Date:
January 4th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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
013/09:06:03
422 -3
9 5
1 5
1
N/A -2
9 -0
0 194
1
000/00:12:06
843 -1
7 0
2 187
1
Coasting Arc #1 (Orbit 1458)
---------------------------------------
Vector Time (GMT): 2011/001/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -562965
77 A = 6730643
73 meter
Y = -5535824
83 meter E =
0010891
Z = -3797568
81 I = 51
34246
XDOT = 5498
360097 Wp = 100
25354
YDOT = -3405
549071 meter/sec RA = 297
28210 deg
ZDOT = 4157
482877 TA = 213
53677
MA = 213
60576
Ha = 194
363 n
mi
Hp = 184
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1847000
57 X = -482573
42
Y = -18162154
95 feet Y = -5541670
23 meter
Z = -12459215
27 Z = -3800109
20
XDOT = 18039
239163 XDOT = 5515
836656
YDOT = -11173
061255 feet/sec YDOT = -3343
965959 meter/sec
ZDOT = 13640
035685 ZDOT = 4184
235862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17619222
41 X = -5370338
99
Y = 4752701
78 feet Y = 1448623
50 meter
Z = -12469248
42 Z = -3800626
92
XDOT = -13642
498569 XDOT = -4158
233564
YDOT = -14577
297837 feet/sec YDOT = -4443
160381 meter/sec
ZDOT = 13747
775107 ZDOT = 4190
321853
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 11001
16554370
00016717 00000-0 10270-3 0 9001
2 25544 51
6459 297
9219 0004718 95
2596 264
9105 15
72339989 14599
Satellite: ISS
Catalog Number: 25544
Epoch time: 11001
16554370 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 297
9219 deg
Eccentricity:
0004718
Arg of perigee: 95
2596 deg
Mean anomaly: 264
9105 deg
Mean motion: 15
72339989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1459
Checksum: 334
Coasting Arc #2 (Orbit 1474)
---------------------------------------
Vector Time (GMT): 2011/002/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4413301
78 A = 6732081
12 meter
Y = 3901806
82 meter E =
0009491
Z = -3265582
55 I = 51
33527
XDOT = -1688
068446 Wp = 97
24066
YDOT = -5840
792587 meter/sec RA = 292
18870 deg
ZDOT = -4710
273289 TA = 121
14422
MA = 121
05110
Ha = 194
292 n
mi
Hp = 184
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14479336
54 X = -4440740
99
Y = 12801203
47 feet Y = 3852301
68 meter
Z = -10713853
52 Z = -3287088
32
XDOT = -5538
282304 XDOT = -1599
748625
YDOT = -19162
705339 feet/sec YDOT = -5859
175062 meter/sec
ZDOT = -15453
652524 ZDOT = -4718
260222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15214829
93 X = 4637480
16
Y = 11839202
74 feet Y = 3608589
00 meter
Z = -10800503
83 Z = -3291993
57
XDOT = -16985
570638 XDOT = -5177
201930
YDOT = 7739
837646 feet/sec YDOT = 2359
102515 meter/sec
ZDOT = -15485
591868 ZDOT = -4720
008401
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 11002
18242921
00016717 00000-0 10270-3 0 9011
2 25544 51
6464 292
7126 0004800 100
3292 259
8412 15
72382524 14753
Satellite: ISS
Catalog Number: 25544
Epoch time: 11002
18242921 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 292
7126 deg
Eccentricity:
0004800
Arg of perigee: 100
3292 deg
Mean anomaly: 259
8412 deg
Mean motion: 15
72382524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1475
Checksum: 278
Coasting Arc #3 (Orbit 1490)
---------------------------------------
Vector Time (GMT): 2011/003/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2309334
18 A = 6728201
36 meter
Y = 4519033
24 meter E =
0013575
Z = 4407214
32 I = 51
31207
XDOT = -4388
