Date:
November 3rd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18535 45 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 2626)
---------------------------------------
Vector Time (GMT): 2009/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 150205
87 A = 6716960
71 meter
Y = -4560681
41 meter E =
0006862
Z = -4935191
49 I = 51
46915
XDOT = 7133
881231 Wp = 120
53489
YDOT = -2013
996978 meter/sec RA = 331
34239 deg
ZDOT = 2076
994299 TA = 169
64760
MA = 169
63346
Ha = 185
301 n
mi
Hp = 183
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 492801
43 X = 225167
94
Y = -14962865
53 feet Y = -4558582
84 meter
Z = -16191573
12 Z = -4934279
45
XDOT = 23405
122150 XDOT = 7145
781958
YDOT = -6607
601635 feet/sec YDOT = -1934
155066 meter/sec
ZDOT = 6814
285757 ZDOT = 2111
680602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8785009
74 X = 2677670
97
Y = 12127040
10 feet Y = 3696321
82 meter
Z = -16188135
80 Z = -4934143
79
XDOT = -13402
013626 XDOT = -4084
933753
YDOT = 18993
011194 feet/sec YDOT = 5789
069812 meter/sec
ZDOT = 6950
983314 ZDOT = 2118
659714
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
51224173
00016717 00000-0 10270-3 0 9007
2 25544 51
6446 331
8295 0006365 269
1559 90
8876 15
75622694 26278
Satellite: ISS
Catalog Number: 25544
Epoch time: 09303
51224173 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 331
8295 deg
Eccentricity:
0006365
Arg of perigee: 269
1559 deg
Mean anomaly: 90
8876 deg
Mean motion: 15
75622694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 329
Coasting Arc #2 (Orbit 2642)
---------------------------------------
Vector Time (GMT): 2009/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6039513
98 A = 6724928
00 meter
Y = 1797127
50 meter E =
0004221
Z = -2341201
22 I = 51
47038
XDOT = 461
799751 Wp = 211
15843
YDOT = -5477
428388 meter/sec RA = 326
22016 deg
ZDOT = -5395
044758 TA = 355
27856
MA = 355
28254
Ha = 185
252 n
mi
Hp = 183
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19814678
41 X = -6047787
41
Y = 5896087
59 feet Y = 1729543
73 meter
Z = -7681106
36 Z = -2370562
24
XDOT = 1515
091045 XDOT = 549
223943
YDOT = -17970
565578 feet/sec YDOT = -5471
775682 meter/sec
ZDOT = -17700
278078 ZDOT = -5392
588678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11607647
34 X = 3538010
91
Y = -17054530
48 feet Y = -5198220
89 meter
Z = -7796809
42 Z = -2376467
51
XDOT = 8848
203139 XDOT = 2696
932317
YDOT = 14111
080251 feet/sec YDOT = 4301
057261 meter/sec
ZDOT = -17690
784402 ZDOT = -5392
151086
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 09304
52700113
00016717 00000-0 10270-3 0 9013
2 25544 51
6440 326
6057 0006264 272
8450 87
1997 15
75683339 26433
Satellite: ISS
Catalog Number: 25544
Epoch time: 09304
52700113 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 326
6057 deg
Eccentricity:
0006264
Arg of perigee: 272
8450 deg
Mean anomaly: 87
1997 deg
Mean motion: 15
75683339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2643
Checksum: 310
Coasting Arc #3 (Orbit 2658)
---------------------------------------
Vector Time (GMT): 2009/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -619984
14 A = 6718718
03 meter
Y = 5029124
52 meter E =
0004842
Z = 4412051
21 I = 51
42439
XDOT = -6668
756329 Wp = 30
87286
YDOT = 2047
348574 meter/sec RA = 321
01296 deg
ZDOT = -3265
114664 TA = 91
99116
MA = 91
93571
Ha = 185
335 n
mi
Hp = 183
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2034068
71 X = -697608
30
Y = 16499752
35 feet Y = 5021757
57 meter
Z = 14475233
64 Z = 4408850
56
XDOT = -21879
121814 XDOT = -6675
292608
YDOT = 6717
022881 feet/sec YDOT = 1972
737989 meter/sec
ZDOT = -10712
