Date:
January 29th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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
040/21:38:57
748 0
4 1
9 1
9
N/A 1
7 0
1 191
5
000/00:04:55
496 -0
7 -0
0 188
4
Coasting Arc #1 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2011/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6380428
46 A = 6736561
88 meter
Y = -1671771
05 meter E =
0009406
Z = -1341371
57 I = 51
79659
XDOT = 83
162364 Wp = 169
60722
YDOT = 5001
015448 meter/sec RA = 156
10765 deg
ZDOT = -5852
656746 TA = 25
08373
MA = 25
03806
Ha = 191
922 n
mi
Hp = 187
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20933164
25 X = 6405164
34
Y = -5484813
15 feet Y = -1600282
85 meter
Z = -4400825
36 Z = -1310316
02
XDOT = 272
842402 XDOT = 55
664539
YDOT = 16407
530997 feet/sec YDOT = 5001
792085 meter/sec
ZDOT = -19201
629745 ZDOT = -5852
319188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16904872
06 X = 5152605
00
Y = 13549636
33 feet Y = 4129929
15 meter
Z = -4275565
51 Z = -1303192
37
XDOT = -11948
744895 XDOT = -3641
977444
YDOT = 8865
327644 feet/sec YDOT = 2702
151866 meter/sec
ZDOT = -19200
330364 ZDOT = -5852
260695
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 11028
52928097
00016717 00000-0 10270-3 0 9001
2 25544 51
6429 156
9755 0004240 239
9015 120
1727 15
72201645 18929
Satellite: ISS
Catalog Number: 25544
Epoch time: 11028
52928097 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 156
9755 deg
Eccentricity:
0004240
Arg of perigee: 239
9015 deg
Mean anomaly: 120
1727 deg
Mean motion: 15
72201645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 304
Coasting Arc #2 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2011/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1141869
31 A = 6725397
00 meter
Y = -4073919
47 meter E =
0000955
Z = 5228640
32 I = 51
78782
XDOT = 6995
623075 Wp = 264
72459
YDOT = -3089
420893 meter/sec RA = 150
97739 deg
ZDOT = -879
603648 TA = 193
63616
MA = 193
63874
Ha = 191
748 n
mi
Hp = 187
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3746290
37 X = -1121628
34
Y = -13365877
54 feet Y = -4086575
77 meter
Z = 17154331
76 Z = 5223142
10
XDOT = 22951
519275 XDOT = 7033
922494
YDOT = -10135
895318 feet/sec YDOT = -3010
977403 meter/sec
ZDOT = -2885
838739 ZDOT = -845
526859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8239452
08 X = 2511384
99
Y = -11204968
00 feet Y = -3415274
25 meter
Z = 17132209
25 Z = 5221897
38
XDOT = 21229
111620 XDOT = 6470
633222
YDOT = 11409
527063 feet/sec YDOT = 3477
623849 meter/sec
ZDOT = -2748
356435 ZDOT = -837
699041
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 11029
54627386
00016717 00000-0 10270-3 0 9012
2 25544 51
6440 151
7673 0004168 245
4199 114
6529 15
72222655 19088
Satellite: ISS
Catalog Number: 25544
Epoch time: 11029
54627386 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 151
7673 deg
Eccentricity:
0004168
Arg of perigee: 245
4199 deg
Mean anomaly: 114
6529 deg
Mean motion: 15
72222655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 314
Coasting Arc #3 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2011/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5656533
80 A = 6737181
30 meter
Y = 3645204
05 meter E =
0008922
Z = 197950
84 I = 51
85447
XDOT = -2423
667856 Wp = 36
90079
YDOT = -4096
714606 meter/sec RA = 145
87749 deg
ZDOT = 6049
288894 TA = 325
24187
MA = 325
30013
Ha = 191
564 n
mi
Hp = 187
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18558181
76 X = -5697836
34
Y = 11959330
89 feet Y = 3581718
33 meter
Z = 649445
01 Z = 170372
06
XDOT = -7951
666195 XDOT = -2407
063060
YDOT = -13440
664719 feet/sec YDOT = -4123
725115 meter/sec
ZDOT = 19846
748341 ZDOT = 6037
555066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20925882
77 X = -6378209
07
Y = -7047787
78 feet Y = -2148165
72 meter
Z = 538146
88 Z = 164027
17
XDOT = 4956
705660 XDOT = 1510
803885