064542 Wp = 80
23456
YDOT = 5430
534086 meter/sec RA = 286
99459 deg
ZDOT = -3258
225488 TA = 42
62270
MA = 42
51744
Ha = 194
243 n
mi
Hp = 184
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7576555
71 X = 2237220
65
Y = 14826224
54 feet Y = 4544453
74 meter
Z = 14459364
57 Z = 4418258
46
XDOT = -14396
537211 XDOT = -4432
635963
YDOT = 17816
712879 feet/sec YDOT = 5381
215380 meter/sec
ZDOT = -10689
716169 ZDOT = -3279
649931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13037180
16 X = 3973732
51
Y = -10294186
47 feet Y = -3137668
03 meter
Z = 14503655
15 Z = 4420714
09
XDOT = 19564
045300 XDOT = 5963
121008
YDOT = 9544
742758 feet/sec YDOT = 2909
237593 meter/sec
ZDOT = -10776
090819 ZDOT = -3284
552482
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 11003
19929440
00016717 00000-0 10270-3 0 9022
2 25544 51
6465 287
5040 0004906 102
5684 257
6027 15
72410935 14911
Satellite: ISS
Catalog Number: 25544
Epoch time: 11003
19929440 = yrday
fracday
Element set: 902
Inclination: 51
6465 deg
RA of node: 287
5040 deg
Eccentricity:
0004906
Arg of perigee: 102
5684 deg
Mean anomaly: 257
6027 deg
Mean motion: 15
72410935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1491
Checksum: 297
Coasting Arc #4 (Orbit 1506)
---------------------------------------
Vector Time (GMT): 2011/004/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3115361
64 A = 6734018
99 meter
Y = -5456149
27 meter E =
0018182
Z = 2403686
08 I = 51
32444
XDOT = 3455
501710 Wp = 82
43800
YDOT = 4340
502032 meter/sec RA = 281
89325 deg
ZDOT = 5341
804092 TA = 304
80024
MA = 304
97119
Ha = 194
162 n
mi
Hp = 184
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10221002
75 X = 3164465
29
Y = -17900752
21 feet Y = -5421037
21 meter
Z = 7886109
18 Z = 2418938
77
XDOT = 11336
947869 XDOT = 3380
759467
YDOT = 14240
492231 feet/sec YDOT = 4378
724869 meter/sec
ZDOT = 17525
603976 ZDOT = 5358
409733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19675828
10 X = -5997192
41
Y = -6065739
07 feet Y = -1848837
27 meter
Z = 7947650
14 Z = 2422443
76
XDOT = 11035
544434 XDOT = 3363
633944
YDOT = -12609
247523 feet/sec YDOT = -3843
298645 meter/sec
ZDOT = 17592
287815 ZDOT = 5362
129326
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 11004
21613736
00016717 00000-0 10270-3 0 9035
2 25544 51
6466 282
2949 0004834 106
6134 253
5559 15
72460907 15074
Satellite: ISS
Catalog Number: 25544
Epoch time: 11004
21613736 = yrday
fracday
Element set: 903
Inclination: 51
6466 deg
RA of node: 282
2949 deg
Eccentricity:
0004834
Arg of perigee: 106
6134 deg
Mean anomaly: 253
5559 deg
Mean motion: 15
72460907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1507
Checksum: 303
Coasting Arc #5 (Orbit 1521)
---------------------------------------
Vector Time (GMT): 2011/005/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3581402
64 A = 6726072
84 meter
Y = -2972254
74 meter E =
0017151
Z = -4871764
18 I = 51
29253
XDOT = 2627
144799 Wp = 107
30131
YDOT = -6860
671012 meter/sec RA = 276
70774 deg
ZDOT = 2255
902023 TA = 184
78719
MA = 184
80361
Ha = 194
100 n
mi
Hp = 184
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11750008
66 X = -3524234
45
Y = -9751491
94 feet Y = -3011983
88 meter
Z = -15983478
28 Z = -4889023
83
XDOT = 8619
241467 XDOT = 2692
708299
YDOT = -22508
763162 feet/sec YDOT = -6830
926399 meter/sec
ZDOT = 7401
253355 ZDOT = 2268
