Date:
October 20th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12109 4 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 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 2506)
---------------------------------------
Vector Time (GMT): 2009/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1701607
29 A = 6723807
08 meter
Y = 5446231
73 meter E =
0011422
Z = 3556979
33 I = 51
87499
XDOT = -6182
266696 Wp = 132
00662
YDOT = -1004
031728 meter/sec RA = 43
35862 deg
ZDOT = 4478
195582 TA = 270
25206
MA = 270
38294
Ha = 189
226 n
mi
Hp = 182
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5582701
08 X = 1623300
58
Y = 17868214
32 feet Y = 5464822
57 meter
Z = 11669879
69 Z = 3565055
24
XDOT = -20283
027219 XDOT = -6192
334689
YDOT = -3294
067348 feet/sec YDOT = -1073
221391 meter/sec
ZDOT = 14692
242722 ZDOT = 4448
137119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12396015
70 X = -3778305
58
Y = -14001024
59 feet Y = -4267512
29 meter
Z = 11701958
46 Z = 3566756
94
XDOT = 18891
807713 XDOT = 5758
222991
YDOT = -4500
122533 feet/sec YDOT = -1371
637348 meter/sec
ZDOT = 14573
658326 ZDOT = 4442
051058
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 09289
55594074
00001200 00000-0 20000-3 0 9007
2 25544 51
6432 43
6196 0007881 207
9997 152
0744 15
74999284 25074
Satellite: ISS
Catalog Number: 25544
Epoch time: 09289
55594074 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 43
6196 deg
Eccentricity:
0007881
Arg of perigee: 207
9997 deg
Mean anomaly: 152
0744 deg
Mean motion: 15
74999284 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2507
Checksum: 333
Coasting Arc #2 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2009/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5592589
25 A = 6723646
07 meter
Y = 733293
54 meter E =
0007561
Z = -3667387
23 I = 51
85175
XDOT = 2077
494185 Wp = 169
49929
YDOT = 5990
275539 meter/sec RA = 38
18049 deg
ZDOT = 4359
957857 TA = 146
62088
MA = 146
57319
Ha = 189
032 n
mi
Hp = 183
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18348389
91 X = 5601789
75
Y = 2405818
71 feet Y = 795884
35 meter
Z = -12032110
34 Z = -3640195
42
XDOT = 6815
925804 XDOT = 1989
175028
YDOT = 19653
134972 feet/sec YDOT = 6013
013799 meter/sec
ZDOT = 14304
323678 ZDOT = 4369
835627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17674244
74 X = -5387109
80
Y = 5713328
84 feet Y = 1741422
63 meter
Z = -11924848
07 Z = -3634693
69
XDOT = -14083
281275 XDOT = -4292
584133
YDOT = -13588
418892 feet/sec YDOT = -4141
750078 meter/sec
ZDOT = 14343
521215 ZDOT = 4371
905266
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 09290
50769140
00001200 00000-0 20000-3 0 9013
2 25544 51
6435 38
7258 0007708 212
8078 147
2608 15
74979502 25227
Satellite: ISS
Catalog Number: 25544
Epoch time: 09290
50769140 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 38
7258 deg
Eccentricity:
0007708
Arg of perigee: 212
8078 deg
Mean anomaly: 147
2608 deg
Mean motion: 15
74979502 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2522
Checksum: 302
Coasting Arc #3 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2009/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1880084
92 A = 6722115
26 meter
Y = -5025688
02 meter E =
0004541
Z = -4048457
57 I = 51
82335
XDOT = 6612
073917 Wp = 146
37204
YDOT = 657
387356 meter/sec RA = 33
10323 deg
ZDOT = -3892
456603 TA = 83
63880
MA = 83
58709
Ha = 188
834 n
mi
Hp = 183
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6168257
62 X = -1804079
81
Y = -16488477
76 feet Y = -5046287
48 meter
Z = -13282341
12 Z = -4057406
41
XDOT = 21693
155896 XDOT = 6623
140883
YDOT = 2156
782664 feet/sec YDOT = 731
