Date:
December 11th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 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
356/16:56:17
307 5
1 7
1 7
2
N/A -4
4 -0
6 193
2
000/00:18:34
615 -2
6 0
4 187
4
Coasting Arc #1 (Orbit 1120)
---------------------------------------
Vector Time (GMT): 2010/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4832503
32 A = 6734586
92 meter
Y = -4657451
34 meter E =
0005973
Z = 539973
69 I = 51
91836
XDOT = 2951
996021 Wp = 103
69199
YDOT = -3767
733175 meter/sec RA = 47
55772 deg
ZDOT = -6025
005552 TA = 70
46041
MA = 70
39592
Ha = 192
060 n
mi
Hp = 186
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15854669
69 X = -4782686
76
Y = -15280352
16 feet Y = -4711212
81 meter
Z = 1771567
22 Z = 516617
96
XDOT = 9685
026314 XDOT = 3023
176472
YDOT = -12361
329315 feet/sec YDOT = -3734
323601 meter/sec
ZDOT = -19767
078584 ZDOT = -6010
492238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18174231
14 X = 5539505
65
Y = -12445103
45 feet Y = -3793267
53 meter
Z = 1677762
27 Z = 511381
94
XDOT = 9215
552178 XDOT = 2808
900304
YDOT = 10775
756736 feet/sec YDOT = 3284
450653 meter/sec
ZDOT = -19708
575476 ZDOT = -6007
173805
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 10344
53276563
00016717 00000-0 10270-3 0 9006
2 25544 51
6454 47
9952 0008167 328
2358 31
8312 15
73112134 11217
Satellite: ISS
Catalog Number: 25544
Epoch time: 10344
53276563 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 47
9952 deg
Eccentricity:
0008167
Arg of perigee: 328
2358 deg
Mean anomaly: 31
8312 deg
Mean motion: 15
73112134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1121
Checksum: 287
Coasting Arc #2 (Orbit 1136)
---------------------------------------
Vector Time (GMT): 2010/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2010196
99 A = 6722766
00 meter
Y = 3722315
52 meter E =
0005544
Z = 5225033
46 I = 51
85768
XDOT = -6106
657950 Wp = 348
96540
YDOT = -4596
827599 meter/sec RA = 42
45904 deg
ZDOT = 930
890444 TA = 92
22387
MA = 92
16039
Ha = 192
209 n
mi
Hp = 185
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6595134
48 X = -2077053
48
Y = 12212321
25 feet Y = 3699462
05 meter
Z = 17142498
22 Z = 5215105
83
XDOT = -20034
967028 XDOT = -6059
323599
YDOT = -15081
455378 feet/sec YDOT = -4664
851339 meter/sec
ZDOT = 3054
102508 ZDOT = 901
338906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10759120
78 X = -3279380
01
Y = -8845882
91 feet Y = -2696225
11 meter
Z = 17102441
65 Z = 5212824
21
XDOT = 17893
589405 XDOT = 5453
966051
YDOT = -16123
421725 feet/sec YDOT = -4914
418942 meter/sec
ZDOT = 2935
373825 ZDOT = 894
701942
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 10345
54916621
00016717 00000-0 10270-3 0 9015
2 25544 51
6455 42
7824 0008202 331
6060 28
4655 15
73154525 11376
Satellite: ISS
Catalog Number: 25544
Epoch time: 10345
54916621 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 42
7824 deg
Eccentricity:
0008202
Arg of perigee: 331
6060 deg
Mean anomaly: 28
4655 deg
Mean motion: 15
73154525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1137
Checksum: 285
Coasting Arc #3 (Orbit 1151)
---------------------------------------
Vector Time (GMT): 2010/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5748686
65 A = 6734157
85 meter
Y = 3316847
33 meter E =
0015587
Z = -1080912
97 I = 51
87208
XDOT = -1575
479483 Wp = 9
52545
YDOT = 4655
430920 meter/sec RA = 37
32804 deg
ZDOT = 5933
623088 TA = 338
68334
MA = 338
74820
Ha = 192
472 n
mi
Hp = 185
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18860520
51 X = 5716420
68
Y = 10882045
06 feet Y = 3380952
28 meter
Z = -3546302
41 Z = -1053063
94
XDOT = -5168
895943 XDOT = -1656
244816
YDOT = 15273
723490 feet/sec YDOT = 4637
360970 meter/sec
ZDOT = 19467
267349 ZDOT = 5925
773532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13908264
51 X = -4239239
02
Y = 16777353
24 feet Y = 5113737
27 meter