822826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6770587
18 X = -2063674
97
Y = 13604821
30 feet Y = 4146749
53 meter
Z = -16052845
94 Z = -4892907
44
XDOT = -22894
301669 XDOT = -6978
183149
YDOT = -2604
866618 feet/sec YDOT = -793
963345 meter/sec
ZDOT = 7453
446730 ZDOT = 2271
810563
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 11005
16941019
00016717 00000-0 10270-3 0 9049
2 25544 51
6462 277
4123 0004815 109
3862 250
7822 15
72506544 15224
Satellite: ISS
Catalog Number: 25544
Epoch time: 11005
16941019 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 277
4123 deg
Eccentricity:
0004815
Arg of perigee: 109
3862 deg
Mean anomaly: 250
7822 deg
Mean motion: 15
72506544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1522
Checksum: 287
Coasting Arc #6 (Orbit 1537)
---------------------------------------
Vector Time (GMT): 2011/006/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1415744
80 A = 6735387
70 meter
Y = 6397185
95 meter E =
0012563
Z = -1545614
89 I = 51
32042
XDOT = -4534
698555 Wp = 132
06099
YDOT = -2382
358498 meter/sec RA = 271
59293 deg
ZDOT = -5744
899011 TA = 65
04325
MA = 64
91278
Ha = 194
047 n
mi
Hp = 184
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4644832
02 X = -1479665
95
Y = 20988142
87 feet Y = 6380997
00 meter
Z = -5070914
98 Z = -1552647
00
XDOT = -14877
619932 XDOT = -4479
814457
YDOT = -7816
136806 feet/sec YDOT = -2432
760734 meter/sec
ZDOT = -18848
093867 ZDOT = -5766
795062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21475484
12 X = 6545727
56
Y = -768508
58 feet Y = -234241
42 meter
Z = -5099388
30 Z = -1554293
55
XDOT = -3941
436238 XDOT = -1201
349765
YDOT = 14682
437780 feet/sec YDOT = 4475
207035 meter/sec
ZDOT = -18936
146078 ZDOT = -5771
737325
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 11006
18621503
00016717 00000-0 10270-3 0 9056
2 25544 51
6451 272
2028 0004776 113
8788 246
2876 15
72502962 15388
Satellite: ISS
Catalog Number: 25544
Epoch time: 11006
18621503 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 272
2028 deg
Eccentricity:
0004776
Arg of perigee: 113
8788 deg
Mean anomaly: 246
2876 deg
Mean motion: 15
72502962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1538
Checksum: 308
Coasting Arc #7 (Orbit 1553)
---------------------------------------
Vector Time (GMT): 2011/007/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4190772
48 A = 6724648
62 meter
Y = 1129223
24 meter E =
0007470
Z = 5130072
46 I = 51
28567
XDOT = -522
275454 Wp = 87
93101
YDOT = 7585
965240 meter/sec RA = 266
41946 deg
ZDOT = -1241
339864 TA = 13
99595
MA = 13
97526
Ha = 193
724 n
mi
Hp = 184
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13749253
55 X = 4152913
40
Y = 3704800
65 feet Y = 1175874
85 meter
Z = 16830946
41 Z = 5150338
94
XDOT = -1713
502145 XDOT = -601
034249
YDOT = 24888
337401 feet/sec YDOT = 7579
684585 meter/sec
ZDOT = -4072
637350 ZDOT = -1244
067664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -60701
39 X = -18501
78
Y = -14142579
65 feet Y = -4310658
28 meter
Z = 16912481
61 Z = 5154924
39
XDOT = 23408
791540 XDOT = 7134
999661
YDOT = -4991
229968 feet/sec YDOT = -1521
326894 meter/sec
ZDOT = -4083
806897 ZDOT = -1244
744342
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 11007
20299740
00016717 00000-0 10270-3 0 9065
2 25544 51
6454 266
9929 0004588 117
1560 243
0071 15
72580852 15541
Satellite: ISS
Catalog Number: 25544