318452 ZDOT = -3297
528521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9017098
41 X = -2748411
60
Y = -13979676
96 feet Y = -4261005
54 meter
Z = 14462787
43 Z = 4408257
61
XDOT = 11328
644929 XDOT = 3452
970974
YDOT = -18541
081646 feet/sec YDOT = -5651
321686 meter/sec
ZDOT = -10840
046402 ZDOT = -3304
046143
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 09305
54173028
00016717 00000-0 10270-3 0 9026
2 25544 51
6427 321
3813 0006213 277
7881 82
2578 15
75754603 26597
Satellite: ISS
Catalog Number: 25544
Epoch time: 09305
54173028 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 321
3813 deg
Eccentricity:
0006213
Arg of perigee: 277
7881 deg
Mean anomaly: 82
2578 deg
Mean motion: 15
75754603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2659
Checksum: 317
Coasting Arc #4 (Orbit 2674)
---------------------------------------
Vector Time (GMT): 2009/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5579566
14 A = 6722206
16 meter
Y = -1705209
61 meter E =
0006694
Z = 3331910
03 I = 51
41349
XDOT = -927
753988 Wp = 78
20107
YDOT = 6069
785829 meter/sec RA = 315
89769 deg
ZDOT = 4653
490515 TA = 321
17691
MA = 321
22498
Ha = 185
366 n
mi
Hp = 183
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18305663
19 X = 5582032
99
Y = -5594519
73 feet Y = -1642801
84 meter
Z = 10931463
37 Z = 3359022
54
XDOT = -3043
812297 XDOT = -1018
165079
YDOT = 19913
995503 feet/sec YDOT = 6058
905600 meter/sec
ZDOT = 15267
357333 ZDOT = 4648
763734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10061540
57 X = -3066757
57
Y = 16211543
99 feet Y = 4941278
61 meter
Z = 11038301
04 Z = 3364474
16
XDOT = -9555
546016 XDOT = -2912
530426
YDOT = -16327
836898 feet/sec YDOT = -4976
724686 meter/sec
ZDOT = 15248
926932 ZDOT = 4647
872929
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 09306
55643084
00016717 00000-0 10270-3 0 9033
2 25544 51
6422 316
1567 0006175 282
1509 77
8963 15
75771691 26756
Satellite: ISS
Catalog Number: 25544
Epoch time: 09306
55643084 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 316
1567 deg
Eccentricity:
0006175
Arg of perigee: 282
1509 deg
Mean anomaly: 77
8963 deg
Mean motion: 15
75771691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2675
Checksum: 333
Coasting Arc #5 (Orbit 2689)
---------------------------------------
Vector Time (GMT): 2009/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 953516
77 A = 6721267
32 meter
Y = -5568643
33 meter E =
0000873
Z = -3639890
16 I = 51
39022
XDOT = 6106
613377 Wp = 330
05854
YDOT = -1789
815787 meter/sec RA = 310
67982 deg
ZDOT = 4338
232955 TA = 346
06586
MA = 346
06827
Ha = 185
635 n
mi
Hp = 183
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3128335
86 X = 1033398
01
Y = -18269827
21 feet Y = -5557533
78 meter
Z = -11941896
87 Z = -3635063
97
XDOT = 20034
820792 XDOT = 6105
098430
YDOT = -5872
099039 feet/sec YDOT = -1721
536656 meter/sec
ZDOT = 14233
047754 ZDOT = 4367
896218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9878747
48 X = 3011042
23
Y = 15698187
62 feet Y = 4784807
59 meter
Z = -11923054
39 Z = -3634146
98
XDOT = -9718
826101 XDOT = -2962
298196
YDOT = 17014
273496 feet/sec YDOT = 5185
950562 meter/sec
ZDOT = 14349
941571 ZDOT = 4373
862191
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 09307
50768388
00016717 00000-0 10270-3 0 9045
2 25544 51
6427 311
2589 0006199 286
2672 73
7810 15
75811439 26901
Satellite: ISS
Catalog Number: 25544
Epoch time: 09307
50768388 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 311
2589 deg
Eccentricity:
0006199
Arg of perigee: 286
2672 deg
Mean anomaly: 73
7810 deg
Mean motion: 15
75811439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2690