Z = -3434384
42 Z = -1046800
37
XDOT = -12941
993985 XDOT = -3944
719767
YDOT = -6769
071591 feet/sec YDOT = -2063
213021 meter/sec
ZDOT = 19435
537756 ZDOT = 5923
951908
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 10346
50202075
00016717 00000-0 10270-3 0 9024
2 25544 51
6451 37
8956 0008401 336
7805 23
2977 15
73137302 11528
Satellite: ISS
Catalog Number: 25544
Epoch time: 10346
50202075 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 37
8956 deg
Eccentricity:
0008401
Arg of perigee: 336
7805 deg
Mean anomaly: 23
2977 deg
Mean motion: 15
73137302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1152
Checksum: 286
Coasting Arc #4 (Orbit 1167)
---------------------------------------
Vector Time (GMT): 2010/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 724577
69 A = 6723105
80 meter
Y = -4307060
71 meter E =
0015158
Z = -5122839
52 I = 51
81107
XDOT = 6931
476619 Wp = 45
86156
YDOT = 2968
664475 meter/sec RA = 32
23545 deg
ZDOT = -1507
944475 TA = 209
64773
MA = 209
73374
Ha = 192
422 n
mi
Hp = 185
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2377223
38 X = 797572
14
Y = -14130776
61 feet Y = -4298549
59 meter
Z = -16807216
28 Z = -5119142
48
XDOT = 22741
065022 XDOT = 6905
090650
YDOT = 9739
712846 feet/sec YDOT = 3046
028985 meter/sec
ZDOT = -4947
324393 ZDOT = -1474
335094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13592814
18 X = 4143089
76
Y = 4590205
77 feet Y = 1399094
72 meter
Z = -16792199
72 Z = -5118262
48
XDOT = -12743
033663 XDOT = -3884
076661
YDOT = 20039
935165 feet/sec YDOT = 6108
172238 meter/sec
ZDOT = -4812
228307 ZDOT = -1466
767188
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 10347
51837446
00016717 00000-0 10270-3 0 9033
2 25544 51
6456 32
6826 0008243 340
8963 19
1890 15
73198068 11688
Satellite: ISS
Catalog Number: 25544
Epoch time: 10347
51837446 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 32
6826 deg
Eccentricity:
0008243
Arg of perigee: 340
8963 deg
Mean anomaly: 19
1890 deg
Mean motion: 15
73198068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1168
Checksum: 325
Coasting Arc #5 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2010/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6285620
43 A = 6733253
45 meter
Y = -1859236
81 meter E =
0010407
Z = 1535335
39 I = 51
81966
XDOT = 78
109200 Wp = 81
40038
YDOT = -5071
600490 meter/sec RA = 27
09174 deg
ZDOT = -5787
005048 TA = 81
73426
MA = 81
61626
Ha = 192
516 n
mi
Hp = 184
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20622114
26 X = -6271821
37
Y = -6099858
29 feet Y = -1929449
35 meter
Z = 5037189
59 Z = 1504832
99
XDOT = 256
263780 XDOT = 162
927432
YDOT = -16639
109219 feet/sec YDOT = -5070
252407 meter/sec
ZDOT = -18986
237033 ZDOT = -5786
419893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8822316
32 X = 2689042
01
Y = -19643497
33 feet Y = -5987337
99 meter
Z = 4914559
39 Z = 1497957
70
XDOT = 15006
519530 XDOT = 4573
987153
YDOT = 1961
029059 feet/sec YDOT = 597
721657 meter/sec
ZDOT = -18983
708134 ZDOT = -5786
234239
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 10348
53470201
00016717 00000-0 10270-3 0 9049
2 25544 51
6458 27
4696 0008393 345
7714 14
3212 15
73279119 11841
Satellite: ISS
Catalog Number: 25544
Epoch time: 10348
53470201 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 27
4696 deg
Eccentricity:
0008393
Arg of perigee: 345
7714 deg
Mean anomaly: 14
3212 deg
Mean motion: 15
73279119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1184
Checksum: 304
Coasting Arc #6 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2010/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 592290
53 A = 6723360
48 meter
Y = 4472691
19 meter E =
0005970
Z = 4980391
50 I = 51
75854
XDOT = -7330
771712 Wp = 34
36989
YDOT = -1257
878372 meter/sec RA = 22
00285 deg
ZDOT = 2005
130426 TA = 36
29614
MA = 36
25566
Ha = 192
629 n
mi
Hp = 184