389140 meter/sec
ZDOT = -12770
526912 ZDOT = -3860
307344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12774410
95 X = 3893640
46
Y = 12074262
05 feet Y = 3680235
07 meter
Z = -13317826
67 Z = -4059273
57
XDOT = -19583
674405 XDOT = -5969
103959
YDOT = 6794
158794 feet/sec YDOT = 2070
859600 meter/sec
ZDOT = -12643
722807 ZDOT = -3853
806712
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 09291
52287158
00001200 00000-0 20000-3 0 9021
2 25544 51
6441 33
5052 0007717 216
2287 143
8355 15
75013963 25388
Satellite: ISS
Catalog Number: 25544
Epoch time: 09291
52287158 = yrday
fracday
Element set: 902
Inclination: 51
6441 deg
RA of node: 33
5052 deg
Eccentricity:
0007717
Arg of perigee: 216
2287 deg
Mean anomaly: 143
8355 deg
Mean motion: 15
75013963 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2538
Checksum: 291
Coasting Arc #4 (Orbit 2553)
---------------------------------------
Vector Time (GMT): 2009/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5942212
46 A = 6725097
16 meter
Y = -379456
89 meter E =
0010878
Z = 3110896
59 I = 51
80748
XDOT = -2210
962297 Wp = 129
77699
YDOT = -5528
512258 meter/sec RA = 27
92311 deg
ZDOT = -4893
158945 TA = 14
12326
MA = 14
09287
Ha = 188
740 n
mi
Hp = 183
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19495447
70 X = -5952640
30
Y = -1244937
29 feet Y = -445964
42 meter
Z = 10206353
63 Z = 3082003
11
XDOT = -7253
813310 XDOT = -2125
206370
YDOT = -18138
163577 feet/sec YDOT = -5552
757199 meter/sec
ZDOT = -16053
671081 ZDOT = -4903
691661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17943932
96 X = 5469310
77
Y = -7870876
41 feet Y = -2399043
13 meter
Z = 10092402
03 Z = 3076164
14
XDOT = 14113
610898 XDOT = 4301
828602
YDOT = 11518
990437 feet/sec YDOT = 3510
988285 meter/sec
ZDOT = -16095
411903 ZDOT = -4905
881548
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 09292
53803233
00001200 00000-0 20000-3 0 9032
2 25544 51
6440 28
2851 0007516 219
4754 140
5863 15
75040154 25544
Satellite: ISS
Catalog Number: 25544
Epoch time: 09292
53803233 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 28
2851 deg
Eccentricity:
0007516
Arg of perigee: 219
4754 deg
Mean anomaly: 140
5863 deg
Mean motion: 15
75040154 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2554
Checksum: 278
Coasting Arc #5 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2009/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1926576
72 A = 6720271
36 meter
Y = 4634096
10 meter E =
0009307
Z = 4471486
35 I = 51
76548
XDOT = -6995
395447 Wp = 160
77217
YDOT = -200
550701 meter/sec RA = 22
83762 deg
ZDOT = 3211
364619 TA = 257
10511
MA = 257
20909
Ha = 188
287 n
mi
Hp = 183
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6320789
78 X = 1852891
95
Y = 15203727
35 feet Y = 4655228
25 meter
Z = 14670230
81 Z = 4480666
92
XDOT = -22950
772464 XDOT = -7008
233628
YDOT = -657
974741 feet/sec YDOT = -278
849092 meter/sec
ZDOT = 10535
973159 ZDOT = 3177
348794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12700018
62 X = -3870965
68
Y = -10428176
22 feet Y = -3178508
11 meter
Z = 14706598
81 Z = 4482571
32
XDOT = 19810
709565 XDOT = 6038
304275
YDOT = -9408
675566 feet/sec YDOT = -2867
764313 meter/sec
ZDOT = 10401
829611 ZDOT = 3170
477666
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 09293
55317063
00001200 00000-0 20000-3 0 9047
2 25544 51
6444 23
0635 0007504 224
5560 135
5001 15
75112733 25709
Satellite: ISS
Catalog Number: 25544
Epoch time: 09293
55317063 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 23
0635 deg
Eccentricity:
0007504
Arg of perigee: 224
5560 deg
Mean anomaly: 135
5001 deg
Mean motion: 15