Checksum: 340
Coasting Arc #6 (Orbit 2705)
---------------------------------------
Vector Time (GMT): 2009/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5078641
05 A = 6719105
40 meter
Y = 1336240
98 meter E =
0005386
Z = -4196390
13 I = 51
36383
XDOT = 1229
430429 Wp = 21
50704
YDOT = -6685
877838 meter/sec RA = 305
56196 deg
ZDOT = -3613
389207 TA = 211
54469
MA = 211
57699
Ha = 185
752 n
mi
Hp = 183
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16662208
16 X = -5072819
68
Y = 4383992
70 feet Y = 1279481
42 meter
Z = -13767684
14 Z = -4221048
77
XDOT = 4033
564399 XDOT = 1321
655480
YDOT = -21935
294745 feet/sec YDOT = -6671
613748 meter/sec
ZDOT = -11854
951468 ZDOT = -3607
192814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9112906
71 X = 2777613
97
Y = -14529904
98 feet Y = -4428715
04 meter
Z = -13864865
38 Z = -4226010
97
XDOT = 10931
487647 XDOT = 3331
917435
YDOT = 18156
091779 feet/sec YDOT = 5533
976774 meter/sec
ZDOT = -11830
740669 ZDOT = -3606
009756
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 09308
52232505
00016717 00000-0 10270-3 0 9056
2 25544 51
6416 306
0332 0006182 289
9277 70
1221 15
75861696 27065
Satellite: ISS
Catalog Number: 25544
Epoch time: 09308
52232505 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 306
0332 deg
Eccentricity:
0006182
Arg of perigee: 289
9277 deg
Mean anomaly: 70
1221 deg
Mean motion: 15
75861696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2706
Checksum: 305
Coasting Arc #7 (Orbit 2721)
---------------------------------------
Vector Time (GMT): 2009/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1146842
09 A = 6723705
01 meter
Y = 6086823
98 meter E =
0007727
Z = 2608801
40 I = 51
36336
XDOT = -5536
429170 Wp = 92
82172
YDOT = 1199
401550 meter/sec RA = 300
34439 deg
ZDOT = -5219
361179 TA = 57
38120
MA = 57
30664
Ha = 185
894 n
mi
Hp = 182
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3762605
29 X = -1227494
23
Y = 19969894
94 feet Y = 6073548
16 meter
Z = 8559059
71 Z = 2603034
44
XDOT = -18164
137697 XDOT = -5524
074168
YDOT = 3935
044457 feet/sec YDOT = 1137
559418 meter/sec
ZDOT = -17123
888383 ZDOT = -5246
227817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11154115
53 X = -3399774
41
Y = -16997791
63 feet Y = -5180926
89 meter
Z = 8536521
08 Z = 2601931
62
XDOT = 8999
304769 XDOT = 2742
988094
YDOT = -14579
790274 feet/sec YDOT = -4443
920075 meter/sec
ZDOT = -17229
785865 ZDOT = -5251
638732
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 09309
53693468
00016717 00000-0 10270-3 0 9068
2 25544 51
6414 300
8079 0006292 295
0611 64
9900 15
75942438 27222
Satellite: ISS
Catalog Number: 25544
Epoch time: 09309
53693468 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 300
8079 deg
Eccentricity:
0006292
Arg of perigee: 295
0611 deg
Mean anomaly: 64
9900 deg
Mean motion: 15
75942438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2722
Checksum: 324
Coasting Arc #8 (Orbit 2737)
---------------------------------------
Vector Time (GMT): 2009/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4604888
83 A = 6716262
32 meter
Y = -682833
84 meter E =
0000582
Z = 4841275
62 I = 51
32402
XDOT = -1357
645728 Wp = 168
77424
YDOT = 7222
898172 meter/sec RA = 295
21400 deg
ZDOT = 2309
493851 TA = 258
64052
MA = 258
64706
Ha = 185
887 n
mi
Hp = 182
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15107902
99 X = 4588663
57
Y = -2240268
49 feet Y = -631430
37 meter
Z = 15883450
21 Z = 4863607
22
XDOT = -4454
218268 XDOT = -1449
531887
YDOT = 23697
172480 feet/sec YDOT = 7207
202228 meter/sec
ZDOT = 7577
079563 ZDOT = 2302
675646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9018888