YDOT = -13165
109681 feet/sec YDOT = -4012
725431 meter/sec
ZDOT = 19799
471530 ZDOT = 6034
878922
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 11030
56324918
00016717 00000-0 10270-3 0 9022
2 25544 51
6447 146
5589 0004107 250
0732 109
9988 15
72239684 19245
Satellite: ISS
Catalog Number: 25544
Epoch time: 11030
56324918 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 146
5589 deg
Eccentricity:
0004107
Arg of perigee: 250
0732 deg
Mean anomaly: 109
9988 deg
Mean motion: 15
72239684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 321
Coasting Arc #4 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2011/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2976194
28 A = 6725080
88 meter
Y = 2927992
82 meter E =
0010913
Z = -5281495
77 I = 51
83913
XDOT = -5740
860535 Wp = 91
31232
YDOT = 5100
779151 meter/sec RA = 140
77276 deg
ZDOT = -408
213123 TA = 174
82240
MA = 174
81110
Ha = 191
401 n
mi
Hp = 187
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9764416
93 X = 2968887
49
Y = 9606275
65 feet Y = 2961233
88 meter
Z = -17327742
03 Z = -5267055
43
XDOT = -18834
844275 XDOT = -5795
488772
YDOT = 16734
839734 feet/sec YDOT = 5036
275964 meter/sec
ZDOT = -1339
281899 ZDOT = -436
233760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1116470
65 X = -340300
25
Y = 13725597
01 feet Y = 4183561
97 meter
Z = -17269525
00 Z = -5263751
22
XDOT = -23892
508903 XDOT = -7282
436714
YDOT = -3766
872140 feet/sec YDOT = -1148
142628 meter/sec
ZDOT = -1452
398166 ZDOT = -442
690961
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 11031
51664725
00016717 00000-0 10270-3 0 9032
2 25544 51
6451 141
6767 0004148 254
9550 105
1154 15
72276516 19394
Satellite: ISS
Catalog Number: 25544
Epoch time: 11031
51664725 = yrday
fracday
Element set: 903
Inclination: 51
6451 deg
RA of node: 141
6767 deg
Eccentricity:
0004148
Arg of perigee: 254
9550 deg
Mean anomaly: 105
1154 deg
Mean motion: 15
72276516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 300
Coasting Arc #5 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2011/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4247903
08 A = 6736686
08 meter
Y = -5141440
33 meter E =
0011281
Z = 902548
27 I = 51
90137
XDOT = 4213
209962 Wp = 140
86874
YDOT = 2427
420800 meter/sec RA = 135
65475 deg
ZDOT = -5970
065712 TA = 29
31939
MA = 29
25613
Ha = 191
361 n
mi
Hp = 187
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13936689
90 X = 4300695
65
Y = -16868242
54 feet Y = -5093642
57 meter
Z = 2961116
37 Z = 923311
92
XDOT = 13822
867330 XDOT = 4214
753492
YDOT = 7963
979002 feet/sec YDOT = 2474
544335 meter/sec
ZDOT = -19586
829763 ZDOT = -5949
594765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21865701
36 X = 6664665
77
Y = -395509
33 feet Y = -120551
24 meter
Z = 3044966
06 Z = 928105
66
XDOT = 2986
568575 XDOT = 910
306102
YDOT = 14173
578147 feet/sec YDOT = 4320
106619 meter/sec
ZDOT = -19504
266682 ZDOT = -5944
900485
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 11032
53358941
00016717 00000-0 10270-3 0 9046
2 25544 51
6452 136
4684 0004091 257
8137 102
2567 15
72286428 19552
Satellite: ISS
Catalog Number: 25544
Epoch time: 11032
53358941 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 136
4684 deg
Eccentricity:
0004091
Arg of perigee: 257
8137 deg
Mean anomaly: 102
2567 deg
Mean motion: 15
72286428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1955
Checksum: 312
Coasting Arc #6 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2011/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4224694
67 A = 6725710
35 meter
Y = -1208453
12 meter E =
0003430
Z = 5092601
62 I = 51
88683
XDOT = 3837
656926 Wp = 178
81793
YDOT = -6466
760335 meter/sec RA = 130
57244 deg
ZDOT = 1645
713315 TA = 255
39605
MA = 255
43410
Ha = 191
301 n
mi
Hp = 187
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13860546
81 X = -4235605
62
Y = -3964741