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1943210
40 X = 518037
93
Y = 14674183
69 feet Y = 4478899
01 meter
Z = 16339867
11 Z = 4983088
84
XDOT = -24051
088293 XDOT = -7325
901704
YDOT = -4126
897546 feet/sec YDOT = -1339
828391 meter/sec
ZDOT = 6578
511897 ZDOT = 1969
528882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14790073
36 X = -4508014
36
Y = 109454
91 feet Y = 33361
86 meter
Z = 16350557
80 Z = 4983650
02
XDOT = 6935
558312 XDOT = 2113
958174
YDOT = -22359
874606 feet/sec YDOT = -6815
289780 meter/sec
ZDOT = 6435
355183 ZDOT = 1961
496260
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 10349
55100607
00016717 00000-0 10270-3 0 9053
2 25544 51
6453 22
2566 0008307 350
5454 9
5551 15
73297981 12003
Satellite: ISS
Catalog Number: 25544
Epoch time: 10349
55100607 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 22
2566 deg
Eccentricity:
0008307
Arg of perigee: 350
5454 deg
Mean anomaly: 9
5551 deg
Mean motion: 15
73297981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 290
Coasting Arc #7 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2010/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6424247
36 A = 6732402
07 meter
Y = 331963
52 meter E =
0014160
Z = -1959687
13 I = 51
76163
XDOT = 1446
049831 Wp = 14
32635
YDOT = 5065
590341 meter/sec RA = 16
84799 deg
ZDOT = 5620
564259 TA = 323
89499
MA = 323
99052
Ha = 192
721 n
mi
Hp = 184
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21076927
03 X = 6429577
74
Y = 1089119
15 feet Y = 403833
29 meter
Z = -6429419
72 Z = -1928464
75
XDOT = 4744
257975 XDOT = 1361
993940
YDOT = 16619
390883 feet/sec YDOT = 5081
290471 meter/sec
ZDOT = 18440
171453 ZDOT = 5627
385526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3202381
58 X = -976085
91
Y = 20898964
73 feet Y = 6370004
45 meter
Z = -6303847
78 Z = -1921412
80
XDOT = -15477
344392 XDOT = -4717
494571
YDOT = 3176
555996 feet/sec YDOT = 968
214267 meter/sec
ZDOT = 18467
422474 ZDOT = 5628
870370
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 10350
50376848
00016717 00000-0 10270-3 0 9063
2 25544 51
6463 17
3696 0008298 354
4048 5
7021 15
73355938 12157
Satellite: ISS
Catalog Number: 25544
Epoch time: 10350
50376848 = yrday
fracday
Element set: 906
Inclination: 51
6463 deg
RA of node: 17
3696 deg
Eccentricity:
0008298
Arg of perigee: 354
4048 deg
Mean anomaly: 5
7021 deg
Mean motion: 15
73355938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1215
Checksum: 314
Coasting Arc #8 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2010/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1889182
43 A = 6723824
32 meter
Y = -4291641
54 meter E =
0016383
Z = -4833086
93 I = 51
70342
XDOT = 7277
349566 Wp = 42
83180
YDOT = -450
798772 meter/sec RA = 11
76099 deg
ZDOT = -2437
359294 TA = 203
30462
MA = 203
37897
Ha = 192
758 n
mi
Hp = 184
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6198105
09 X = -1817573
50
Y = -14080188
78 feet Y = -4312366
61 meter
Z = -15856584
43 Z = -4842091
23
XDOT = 23875
818787 XDOT = 7293
690020
YDOT = -1478
998597 feet/sec YDOT = -369
327444 meter/sec
ZDOT = -7996
585609 ZDOT = -2401
965801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14539966
59 X = 4431781
82
Y = -4910487
16 feet Y = -1496716
49 meter
Z = -15892639
18 Z = -4844076
42
XDOT = -874
940875 XDOT = -266
681979
YDOT = 22902
863047 feet/sec YDOT = 6980
792657 meter/sec
ZDOT = -7854
208789 ZDOT = -2393
962839
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 10351
52002382
00016717 00000-0 10270-3 0 9076
2 25544 51
6463 12
1562 0008351 358
2507 1
8625 15
73363342 12317
Satellite: ISS
Catalog Number: 25544
Epoch time: 10351
52002382 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 12
1562 deg
Eccentricity:
0008351
Arg of perigee: 358
2507 deg
Mean anomaly: 1
8625 deg
Mean motion: 15
73363342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 267
