc #14 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2010/293/19:25:01
559
Vector Time (MET): N/A
Weight (LBS) : 812425
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1725448
81 A = 6727696
87 meter
Y = -4251927
29 meter E =
0018185
Z = -4936651
41 I = 51
36120
XDOT = 5686
195648 Wp = 108
47127
YDOT = -4727
770144 meter/sec RA = 307
23106 deg
ZDOT = 2085
209535 TA = 181
85704
MA = 181
86380
Ha = 195
326 n
mi
Hp = 185
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5660921
30 X = -1653792
83
Y = -13949892
67 feet Y = -4270822
05 meter
Z = -16196362
89 Z = -4944859
42
XDOT = 18655
497532 XDOT = 5728
510036
YDOT = -15511
056903 feet/sec YDOT = -4663
946921 meter/sec
ZDOT = 6841
238632 ZDOT = 2112
936860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4798524
77 X = 1462590
35
Y = -14232150
30 feet Y = -4337959
41 meter
Z = -16229225
62 Z = -4946667
97
XDOT = 23190
831892 XDOT = 7068
565561
YDOT = -106
629659 feet/sec YDOT = -32
500720 meter/sec
ZDOT = 6952
411717 ZDOT = 2119
095091
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 10293
82133000
00016717 00000-0 10270-3 0 9133
2 25544 51
6465 307
7991 0005561 115
8647 244
3089 15
71860801 3239
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
82133000 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 307
7991 deg
Eccentricity:
0005561
Arg of perigee: 115
8647 deg
Mean anomaly: 244
3089 deg
Mean motion: 15
71860801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 296
Coasting Arc #15 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2010/294/19:25:01
559
Vector Time (MET): N/A
Weight (LBS) : 812425
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4293912
49 A = 6737592
64 meter
Y = 5046277
25 meter E =
0014533
Z = -1193483
62 I = 51
37738
XDOT = -3040
503733 Wp = 134
15570
YDOT = -3960
013247 meter/sec RA = 302
12067 deg
ZDOT = -5858
604200 TA = 58
95894
MA = 58
81633
Ha = 195
234 n
mi
Hp = 185
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14087639
41 X = -4344223
88
Y = 16556027
72 feet Y = 4997978
74 meter
Z = -3915628
67 Z = -1214466
57
XDOT = -9975
405947 XDOT = -2967
535359
YDOT = -12992
169447 feet/sec YDOT = -3993
606429 meter/sec
ZDOT = -19221
142389 ZDOT = -5873
197819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21375884
65 X = -6515369
64
Y = 3869004
30 feet Y = 1179272
51 meter
Z = -3999768
39 Z = -1219129
40
XDOT = 907
051270 XDOT = 276
469227
YDOT = -14740
447371 feet/sec YDOT = -4492
888359 meter/sec
ZDOT = -19279
600940 ZDOT = -5876
422366
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 10294
83853368
00016717 00000-0 10270-3 0 9142
2 25544 51
6466 302
5918 0005580 121
1658 239
0052 15
71871812 3397
Satellite: ISS
Catalog Number: 25544
Epoch time: 10294
83853368 = yrday
fracday
Element set: 914
Inclination: 51
6466 deg
RA of node: 302
5918 deg
Eccentricity:
0005580
Arg of perigee: 121
1658 deg
Mean anomaly: 239
0052 deg
Mean motion: 15
71871812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 313
Coasting Arc #16 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2010/295/19:25:01
559
Vector Time (MET): N/A
Weight (LBS) : 812425
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3422000
27 A = 6725978
23 meter
Y = 2490570
81 meter E =
0007363
Z = 5221094
73 I = 51
32400
XDOT = -3902
821119 Wp = 103
86073
YDOT = 6615
058557 meter/sec RA = 296
96358 deg
ZDOT = -598
575800 TA = 351
84510
MA = 351
85706
Ha = 194
918 n
mi
Hp = 185
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11227035
02 X = 3368532
03
Y = 8171164
06 feet Y = 2528539
01 meter
Z = 17129575
89 Z = 5237589
27
XDOT = -12804
531229 XDOT = -3973
594001
YDOT = 21702
948021 feet/sec YDOT = 6571
019118 meter/sec
ZDOT = -1963
831364 ZDOT = -617
708547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3641127
93 X = 1109815
79
Y = 13314951
03 feet Y = 4058397
07 meter
Z = 17195664
39 Z = 5241238
51
XDOT = -22536
417621 XDOT = -6869
100091
YDOT = 8793
776166 feet/sec YDOT = 2680
342976 meter/sec
ZDOT = -2040
566076 ZDOT = -621
964540
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 10295
85570830
00016717 00000-0 10270-3 0 9156
2 25544 51
6464 297
3846 0005441 124
0373 236
1306 15
71979969 3558
Satellite: ISS
Catalog Number: 25544
Epoch time: 10295
85570830 = yrday
fracday
Element set: 915
Inclination: 51
6464 deg
RA of node: 297
3846 deg
Eccentricity:
0005441
Arg of perigee: 124
0373 deg
Mean anomaly: 236
1306 deg
Mean motion: 15
71979969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 328
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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