Epoch time: 11007
20299740 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 266
9929 deg
Eccentricity:
0004588
Arg of perigee: 117
1560 deg
Mean anomaly: 243
0071 deg
Mean motion: 15
72580852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1554
Checksum: 310
Coasting Arc #8 (Orbit 1569)
---------------------------------------
Vector Time (GMT): 2011/008/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -517967
12 A = 6736148
21 meter
Y = -6681831
65 meter E =
0015728
Z = 624753
58 I = 51
32626
XDOT = 4860
808537 Wp = 67
42826
YDOT = 191
697640 meter/sec RA = 261
28834 deg
ZDOT = 5966
643729 TA = 299
39970
MA = 299
55663
Ha = 193
928 n
mi
Hp = 184
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1699367
18 X = -446246
00
Y = -21922019
84 feet Y = -6687222
90 meter
Z = 2049716
46 Z = 622411
10
XDOT = 15947
534569 XDOT = 4829
319387
YDOT = 628
929265 feet/sec YDOT = 245
877663 meter/sec
ZDOT = 19575
602786 ZDOT = 5990
180585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20543938
41 X = -6261792
43
Y = 7838834
11 feet Y = 2389276
64 meter
Z = 2040444
69 Z = 621927
54
XDOT = -3299
443278 XDOT = -1005
670311
YDOT = -13864
747788 feet/sec YDOT = -4225
975126 meter/sec
ZDOT = 19670
328329 ZDOT = 5995
516075
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 11008
21976358
00016717 00000-0 10270-3 0 9075
2 25544 51
6446 261
7834 0004668 118
4887 241
6746 15
72547813 15706
Satellite: ISS
Catalog Number: 25544
Epoch time: 11008
21976358 = yrday
fracday
Element set: 907
Inclination: 51
6446 deg
RA of node: 261
7834 deg
Eccentricity:
0004668
Arg of perigee: 118
4887 deg
Mean anomaly: 241
6746 deg
Mean motion: 15
72547813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1570
Checksum: 335
Coasting Arc #9 (Orbit 1584)
---------------------------------------
Vector Time (GMT): 2011/009/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4148570
94 A = 6724174
90 meter
Y = 760793
71 meter E =
0019074
Z = -5253238
99 I = 51
29100
XDOT = -1664
553633 Wp = 98
93247
YDOT = -7498
844149 meter/sec RA = 256
13182 deg
ZDOT = 226
299479 TA = 173
24314
MA = 173
21739
Ha = 193
809 n
mi
Hp = 184
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13610797
05 X = -4131251
12
Y = 2496042
36 feet Y = 714499
01 meter
Z = -17235036
07 Z = -5273350
28
XDOT = -5461
133965 XDOT = -1581
675738
YDOT = -24602
507052 feet/sec YDOT = -7516
994809 meter/sec
ZDOT = 742
452360 ZDOT = 218
414133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6421872
41 X = 1957386
71
Y = 12142743
62 feet Y = 3701108
26 meter
Z = -17315999
08 Z = -5277916
52
XDOT = -20955
421639 XDOT = -6387
212516
YDOT = 12106
644725 feet/sec YDOT = 3690
105312 meter/sec
ZDOT = 710
877017 ZDOT = 216
675315
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 11009
17296058
00016717 00000-0 10270-3 0 9084
2 25544 51
6436 256
8988 0004570 123
0068 237
1535 15
72579060 15856
Satellite: ISS
Catalog Number: 25544
Epoch time: 11009
17296058 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 256
8988 deg
Eccentricity:
0004570
Arg of perigee: 123
0068 deg
Mean anomaly: 237
1535 deg
Mean motion: 15
72579060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1585
Checksum: 324
Coasting Arc #10 (Orbit 1600)
---------------------------------------
Vector Time (GMT): 2011/010/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2358474
65 A = 6736013
05 meter
Y = 6297228
28 meter E =
