Date:
February 25th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
055/15:46:00
000 0
0 0
0 0
0
N/A 0
0 0
0 192
5
000/00:00:00
000 0
0 0
0 185
9
056/10:34:39
082 -1
4 1
5 1
5
N/A -0
3 -0
3 193
2
000/00:03:18
165 0
6 0
1 185
7
Coasting Arc #1 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2011/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 829765
07 A = 6726940
89 meter
Y = 4865302
81 meter E =
0005839
Z = 4565444
98 I = 51
82256
XDOT = -6867
114884 Wp = 82
38128
YDOT = -1692
377229 meter/sec RA = 33
65903 deg
ZDOT = 3049
076482 TA = 337
36660
MA = 337
39233
Ha = 192
253 n
mi
Hp = 186
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2722326
33 X = 753120
91
Y = 15962279
57 feet Y = 4874153
58 meter
Z = 14978494
03 Z = 4569289
35
XDOT = -22529
904475 XDOT = -6862
491648
YDOT = -5552
418731 feet/sec YDOT = -1769
143364 meter/sec
ZDOT = 10003
531765 ZDOT = 3015
727946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5628300
08 X = -1715505
87
Y = 15167954
24 feet Y = 4623192
45 meter
Z = 14993869
27 Z = 4570131
35
XDOT = -15758
269573 XDOT = -4803
120566
YDOT = -15611
274679 feet/sec YDOT = -4758
316522 meter/sec
ZDOT = 9868
944153 ZDOT = 3008
054178
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 11052
55294961
00016717 00000-0 10270-3 0 9007
2 25544 51
6416 33
9243 0004700 335
9798 24
1145 15
72649460 22706
Satellite: ISS
Catalog Number: 25544
Epoch time: 11052
55294961 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 33
9243 deg
Eccentricity:
0004700
Arg of perigee: 335
9798 deg
Mean anomaly: 24
1145 deg
Mean motion: 15
72649460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 297
Coasting Arc #2 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2011/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5984350
14 A = 6732089
50 meter
Y = 535922
39 meter E =
0006618
Z = -3031679
10 I = 51
81387
XDOT = 2012
346941 Wp = 24
72681
YDOT = 5531
628469 meter/sec RA = 28
50001 deg
ZDOT = 4959
858103 TA = 300
30448
MA = 300
36994
Ha = 192
475 n
mi
Hp = 186
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19633694
68 X = 5992639
73
Y = 1758275
57 feet Y = 602889
18 meter
Z = -9946453
74 Z = -3002587
42
XDOT = 6602
188128 XDOT = 1926
247894
YDOT = 18148
387365 feet/sec YDOT = 5553
650647 meter/sec
ZDOT = 16272
500337 ZDOT = 4969
424480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16421954
29 X = 5005411
67
Y = 11009776
26 feet Y = 3355779
80 meter
Z = -9829022
63 Z = -2995886
10
XDOT = -2219
708606 XDOT = -676
567183
YDOT = 17843
611991 feet/sec YDOT = 5438
732935 meter/sec
ZDOT = 16310
948533 ZDOT = 4971
577113
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 11053
50610716
00016717 00000-0 10270-3 0 9014
2 25544 51
6419 29
0394 0004688 341
9562 18
1433 15
72660467 22852
Satellite: ISS
Catalog Number: 25544
Epoch time: 11053
50610716 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 29
0394 deg
Eccentricity:
0004688
Arg of perigee: 341
9562 deg
Mean anomaly: 18
1433 deg
Mean motion: 15
72660467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 300
Coasting Arc #3 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2011/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2637256
85 A = 6728507
77 meter
Y = -4654692
39 meter E =
0009296
Z = -4090754
53 I = 51
77587
XDOT = 6655
777127 Wp = 39
93053
YDOT = -402
919660 meter/sec RA = 23
43473 deg
ZDOT = -3830
239835 TA = 190
71109
MA = 190
73090
Ha = 192
383 n
mi
Hp = 185
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8652417
49 X = -2565139