21 feet Y = -1255757
32 meter
Z = 16708010
58 Z = 5072052
23
XDOT = 12590
737945 XDOT = 3901
689933
YDOT = -21216
405298 feet/sec YDOT = -6423
487343 meter/sec
ZDOT = 5399
321899 ZDOT = 1664
511415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6292650
93 X = -1918000
00
Y = -13076694
73 feet Y = -3985776
55 meter
Z = 16625105
94 Z = 5067332
29
XDOT = 23253
734108 XDOT = 7087
738156
YDOT = -4214
804055 feet/sec YDOT = -1284
672276 meter/sec
ZDOT = 5475
267167 ZDOT = 1668
861433
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 11033
55051218
00016717 00000-0 10270-3 0 9057
2 25544 51
6460 131
2594 0004100 263
6871 96
3825 15
72355378 19714
Satellite: ISS
Catalog Number: 25544
Epoch time: 11033
55051218 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 131
2594 deg
Eccentricity:
0004100
Arg of perigee: 263
6871 deg
Mean anomaly: 96
3825 deg
Mean motion: 15
72355378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 295
Coasting Arc #7 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2011/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2384334
24 A = 6735285
71 meter
Y = 5985557
34 meter E =
0005371
Z = -1951364
86 I = 51
93777
XDOT = -5236
883276 Wp = 2
99891
YDOT = -251
026476 meter/sec RA = 125
43849 deg
ZDOT = 5634
787701 TA = 335
39918
MA = 335
42479
Ha = 191
190 n
mi
Hp = 187
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7822618
89 X = -2441609
60
Y = 19637655
31 feet Y = 5958574
03 meter
Z = -6402115
67 Z = -1963086
68
XDOT = -17181
375577 XDOT = -5261
058895
YDOT = -823
577678 feet/sec YDOT = -309
723638 meter/sec
ZDOT = 18486
836289 ZDOT = 5609
289058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19732528
36 X = -6014474
64
Y = 7539839
37 feet Y = 2298143
04 meter
Z = -6449504
19 Z = -1965808
88
XDOT = -10533
664036 XDOT = -3210
660798
YDOT = -11858
764695 feet/sec YDOT = -3614
551479 meter/sec
ZDOT = 18383
938622 ZDOT = 5603
424492
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 11034
50386382
00016717 00000-0 10270-3 0 9067
2 25544 51
6459 126
3770 0004106 270
9693 89
0999 15
72318350 19868
Satellite: ISS
Catalog Number: 25544
Epoch time: 11034
50386382 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 126
3770 deg
Eccentricity:
0004106
Arg of perigee: 270
9693 deg
Mean anomaly: 89
0999 deg
Mean motion: 15
72318350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 329
Coasting Arc #8 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2011/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4743018
85 A = 6727335
80 meter
Y = -793653
58 meter E =
0007398
Z = -4711450
68 I = 51
92732
XDOT = -1583
908675 Wp = 58
83197
YDOT = 6997
620406 meter/sec RA = 120
37548 deg
ZDOT = -2772
729625 TA = 183
91286
MA = 183
91864
Ha = 191
157 n
mi
Hp = 187
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15561085
47 X = 4774427
77
Y = -2603850
32 feet Y = -740438
75 meter
Z = -15457515
36 Z = -4688333
52
XDOT = -5196
550772 XDOT = -1648
570675
YDOT = 22958
072198 feet/sec YDOT = 6979
546583 meter/sec
ZDOT = -9096
881973 ZDOT = -2780
581206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12667594
61 X = 3861082
84
Y = 9556953
84 feet Y = 2912959
53 meter
Z = -15364207
71 Z = -4683010
51
XDOT = -19491
232864 XDOT = -5940
927777
YDOT = 11156
702846 feet/sec YDOT = 3400
563028 meter/sec
ZDOT = -9128
669929 ZDOT = -2782
418594
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 11035
52075461
00016717 00000-0 10270-3 0 9074
2 25544 51
6452 121
1685 0004073 273
2498 86
8198 15
72361829 20026
Satellite: ISS
Catalog Number: 25544
Epoch time: 11035
52075461 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 121
1685 deg
Eccentricity:
0004073
Arg of perigee: 273
2498 deg
Mean anomaly: 86
8198 deg
Mean motion: 15
72361829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 304
Coasting Arc #9 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2011/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 377337
