Date:
March 9th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20989 63 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 714)
---------------------------------------
Vector Time (GMT): 2010/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3538470
99 A = 6731290
76 meter
Y = 5350909
38 meter E =
0019407
Z = 2000265
91 I = 51
88616
XDOT = -5126
245037 Wp = 49
53740
YDOT = 1283
412060 meter/sec RA = 42
36518 deg
ZDOT = 5612
059819 TA = 332
69352
MA = 332
79541
Ha = 192
405 n
mi
Hp = 183
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11609156
78 X = 3468656
32
Y = 17555476
98 feet Y = 5390088
41 meter
Z = 6562552
19 Z = 2017285
83
XDOT = -16818
389230 XDOT = -5167
477560
YDOT = 4210
669489 feet/sec YDOT = 1225
857079 meter/sec
ZDOT = 18412
269746 ZDOT = 5587
056488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5704649
21 X = 1738777
08
Y = 20236865
79 feet Y = 6168196
69 meter
Z = 6630280
91 Z = 2020909
62
XDOT = -15930
778484 XDOT = -4855
701282
YDOT = -1533
646841 feet/sec YDOT = -467
455557 meter/sec
ZDOT = 18312
977224 ZDOT = 5581
795458
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 10064
55953376
00016717 00000-0 10270-3 0 9001
2 25544 51
6442 42
6164 0007589 13
1385 346
9974 15
73689781 7157
Satellite: ISS
Catalog Number: 25544
Epoch time: 10064
55953376 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 42
6164 deg
Eccentricity:
0007589
Arg of perigee: 13
1385 deg
Mean anomaly: 346
9974 deg
Mean motion: 15
73689781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 332
Coasting Arc #2 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2010/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4282605
51 A = 6722697
56 meter
Y = -1617277
15 meter E =
0014779
Z = -4934025
76 I = 51
83384
XDOT = 4667
925050 Wp = 73
87764
YDOT = 5706
538127 meter/sec RA = 37
21201 deg
ZDOT = 2190
555086 TA = 217
31011
MA = 217
41285
Ha = 192
673 n
mi
Hp = 183
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14050543
02 X = 4324340
28
Y = -5306027
39 feet Y = -1569153
32 meter
Z = -16187748
55 Z = -4913119
63
XDOT = 15314
714732 XDOT = 4593
125373
YDOT = 18722
237951 feet/sec YDOT = 5758
319482 meter/sec
ZDOT = 7186
860519 ZDOT = 2213
049776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15072975
86 X = 4594243
04
Y = -1028474
63 feet Y = -313479
07 meter
Z = -16104736
19 Z = -4908723
59
XDOT = 9188
862879 XDOT = 2800
765405
YDOT = 21215
642113 feet/sec YDOT = 6466
527716 meter/sec
ZDOT = 7276
337678 ZDOT = 2217
827724
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 10065
51208237
00016717 00000-0 10270-3 0 9018
2 25544 51
6444 37
7273 0007834 16
5794 343
5623 15
73656771 7303
Satellite: ISS
Catalog Number: 25544
Epoch time: 10065
51208237 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 37
7273 deg
Eccentricity:
0007834
Arg of perigee: 16
5794 deg
Mean anomaly: 343
5623 deg
Mean motion: 15
73656771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 730
Checksum: 305
Coasting Arc #3 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2010/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4567097
43 A = 6731432
16 meter
Y = -4588506
69 meter E =
0007407
Z = -1854252
48 I = 51
83996
XDOT = 4645
267125 Wp = 75
11438
YDOT = -2340
609214 meter/sec RA = 32
12739 deg
ZDOT = -5666
316637 TA = 125
38406
MA = 125
31484
Ha = 192
634 n
mi
Hp = 182
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14983915
45 X = -4506440
98
Y = -15054155
81 feet Y = -4639239
58 meter
Z = -6083505
50 Z = -1876291
71
XDOT = 15240
377707 XDOT = 4698
620581
YDOT = -7679
164088 feet/sec YDOT = -2288
364901 meter/sec
ZDOT = -18590
277681 ZDOT = -5643
