Date:
March 3rd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 651)
---------------------------------------
Vector Time (GMT): 2010/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1024297
05 A = 6730881
41 meter
Y = 6176639
95 meter E =
0017186
Z = 2441355
29 I = 51
95461
XDOT = -5374
119916 Wp = 49
29045
YDOT = -1242
105361 meter/sec RA = 62
81721 deg
ZDOT = 5383
772090 TA = 338
18099
MA = 338
25410
Ha = 192
238 n
mi
Hp = 184
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3360554
64 X = 943293
21
Y = 20264566
75 feet Y = 6187641
60 meter
Z = 8009695
85 Z = 2446133
80
XDOT = -17631
627021 XDOT = -5385
983939
YDOT = -4075
148822 feet/sec YDOT = -1302
267708 meter/sec
ZDOT = 17663
294258 ZDOT = 5357
636451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4374763
55 X = -1333427
93
Y = 20062407
14 feet Y = 6115021
69 meter
Z = 8028853
25 Z = 2447194
47
XDOT = -13529
035345 XDOT = -4123
649973
YDOT = -9995
011361 feet/sec YDOT = -3046
479463 meter/sec
ZDOT = 17559
431653 ZDOT = 5352
114768
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 10060
55863775
00016717 00000-0 10270-3 0 9000
2 25544 51
6429 63
1453 0007540 357
6738 2
4389 15
73541563 6525
Satellite: ISS
Catalog Number: 25544
Epoch time: 10060
55863775 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 63
1453 deg
Eccentricity:
0007540
Arg of perigee: 357
6738 deg
Mean anomaly: 2
4389 deg
Mean motion: 15
73541563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 309
Coasting Arc #2 (Orbit 666)
---------------------------------------
Vector Time (GMT): 2010/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4728466
37 A = 6723774
83 meter
Y = 491701
62 meter E =
0011647
Z = -4762527
43 I = 51
91559
XDOT = 1941
030429 Wp = 69
62087
YDOT = 6955
120856 meter/sec RA = 57
66410 deg
ZDOT = 2654
386965 TA = 226
32936
MA = 226
42596
Ha = 192
447 n
mi
Hp = 183
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15513341
12 X = 4745751
83
Y = 1613194
30 feet Y = 544674
28 meter
Z = -15625089
99 Z = -4739514
92
XDOT = 6368
210070 XDOT = 1850
218409
YDOT = 22818
637978 feet/sec YDOT = 6976
319139 meter/sec
ZDOT = 8708
618651 ZDOT = 2663
595036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14039473
64 X = 4279231
57
Y = 7000585
58 feet Y = 2133778
49 meter
Z = -15533659
16 Z = -4734659
31
XDOT = -1605
809929 XDOT = -489
450866
YDOT = 22558
504074 feet/sec YDOT = 6875
832042 meter/sec
ZDOT = 8745
386335 ZDOT = 2665
593755
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 10061
51125960
00016717 00000-0 10270-3 0 9015
2 25544 51
6429 58
2564 0007656 1
4164 358
7019 15
73531791 6673
Satellite: ISS
Catalog Number: 25544
Epoch time: 10061
51125960 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 58
2564 deg
Eccentricity:
0007656
Arg of perigee: 1
4164 deg
Mean anomaly: 358
7019 deg
Mean motion: 15
73531791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 667
Checksum: 302
Coasting Arc #3 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2010/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2332309
10 A = 6731175
09 meter
Y = -5914349
41 meter E =
0005876
Z = -2221467
80 I = 51
92386
XDOT = 5378
134334 Wp = 56
28175
YDOT = -58
389770 meter/sec RA = 52
59112 deg
ZDOT = -5498
187991 TA = 148
49198
MA = 148
45678
Ha = 192
422 n
mi
Hp = 183
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7651932
75 X = -2255209
06
Y = -19404033
49 feet Y = -5939999
79 meter
Z = -7288280
20 Z = -2232610
24
XDOT = 17644
797685 XDOT = 5405
096508
YDOT = -191
567487 feet/sec YDOT = 1
901969 meter/sec
ZDOT = -18038
674511 ZDOT = -5471