0017305
Z = 222303
69 I = 51
34022
XDOT = -4434
878170 Wp = 130
46564
YDOT = 1883
497819 meter/sec RA = 250
98328 deg
ZDOT = -6008
211380 TA = 47
10926
MA = 46
96410
Ha = 193
707 n
mi
Hp = 184
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7737777
73 X = 2286802
68
Y = 20660197
75 feet Y = 6323201
41 meter
Z = 729342
82 Z = 233587
19
XDOT = -14550
125229 XDOT = -4426
423822
YDOT = 6179
454786 feet/sec YDOT = 1833
951879 meter/sec
ZDOT = -19711
979592 ZDOT = -6029
735073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17164932
31 X = 5231871
37
Y = -13856910
18 feet Y = -4223586
22 meter
Z = 774632
40 Z = 236107
96
XDOT = 9406
207686 XDOT = 2867
012103
YDOT = 10493
963403 feet/sec YDOT = 3198
560045 meter/sec
ZDOT = -19798
652638 ZDOT = -6034
629324
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 11010
18968570
00016717 00000-0 10270-3 0 9093
2 25544 51
6438 251
6883 0004645 124
7044 235
4556 15
72645637 16017
Satellite: ISS
Catalog Number: 25544
Epoch time: 11010
18968570 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 251
6883 deg
Eccentricity:
0004645
Arg of perigee: 124
7044 deg
Mean anomaly: 235
4556 deg
Mean motion: 15
72645637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1601
Checksum: 314
Coasting Arc #11 (Orbit 1616)
---------------------------------------
Vector Time (GMT): 2011/011/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3456340
26 A = 6724058
65 meter
Y = -2477093
47 meter E =
0007715
Z = 5203776
33 I = 51
31109
XDOT = 3678
338605 Wp = 125
32987
YDOT = 6726
734238 meter/sec RA = 245
84465 deg
ZDOT = 753
714075 TA = 317
43960
MA = 317
49937
Ha = 193
497 n
mi
Hp = 184
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11339699
02 X = 3458504
00
Y = -8126947
09 feet Y = -2438430
73 meter
Z = 17072756
97 Z = 5220572
17
XDOT = 12068
040043 XDOT = 3599
184254
YDOT = 22069
338051 feet/sec YDOT = 6767
425029 meter/sec
ZDOT = 2472
815206 ZDOT = 771
391268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11394489
52 X = -3473040
41
Y = -7904868
55 feet Y = -2409403
93 meter
Z = 17140412
34 Z = 5224397
68
XDOT = 16243
716189 XDOT = 4951
084694
YDOT = -17861
868433 feet/sec YDOT = -5444
297499 meter/sec
ZDOT = 2543
842196 ZDOT = 775
363101
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 11011
20639002
00016717 00000-0 10270-3 0 9104
2 25544 51
6436 246
4778 0004576 129
5293 230
6275 15
72678691 16170
Satellite: ISS
Catalog Number: 25544
Epoch time: 11011
20639002 = yrday
fracday
Element set: 910
Inclination: 51
6436 deg
RA of node: 246
4778 deg
Eccentricity:
0004576
Arg of perigee: 129
5293 deg
Mean anomaly: 230
6275 deg
Mean motion: 15
72678691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1617
Checksum: 308
Coasting Arc #12 (Orbit 1631)
---------------------------------------
Vector Time (GMT): 2011/012/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3977582
66 A = 6735438
69 meter
Y = -5325741
92 meter E =
0010366
Z = -1076042
66 I = 51
36271
XDOT = 3334
202196 Wp = 63
73423
YDOT = -3669
385493 meter/sec RA = 240
68033 deg
ZDOT = 5884
648063 TA = 284
46090
MA = 284
57590
Ha = 193
562 n
mi
Hp = 184
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13049811
88 X = -3912506
42
Y = -17472906
57 feet Y = -5369857
74 meter
Z = -3530323
70 Z = -1095207
78
XDOT = 10938
983583 XDOT = 3346
399851
YDOT = -12038
666316 feet/sec YDOT = -3632
032525 meter/sec
ZDOT = 19306