Coasting Arc #9 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2010/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6233881
30 A = 6731632
03 meter
Y = 1097429
14 meter E =
0014336
Z = 2286875
92 I = 51
69852
XDOT = -2826
746107 Wp = 72
86813
YDOT = -4652
538284 meter/sec RA = 6
59528 deg
ZDOT = -5440
761217 TA = 81
47437
MA = 81
31194
Ha = 192
877 n
mi
Hp = 183
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20452366
47 X = -6256799
01
Y = 3600489
32 feet Y = 1027589
70 meter
Z = 7502873
74 Z = 2256535
81
XDOT = -9274
101400 XDOT = -2748
079902
YDOT = -15264
233216 feet/sec YDOT = -4683
708109 meter/sec
ZDOT = -17850
266461 ZDOT = -5454
303243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2238638
16 X = -682336
91
Y = -20689810
80 feet Y = -6306254
33 meter
Z = 7380796
71 Z = 2249666
84
XDOT = 14328
619505 XDOT = 4367
363225
YDOT = -7975
751330 feet/sec YDOT = -2431
009005 meter/sec
ZDOT = -17904
554268 ZDOT = -5457
308141
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 10352
53625394
00016717 00000-0 10270-3 0 9083
2 25544 51
6449 6
9423 0008481 2
9115 357
2095 15
73420002 12473
Satellite: ISS
Catalog Number: 25544
Epoch time: 10352
53625394 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 6
9423 deg
Eccentricity:
0008481
Arg of perigee: 2
9115 deg
Mean anomaly: 357
2095 deg
Mean motion: 15
73420002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 290
Coasting Arc #10 (Orbit 1262)
---------------------------------------
Vector Time (GMT): 2010/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3017490
51 A = 6724221
49 meter
Y = 3774128
23 meter E =
0009282
Z = 4667136
31 I = 51
64290
XDOT = -6883
193687 Wp = 58
41530
YDOT = 2037
865616 meter/sec RA = 1
50746 deg
ZDOT = 2803
028284 TA = 3
95282
MA = 3
94549
Ha = 192
891 n
mi
Hp = 183
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9899903
24 X = 2952390
92
Y = 12382310
46 feet Y = 3807506
93 meter
Z = 15312126
99 Z = 4681637
85
XDOT = -22582
656454 XDOT = -6919
086632
YDOT = 6685
910813 feet/sec YDOT = 1960
692494 meter/sec
ZDOT = 9196
287020 ZDOT = 2769
502534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12847764
11 X = -3915998
50
Y = 9191276
99 feet Y = 2801501
23 meter
Z = 15370306
24 Z = 4684869
34
XDOT = -4901
099390 XDOT = -1493
855094
YDOT = -22000
028747 feet/sec YDOT = -6705
608762 meter/sec
ZDOT = 9061
355788 ZDOT = 2761
901244
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 10353
55245958
00016717 00000-0 10270-3 0 9091
2 25544 51
6442 1
7280 0008494 6
8518 353
2760 15
73434558 12638
Satellite: ISS
Catalog Number: 25544
Epoch time: 10353
55245958 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 1
7280 deg
Eccentricity:
0008494
Arg of perigee: 6
8518 deg
Mean anomaly: 353
2760 deg
Mean motion: 15
73434558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1263
Checksum: 313
Coasting Arc #11 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2010/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5709824
82 A = 6730749
34 meter
Y = -2426263
30 meter E =
0012843
Z = -2597537
33 I = 51
63522
XDOT = 4044
689882 Wp = 25
42268
YDOT = 3911
649941 meter/sec RA = 356
33373 deg
ZDOT = 5258
128346 TA = 305
06814
MA = 305
18853
Ha = 193
021 n
mi
Hp = 183
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18733021
05 X = 5749149
80
Y = -7960181
43 feet Y = -2362192
31 meter
Z = -8522104
10 Z = -2569703
74
XDOT = 13269
979927 XDOT = 3975
105322
YDOT = 12833
497182 feet/sec YDOT = 3956
490181 meter/sec
ZDOT = 17251
077251 ZDOT = 5277
609150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7360867
08 X = 2243592
29
Y = 19026443
41 feet Y = 5799259
95 meter
Z = -8410048
23 Z = -2563382
70
XDOT = -11857
876659 XDOT = -3614
280806
YDOT = 12216
613285 feet/sec YDOT = 3723
623729 meter/sec
ZDOT = 17329
279458 ZDOT = 5281
964379
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 10354
50512836
00016717 00000-0 10270-3 0 9101
2 25544 51
6448 356
8407 0008497 10