995759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -653068
40 X = -199055
25
Y = -20832491
86 feet Y = -6349743
52 meter
Z = -7332694
15 Z = -2235005
18
XDOT = 15265
677669 XDOT = 4652
978554
YDOT = 5825
915303 feet/sec YDOT = 1775
738984 meter/sec
ZDOT = -17934
629883 ZDOT = -5466
475188
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 10062
52736845
00016717 00000-0 10270-3 0 9028
2 25544 51
6427 53
0410 0007685 5
9189 354
2064 15
73588001 6837
Satellite: ISS
Catalog Number: 25544
Epoch time: 10062
52736845 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 53
0410 deg
Eccentricity:
0007685
Arg of perigee: 5
9189 deg
Mean anomaly: 354
2064 deg
Mean motion: 15
73588001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 683
Checksum: 299
Coasting Arc #4 (Orbit 698)
---------------------------------------
Vector Time (GMT): 2010/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4622765
03 A = 6723145
27 meter
Y = 586469
81 meter E =
0013329
Z = 4844437
75 I = 51
87765
XDOT = -3375
227148 Wp = 32
24825
YDOT = -6485
003880 meter/sec RA = 47
43836 deg
ZDOT = -2421
625501 TA = 81
38648
MA = 81
23548
Ha = 192
539 n
mi
Hp = 183
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15166551
95 X = -4652512
71
Y = 1924113
54 feet Y = 534609
32 meter
Z = 15893824
65 Z = 4821908
22
XDOT = -11073
579882 XDOT = -3290
696088
YDOT = -21276
259450 feet/sec YDOT = -6522
275208 meter/sec
ZDOT = -7944
965556 ZDOT = -2437
816454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15074898
81 X = -4594829
16
Y = -3051280
41 feet Y = -930030
27 meter
Z = 15804343
93 Z = 4817164
03
XDOT = -3874
343092 XDOT = -1180
899775
YDOT = -22584
868536 feet/sec YDOT = -6883
867930 meter/sec
ZDOT = -8009
437234 ZDOT = -2441
276469
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 10063
54345475
00016717 00000-0 10270-3 0 9037
2 25544 51
6426 47
8262 0007720 8
4016 351
7275 15
73626362 6995
Satellite: ISS
Catalog Number: 25544
Epoch time: 10063
54345475 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 47
8262 deg
Eccentricity:
0007720
Arg of perigee: 8
4016 deg
Mean anomaly: 351
7275 deg
Mean motion: 15
73626362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 699
Checksum: 306
Coasting Arc #5 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2010/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3532049
60 A = 6731250
29 meter
Y = 5352386
33 meter E =
0019308
Z = 2007676
63 I = 51
88495
XDOT = -5132
339303 Wp = 49
52378
YDOT = 1274
583511 meter/sec RA = 42
36090 deg
ZDOT = 5608
456393 TA = 332
79429
MA = 332
89531
Ha = 192
359 n
mi
Hp = 183
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11588089
22 X = 3462182
89
Y = 17560322
62 feet Y = 5391493
26 meter
Z = 6586865
59 Z = 2024665
23
XDOT = -16838
383541 XDOT = -5173
455145
YDOT = 4181
704432 feet/sec YDOT = 1216
961032 meter/sec
ZDOT = 18400
447484 ZDOT = 5583
423741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5682967
98 X = 1732168
64
Y = 20235054
87 feet Y = 6167644
72 meter
Z = 6654469
92 Z = 2028282
43
XDOT = -15941
117789 XDOT = -4858
852702
YDOT = -1565
707860 feet/sec YDOT = -477
227756 meter/sec
ZDOT = 18301
038293 ZDOT = 5578
156472
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 10064
55951801
00016717 00000-0 10270-3 0 9046
2 25544 51
6431 42
6120 0007535 12
5660 347
5689 15
73699408 7154
Satellite: ISS
Catalog Number: 25544
Epoch time: 10064
55951801 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 42
6120 deg
Eccentricity:
0007535
Arg of perigee: 12
5660 deg
Mean anomaly: 347
5689 deg
Mean motion: 15
73699408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 304