75112733 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2570
Checksum: 258
Coasting Arc #6 (Orbit 2584)
---------------------------------------
Vector Time (GMT): 2009/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6257163
80 A = 6726492
90 meter
Y = -49657
29 meter E =
0001923
Z = -2468409
13 I = 51
75765
XDOT = 2150
587237 Wp = 235
86096
YDOT = 5105
277871 meter/sec RA = 17
65868 deg
ZDOT = 5344
804743 TA = 96
28454
MA = 96
26264
Ha = 188
076 n
mi
Hp = 184
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20528752
63 X = 6269245
43
Y = -162917
63 feet Y = 20381
57 meter
Z = -8098455
14 Z = -2437981
65
XDOT = 7055
732405 XDOT = 2067
374497
YDOT = 16749
599314 feet/sec YDOT = 5128
861685 meter/sec
ZDOT = 17535
448631 ZDOT = 5355
050499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17864059
05 X = -5444965
20
Y = 10210808
93 feet Y = 3112254
56 meter
Z = -7978469
61 Z = -2431837
54
XDOT = -13515
760440 XDOT = -4119
603782
YDOT = -9902
252206 feet/sec YDOT = -3018
206472 meter/sec
ZDOT = 17576
027489 ZDOT = 5357
173179
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 09294
50484719
00001200 00000-0 20000-3 0 9057
2 25544 51
6441 18
1694 0007383 229
7813 130
2706 15
75092195 25858
Satellite: ISS
Catalog Number: 25544
Epoch time: 09294
50484719 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 18
1694 deg
Eccentricity:
0007383
Arg of perigee: 229
7813 deg
Mean anomaly: 130
2706 deg
Mean motion: 15
75092195 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2585
Checksum: 307
Coasting Arc #7 (Orbit 2600)
---------------------------------------
Vector Time (GMT): 2009/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1786805
38 A = 6718732
63 meter
Y = -4311886
77 meter E =
0005762
Z = -4837423
20 I = 51
70228
XDOT = 7303
769251 Wp = 98
03738
YDOT = -324
092212 meter/sec RA = 12
56175 deg
ZDOT = -2412
147102 TA = 148
44934
MA = 148
41477
Ha = 187
854 n
mi
Hp = 184
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5862222
37 X = -1714956
43
Y = -14146610
14 feet Y = -4331466
06 meter
Z = -15870811
04 Z = -4845929
27
XDOT = 23962
497544 XDOT = 7318
568518
YDOT = -1063
294659 feet/sec YDOT = -242
334365 meter/sec
ZDOT = -7913
868446 ZDOT = -2376
628616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12116097
35 X = 3692986
47
Y = 9307092
75 feet Y = 2836801
87 meter
Z = -15904498
80 Z = -4847691
23
XDOT = -19517
269033 XDOT = -5948
863601
YDOT = 12141
552069 feet/sec YDOT = 3700
745071 meter/sec
ZDOT = -7773
814107 ZDOT = -2369
458540
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 09295
51994903
00001200 00000-0 20000-3 0 9061
2 25544 51
6433 12
9483 0007371 233
1734 126
8755 15
75129969 26019
Satellite: ISS
Catalog Number: 25544
Epoch time: 09295
51994903 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 12
9483 deg
Eccentricity:
0007371
Arg of perigee: 233
1734 deg
Mean anomaly: 126
8755 deg
Mean motion: 15
75129969 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2601
Checksum: 312
Coasting Arc #8 (Orbit 2616)
---------------------------------------
Vector Time (GMT): 2009/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6471278
53 A = 6727566
93 meter
Y = 537581
58 meter E =
0012026
Z = 1728794
61 I = 51
70278
XDOT = -1927
449524 Wp = 145
63649
YDOT = -4799
154119 meter/sec RA = 7
38743 deg
ZDOT = -5713
106660 TA = 15
22738
MA = 15
19122
Ha = 187
608 n
mi
Hp = 184
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21231228
76 X = -6485207
23
Y = 1763719
08 feet Y = 465138
01 meter
Z = 5671898
34 Z = 1697322
70
XDOT = -6323
653293 XDOT = -1845
887504
YDOT = -15745
256296 feet/sec YDOT = -4820
251830 meter/sec
ZDOT = -18743
788254 ZDOT = -5722