6794 349
4548 15
73495627 12782
Satellite: ISS
Catalog Number: 25544
Epoch time: 10354
50512836 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 356
8407 deg
Eccentricity:
0008497
Arg of perigee: 10
6794 deg
Mean anomaly: 349
4548 deg
Mean motion: 15
73495627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1278
Checksum: 337
Coasting Arc #12 (Orbit 1293)
---------------------------------------
Vector Time (GMT): 2010/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3971787
90 A = 6724603
23 meter
Y = -3019098
98 meter E =
0016519
Z = -4524891
16 I = 51
58337
XDOT = 6141
892518 Wp = 44
02899
YDOT = -3431
039187 meter/sec RA = 351
24404 deg
ZDOT = -3096
974992 TA = 195
00117
MA = 195
05022
Ha = 193
017 n
mi
Hp = 183
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13030800
19 X = -3915751
50
Y = -9905180
39 feet Y = -3063199
86 meter
Z = -14845443
45 Z = -4544050
47
XDOT = 20150
566004 XDOT = 6194
847083
YDOT = -11256
690245 feet/sec YDOT = -3362
060263 meter/sec
ZDOT = -10160
679106 ZDOT = -3067
009636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10092601
59 X = 3076224
96
Y = -12796998
59 feet Y = -3900525
17 meter
Z = -14922391
36 Z = -4548344
89
XDOT = 10029
399347 XDOT = 3056
960921
YDOT = 19636
030274 feet/sec YDOT = 5985
062028 meter/sec
ZDOT = -10040
003074 ZDOT = -3060
192937
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 10355
52128439
00016717 00000-0 10270-3 0 9117
2 25544 51
6436 351
6255 0008524 14
0050 346
1348 15
73512818 12949
Satellite: ISS
Catalog Number: 25544
Epoch time: 10355
52128439 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 351
6255 deg
Eccentricity:
0008524
Arg of perigee: 14
0050 deg
Mean anomaly: 346
1348 deg
Mean motion: 15
73512818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1294
Checksum: 290
Coasting Arc #13 (Orbit 1309)
---------------------------------------
Vector Time (GMT): 2010/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4988880
35 A = 6730005
92 meter
Y = 3533790
53 meter E =
0016934
Z = 2808180
55 I = 51
57178
XDOT = -4965
967235 Wp = 69
17907
YDOT = -2935
082986 meter/sec RA = 346
06124 deg
ZDOT = -5098
209764 TA = 78
62484
MA = 78
43465
Ha = 193
061 n
mi
Hp = 182
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16367717
69 X = -5041666
62
Y = 11593800
95 feet Y = 3477706
30 meter
Z = 9213190
76 Z = 2783817
03
XDOT = -16292
543422 XDOT = -4908
011489
YDOT = -9629
537355 feet/sec YDOT = -2990
290610 meter/sec
ZDOT = -16726
409986 ZDOT = -5122
193944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11638265
25 X = -3547343
25
Y = -16391097
36 feet Y = -4996006
47 meter
Z = 9115042
32 Z = 2778264
90
XDOT = 8391
426165 XDOT = 2557
706695
YDOT = -15369
755104 feet/sec YDOT = -4684
701356 meter/sec
ZDOT = -16822
774640 ZDOT = -5127
581710
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 10356
53741379
00016717 00000-0 10270-3 0 9124
2 25544 51
6434 346
4105 0008665 17
0647 343
0806 15
73585901 13101
Satellite: ISS
Catalog Number: 25544
Epoch time: 10356
53741379 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 346
4105 deg
Eccentricity:
0008665
Arg of perigee: 17
0647 deg
Mean anomaly: 343
0806 deg
Mean motion: 15
73585901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1310
Checksum: 299
Coasting Arc #14 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2010/356/17:05:34
615
Vector Time (MET): N/A
Weight (LBS) : 812550
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1032042
45 A = 6725698
53 meter
Y = -4059685
84 meter E =
0013471
Z = -5272821
83 I = 51
53816
XDOT = 7436
822745 Wp = 69
41458
YDOT = -1951
288353 meter/sec RA = 344
99313 deg
ZDOT = 51
506080 TA = 201
04785
MA = 201
10334
Ha = 193
230 n
mi
Hp = 187
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3385966
03 X = -960955
36
Y = -13319179
28 feet Y = -4070828
53 meter
Z = -17299284
21 Z = -5277663
38
XDOT = 24399
024754 XDOT = 7457
839488
YDOT = -6401