Coasting Arc #6 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2010/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4291484
06 A = 6722681
62 meter
Y = -1606658
83 meter E =
0014653
Z = -4929649
84 I = 51
83273
XDOT = 4657
630338 Wp = 73
90195
YDOT = 5710
311234 meter/sec RA = 37
20738 deg
ZDOT = 2202
947617 TA = 217
41220
MA = 217
51430
Ha = 192
624 n
mi
Hp = 183
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14079672
10 X = 4333078
17
Y = -5271190
38 feet Y = -1558436
50 meter
Z = -16173391
87 Z = -4908700
93
XDOT = 15280
939428 XDOT = 4582
729034
YDOT = 18734
616910 feet/sec YDOT = 5761
976899 meter/sec
ZDOT = 7227
518428 ZDOT = 2225
392048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15090813
83 X = 4599680
06
Y = -986773
18 feet Y = -300768
46 meter
Z = -16090209
32 Z = -4904295
80
XDOT = 9155
768645 XDOT = 2790
678283
YDOT = 21216
450616 feet/sec YDOT = 6466
774148 meter/sec
ZDOT = 7316
796017 ZDOT = 2230
159426
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 10065
51205991
00016717 00000-0 10270-3 0 9056
2 25544 51
6432 37
7228 0007778 16
0298 344
1109 15
73668831 7307
Satellite: ISS
Catalog Number: 25544
Epoch time: 10065
51205991 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 37
7228 deg
Eccentricity:
0007778
Arg of perigee: 16
0298 deg
Mean anomaly: 344
1109 deg
Mean motion: 15
73668831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 730
Checksum: 307
Coasting Arc #7 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2010/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4555081
63 A = 6731366
20 meter
Y = -4594287
02 meter E =
0007306
Z = -1869181
02 I = 51
83870
XDOT = 4660
983963 Wp = 74
78334
YDOT = -2325
198273 meter/sec RA = 32
12274 deg
ZDOT = -5659
808935 TA = 125
88825
MA = 125
82040
Ha = 192
580 n
mi
Hp = 182
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14944493
54 X = -4494288
92
Y = -15073120
16 feet Y = -4644884
79 meter
Z = -6132483
67 Z = -1891161
55
XDOT = 15291
942137 XDOT = 4714
132311
YDOT = -7628
603257 feet/sec YDOT = -2272
779351 meter/sec
ZDOT = -18568
926953 ZDOT = -5637
037012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10281691
90 X = -3133859
69
Y = -18540333
22 feet Y = -5651093
56 meter
Z = -6219891
51 Z = -1895822
93
XDOT = 15537
251425 XDOT = 4735
754234
YDOT = -2434
963942 feet/sec YDOT = -742
177009 meter/sec
ZDOT = -18478
514242 ZDOT = -5632
251141
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 10066
52808036
00016717 00000-0 10270-3 0 9068
2 25544 51
6439 32
5073 0007845 19
6032 340
5432 15
73733808 7468
Satellite: ISS
Catalog Number: 25544
Epoch time: 10066
52808036 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 32
5073 deg
Eccentricity:
0007845
Arg of perigee: 19
6032 deg
Mean anomaly: 340
5432 deg
Mean motion: 15
73733808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 746
Checksum: 300
Coasting Arc #8 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2010/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3820438
22 A = 6722243
06 meter
Y = 2438888
26 meter E =
0013374
Z = 4960693
73 I = 51
78189
XDOT = -5717
592434 Wp = 37
33722
YDOT = -4732
289712 meter/sec RA = 26
96789 deg
ZDOT = -2063
445640 TA = 72
66977
MA = 72
52351
Ha = 192
700 n
mi
Hp = 182
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12534246
13 X = -3871524
12
Y = 8001601
91 feet Y = 2395880
34 meter
Z = 16275241
88 Z = 4942010
20
XDOT = -18758
505361 XDOT = -5654
226502
YDOT = -15525
884883 feet/sec YDOT = -4795
872978 meter/sec
ZDOT = -6769
834777 ZDOT = -2091
067219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14245945