47 X = -2748957
20
Y = 12211581
88 feet Y = 3722090
16 meter
Z = 15971488
50 Z = 4868109
70
XDOT = -12708
619189 XDOT = -3873
587129
YDOT = -19263
766527 feet/sec YDOT = -5871
596037 meter/sec
ZDOT = 7550
434815 ZDOT = 2301
372532
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 09310
55151473
00016717 00000-0 10270-3 0 9078
2 25544 51
6410 295
5827 0006300 298
3725 61
6804 15
75961486 27389
Satellite: ISS
Catalog Number: 25544
Epoch time: 09310
55151473 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 295
5827 deg
Eccentricity:
0006300
Arg of perigee: 298
3725 deg
Mean anomaly: 61
6804 deg
Mean motion: 15
75961486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2738
Checksum: 321
Coasting Arc #9 (Orbit 2752)
---------------------------------------
Vector Time (GMT): 2009/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1184525
33 A = 6725600
00 meter
Y = -6469036
22 meter E =
0010221
Z = -1375959
66 I = 51
34426
XDOT = 5055
739932 Wp =
68553
YDOT = -307
288369 meter/sec RA = 290
01022 deg
ZDOT = 5807
572809 TA = 344
11145
MA = 344
14349
Ha = 186
042 n
mi
Hp = 182
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3886237
96 X = 1263459
46
Y = -21223872
11 feet Y = -6455348
71 meter
Z = -4514303
33 Z = -1370013
86
XDOT = 16587
073269 XDOT = 5030
587695
YDOT = -1008
163940 feet/sec YDOT = -250
893158 meter/sec
ZDOT = 19053
716565 ZDOT = 5832
072908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12565573
59 X = 3829986
83
Y = 17546256
16 feet Y = 5348098
88 meter
Z = -4491078
09 Z = -1368880
60
XDOT = -9428
802383 XDOT = -2873
898966
YDOT = 11645
111828 feet/sec YDOT = 3549
430085 meter/sec
ZDOT = 19150
324951 ZDOT = 5837
019045
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 09311
50265426
00016717 00000-0 10270-3 0 9089
2 25544 51
6408 290
6843 0006084 302
2682 57
7892 15
76025384 27535
Satellite: ISS
Catalog Number: 25544
Epoch time: 09311
50265426 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 290
6843 deg
Eccentricity:
0006084
Arg of perigee: 302
2682 deg
Mean anomaly: 57
7892 deg
Mean motion: 15
76025384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2753
Checksum: 318
Coasting Arc #10 (Orbit 2768)
---------------------------------------
Vector Time (GMT): 2009/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4254248
59 A = 6714466
26 meter
Y = -209796
82 meter E =
0011001
Z = -5199425
86 I = 51
29793
XDOT = 1343
488911 Wp = 61
37882
YDOT = -7537
355742 meter/sec RA = 284
85592 deg
ZDOT = -791
198727 TA = 201
02964
MA = 201
07491
Ha = 186
181 n
mi
Hp = 182
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13957508
49 X = -4226328
19
Y = -688309
77 feet Y = -257213
95 meter
Z = -17058483
78 Z = -5220025
48
XDOT = 4407
772018 XDOT = 1431
516638
YDOT = -24728
857420 feet/sec YDOT = -7521
839826 meter/sec
ZDOT = -2595
796349 ZDOT = -784
458540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9948012
46 X = 3032154
20
Y = -9671828
87 feet Y = -2947973
44 meter
Z = -17139733
28 Z = -5224190
70
XDOT = 14377
430132 XDOT = 4382
240704
YDOT = 19364
193349 feet/sec YDOT = 5902
206133 meter/sec
ZDOT = -2569
483334 ZDOT = -783
178520
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 09312
51717276
00016717 00000-0 10270-3 0 9097
2 25544 51
6409 285
4581 0006217 306
4747 53
5844 15
76049882 27690
Satellite: ISS
Catalog Number: 25544
Epoch time: 09312
51717276 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 285
4581 deg
Eccentricity:
0006217
Arg of perigee: 306
4747 deg
Mean anomaly: 53
5844 deg
Mean motion: 15
76049882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2769
Checksum: 341
Coasting Arc #11 (Orbit 2784)