864674 feet/sec YDOT = -1868
007821 meter/sec
ZDOT = 168
983201 ZDOT = 87
684663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -144290
39 X = -43979
71
Y = -13717719
60 feet Y = -4181160
93 meter
Z = -17318599
42 Z = -5278709
10
XDOT = 24215
016073 XDOT = 7380
736899
YDOT = -632
205502 feet/sec YDOT = -192
696237 meter/sec
ZDOT = 314
598054 ZDOT = 95
889487
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 10356
72794815
00016717 00000-0 10270-3 0 9139
2 25544 51
6453 345
4324 0005393 333
7381 26
3507 15
72039030 13130
Satellite: ISS
Catalog Number: 25544
Epoch time: 10356
72794815 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 345
4324 deg
Eccentricity:
0005393
Arg of perigee: 333
7381 deg
Mean anomaly: 26
3507 deg
Mean motion: 15
72039030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1313
Checksum: 293
Coasting Arc #15 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2010/357/17:05:34
615
Vector Time (MET): N/A
Weight (LBS) : 812550
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6130555
23 A = 6737603
15 meter
Y = 2729345
01 meter E =
0008802
Z = 568903
86 I = 51
54951
XDOT = -2422
495894 Wp = 112
66543
YDOT = -4178
025192 meter/sec RA = 339
86095 deg
ZDOT = -5990
540232 TA = 61
14238
MA = 61
05408
Ha = 193
323 n
mi
Hp = 187
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20113370
17 X = -6163383
24
Y = 8954543
98 feet Y = 2660605
82 meter
Z = 1866482
47 Z = 539042
54
XDOT = -7947
821173 XDOT = -2346
495748
YDOT = -13707
431731 feet/sec YDOT = -4204
689318 meter/sec
ZDOT = -19654
003387 ZDOT = -6002
124505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21566449
08 X = -6573453
68
Y = 4478187
43 feet Y = 1364951
53 meter
Z = 1746249
03 Z = 532256
70
XDOT = -4415
303343 XDOT = -1345
784459
YDOT = -13485
527271 feet/sec YDOT = -4110
388712 meter/sec
ZDOT = -19700
443316 ZDOT = -6004
695123
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 10357
74504266
00016717 00000-0 10270-3 0 9142
2 25544 51
6456 340
2245 0005319 337
2885 22
8041 15
72051230 13291
Satellite: ISS
Catalog Number: 25544
Epoch time: 10357
74504266 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 340
2245 deg
Eccentricity:
0005319
Arg of perigee: 337
2885 deg
Mean anomaly: 22
8041 deg
Mean motion: 15
72051230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1329
Checksum: 287
Coasting Arc #16 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2010/358/17:05:34
615
Vector Time (MET): N/A
Weight (LBS) : 812550
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3099436
12 A = 6726007
35 meter
Y = 3051269
91 meter E =
0003106
Z = 5128585
33 I = 51
48321
XDOT = -6330
721535 Wp = 32
55696
YDOT = 4171
039809 meter/sec RA = 334
74787 deg
ZDOT = 1346
565885 TA = 44
54022
MA = 44
51525
Ha = 193
249 n
mi
Hp = 187
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10168753
68 X = 3040172
45
Y = 10010728
05 feet Y = 3085597
80 meter
Z = 16826067
34 Z = 5143498
56
XDOT = -20770
083776 XDOT = -6383
433664
YDOT = 13684
513810 feet/sec YDOT = 4099
951006 meter/sec
ZDOT = 4417
867077 ZDOT = 1315
683978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7917321
31 X = 2413199
54
Y = 11786245
54 feet Y = 3592447
64 meter
Z = 16885947
09 Z = 5146836
67
XDOT = -22210
232242 XDOT = -6769
678787
YDOT = 8778
669039 feet/sec YDOT = 2675
738323 meter/sec
ZDOT = 4293
475825 ZDOT = 1308
651432
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 10358
76211180
00016717 00000-0 10270-3 0 9156
2 25544 51
6457 335
0165 0005370 340
7054 19
3904 15
72124620 13450
Satellite: ISS
Catalog Number: 25544
Epoch time: 10358
76211180 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 335
0165 deg
Eccentricity:
0005370
Arg of perigee: 340
7054 deg
Mean anomaly: 19
3904 deg
Mean motion: 15
72124620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 280
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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