588132 ZDOT = 5900
874916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11847553
17 X = -3611134
21
Y = 18294413
50 feet Y = 5576137
24 meter
Z = -3607375
49 Z = -1099528
05
XDOT = -13717
829472 XDOT = -4181
194423
YDOT = -5094
473981 feet/sec YDOT = -1552
795669 meter/sec
ZDOT = 19371
976234 ZDOT = 5904
578356
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 11012
15953377
00016717 00000-0 10270-3 0 9114
2 25544 51
6434 241
5927 0004485 130
5171 229
6383 15
72667677 16323
Satellite: ISS
Catalog Number: 25544
Epoch time: 11012
15953377 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 241
5927 deg
Eccentricity:
0004485
Arg of perigee: 130
5171 deg
Mean anomaly: 229
6383 deg
Mean motion: 15
72667677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1632
Checksum: 311
Coasting Arc #13 (Orbit 1647)
---------------------------------------
Vector Time (GMT): 2011/013/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2284560
64 A = 6724728
18 meter
Y = 3819086
25 meter E =
0016452
Z = -5055654
34 I = 51
34357
XDOT = -5272
198980 Wp = 91
09226
YDOT = -5342
451522 meter/sec RA = 235
55822 deg
ZDOT = -1658
284188 TA = 162
89863
MA = 162
84313
Ha = 193
479 n
mi
Hp = 184
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7495277
70 X = -2302537
31
Y = 12529810
53 feet Y = 3793438
71 meter
Z = -16586792
47 Z = -5066796
10
XDOT = -17297
240747 XDOT = -5204
011252
YDOT = -17527
728091 feet/sec YDOT = -5401
027073 meter/sec
ZDOT = -5440
564921 ZDOT = -1683
731046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14361952
78 X = 4377523
21
Y = 2327536
39 feet Y = 709433
09 meter
Z = -16631714
01 Z = -5069346
43
XDOT = -9870
440514 XDOT = -3008
510269
YDOT = 21413
491001 feet/sec YDOT = 6526
832057 meter/sec
ZDOT = -5542
913549 ZDOT = -1689
480050
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 11013
17620058
00016717 00000-0 10270-3 0 9125
2 25544 51
6441 236
3814 0004571 135
1175 225
0358 15
72708763 16480
Satellite: ISS
Catalog Number: 25544
Epoch time: 11013
17620058 = yrday
fracday
Element set: 912
Inclination: 51
6441 deg
RA of node: 236
3814 deg
Eccentricity:
0004571
Arg of perigee: 135
1175 deg
Mean anomaly: 225
0358 deg
Mean motion: 15
72708763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1648
Checksum: 289
Coasting Arc #14 (Orbit 1653)
---------------------------------------
Vector Time (GMT): 2011/013/09:12:06
843
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3112376
04 A = 6726622
39 meter
Y = 2852358
55 meter E =
0014889
Z = -5248942
58 I = 51
34812
XDOT = -4812
443920 Wp = 106
06633
YDOT = -5980
855671 meter/sec RA = 233
57599 deg
ZDOT = -401
538832 TA = 160
12752
MA = 160
06946
Ha = 194
138 n
mi
Hp = 187
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10211207
47 X = -3118542
08
Y = 9358131
73 feet Y = 2817519
95 meter
Z = -17220940
24 Z = -5264077
20
XDOT = -15788
858004 XDOT = -4743
256605
YDOT = -19622
229893 feet/sec YDOT = -6034
284448 meter/sec
ZDOT = -1317
384621 ZDOT = -424
749869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5280622
91 X = -1609533
86
Y = -12722201
94 feet Y = -3877727
15 meter
Z = -17281920
31 Z = -5267529
31
XDOT = 22943
573902 XDOT = 6993
201325
YDOT = -7629
089724 feet/sec YDOT = -2325
346548 meter/sec
ZDOT = -1410
724951 ZDOT = -429
988965
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 11013
40005544
00016717 00000-0 10270-3 0 9139
2 25544 51
6448 234