---------------------------------------
Vector Time (GMT): 2009/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1150019
59 A = 6726151
45 meter
Y = 6623994
45 meter E =
0005927
Z = -25565
59 I = 51
33171
XDOT = -4737
747970 Wp = 139
50073
YDOT = -842
723964 meter/sec RA = 279
67483 deg
ZDOT = -6013
162076 TA = 40
77832
MA = 40
73398
Ha = 186
324 n
mi
Hp = 182
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3773030
14 X = -1223880
58
Y = 21732265
26 feet Y = 6610721
28 meter
Z = -83876
60 Z = -31331
68
XDOT = -15543
792551 XDOT = -4698
761123
YDOT = -2764
842402 feet/sec YDOT = -895
486100 meter/sec
ZDOT = -19728
222033 ZDOT = -6036
083681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13633250
45 X = -4155414
74
Y = -17339472
67 feet Y = -5285071
27 meter
Z = -106371
83 Z = -32422
13
XDOT = 11110
026325 XDOT = 3386
336024
YDOT = -8626
171801 feet/sec YDOT = -2629
257165 meter/sec
ZDOT = -19818
657060 ZDOT = -6040
726672
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 09313
53165875
00016717 00000-0 10270-3 0 9104
2 25544 51
6411 280
2323 0006323 310
8391 49
2225 15
76118517 27857
Satellite: ISS
Catalog Number: 25544
Epoch time: 09313
53165875 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 280
2323 deg
Eccentricity:
0006323
Arg of perigee: 310
8391 deg
Mean anomaly: 49
2225 deg
Mean motion: 15
76118517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2785
Checksum: 295
Coasting Arc #12 (Orbit 2800)
---------------------------------------
Vector Time (GMT): 2009/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4068287
23 A = 6714222
26 meter
Y = 1287414
25 meter E =
0006322
Z = 5186050
99 I = 51
28782
XDOT = -1284
316092 Wp = 344
71675
YDOT = 7546
356876 meter/sec RA = 274
49200 deg
ZDOT = -860
062868 TA = 113
54314
MA = 113
47671
Ha = 186
318 n
mi
Hp = 181
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13347399
04 X = 4028395
50
Y = 4223800
02 feet Y = 1332685
16 meter
Z = 17014602
98 Z = 5205718
13
XDOT = -4213
635471 XDOT = -1364
427224
YDOT = 24758
388700 feet/sec YDOT = 7531
546976 meter/sec
ZDOT = -2821
728569 ZDOT = -866
496715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11878077
97 X = -3620438
16
Y = 7228930
48 feet Y = 2203378
01 meter
Z = 17092223
09 Z = 5209709
60
XDOT = -15407
986310 XDOT = -4696
354227
YDOT = -18541
619579 feet/sec YDOT = -5651
485648 meter/sec
ZDOT = -2846
813214 ZDOT = -867
708668
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 09314
54611323
00016717 00000-0 10270-3 0 9111
2 25544 51
6410 275
0065 0006305 314
2377 45
8269 15
76150984 28016
Satellite: ISS
Catalog Number: 25544
Epoch time: 09314
54611323 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 275
0065 deg
Eccentricity:
0006305
Arg of perigee: 314
2377 deg
Mean anomaly: 45
8269 deg
Mean motion: 15
76150984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2801
Checksum: 291
Coasting Arc #13 (Orbit 2816)
---------------------------------------
Vector Time (GMT): 2009/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1103720
84 A = 6724893
34 meter
Y = -6459154
68 meter E =
0013889
Z = 1472056
60 I = 51
32345
XDOT = 4647
867809 Wp = 35
80952
YDOT = 2114
158238 meter/sec RA = 269
33733 deg
ZDOT = 5775
422374 TA = 340
49591
MA = 340
54900
Ha = 186
334 n
mi
Hp = 181
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3621131
36 X = 1168715
08
Y = -21191452
37 feet Y = -6446448
81 meter
Z = 4829582
03 Z = 1477576
50
XDOT = 15248
910135 XDOT = 4595
824997
YDOT = 6936
214692 feet/sec YDOT = 2165
842491 meter/sec
ZDOT = 18948
236134 ZDOT = 5797
875708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13922759
51 X = 4243657
10
Y = 16374942
30 feet Y = 4991082