272385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17259703
74 X = 5260757
70
Y = -12544747
16 feet Y = -3823638
94 meter
Z = 5547806
38 Z = 1690971
39
XDOT = 12569
487568 XDOT = 3831
179811
YDOT = 8974
390572 feet/sec YDOT = 2735
394246 meter/sec
ZDOT = -18780
091551 ZDOT = -5724
171905
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 09296
53503104
00001200 00000-0 20000-3 0 9074
2 25544 51
6433 7
7269 0007130 237
4806 122
5670 15
75184911 26177
Satellite: ISS
Catalog Number: 25544
Epoch time: 09296
53503104 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 7
7269 deg
Eccentricity:
0007130
Arg of perigee: 237
4806 deg
Mean anomaly: 122
5670 deg
Mean motion: 15
75184911 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2617
Checksum: 283
Coasting Arc #9 (Orbit 2632)
---------------------------------------
Vector Time (GMT): 2009/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1542549
62 A = 6717345
86 meter
Y = 4098657
31 meter E =
0006650
Z = 5097080
44 I = 51
63907
XDOT = -7491
618164 Wp = 202
12743
YDOT = 912
781335 meter/sec RA = 2
27344 deg
ZDOT = 1527
826687 TA = 233
18434
MA = 233
24536
Ha = 187
258 n
mi
Hp = 184
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5060858
34 X = 1471841
96
Y = 13447038
42 feet Y = 4115511
58 meter
Z = 16722704
86 Z = 5104402
59
XDOT = -24578
799751 XDOT = -7508
690277
YDOT = 2994
689420 feet/sec YDOT = 828
910166 meter/sec
ZDOT = 5012
554747 ZDOT = 1491
390336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11373823
32 X = -3466741
35
Y = -8723542
17 feet Y = -2658935
65 meter
Z = 16751714
60 Z = 5105922
61
XDOT = 18575
992780 XDOT = 5661
962599
YDOT = -14835
837587 feet/sec YDOT = -4521
963297 meter/sec
ZDOT = 4868
896144 ZDOT = 1484
039545
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 09297
55009227
00001200 00000-0 20000-3 0 9085
2 25544 51
6434 2
5047 0007209 241
9242 118
1193 15
75224285 26334
Satellite: ISS
Catalog Number: 25544
Epoch time: 09297
55009227 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 2
5047 deg
Eccentricity:
0007209
Arg of perigee: 241
9242 deg
Mean anomaly: 118
1193 deg
Mean motion: 15
75224285 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2633
Checksum: 281
Coasting Arc #10 (Orbit 2647)
---------------------------------------
Vector Time (GMT): 2009/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6577185
43 A = 6728439
41 meter
Y = -1059647
39 meter E =
0005250
Z = -917996
48 I = 51
64543
XDOT = 1575
642298 Wp = 358
80773
YDOT = 4632
066677 meter/sec RA = 357
10761 deg
ZDOT = 5946
762003 TA = 351
16752
MA = 351
17675
Ha = 186
996 n
mi
Hp = 184
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21578692
36 X = 6593005
28
Y = -3476533
43 feet Y = -986008
97 meter
Z = -3011799
47 Z = -886005
61
XDOT = 5169
430111 XDOT = 1494
839885
YDOT = 15197
069149 feet/sec YDOT = 4649
234616 meter/sec
ZDOT = 19510
374027 ZDOT = 5954
220342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16156753
98 X = -4924578
61
Y = 14745485
96 feet Y = 4494424
12 meter
Z = -2885676
53 Z = -879554
21
XDOT = -11483
428313 XDOT = -3500
148950
YDOT = -8761
589426 feet/sec YDOT = -2670
532457 meter/sec
ZDOT = 19539
939001 ZDOT = 5955
773407
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 09298
50169609
00001200 00000-0 20000-3 0 9093
2 25544 51
6427 357
6092 0006989 247
4111 112
6313 15
75194061 26487
Satellite: ISS
Catalog Number: 25544
Epoch time: 09298
50169609 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 357
6092 deg
Eccentricity:
0006989
Arg of perigee: 247
4111 deg
Mean anomaly: 112
6313 deg
Mean motion: 15
75194061 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2648
Checksum: 312