620567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10325048
23 X = -3147074
70
Y = -18532800
64 feet Y = -5648797
63 meter
Z = -6171146
41 Z = -1880965
43
XDOT = 15501
934850 XDOT = 4724
989742
YDOT = -2494
379960 feet/sec YDOT = -760
287012 meter/sec
ZDOT = -18500
166592 ZDOT = -5638
850777
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 10066
52811156
00016717 00000-0 10270-3 0 9021
2 25544 51
6450 32
5121 0007904 20
1449 340
0024 15
73719172 7460
Satellite: ISS
Catalog Number: 25544
Epoch time: 10066
52811156 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 32
5121 deg
Eccentricity:
0007904
Arg of perigee: 20
1449 deg
Mean anomaly: 340
0024 deg
Mean motion: 15
73719172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 746
Checksum: 265
Coasting Arc #4 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2010/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3800393
49 A = 6722260
26 meter
Y = 2455152
33 meter E =
0013403
Z = 4968011
10 I = 51
78297
XDOT = -5734
879842 Wp = 37
43359
YDOT = -4721
422964 meter/sec RA = 26
97307 deg
ZDOT = -2040
435039 TA = 72
34143
MA = 72
19512
Ha = 192
759 n
mi
Hp = 182
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12468482
57 X = -3851698
29
Y = 8054961
73 feet Y = 2412367
34 meter
Z = 16299249
02 Z = 4949424
42
XDOT = -18815
222578 XDOT = -5671
745918
YDOT = -15490
232821 feet/sec YDOT = -4785
200845 meter/sec
ZDOT = -6694
340680 ZDOT = -2068
141163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14195998
04 X = -4326940
20
Y = 4606409
83 feet Y = 1404033
71 meter
Z = 16225461
87 Z = 4945520
78
XDOT = -13898
394399 XDOT = -4236
230613
YDOT = -18709
626008 feet/sec YDOT = -5702
694007 meter/sec
ZDOT = -6804
494008 ZDOT = -2074
009774
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 10067
54411960
00016717 00000-0 10270-3 0 9034
2 25544 51
6451 27
2974 0007852 23
6292 336
5231 15
73742358 7624
Satellite: ISS
Catalog Number: 25544
Epoch time: 10067
54411960 = yrday
fracday
Element set: 903
Inclination: 51
6451 deg
RA of node: 27
2974 deg
Eccentricity:
0007852
Arg of perigee: 23
6292 deg
Mean anomaly: 336
5231 deg
Mean motion: 15
73742358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 302
Coasting Arc #5 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2010/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5398513
51 A = 6731460
57 meter
Y = 3617972
86 meter E =
0020833
Z = 1708704
40 I = 51
78739
XDOT = -4003
522977 Wp = 51
37550
YDOT = 3252
256878 meter/sec RA = 21
88270 deg
ZDOT = 5728
684481 TA = 327
50732
MA = 327
63539
Ha = 192
611 n
mi
Hp = 182
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17711658
49 X = 5349355
05
Y = 11869989
70 feet Y = 3678067
44 meter
Z = 5605985
56 Z = 1734810
34
XDOT = -13134
917904 XDOT = -4067
421112
YDOT = 10670
134113 feet/sec YDOT = 3207
130021 meter/sec
ZDOT = 18794
896592 ZDOT = 5709
080437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14363471
90 X = 4377986
23
Y = 15719919
93 feet Y = 4791431
59 meter
Z = 5709760
82 Z = 1740335
10
XDOT = -14249
558237 XDOT = -4343
265351
YDOT = 6181
977361 feet/sec YDOT = 1884
266700 meter/sec
ZDOT = 18717
081924 ZDOT = 5704
966570
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 10068
56010487
00016717 00000-0 10270-3 0 9047
2 25544 51
6453 22
0823 0007780 27
5836 332
5739 15
73791987 7787
Satellite: ISS
Catalog Number: 25544
Epoch time: 10068
56010487 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 22
0823 deg
Eccentricity:
0007780
Arg of perigee: 27
5836 deg
Mean anomaly: 332
5739 deg
Mean motion: 15
73791987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 328