41 meter
Z = 4851096
88 Z = 1478614
33
XDOT = -13850
712496 XDOT = -4221
697169
YDOT = 6121
077272 feet/sec YDOT = 1865
704353 meter/sec
ZDOT = 19036
881433 ZDOT = 5802
441461
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 09315
56053354
00016717 00000-0 10270-3 0 9129
2 25544 51
6410 269
7800 0006232 317
2767 42
7912 15
76229184 28175
Satellite: ISS
Catalog Number: 25544
Epoch time: 09315
56053354 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 269
7800 deg
Eccentricity:
0006232
Arg of perigee: 317
2767 deg
Mean anomaly: 42
7912 deg
Mean motion: 15
76229184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2817
Checksum: 308
Coasting Arc #14 (Orbit 2831)
---------------------------------------
Vector Time (GMT): 2009/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4086645
75 A = 6715770
54 meter
Y = -2392442
25 meter E =
0007357
Z = -4767756
00 I = 51
29492
XDOT = 1279
873036 Wp = 79
62922
YDOT = -7167
466144 meter/sec RA = 264
12690 deg
ZDOT = 2504
153964 TA = 214
97755
MA = 215
02590
Ha = 186
451 n
mi
Hp = 181
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13407630
40 X = -4036427
86
Y = -7849219
99 feet Y = -2437860
79 meter
Z = -15642244
09 Z = -4787487
39
XDOT = 4199
058516 XDOT = 1347
760753
YDOT = -23515
308872 feet/sec YDOT = -7152
774251 meter/sec
ZDOT = 8215
728227 ZDOT = 2510
536686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14482059
79 X = 4414131
82
Y = -5403784
05 feet Y = -1647073
38 meter
Z = -15720167
61 Z = -4791507
09
XDOT = 15262
370267 XDOT = 4651
970457
YDOT = 16973
616836 feet/sec YDOT = 5173
558411 meter/sec
ZDOT = 8240
612988 ZDOT = 2511
738839
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 09316
51152467
00016717 00000-0 10270-3 0 9131
2 25544 51
6414 264
8800 0006353 321
3356 38
7353 15
76250847 28320
Satellite: ISS
Catalog Number: 25544
Epoch time: 09316
51152467 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 264
8800 deg
Eccentricity:
0006353
Arg of perigee: 321
3356 deg
Mean anomaly: 38
7353 deg
Mean motion: 15
76250847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2832
Checksum: 305
Coasting Arc #15 (Orbit 2847)
---------------------------------------
Vector Time (GMT): 2009/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1183214
67 A = 6721969
46 meter
Y = 5963082
53 meter E =
0003295
Z = -2872937
70 I = 51
32154
XDOT = -4756
598558 Wp = 9
36776
YDOT = -3368
019397 meter/sec RA = 258
99391 deg
ZDOT = -5029
280845 TA = 203
81494
MA = 203
83019
Ha = 186
589 n
mi
Hp = 181
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3881937
88 X = -1235850
35
Y = 19563919
05 feet Y = 5949556
83 meter
Z = -9425648
62 Z = -2878813
75
XDOT = -15605
638314 XDOT = -4694
151226
YDOT = -11049
932404 feet/sec YDOT = -3420
861303 meter/sec
ZDOT = -16500
265240 ZDOT = -5052
237379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13051636
25 X = -3978138
73
Y = -15067790
44 feet Y = -4592662
53 meter
Z = -9448582
15 Z = -2879927
84
XDOT = 17160
392365 XDOT = 5230
487593
YDOT = -4455
600904 feet/sec YDOT = -1358
067156 meter/sec
ZDOT = -16590
952320 ZDOT = -5056
922267
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 09317
52588282
00016717 00000-0 10270-3 0 9142
2 25544 51
6422 259
6530 0006367 325
4580 34
6170 15
76319021 28489
Satellite: ISS
Catalog Number: 25544
Epoch time: 09317
52588282 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 259
6530 deg
Eccentricity:
0006367
Arg of perigee: 325
4580 deg
Mean anomaly: 34
6170 deg
Mean motion: 15
76319021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2848
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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