Coasting Arc #11 (Orbit 2663)
---------------------------------------
Vector Time (GMT): 2009/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1188972
01 A = 6716631
34 meter
Y = -4033652
22 meter E =
0008435
Z = -5244336
24 I = 51
57624
XDOT = 7528
715583 Wp = 98
56386
YDOT = -1503
921212 meter/sec RA = 351
97381 deg
ZDOT = -552
130861 TA = 166
19438
MA = 166
17130
Ha = 186
751 n
mi
Hp = 184
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3900826
80 X = -1118302
23
Y = -13233767
12 feet Y = -4046552
92 meter
Z = -17205827
54 Z = -5249940
65
XDOT = 24700
510444 XDOT = 7547
655328
YDOT = -4934
124710 feet/sec YDOT = -1419
624783 meter/sec
ZDOT = -1811
452955 ZDOT = -515
509807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10585737
56 X = 3226532
81
Y = 8804859
20 feet Y = 2683721
08 meter
Z = -17228063
10 Z = -5251113
63
XDOT = -17014
220491 XDOT = -5185
934406
YDOT = 17206
360731 feet/sec YDOT = 5244
498751 meter/sec
ZDOT = -1667
087037 ZDOT = -508
128129
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 09299
51672100
00001200 00000-0 20000-3 0 9102
2 25544 51
6427 352
3869 0006975 250
4179 109
6232 15
75246691 26645
Satellite: ISS
Catalog Number: 25544
Epoch time: 09299
51672100 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 352
3869 deg
Eccentricity:
0006975
Arg of perigee: 250
4179 deg
Mean anomaly: 109
6232 deg
Mean motion: 15
75246691 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2664
Checksum: 309
Coasting Arc #12 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2009/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6537749
82 A = 6728446
31 meter
Y = 1560321
79 meter E =
0010603
Z = 35995
01 I = 51
58776
XDOT = -1144
390256 Wp = 167
76915
YDOT = -4648
515261 meter/sec RA = 346
82000 deg
ZDOT = -6037
042034 TA = 11
83926
MA = 11
81435
Ha = 186
335 n
mi
Hp = 184
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21449310
44 X = -6554886
57
Y = 5119165
98 feet Y = 1487117
00 meter
Z = 118093
87 Z = 4192
46
XDOT = -3754
561207 XDOT = -1062
997377
YDOT = -15251
034320 feet/sec YDOT = -4660
857562 meter/sec
ZDOT = -19806
568354 ZDOT = -6042
403750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14573373
85 X = 4441964
35
Y = -16550209
87 feet Y = -5044503
97 meter
Z = -7264
94 Z = -2214
35
XDOT = 10560
020364 XDOT = 3218
694207
YDOT = 9300
065403 feet/sec YDOT = 2834
659935 meter/sec
ZDOT = -19827
869013 ZDOT = -6043
534475
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 09300
53172578
00001200 00000-0 20000-3 0 9112
2 25544 51
6433 347
1647 0006771 255
1788 104
8626 15
75313418 26804
Satellite: ISS
Catalog Number: 25544
Epoch time: 09300
53172578 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 347
1647 deg
Eccentricity:
0006771
Arg of perigee: 255
1788 deg
Mean anomaly: 104
8626 deg
Mean motion: 15
75313418 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2680
Checksum: 298
Coasting Arc #13 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2009/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 806714
75 A = 6716369
67 meter
Y = 4123578
80 meter E =
0004094
Z = 5243228
91 I = 51
51772
XDOT = -7406
059895 Wp = 265
87291
YDOT = 2054
806139 meter/sec RA = 341
66467 deg
ZDOT = -477
142840 TA = 188
66348
MA = 188
67055
Ha = 186
028 n
mi
Hp = 184
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2646701
93 X = 735073
10
Y = 13528801
84 feet Y = 4132199
59 meter
Z = 17202194
58 Z = 5246973
82
XDOT = -24298
096769 XDOT = -7426
168739
YDOT = 6741
489957 feet/sec YDOT = 1971
874757 meter/sec
ZDOT = -1565
429265 ZDOT = -513
171047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10044532
98 X = -3061573
65
Y = -9414229