80 A = 6733106
31 meter
Y = -6073258
12 meter E =
0009478
Z = 2872522
04 I = 51
96169
XDOT = 5385
422040 Wp = 98
25310
YDOT = -2080
548297 meter/sec RA = 115
22951 deg
ZDOT = -5093
377547 TA = 48
92579
MA = 48
84396
Ha = 191
173 n
mi
Hp = 187
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1237984
92 X = 431268
28
Y = -19925387
54 feet Y = -6068736
86 meter
Z = 9424284
91 Z = 2874486
29
XDOT = 17668
707480 XDOT = 5433
028868
YDOT = -6825
945856 feet/sec YDOT = -2020
059240 meter/sec
ZDOT = -16710
556256 ZDOT = -5067
100214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15038282
44 X = 4583668
49
Y = -13124501
63 feet Y = -4000348
10 meter
Z = 9432303
00 Z = 2874965
95
XDOT = 16366
810538 XDOT = 4988
603852
YDOT = 6789
755588 feet/sec YDOT = 2069
517503 meter/sec
ZDOT = -16604
470249 ZDOT = -5061
042532
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 11036
53762779
00016717 00000-0 10270-3 0 9082
2 25544 51
6450 115
9595 0003950 280
0615 80
0101 15
72414470 20183
Satellite: ISS
Catalog Number: 25544
Epoch time: 11036
53762779 = yrday
fracday
Element set: 908
Inclination: 51
6450 deg
RA of node: 115
9595 deg
Eccentricity:
0003950
Arg of perigee: 280
0615 deg
Mean anomaly: 80
0101 deg
Mean motion: 15
72414470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2018
Checksum: 289
Coasting Arc #10 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2011/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4489837
81 A = 6729218
19 meter
Y = 2805136
70 meter E =
0006429
Z = 4149755
61 I = 51
96051
XDOT = -685
510381 Wp = 105
28527
YDOT = -6679
678044 meter/sec RA = 110
17698 deg
ZDOT = 3767
148798 TA = 306
27796
MA = 306
33734
Ha = 191
266 n
mi
Hp = 187
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14730439
00 X = -4541029
94
Y = 9203204
39 feet Y = 2754642
56 meter
Z = 13614683
76 Z = 4127820
07
XDOT = -2249
049806 XDOT = -629
065683
YDOT = -21914
954212 feet/sec YDOT = -6687
028079 meter/sec
ZDOT = 12359
412068 ZDOT = 3763
956052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17014760
47 X = -5186098
99
Y = -3819270
18 feet Y = -1164113
55 meter
Z = 13526105
11 Z = 4122756
84
XDOT = 13427
162870 XDOT = 4092
599243
YDOT = -16015
969423 feet/sec YDOT = -4881
667480 meter/sec
ZDOT = 12346
630418 ZDOT = 3763
252951
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 11037
55448273
00016717 00000-0 10270-3 0 9096
2 25544 51
6448 110
7498 0004021 283
5424 76
5291 15
72447251 20342
Satellite: ISS
Catalog Number: 25544
Epoch time: 11037
55448273 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 110
7498 deg
Eccentricity:
0004021
Arg of perigee: 283
5424 deg
Mean anomaly: 76
5291 deg
Mean motion: 15
72447251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2034
Checksum: 302
Coasting Arc #11 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2011/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1517052
65 A = 6730674
54 meter
Y = 5432219
97 meter E =
0001930
Z = -3674548
51 I = 51
97429
XDOT = -4683
208989 Wp = 84
23736
YDOT = 4262
898236 meter/sec RA = 105
02603 deg
ZDOT = 4370
657796 TA = 231
89705
MA = 231
91445
Ha = 191
255 n
mi
Hp = 187
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4977206
85 X = 1474045
70
Y = 17822244
01 feet Y = 5448943
95 meter
Z = -12055605
35 Z = -3667283
52
XDOT = -15364
858887 XDOT = -4751
760871
YDOT = 13985
886601 feet/sec YDOT = 4210
144654 meter/sec
ZDOT = 14339
428463 ZDOT = 4347
740561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8611567
09 X = -2624805
65
Y = 16399690
52 feet Y = 4998625
67 meter
Z = -12026373
23 Z = -3665638
56
XDOT = -19638
756637 XDOT = -5985
893023
YDOT = 130
055218 feet/sec YDOT = 39
640830 meter/sec
ZDOT = 14246
857305 ZDOT = 4342
442107
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 11038
50777015
00016717 00000-0 10270-3 0 9103
2 25544 51
6438 105
8663 0003884 289
0490 71
0252 15
72479406 20490
Satellite: ISS