32
Y = -15271300
48 feet Y = -4683780
72 meter
Z = -13421110
66 Z = -4103390
79
XDOT = 21836
539132 XDOT = 6678
394339
YDOT = -1321
914894 feet/sec YDOT = -328
364423 meter/sec
ZDOT = -12566
403658 ZDOT = -3797
851561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -474629
38 X = -144667
04
Y = -17506679
57 feet Y = -5336035
93 meter
Z = -13471972
96 Z = -4106257
36
XDOT = 18729
915992 XDOT = 5708
878395
YDOT = 9067
349794 feet/sec YDOT = 2763
728217 meter/sec
ZDOT = -12435
636326 ZDOT = -3790
381952
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 11054
52278029
00016717 00000-0 10270-3 0 9025
2 25544 51
6425 23
8283 0004695 345
3926 14
7107 15
72722387 23017
Satellite: ISS
Catalog Number: 25544
Epoch time: 11054
52278029 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 23
8283 deg
Eccentricity:
0004695
Arg of perigee: 345
3926 deg
Mean anomaly: 14
7107 deg
Mean motion: 15
72722387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 296
Coasting Arc #4 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2011/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5529036
01 A = 6730017
51 meter
Y = 1197408
57 meter E =
0012309
Z = 3641080
26 I = 51
75261
XDOT = -3963
004604 Wp = 62
86088
YDOT = -4940
818307 meter/sec RA = 18
26710 deg
ZDOT = -4376
253041 TA = 73
57732
MA = 73
44207
Ha = 192
452 n
mi
Hp = 185
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18139881
92 X = -5559702
16
Y = 3928505
79 feet Y = 1135408
16 meter
Z = 11945801
38 Z = 3614146
12
XDOT = -13001
983608 XDOT = -3886
202186
YDOT = -16210
033815 feet/sec YDOT = -4984
705693 meter/sec
ZDOT = -14357
785567 ZDOT = -4395
318354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18029038
83 X = -5495251
04
Y = -4693528
53 feet Y = -1430587
50 meter
Z = 11837026
36 Z = 3607925
63
XDOT = -4573
591920 XDOT = -1394
030817
YDOT = -18975
724968 feet/sec YDOT = -5783
800970 meter/sec
ZDOT = -14434
587428 ZDOT = -4399
662248
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 11055
53942351
00016717 00000-0 10270-3 0 9034
2 25544 51
6425 18
6177 0004782 348
0527 12
0521 15
72774148 23175
Satellite: ISS
Catalog Number: 25544
Epoch time: 11055
53942351 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 18
6177 deg
Eccentricity:
0004782
Arg of perigee: 348
0527 deg
Mean anomaly: 12
0521 deg
Mean motion: 15
72774148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 293
Coasting Arc #5 (Orbit 2318)
---------------------------------------
Vector Time (GMT): 2011/055/15:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 891256
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4743173
36 A = 6727714
54 meter
Y = -2066590
61 meter E =
0007291
Z = -4305447
57 I = 51
74347
XDOT = 5145
804388 Wp = 76
38562
YDOT = 4518
082436 meter/sec RA = 17
46616 deg
ZDOT = 3506
941931 TA = 229
06782
MA = 229
13097
Ha = 192
459 n
mi
Hp = 185
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15561592
40 X = 4786844
59
Y = -6780152
93 feet Y = -2013305
49 meter
Z = -14125484
16 Z = -4282299
49
XDOT = 16882
560327 XDOT = 5077
864073
YDOT = 14823
105106 feet/sec YDOT = 4575
246130 meter/sec
ZDOT = 11505
714997 ZDOT = 3531
774727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10186035
32 X = 3104703
57
Y = -13675218
41 feet Y = -4168206
57 meter
Z = -14031964
24 Z = -4276942
70
XDOT = 20966
771442 XDOT = 6390
671935
YDOT = 3731
062702 feet/sec YDOT = 1137
227911 meter/sec
ZDOT = 11605
814151 ZDOT = 3537
452153
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 11055