Coasting Arc #6 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2010/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3169613
89 A = 6721901
63 meter
Y = -3179766
31 meter E =
0017002
Z = -5015852
86 I = 51
72718
XDOT = 6554
259502 Wp = 77
69374
YDOT = 3540
168276 meter/sec RA = 16
72556 deg
ZDOT = 1906
458698 TA = 210
66644
MA = 210
76592
Ha = 192
718 n
mi
Hp = 182
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10398995
69 X = 3229300
60
Y = -10432304
18 feet Y = -3143988
32 meter
Z = -16456210
16 Z = -5000310
08
XDOT = 21503
476058 XDOT = 6504
924553
YDOT = 11614
725316 feet/sec YDOT = 3613
186143 meter/sec
ZDOT = 6254
785756 ZDOT = 1938
178595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12534699
16 X = 3820576
30
Y = -7866365
62 feet Y = -2397668
24 meter
Z = -16394527
86 Z = -4997052
09
XDOT = 17809
331851 XDOT = 5428
284348
YDOT = 15141
334494 feet/sec YDOT = 4615
078754 meter/sec
ZDOT = 6380
861126 ZDOT = 1944
886471
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 10069
51257202
00016717 00000-0 10270-3 0 9052
2 25544 51
6458 17
1928 0007852 30
4003 329
7614 15
73805028 7931
Satellite: ISS
Catalog Number: 25544
Epoch time: 10069
51257202 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 17
1928 deg
Eccentricity:
0007852
Arg of perigee: 30
4003 deg
Mean anomaly: 329
7614 deg
Mean motion: 15
73805028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 297
Coasting Arc #7 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2010/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6003460
72 A = 6731357
67 meter
Y = -2564470
78 meter E =
0009156
Z = -1650071
50 I = 51
73126
XDOT = 3258
306751 Wp = 87
23338
YDOT = -3952
024647 meter/sec RA = 11
62904 deg
ZDOT = -5739
490348 TA = 110
95381
MA = 110
85581
Ha = 192
692 n
mi
Hp = 182
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19696393
45 X = -5966322
59
Y = -8413618
05 feet Y = -2631397
50 meter
Z = -5413620
41 Z = -1679145
28
XDOT = 10689
982779 XDOT = 3330
137615
YDOT = -12965
960129 feet/sec YDOT = -3915
187070 meter/sec
ZDOT = -18830
348911 ZDOT = -5723
487121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17542798
03 X = -5347044
84
Y = -12236124
61 feet Y = -3729570
78 meter
Z = -5529164
61 Z = -1685289
37
XDOT = 12318
991669 XDOT = 3754
828661
YDOT = -9220
357719 feet/sec YDOT = -2810
365033 meter/sec
ZDOT = -18766
854411 ZDOT = -5720
137225
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 10070
52851498
00016717 00000-0 10270-3 0 9063
2 25544 51
6466 11
9773 0007870 34
1819 325
9849 15
73851463 8096
Satellite: ISS
Catalog Number: 25544
Epoch time: 10070
52851498 = yrday
fracday
Element set: 906
Inclination: 51
6466 deg
RA of node: 11
9773 deg
Eccentricity:
0007870
Arg of perigee: 34
1819 deg
Mean anomaly: 325
9849 deg
Mean motion: 15
73851463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 333
Coasting Arc #8 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2010/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2501102
34 A = 6721620
07 meter
Y = 3705800
68 meter E =
0013357
Z = 5013705
68 I = 51
66901
XDOT = -7122
302589 Wp = 44
68828
YDOT = -2282
487141 meter/sec RA = 6
46894 deg
ZDOT = -1853
612591 TA = 63
23840
MA = 63
10179
Ha = 192
783 n
mi
Hp = 181
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8205716
34 X = -2566710
53
Y = 12158138
71 feet Y = 3677465
44 meter
Z = 16449165
63 Z = 5001395
93
XDOT = -23367
134477 XDOT = -7087
245745
YDOT = -7488
474871 feet/sec YDOT = -2361
937100 meter/sec
ZDOT = -6081
406140 ZDOT = -1888
126648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10423657
55 X = -3177130
82
Y = 10397371
12 feet Y = 3169118