4283 0004960 186
9196 173
1898 15
71736254 16549
Satellite: ISS
Catalog Number: 25544
Epoch time: 11013
40005544 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 234
4283 deg
Eccentricity:
0004960
Arg of perigee: 186
9196 deg
Mean anomaly: 173
1898 deg
Mean motion: 15
71736254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1654
Checksum: 312
Coasting Arc #15 (Orbit 1669)
---------------------------------------
Vector Time (GMT): 2011/014/09:12:06
843
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5009158
81 A = 6738164
18 meter
Y = 4363676
08 meter E =
0016401
Z = 1066990
30 I = 51
40566
XDOT = -2478
134929 Wp = 139
95932
YDOT = 4295
087502 meter/sec RA = 228
42534 deg
ZDOT = -5893
883010 TA = 28
33436
MA = 28
24526
Ha = 194
074 n
mi
Hp = 187
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16434248
07 X = 4954807
86
Y = 14316522
57 feet Y = 4419387
53 meter
Z = 3500624
34 Z = 1091192
97
XDOT = -8130
363940 XDOT = -2497
347993
YDOT = 14091
494430 feet/sec YDOT = 4267
268558 meter/sec
ZDOT = -19336
886517 ZDOT = -5905
968031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18929959
35 X = -5769851
61
Y = 10770922
20 feet Y = 3282977
09 meter
Z = 3597995
61 Z = 1096669
06
XDOT = -9872
165634 XDOT = -3009
036085
YDOT = -10834
422704 feet/sec YDOT = -3302
332040 meter/sec
ZDOT = -19385
617154 ZDOT = -5908
736108
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 11014
41735439
00016717 00000-0 10270-3 0 9145
2 25544 51
6446 229
2221 0005057 190
8415 169
2639 15
71717502 16709
Satellite: ISS
Catalog Number: 25544
Epoch time: 11014
41735439 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 229
2221 deg
Eccentricity:
0005057
Arg of perigee: 190
8415 deg
Mean anomaly: 169
2639 deg
Mean motion: 15
71717502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1670
Checksum: 298
Coasting Arc #16 (Orbit 1685)
---------------------------------------
Vector Time (GMT): 2011/015/09:12:06
843
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1062280
20 A = 6727848
84 meter
Y = -4430533
24 meter E =
0008897
Z = 4949638
29 I = 51
39263
XDOT = 6382
354269 Wp = 155
39850
YDOT = 3799
183363 meter/sec RA = 223
31684 deg
ZDOT = 2021
695447 TA = 274
91188
MA = 275
01345
Ha = 193
843 n
mi
Hp = 187
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3485171
27 X = 1087700
06
Y = -14535870
20 feet Y = -4418512
54 meter
Z = 16238970
76 Z = 4954860
11
XDOT = 20939
482511 XDOT = 6329
575785
YDOT = 12464
512347 feet/sec YDOT = 3870
259397 meter/sec
ZDOT = 6632
859078 ZDOT = 2052
572852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12739226
50 X = 3882916
24
Y = 7775878
78 feet Y = 2370087
85 meter
Z = 16260071
65 Z = 4956069
84
XDOT = -17823
473645 XDOT = -5432
594767
YDOT = 15006
898151 feet/sec YDOT = 4574
102556 meter/sec
ZDOT = 6757
128958 ZDOT = 2059
572906
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 11015
43463260
00016717 00000-0 10270-3 0 9159
2 25544 51
6447 224
0156 0004876 195
7490 164
3521 15
71777519 16862
Satellite: ISS
Catalog Number: 25544
Epoch time: 11015
43463260 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 224
0156 deg
Eccentricity:
0004876
Arg of perigee: 195
7490 deg
Mean anomaly: 164
3521 deg
Mean motion: 15
71777519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1686
Checksum: 315
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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