Catalog Number: 25544
Epoch time: 11038
50777015 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 105
8663 deg
Eccentricity:
0003884
Arg of perigee: 289
0490 deg
Mean anomaly: 71
0252 deg
Mean motion: 15
72479406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 307
Coasting Arc #12 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2011/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3554217
77 A = 6731356
16 meter
Y = -4544918
59 meter E =
0002388
Z = -3470452
00 I = 51
98318
XDOT = 2657
157719 Wp = 38
96731
YDOT = 5578
157158 meter/sec RA = 99
97692 deg
ZDOT = -4583
767096 TA = 181
89591
MA = 181
89681
Ha = 191
352 n
mi
Hp = 187
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11660819
44 X = 3621634
27
Y = -14911150
23 feet Y = -4504796
36 meter
Z = -11385997
38 Z = -3453022
00
XDOT = 8717
709052 XDOT = 2616
850939
YDOT = 18301
040546 feet/sec YDOT = 5607
645564 meter/sec
ZDOT = -15038
605958 ZDOT = -4570
956969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18723329
61 X = 5706870
87
Y = -3058275
63 feet Y = -932162
41 meter
Z = -11315561
23 Z = -3448983
06
XDOT = -6105
576139 XDOT = -1860
979607
YDOT = 18073
589346 feet/sec YDOT = 5508
830033 meter/sec
ZDOT = -14987
000930 ZDOT = -4568
037883
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 11039
52459299
00016717 00000-0 10270-3 0 9118
2 25544 51
6436 100
6562 0003869 294
7320 65
3440 15
72476091 20657
Satellite: ISS
Catalog Number: 25544
Epoch time: 11039
52459299 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 100
6562 deg
Eccentricity:
0003869
Arg of perigee: 294
7320 deg
Mean anomaly: 65
3440 deg
Mean motion: 15
72476091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2065
Checksum: 309
Coasting Arc #13 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2011/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 848063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3024147
02 A = 6728350
10 meter
Y = -4192221
78 meter E =
0007707
Z = 4305150
98 I = 51
97820
XDOT = 3279
002572 Wp = 49
03849
YDOT = -6002
569691 meter/sec RA = 94
82707 deg
ZDOT = -3532
766495 TA = 76
63328
MA = 76
54737
Ha = 191
401 n
mi
Hp = 187
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9921742
19 X = -2997957
36
Y = -13754008
47 feet Y = -4225893
07 meter
Z = 14124511
09 Z = 4290523
63
XDOT = 10757
882454 XDOT = 3363
042012
YDOT = -19693
470115 feet/sec YDOT = -5965
432109 meter/sec
ZDOT = -11590
441258 ZDOT = -3516
633056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1634397
75 X = 498164
43
Y = -16929399
09 feet Y = -5160080
84 meter
Z = 14065550
87 Z = 4287179
91
XDOT = 19930
698347 XDOT = 6074
876856
YDOT = -7676
085134 feet/sec YDOT = -2339
670749 meter/sec
ZDOT = -11525
200553 ZDOT = -3512
881129
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 11040
54139633
00016717 00000-0 10270-3 0 9120
2 25544 51
6440 95
4464 0004053 300
0495 60
0265 15
72541496 20811
Satellite: ISS
Catalog Number: 25544
Epoch time: 11040
54139633 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 95
4464 deg
Eccentricity:
0004053
Arg of perigee: 300
0495 deg
Mean anomaly: 60
0265 deg
Mean motion: 15
72541496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2081
Checksum: 275
Coasting Arc #14 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2011/040/21:41:25
496
Vector Time (MET): N/A
Weight (LBS) : 847872
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4056105
77 A = 6726358
28 meter
Y = -1787353
41 meter E =
0009660
Z = -5067812
50 I = 51
96997
XDOT = 1033
529796 Wp = 60
61218
YDOT = 7409
277531 meter/sec RA = 92
80759 deg
ZDOT = -1783
860078 TA = 192
25045
MA = 192
27395
Ha = 191
505 n
mi
Hp = 188
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13307433
62 X = 4100408
98
Y = -5864020
39 feet Y = -1741747
99 meter
Z = -16626681
42 Z = -5048000
58
XDOT = 3390
845788 XDOT = 959
266582
YDOT = 24308
653318 feet/sec YDOT = 7420
419818 meter/sec