06 X = -4342164
05
Y = 4538154
59 feet Y = 1383229
52 meter
Z = 16201069
71 Z = 4938086
05
XDOT = -13839
039231 XDOT = -4218
139158
YDOT = -18725
979267 feet/sec YDOT = -5707
678481 meter/sec
ZDOT = -6879
652459 ZDOT = -2096
918069
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 10067
54407799
00016717 00000-0 10270-3 0 9073
2 25544 51
6439 27
2925 0007790 23
0807 337
0704 15
73759680 7620
Satellite: ISS
Catalog Number: 25544
Epoch time: 10067
54407799 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 27
2925 deg
Eccentricity:
0007790
Arg of perigee: 23
0807 deg
Mean anomaly: 337
0704 deg
Mean motion: 15
73759680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 327
Coasting Arc #9 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2010/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5380419
71 A = 6731364
11 meter
Y = 3632346
90 meter E =
0020726
Z = 1734846
08 I = 51
78609
XDOT = -4035
638617 Wp = 51
49473
YDOT = 3230
947055 meter/sec RA = 21
87762 deg
ZDOT = 5718
216087 TA = 327
68872
MA = 327
81550
Ha = 192
547 n
mi
Hp = 182
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17652295
62 X = 5330974
87
Y = 11917148
63 feet Y = 3692237
55 meter
Z = 5691752
24 Z = 1760863
43
XDOT = -13240
284178 XDOT = -4099
245222
YDOT = 10600
219997 feet/sec YDOT = 3185
462692 meter/sec
ZDOT = 18760
551467 ZDOT = 5698
456737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14294138
14 X = 4356853
31
Y = 15751557
63 feet Y = 4801074
76 meter
Z = 5795175
83 Z = 1766369
59
XDOT = -14332
859333 XDOT = -4368
655525
YDOT = 6094
197426 feet/sec YDOT = 1857
511375 meter/sec
ZDOT = 18682
119443 ZDOT = 5694
310006
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 10068
56005116
00016717 00000-0 10270-3 0 9084
2 25544 51
6442 22
0771 0007716 27
0395 333
1169 15
73811868 7786
Satellite: ISS
Catalog Number: 25544
Epoch time: 10068
56005116 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 22
0771 deg
Eccentricity:
0007716
Arg of perigee: 27
0395 deg
Mean anomaly: 333
1169 deg
Mean motion: 15
73811868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 304
Coasting Arc #10 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2010/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3206798
38 A = 6721886
45 meter
Y = -3159741
62 meter E =
0016809
Z = -5004645
52 I = 51
72615
XDOT = 6530
860483 Wp = 77
74811
YDOT = 3563
317257 meter/sec RA = 16
71971 deg
ZDOT = 1943
963938 TA = 210
98759
MA = 211
08687
Ha = 192
651 n
mi
Hp = 182
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10520992
04 X = 3266203
97
Y = -10366606
37 feet Y = -3123549
38 meter
Z = -16419440
67 Z = -4988922
79
XDOT = 21426
707622 XDOT = 6481
086228
YDOT = 11690
673416 feet/sec YDOT = 3636
071008 meter/sec
ZDOT = 6377
834443 ZDOT = 1975
569097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12639027
63 X = 3852375
62
Y = -7775471
31 feet Y = -2369963
66 meter
Z = -16357043
12 Z = -4985626
74
XDOT = 17723
650873 XDOT = 5402
168786
YDOT = 15190
756496 feet/sec YDOT = 4630
142580 meter/sec
ZDOT = 6503
454454 ZDOT = 1982
252918
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 10069
51250542
00016717 00000-0 10270-3 0 9096
2 25544 51
6446 17
1875 0007786 29
8603 330
3003 15
73827429 7932
Satellite: ISS
Catalog Number: 25544
Epoch time: 10069
51250542 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 17
1875 deg
Eccentricity:
0007786
Arg of perigee: 29
8603 deg
Mean anomaly: 330
3003 deg
Mean motion: 15
73827429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 312