66650209
00016717 00000-0 10270-3 0 9047
2 25544 51
6456 17
9674 0004767 348
7615 11
3440 15
72778656 23193
Satellite: ISS
Catalog Number: 25544
Epoch time: 11055
66650209 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 17
9674 deg
Eccentricity:
0004767
Arg of perigee: 348
7615 deg
Mean anomaly: 11
3440 deg
Mean motion: 15
72778656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2319
Checksum: 324
Coasting Arc #6 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2011/056/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 996319
79 A = 6725284
10 meter
Y = 4332634
63 meter E =
0005096
Z = 5041754
92 I = 51
70658
XDOT = -7485
773740 Wp = 66
27118
YDOT = -349
713128 meter/sec RA = 13
48668 deg
ZDOT = 1780
419024 TA = 6
60388
MA = 6
59717
Ha = 193
240 n
mi
Hp = 185
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3268765
72 X = 923305
93
Y = 14214680
54 feet Y = 4343367
91 meter
Z = 16541190
67 Z = 5046417
54
XDOT = -24559
625130 XDOT = -7489
955611
YDOT = -1147
352783 feet/sec YDOT = -433
446937 meter/sec
ZDOT = 5841
269764 ZDOT = 1744
043678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8184812
10 X = -2494730
73
Y = 12047101
77 feet Y = 3671956
62 meter
Z = 16559865
66 Z = 5047447
05
XDOT = -15133
245152 XDOT = -4612
613122
YDOT = -18106
358882 feet/sec YDOT = -5518
818187 meter/sec
ZDOT = 5694
431649 ZDOT = 1735
662767
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 11056
49251151
00016717 00000-0 10270-3 0 9053
2 25544 51
6422 13
7332 0005074 4
5501 355
5707 15
72528458 23321
Satellite: ISS
Catalog Number: 25544
Epoch time: 11056
49251151 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 13
7332 deg
Eccentricity:
0005074
Arg of perigee: 4
5501 deg
Mean anomaly: 355
5707 deg
Mean motion: 15
72528458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 278
Coasting Arc #7 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2011/057/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6390817
24 A = 6734585
46 meter
Y = -660866
19 meter E =
0011545
Z = -2001576
83 I = 51
70797
XDOT = 2240
540120 Wp = 26
51409
YDOT = 4792
059623 meter/sec RA = 8
33496 deg
ZDOT = 5594
055342 TA = 311
21635
MA = 311
31580
Ha = 193
364 n
mi
Hp = 185
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20967248
18 X = 6407455
27
Y = -2168196
16 feet Y = -589307
20 meter
Z = -6566853
12 Z = -1970490
54
XDOT = 7350
853413 XDOT = 2159
613601
YDOT = 15721
980392 feet/sec YDOT = 4816
662293 meter/sec
ZDOT = 18353
199941 ZDOT = 5604
742999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16204706
64 X = 4939194
58
Y = 13541301
97 feet Y = 4127388
84 meter
Z = -6441331
70 Z = -1963317
90
XDOT = -5229
718109 XDOT = -1594
018080
YDOT = 14973
302989 feet/sec YDOT = 4563
862751 meter/sec
ZDOT = 18396
181575 ZDOT = 5607
156144
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 11057
44573372
00016717 00000-0 10270-3 0 9062
2 25544 51
6422 8
8488 0005062 9
8524 350
2737 15
72564899 23478
Satellite: ISS
Catalog Number: 25544
Epoch time: 11057
44573372 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 8
8488 deg
Eccentricity:
0005062
Arg of perigee: 9
8524 deg
Mean anomaly: 350
2737 deg
Mean motion: 15
72564899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 324
Coasting Arc #8 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2011/058/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2844027
81 A = 6726486
13 meter
Y = -3890785
38 meter E =
0014523
Z = -4706226
01 I = 51
65158
XDOT = 6960
599850 Wp = 53
35001
YDOT = -1773