72 meter
Z = 16400341
59 Z = 4998824
12
XDOT = -20767
432200 XDOT = -6329
913334
YDOT = -10947
199798 feet/sec YDOT = -3336
706498 meter/sec
ZDOT = -6218
553301 ZDOT = -1895
415046
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 10071
54443566
00016717 00000-0 10270-3 0 9070
2 25544 51
6468 6
7624 0007845 37
9213 322
2502 15
73883119 8253
Satellite: ISS
Catalog Number: 25544
Epoch time: 10071
54443566 = yrday
fracday
Element set: 907
Inclination: 51
6468 deg
RA of node: 6
7624 deg
Eccentricity:
0007845
Arg of perigee: 37
9213 deg
Mean anomaly: 322
2502 deg
Mean motion: 15
73883119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 825
Checksum: 307
Coasting Arc #9 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2010/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6376226
59 A = 6731298
87 meter
Y = 1407205
66 meter E =
0021569
Z = 1587126
57 I = 51
67202
XDOT = -2438
508374 Wp = 55
10586
YDOT = 4499
841223 meter/sec RA = 1
36696 deg
ZDOT = 5764
034911 TA = 322
41646
MA = 322
56702
Ha = 192
687 n
mi
Hp = 181
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20919378
57 X = 6352307
24
Y = 4616816
48 feet Y = 1478374
83 meter
Z = 5207108
18 Z = 1618043
45
XDOT = -8000
355558 XDOT = -2516
645271
YDOT = 14763
258607 feet/sec YDOT = 4472
136049 meter/sec
ZDOT = 18910
875693 ZDOT = 5751
998637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19803404
39 X = 6036077
66
Y = 8091120
97 feet Y = 2466173
67 meter
Z = 5329944
27 Z = 1624567
01
XDOT = -9906
767595 XDOT = -3019
582763
YDOT = 11730
872396 feet/sec YDOT = 3575
569906 meter/sec
ZDOT = 18863
158165 ZDOT = 5749
490609
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 10072
56033394
00016717 00000-0 10270-3 0 9088
2 25544 51
6470 1
5465 0007844 41
4685 318
7072 15
73908512 8419
Satellite: ISS
Catalog Number: 25544
Epoch time: 10072
56033394 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 1
5465 deg
Eccentricity:
0007844
Arg of perigee: 41
4685 deg
Mean anomaly: 318
7072 deg
Mean motion: 15
73908512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 841
Checksum: 301
Coasting Arc #10 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2010/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1760400
92 A = 6721397
26 meter
Y = -4112364
12 meter E =
0018521
Z = -5031699
63 I = 51
60940
XDOT = 7408
185617 Wp = 82
24478
YDOT = 953
802811 meter/sec RA = 356
20219 deg
ZDOT = 1820
462596 TA = 205
29425
MA = 205
38505
Ha = 192
712 n
mi
Hp = 181
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5775593
57 X = 1830697
98
Y = -13492008
28 feet Y = -4092285
78 meter
Z = -16508200
87 Z = -5022976
53
XDOT = 24305
070921 XDOT = 7388
126090
YDOT = 3129
274314 feet/sec YDOT = 1036
533588 meter/sec
ZDOT = 5972
646311 ZDOT = 1856
402166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7862021
14 X = 2396344
04
Y = -12438660
86 feet Y = -3791303
83 meter
Z = -16473639
68 Z = -5021165
37
XDOT = 22601
083459 XDOT = 6888
810238
YDOT = 6221
622172 feet/sec YDOT = 1896
350438 meter/sec
ZDOT = 6115
417015 ZDOT = 1863
979106
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 10073
51271731
00016717 00000-0 10270-3 0 9094
2 25544 51
6477 356
6567 0007826 44
8470 315
3324 15
73946891 8563
Satellite: ISS
Catalog Number: 25544
Epoch time: 10073
51271731 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 356
6567 deg
Eccentricity:
0007826
Arg of perigee: 44
8470 deg
Mean anomaly: 315
3324 deg
Mean motion: 15
73946891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 331
Coasting Arc #11 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2010/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6528655