Coasting Arc #11 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2010/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5980554
05 A = 6731226
54 meter
Y = -2591540
19 meter E =
0009000
Z = -1690236
19 I = 51
72988
XDOT = 3312
994409 Wp = 86
57035
YDOT = -3928
828328 meter/sec RA = 11
62347 deg
ZDOT = -5724
076672 TA = 112
07619
MA = 111
98059
Ha = 192
620 n
mi
Hp = 182
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19621240
31 X = -5942919
82
Y = -8502428
45 feet Y = -2658207
99 meter
Z = -5545394
34 Z = -1719197
49
XDOT = 10869
404228 XDOT = 3384
486947
YDOT = -12889
856719 feet/sec YDOT = -3891
381091 meter/sec
ZDOT = -18779
779107 ZDOT = -5707
808602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17450399
64 X = -5318881
81
Y = -12307645
56 feet Y = -3751370
37 meter
Z = -5660492
23 Z = -1725318
03
XDOT = 12473
682264 XDOT = 3801
978354
YDOT = -9116
161744 feet/sec YDOT = -2778
606100 meter/sec
ZDOT = -18715
232083 ZDOT = -5704
402739
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 10070
52843295
00016717 00000-0 10270-3 0 9104
2 25544 51
6454 11
9717 0007802 33
6437 326
5220 15
73876724 8093
Satellite: ISS
Catalog Number: 25544
Epoch time: 10070
52843295 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 11
9717 deg
Eccentricity:
0007802
Arg of perigee: 33
6437 deg
Mean anomaly: 326
5220 deg
Mean motion: 15
73876724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 301
Coasting Arc #12 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2010/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2561014
34 A = 6721614
37 meter
Y = 3686621
30 meter E =
0013408
Z = 4997656
47 I = 51
66805
XDOT = -7094
344717 Wp = 44
66033
YDOT = -2322
933548 meter/sec RA = 6
46230 deg
ZDOT = -1909
434208 TA = 63
82420
MA = 63
68638
Ha = 192
708 n
mi
Hp = 181
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8402278
02 X = -2626325
65
Y = 12095214
23 feet Y = 3657617
75 meter
Z = 16396510
74 Z = 4985056
39
XDOT = -23275
409175 XDOT = -7058
566506
YDOT = -7621
173058 feet/sec YDOT = -2402
066837 meter/sec
ZDOT = -6264
547927 ZDOT = -1943
810693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10604732
59 X = -3232322
49
Y = 10298958
75 feet Y = 3139122
63 meter
Z = 16346533
06 Z = 4982423
28
XDOT = -20658
692985 XDOT = -6296
769622
YDOT = -11047
068578 feet/sec YDOT = -3367
146502 meter/sec
ZDOT = -6401
149409 ZDOT = -1951
070340
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 10071
54433647
00016717 00000-0 10270-3 0 9114
2 25544 51
6456 6
7565 0007773 37
4052 322
7651 15
73910276 8255
Satellite: ISS
Catalog Number: 25544
Epoch time: 10071
54433647 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 6
7565 deg
Eccentricity:
0007773
Arg of perigee: 37
4052 deg
Mean anomaly: 322
7651 deg
Mean motion: 15
73910276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 825
Checksum: 303
Coasting Arc #13 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2010/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6351248
04 A = 6731128
80 meter
Y = 1451948
73 meter E =
0021465
Z = 1645235
04 I = 51
67055
XDOT = -2522
560453 Wp = 55
46503
YDOT = 4481
244430 meter/sec RA = 1
36086 deg
ZDOT = 5742
427148 TA = 322
72167
MA = 322
87046
Ha = 192
604 n
mi
Hp = 181
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20837427
97 X = 6326547
96
Y = 4763611
33 feet Y = 1522834
22 meter
Z = 5397752
77 Z = 1676028
67
XDOT = -8276
116972 XDOT = -2600
378186
YDOT = 14702
245506 feet/sec YDOT = 4452
601118 meter/sec
ZDOT = 18839
984080 ZDOT = 5729
983333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19696650
85 X = 6003539
18
Y = 8221713
39 feet Y = 2505978
24 meter
Z = 5520100