658500 meter/sec RA = 3
25143 deg
ZDOT = -2737
356024 TA = 189
63097
MA = 189
65884
Ha = 193
285 n
mi
Hp = 185
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9330799
91 X = -2777447
56
Y = -12765043
91 feet Y = -3922216
86 meter
Z = -15440374
05 Z = -4719880
11
XDOT = 22836
613681 XDOT = 6993
213131
YDOT = -5819
089567 feet/sec YDOT = -1695
638574 meter/sec
ZDOT = -8980
826851 ZDOT = -2703
463090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2437582
98 X = 742975
29
Y = -15568147
70 feet Y = -4745171
42 meter
Z = -15495363
51 Z = -4722986
80
XDOT = 19209
079898 XDOT = 5854
927553
YDOT = 11818
961808 feet/sec YDOT = 3602
419559 meter/sec
ZDOT = -8843
936033 ZDOT = -2695
631703
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 11058
46247669
00016717 00000-0 10270-3 0 9073
2 25544 51
6429 3
6379 0005061 12
4797 347
6490 15
72607648 23632
Satellite: ISS
Catalog Number: 25544
Epoch time: 11058
46247669 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 3
6379 deg
Eccentricity:
0005061
Arg of perigee: 12
4797 deg
Mean anomaly: 347
6490 deg
Mean motion: 15
72607648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 329
Coasting Arc #9 (Orbit 2378)
---------------------------------------
Vector Time (GMT): 2011/059/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5657147
18 A = 6732763
55 meter
Y = 2376355
24 meter E =
0014896
Z = 2762042
67 I = 51
64256
XDOT = -4172
719533 Wp = 80
48120
YDOT = -3929
904384 meter/sec RA = 358
08345 deg
ZDOT = -5139
440835 TA = 67
95454
MA = 67
79639
Ha = 193
318 n
mi
Hp = 185
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18560194
17 X = -5696716
69
Y = 7796441
06 feet Y = 2312872
46 meter
Z = 9061819
79 Z = 2734464
87
XDOT = -13690
024713 XDOT = -4103
498738
YDOT = -12893
387085 feet/sec YDOT = -3976
179429 meter/sec
ZDOT = -16861
682531 ZDOT = -5159
543015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18830605
38 X = -5739568
52
Y = -7258128
52 feet Y = -2212277
57 meter
Z = 8950405
04 Z = 2728083
46
XDOT = -1410
769832 XDOT = -430
002645
YDOT = -17338
886608 feet/sec YDOT = -5284
892638 meter/sec
ZDOT = -16942
703808 ZDOT = -5164
136121
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 11059
47919079
00016717 00000-0 10270-3 0 9087
2 25544 51
6431 358
4276 0005113 15
3714 344
7603 15
72660683 23790
Satellite: ISS
Catalog Number: 25544
Epoch time: 11059
47919079 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 358
4276 deg
Eccentricity:
0005113
Arg of perigee: 15
3714 deg
Mean anomaly: 344
7603 deg
Mean motion: 15
72660683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2379
Checksum: 321
Coasting Arc #10 (Orbit 2394)
---------------------------------------
Vector Time (GMT): 2011/060/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4356582
99 A = 6727832
80 meter
Y = 2856849
71 meter E =
0011030
Z = 4246594
48 I = 51
59732
XDOT = -5823
297605 Wp = 80
96123
YDOT = 3565
161931 meter/sec RA = 353
00513 deg
ZDOT = 3569
551130 TA = 332
76848
MA = 332
82628
Ha = 193
063 n
mi
Hp = 184
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14293251
26 X = 4303684
80
Y = 9372866
50 feet Y = 2905272
14 meter
Z = 13932396
59 Z = 4267629
45
XDOT = -19105
307103 XDOT = -5880
070826
YDOT = 11696
725496 feet/sec YDOT = 3499
725069 meter/sec
ZDOT = 11711
125753 ZDOT = 3541
124310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4051518
90 X = 1234902
96
Y = 16533664
08 feet Y = 5039460
81 meter
Z = 14017220
82 Z = 4272448
90
XDOT = -20809
561776 XDOT = -6342
754429
YDOT = -4748