20 A = 6731036
16 meter
Y = -276955
74 meter E =
0010670
Z = -1620948
22 I = 51
61294
XDOT = 1623
169391 Wp = 95
48682
YDOT = -4857
853679 meter/sec RA = 351
09571 deg
ZDOT = -5740
896374 TA = 102
40133
MA = 102
28189
Ha = 192
675 n
mi
Hp = 181
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21419472
45 X = -6517198
82
Y = -908647
44 feet Y = -349899
18 meter
Z = -5318071
59 Z = -1652636
21
XDOT = 5325
358894 XDOT = 1705
258072
YDOT = -15937
840154 feet/sec YDOT = -4839
244125 meter/sec
ZDOT = -18834
961858 ZDOT = -5732
811145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21067356
45 X = -6421330
25
Y = -3798869
00 feet Y = -1157895
27 meter
Z = -5443933
52 Z = -1659310
94
XDOT = 7268
830112 XDOT = 2215
539418
YDOT = -13518
281891 feet/sec YDOT = -4120
372320 meter/sec
ZDOT = -18802
953338 ZDOT = -5731
140177
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 10074
52857132
00016717 00000-0 10270-3 0 9103
2 25544 51
6482 351
4409 0007760 48
8461 311
3370 15
73977590 8723
Satellite: ISS
Catalog Number: 25544
Epoch time: 10074
52857132 = yrday
fracday
Element set: 910
Inclination: 51
6482 deg
RA of node: 351
4409 deg
Eccentricity:
0007760
Arg of perigee: 48
8461 deg
Mean anomaly: 311
3370 deg
Mean motion: 15
73977590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 310
Coasting Arc #12 (Orbit 887)
---------------------------------------
Vector Time (GMT): 2010/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1059537
20 A = 6721169
27 meter
Y = 4357839
64 meter E =
0013451
Z = 4999156
04 I = 51
55010
XDOT = -7468
846185 Wp = 52
75244
YDOT = 341
987132 meter/sec RA = 345
92603 deg
ZDOT = -1869
637793 TA = 55
35597
MA = 55
22924
Ha = 192
651 n
mi
Hp = 181
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3476171
92 X = -1132473
44
Y = 14297374
15 feet Y = 4345584
05 meter
Z = 16401430
57 Z = 4993831
16
XDOT = -24504
088532 XDOT = -7463
032937
YDOT = 1122
005026 feet/sec YDOT = 258
498336 meter/sec
ZDOT = -6133
982260 ZDOT = -1905
907133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5241094
62 X = -1597485
64
Y = 13773880
72 feet Y = 4198278
84 meter
Z = 16380376
69 Z = 4992738
82
XDOT = -23423
801388 XDOT = -7139
574663
YDOT = -1402
218914 feet/sec YDOT = -427
396325 meter/sec
ZDOT = -6278
017866 ZDOT = -1913
539845
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 10075
54440146
00016717 00000-0 10270-3 0 9110
2 25544 51
6477 346
2253 0007750 51
6906 308
4956 15
74048386 8888
Satellite: ISS
Catalog Number: 25544
Epoch time: 10075
54440146 = yrday
fracday
Element set: 911
Inclination: 51
6477 deg
RA of node: 346
2253 deg
Eccentricity:
0007750
Arg of perigee: 51
6906 deg
Mean anomaly: 308
4956 deg
Mean motion: 15
74048386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 888
Checksum: 322
Coasting Arc #13 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2010/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6457965
49 A = 6730834
89 meter
Y = -864372
81 meter E =
0021871
Z = 1644813
85 I = 51
55410
XDOT = -789
999054 Wp = 60
67492
YDOT = 5092
747711 meter/sec RA = 340
81532 deg
ZDOT = 5731
628990 TA = 317
53633
MA = 317
70532
Ha = 192
649 n
mi
Hp = 181
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21187550
82 X = 6459160
89
Y = -2835868
79 feet Y = -792149
13 meter
Z = 5396370
89 Z = 1676189
58
XDOT = -2591
860414 XDOT = -874
731523
YDOT = 16708
489864 feet/sec YDOT = 5083
440342 meter/sec
ZDOT = 18804
557054 ZDOT = 5727
584804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21333922
73 X = 6502579
65
Y = -676827
62 feet Y = -206297
06 meter
Z = 5520953
33 Z = 1682786
58
XDOT = -4431
460005 XDOT = -1350