ZDOT = -5852
559310 ZDOT = -1779
019816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8974837
02 X = -2735530
32
Y = -11557722
74 feet Y = -3522793
89 meter
Z = -16546673
54 Z = -5043426
10
XDOT = 21882
011989 XDOT = 6669
637254
YDOT = -8630
899581 feet/sec YDOT = -2630
698192 meter/sec
ZDOT = -5833
172587 ZDOT = -1777
951004
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 11040
92269760
00016717 00000-0 10270-3 0 9138
2 25544 51
6451 93
4935 0004895 289
7484 70
3150 15
72173611 20872
Satellite: ISS
Catalog Number: 25544
Epoch time: 11040
92269760 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 93
4935 deg
Eccentricity:
0004895
Arg of perigee: 289
7484 deg
Mean anomaly: 70
3150 deg
Mean motion: 15
72173611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 314
Coasting Arc #15 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2011/041/21:41:25
496
Vector Time (MET): N/A
Weight (LBS) : 847872
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1900818
33 A = 6735504
20 meter
Y = -6101369
38 meter E =
0009211
Z = 2114470
11 I = 52
00078
XDOT = 4216
791049 Wp = 108
75573
YDOT = -3246
826062 meter/sec RA = 87
67708 deg
ZDOT = -5561
405050 TA = 47
75205
MA = 47
67396
Ha = 191
636 n
mi
Hp = 188
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6236280
61 X = -1842721
96
Y = -20017616
06 feet Y = -6122300
62 meter
Z = 6937237
89 Z = 2105377
24
XDOT = 13834
616302 XDOT = 4279
800179
YDOT = -10652
316476 feet/sec YDOT = -3199
319104 meter/sec
ZDOT = -18246
079559 ZDOT = -5540
767100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17673359
22 X = -5386839
89
Y = 11302857
06 feet Y = 3445110
83 meter
Z = 6900667
68 Z = 2103323
51
XDOT = -13109
849617 XDOT = -3995
882163
YDOT = -9376
416547 feet/sec YDOT = -2857
931764 meter/sec
ZDOT = -18162
698708 ZDOT = -5535
990566
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 11041
93971703
00016717 00000-0 10270-3 0 9148
2 25544 51
6449 88
2852 0004859 292
9533 67
1116 15
72158585 21038
Satellite: ISS
Catalog Number: 25544
Epoch time: 11041
93971703 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 88
2852 deg
Eccentricity:
0004859
Arg of perigee: 292
9533 deg
Mean anomaly: 67
1116 deg
Mean motion: 15
72158585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 320
Coasting Arc #16 (Orbit 2118)
---------------------------------------
Vector Time (GMT): 2011/042/21:41:25
496
Vector Time (MET): N/A
Weight (LBS) : 847872
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3131839
30 A = 6728213
35 meter
Y = 3786479
69 meter E =
0003578
Z = 4593709
24 I = 51
97496
XDOT = -3200
522951 Wp = 110
06443
YDOT = -6316
492349 meter/sec RA = 82
62056 deg
ZDOT = 3021
428264 TA = 310
03846
MA = 310
06985
Ha = 191
856 n
mi
Hp = 188
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10275063
31 X = -3196262
72
Y = 12422833
63 feet Y = 3751097
34 meter
Z = 15071224
53 Z = 4578338
54
XDOT = -10500
403383 XDOT = -3144
330192
YDOT = -20723
400096 feet/sec YDOT = -6351
968354 meter/sec
ZDOT = 9912
822387 ZDOT = 3006
016831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14818959
79 X = 4516818
94
Y = 6493945
88 feet Y = 1979354
71 meter
Z = 15009084
85 Z = 4574769
06
XDOT = -16487
755948 XDOT = -5025
468013
YDOT = 14833
485895 feet/sec YDOT = 4521
246501 meter/sec
ZDOT = 9850
758322 ZDOT = 3002
511137
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 11042
95671800
00016717 00000-0 10270-3 0 9157
2 25544 51
6456 83
0766 0004926 298
2944 61
7721 15
72200869 21195
Satellite: ISS
Catalog Number: 25544
Epoch time: 11042
95671800 = yrday
fracday
Element set: 915
Inclination: 51
6456 deg
RA of node: 83
0766 deg
Eccentricity:
0004926
Arg of perigee: 298
2944 deg
Mean anomaly: 61
7721 deg
Mean motion: 15
72200869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2119
Checksum: 316
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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