971268 feet/sec YDOT = -1447
486442 meter/sec
ZDOT = 11596
247983 ZDOT = 3534
536385
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 11060
49587477
00016717 00000-0 10270-3 0 9095
2 25544 51
6440 353
2176 0004905 18
2600 341
8738 15
72736413 23956
Satellite: ISS
Catalog Number: 25544
Epoch time: 11060
49587477 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 353
2176 deg
Eccentricity:
0004905
Arg of perigee: 18
2600 deg
Mean anomaly: 341
8738 deg
Mean motion: 15
72736413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2395
Checksum: 315
Coasting Arc #11 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2011/061/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4411524
09 A = 6730737
65 meter
Y = -3743533
71 meter E =
0008213
Z = -3440215
70 I = 51
57635
XDOT = 5667
087898 Wp = 55
37838
YDOT = 2487
820367 meter/sec RA = 347
82548 deg
ZDOT = 4572
259415 TA = 263
90253
MA = 263
99612
Ha = 193
323 n
mi
Hp = 184
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14473504
24 X = 4469768
57
Y = -12281934
74 feet Y = -3693875
99 meter
Z = -11286796
93 Z = -3418643
39
XDOT = 18592
808064 XDOT = 5616
636883
YDOT = 8162
140312 feet/sec YDOT = 2550
911453 meter/sec
ZDOT = 15000
851099 ZDOT = 4599
666560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19026028
57 X = 5799133
51
Y = 547193
30 feet Y = 166784
52 meter
Z = -11199591
38 Z = -3413635
45
XDOT = 8381
390014 XDOT = 2554
647676
YDOT = 17035
504717 feet/sec YDOT = 5192
421838 meter/sec
ZDOT = 15111
410989 ZDOT = 4605
958069
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 11061
44899231
00016717 00000-0 10270-3 0 9107
2 25544 51
6438 348
3324 0005077 21
4193 338
7181 15
72727335 24105
Satellite: ISS
Catalog Number: 25544
Epoch time: 11061
44899231 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 348
3324 deg
Eccentricity:
0005077
Arg of perigee: 21
4193 deg
Mean anomaly: 338
7181 deg
Mean motion: 15
72727335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 296
Coasting Arc #12 (Orbit 2425)
---------------------------------------
Vector Time (GMT): 2011/062/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5412921
63 A = 6729408
60 meter
Y = -1432893
89 meter E =
0010118
Z = -3744716
72 I = 51
54406
XDOT = 4212
710213 Wp = 52
88518
YDOT = -4835
342370 meter/sec RA = 342
74535 deg
ZDOT = -4241
049378 TA = 172
34158
MA = 172
32611
Ha = 193
237 n
mi
Hp = 184
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17758929
22 X = -5378305
78
Y = -4701095
43 feet Y = -1493231
27 meter
Z = -12285816
00 Z = -3770927
74
XDOT = 13821
227733 XDOT = 4287
068514
YDOT = -15863
984152 feet/sec YDOT = -4787
817944 meter/sec
ZDOT = -13914
203996 ZDOT = -4220
403523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10302501
82 X = -3140202
56
Y = -15123769
04 feet Y = -4609724
80 meter
Z = -12391578
05 Z = -3776952
99
XDOT = 19791
246743 XDOT = 6032
372007
YDOT = -2154
903383 feet/sec YDOT = -656
814551 meter/sec
ZDOT = -13830
711657 ZDOT = -4215
600913
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 11062
46562152
00016717 00000-0 10270-3 0 9110
2 25544 51
6447 343
1214 0005074 25
5550 334
5862 15
72800860 24267
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
46562152 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 343
1214 deg
Eccentricity:
0005074
Arg of perigee: 25
5550 deg
Mean anomaly: 334
5862 deg
Mean motion: 15
72800860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2426
Checksum: 281
Coasting Arc #13 (Orbit 2441)
---------------------------------------