23 Z = 1682526
55
XDOT = -10158
256052 XDOT = -3096
236445
YDOT = 11631
849664 feet/sec YDOT = 3545
387777 meter/sec
ZDOT = 18790
647356 ZDOT = 5727
389314
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 10072
56021579
00016717 00000-0 10270-3 0 9125
2 25544 51
6458 1
5404 0007770 40
9427 319
2318 15
73938887 8411
Satellite: ISS
Catalog Number: 25544
Epoch time: 10072
56021579 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 1
5404 deg
Eccentricity:
0007770
Arg of perigee: 40
9427 deg
Mean anomaly: 319
2318 deg
Mean motion: 15
73938887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 841
Checksum: 310
Coasting Arc #14 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2010/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1847518
61 A = 6721399
84 meter
Y = -4100894
24 meter E =
0018228
Z = -5009465
60 I = 51
60853
XDOT = 7380
582185 Wp = 82
38782
YDOT = 1016
427451 meter/sec RA = 356
19467 deg
ZDOT = 1898
171000 TA = 205
92725
MA = 206
01869
Ha = 192
627 n
mi
Hp = 181
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6061412
77 X = 1917572
93
Y = -13454377
44 feet Y = -4079843
05 meter
Z = -16435254
59 Z = -5000319
88
XDOT = 24214
508482 XDOT = 7359
446942
YDOT = 3334
735732 feet/sec YDOT = 1098
843544 meter/sec
ZDOT = 6227
595144 ZDOT = 1933
973855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8138325
90 X = 2480561
74
Y = -12357935
29 feet Y = -3766698
68 meter
Z = -16399014
52 Z = -4998419
63
XDOT = 22484
644616 XDOT = 6853
319679
YDOT = 6390
493190 feet/sec YDOT = 1947
822324 meter/sec
ZDOT = 6369
824128 ZDOT = 1941
522394
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 10073
51257978
00016717 00000-0 10270-3 0 9136
2 25544 51
6465 356
6504 0007749 44
3176 315
8607 15
73980206 8560
Satellite: ISS
Catalog Number: 25544
Epoch time: 10073
51257978 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 356
6504 deg
Eccentricity:
0007749
Arg of perigee: 44
3176 deg
Mean anomaly: 315
8607 deg
Mean motion: 15
73980206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 330
Coasting Arc #15 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2010/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6505494
60 A = 6730816
00 meter
Y = -342885
79 meter E =
0010422
Z = -1699486
42 I = 51
61137
XDOT = 1739
653500 Wp = 94
38320
YDOT = -4852
649414 meter/sec RA = 351
08901 deg
ZDOT = -5710
961163 TA = 104
40374
MA = 104
28805
Ha = 192
584 n
mi
Hp = 181
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21343486
21 X = -6492921
18
Y = -1124953
38 feet Y = -415564
00 meter
Z = -5575742
83 Z = -1731059
17
XDOT = 5707
524607 XDOT = 1821
529910
YDOT = -15920
765795 feet/sec YDOT = -4832
738449 meter/sec
ZDOT = -18736
749222 ZDOT = -5702
310576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20961256
44 X = -6388990
96
Y = -4002682
37 feet Y = -1220017
59 meter
Z = -5701148
48 Z = -1737710
06
XDOT = 7629
714815 XDOT = 2325
537076
YDOT = -13457
387736 feet/sec YDOT = -4101
811782 meter/sec
ZDOT = -18702
495154 ZDOT = -5700
520523
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 10074
52841137
00016717 00000-0 10270-3 0 9145
2 25544 51
6470 351
4342 0007682 48
2954 311
8865 15
74014310 8727
Satellite: ISS
Catalog Number: 25544
Epoch time: 10074
52841137 = yrday
fracday
Element set: 914
Inclination: 51
6470 deg
RA of node: 351
4342 deg
Eccentricity:
0007682
Arg of perigee: 48
2954 deg
Mean anomaly: 311
8865 deg
Mean motion: 15
74014310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 296
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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