62 feet Y = -2869457
19 meter
Z = 17217103
31 Z = 5247773
09
XDOT = 14932
951699 XDOT = 4551
563678
YDOT = -19051
708641 feet/sec YDOT = -5806
960794 meter/sec
ZDOT = -1707
429532 ZDOT = -520
424521
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 09301
54671103
00001200 00000-0 20000-3 0 9123
2 25544 51
6427 341
9427 0006761 258
9811 101
0592 15
75340886 26969
Satellite: ISS
Catalog Number: 25544
Epoch time: 09301
54671103 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 341
9427 deg
Eccentricity:
0006761
Arg of perigee: 258
9811 deg
Mean anomaly: 101
0592 deg
Mean motion: 15
75340886 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2696
Checksum: 294
Coasting Arc #14 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2009/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6357624
84 A = 6728062
42 meter
Y = -2001632
26 meter E =
0008612
Z = 876848
11 I = 51
52891
XDOT = 702
959749 Wp = 32
05395
YDOT = 4846
169912 meter/sec RA = 336
52356 deg
ZDOT = 5946
374447 TA = 337
53595
MA = 337
57363
Ha = 185
820 n
mi
Hp = 184
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20858349
20 X = 6375275
26
Y = -6567034
98 feet Y = -1930438
82 meter
Z = 2876798
27 Z = 907777
09
XDOT = 2306
298388 XDOT = 619
829750
YDOT = 15899
507586 feet/sec YDOT = 4853
566305 meter/sec
ZDOT = 19509
102518 ZDOT = 5949
587339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12635715
65 X = -3851366
13
Y = 17827484
83 feet Y = 5433817
38 meter
Z = 2998686
85 Z = 913999
75
XDOT = -10055
821755 XDOT = -3065
014471
YDOT = -10421
323128 feet/sec YDOT = -3176
419289 meter/sec
ZDOT = 19521
939316 ZDOT = 5950
287104
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 09302
56167948
00001200 00000-0 20000-3 0 9134
2 25544 51
6427 336
7199 0006558 264
8870 95
1545 15
75321807 27124
Satellite: ISS
Catalog Number: 25544
Epoch time: 09302
56167948 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 336
7199 deg
Eccentricity:
0006558
Arg of perigee: 264
8870 deg
Mean anomaly: 95
1545 deg
Mean motion: 15
75321807 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2712
Checksum: 320
Coasting Arc #15 (Orbit 2726)
---------------------------------------
Vector Time (GMT): 2009/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -434028
21 A = 6717024
53 meter
Y = -4376493
71 meter E =
0007478
Z = -5083592
16 I = 51
46580
XDOT = 7118
241413 Wp = 114
36821
YDOT = -2493
904476 meter/sec RA = 331
34574 deg
ZDOT = 1538
008247 TA = 170
43757
MA = 170
42333
Ha = 185
607 n
mi
Hp = 184
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1423977
06 X = -360361
42
Y = -14358575
16 feet Y = -4380935
63 meter
Z = -16678451
96 Z = -5085521
56
XDOT = 23353
810409 XDOT = 7138
128076
YDOT = -8182
101298 feet/sec YDOT = -2414
192832 meter/sec
ZDOT = 5045
958815 ZDOT = 1572
637992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9916295
93 X = 3022487
00
Y = 10469219
44 feet Y = 3191018
09 meter
Z = -16686211
98 Z = -5085957
41
XDOT = -12517
668491 XDOT = -3815
385356
YDOT = 20123
090702 feet/sec YDOT = 6133
518046 meter/sec
ZDOT = 5182
416660 ZDOT = 1579
600598
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 09303
51319116
00001200 00000-0 20000-3 0 9147
2 25544 51
6434 331
8237 0006678 267
6701 92
3699 15
75368868 27271
Satellite: ISS
Catalog Number: 25544
Epoch time: 09303
51319116 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 331
8237 deg
Eccentricity:
0006678
Arg of perigee: 267
6701 deg
Mean anomaly: 92
3699 deg
Mean motion: 15
75368868 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2727
Checksum: 320
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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