709009
YDOT = 14793
256607 feet/sec YDOT = 4508
984614 meter/sec
ZDOT = 18788
605676 ZDOT = 5726
767010
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 10076
56021078
00016717 00000-0 10270-3 0 9123
2 25544 51
6481 341
0090 0007814 55
6910 304
4992 15
74041996 9040
Satellite: ISS
Catalog Number: 25544
Epoch time: 10076
56021078 = yrday
fracday
Element set: 912
Inclination: 51
6481 deg
RA of node: 341
0090 deg
Eccentricity:
0007814
Arg of perigee: 55
6910 deg
Mean anomaly: 304
4992 deg
Mean motion: 15
74041996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 904
Checksum: 297
Coasting Arc #14 (Orbit 918)
---------------------------------------
Vector Time (GMT): 2010/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 336948
01 A = 6721127
74 meter
Y = -4509452
93 meter E =
0019180
Z = -4988641
75 I = 51
49402
XDOT = 7265
349012 Wp = 87
60263
YDOT = -1595
314098 meter/sec RA = 335
63974 deg
ZDOT = 1939
998257 TA = 201
17143
MA = 201
25091
Ha = 192
598 n
mi
Hp = 181
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1105472
46 X = 411582
43
Y = -14794793
06 feet Y = -4505268
15 meter
Z = -16366934
87 Z = -4986823
13
XDOT = 23836
446891 XDOT = 7273
223943
YDOT = -5233
970137 feet/sec YDOT = -1514
024429 meter/sec
ZDOT = 6364
823679 ZDOT = 1975
312653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2443669
49 X = 744830
46
Y = -14641368
43 feet Y = -4462689
10 meter
Z = -16359808
62 Z = -4986469
67
XDOT = 23087
214121 XDOT = 7036
982864
YDOT = -3388
811693 feet/sec YDOT = -1032
909804 meter/sec
ZDOT = 6505
025678 ZDOT = 1982
731827
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 10077
51250883
00016717 00000-0 10270-3 0 9138
2 25544 51
6484 336
1187 0007699 58
9131 301
2787 15
74095011 9197
Satellite: ISS
Catalog Number: 25544
Epoch time: 10077
51250883 = yrday
fracday
Element set: 913
Inclination: 51
6484 deg
RA of node: 336
1187 deg
Eccentricity:
0007699
Arg of perigee: 58
9131 deg
Mean anomaly: 301
2787 deg
Mean motion: 15
74095011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 919
Checksum: 319
Coasting Arc #15 (Orbit 934)
---------------------------------------
Vector Time (GMT): 2010/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6212427
15 A = 6730469
65 meter
Y = 1892948
05 meter E =
0011521
Z = -1770970
43 I = 51
49874
XDOT = 24
083950 Wp = 101
52850
YDOT = -5197
629223 meter/sec RA = 330
52576 deg
ZDOT = -5673
470392 TA = 98
11521
MA = 97
98449
Ha = 192
552 n
mi
Hp = 181
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20381978
83 X = -6224529
62
Y = 6210459
49 feet Y = 1823409
20 meter
Z = -5810270
44 Z = -1801180
04
XDOT = 79
015583 XDOT = 109
763768
YDOT = -17052
589315 feet/sec YDOT = -5196
881271 meter/sec
ZDOT = -18613
748006 ZDOT = -5673
144881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20718207
58 X = -6314909
67
Y = 4831440
04 feet Y = 1472622
92 meter
Z = -5930191
62 Z = -1807522
40
XDOT = 1684
286129 XDOT = 513
370412
YDOT = -15491
174275 feet/sec YDOT = -4721
709919 meter/sec
ZDOT = -18612
563857 ZDOT = -5673
109464
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 10078
52827227
00016717 00000-0 10270-3 0 9143
2 25544 51
6484 330
9019 0007531 63
1550 297
0382 15
74098218 9354
Satellite: ISS
Catalog Number: 25544
Epoch time: 10078
52827227 = yrday
fracday
Element set: 914
Inclination: 51
6484 deg
RA of node: 330
9019 deg
Eccentricity:
0007531
Arg of perigee: 63
1550 deg
Mean anomaly: 297
0382 deg
Mean motion: 15
74098218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 935
Checksum: 311
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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