Vector Time (GMT): 2011/063/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2900034
07 A = 6728750
13 meter
Y = 4600538
70 meter E =
0014765
Z = 3955948
88 I = 51
51320
XDOT = -6560
630190 Wp = 63
81195
YDOT = -706
027360 meter/sec RA = 337
56025 deg
ZDOT = -3970
565769 TA = 67
46607
MA = 67
30986
Ha = 193
262 n
mi
Hp = 184
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9514547
47 X = -2970479
45
Y = 15093630
90 feet Y = 4567715
31 meter
Z = 12978834
92 Z = 3941689
25
XDOT = -21524
377265 XDOT = -6532
959835
YDOT = -2316
362729 feet/sec YDOT = -779
238022 meter/sec
ZDOT = -13026
790581 ZDOT = -4002
369242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17037293
14 X = -5192966
95
Y = 5437769
13 feet Y = 1657432
03 meter
Z = 12921136
66 Z = 3938362
45
XDOT = -14579
906093 XDOT = -4443
955377
YDOT = -14282
124666 feet/sec YDOT = -4353
191598 meter/sec
ZDOT = -13155
144277 ZDOT = -4009
687975
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 11063
48222176
00016717 00000-0 10270-3 0 9123
2 25544 51
6449 337
9109 0005003 28
9028 331
2411 15
72837153 24429
Satellite: ISS
Catalog Number: 25544
Epoch time: 11063
48222176 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 337
9109 deg
Eccentricity:
0005003
Arg of perigee: 28
9028 deg
Mean anomaly: 331
2411 deg
Mean motion: 15
72837153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2442
Checksum: 286
Coasting Arc #14 (Orbit 2457)
---------------------------------------
Vector Time (GMT): 2011/064/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5918322
02 A = 6730895
34 meter
Y = -232385
82 meter E =
0016298
Z = 3178599
46 I = 51
49311
XDOT = -2369
125084 Wp = 72
21035
YDOT = 5542
083218 meter/sec RA = 332
47488 deg
ZDOT = 4801
092684 TA = 324
96693
MA = 325
07403
Ha = 193
117 n
mi
Hp = 184
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19417066
99 X = 5905039
99
Y = -762420
66 feet Y = -166277
45 meter
Z = 10428475
92 Z = 3207317
85
XDOT = -7772
720093 XDOT = -2454
244004
YDOT = 18182
687724 feet/sec YDOT = 5515
114860 meter/sec
ZDOT = 15751
616416 ZDOT = 4789
376314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15545376
64 X = 4738230
80
Y = 11554817
93 feet Y = 3521908
50 meter
Z = 10544398
20 Z = 3213932
57
XDOT = -16694
542279 XDOT = -5088
496487
YDOT = 8084
166550 feet/sec YDOT = 2464
053964 meter/sec
ZDOT = 15704
162615 ZDOT = 4786
628765
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 11064
49879305
00016717 00000-0 10270-3 0 9138
2 25544 51
6448 332
6998 0005000 32
7109 327
4362 15
72873715 24589
Satellite: ISS
Catalog Number: 25544
Epoch time: 11064
49879305 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 332
6998 deg
Eccentricity:
0005000
Arg of perigee: 32
7109 deg
Mean anomaly: 327
4362 deg
Mean motion: 15
72873715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2458
Checksum: 321
Coasting Arc #15 (Orbit 2472)
---------------------------------------
Vector Time (GMT): 2011/065/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1229898
65 A = 6726887
55 meter
Y = -4951020
82 meter E =
0011533
Z = -4394112
70 I = 51
45349
XDOT = 6825
918351 Wp = 85
64339
YDOT = -1242
014740 meter/sec RA = 327
28712 deg
ZDOT = 3318
318117 TA = 217
79848
MA = 217
87953
Ha = 193
178 n
mi
Hp = 184
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4035100
55 X = 1306515
96
Y = -16243506
64 feet Y = -4936839
48 meter
Z = -14416380
23 Z = -4387951
26
XDOT = 22394
745246 XDOT = 6823
179942
YDOT = -4074
851509 feet/sec YDOT = -1165
698106 meter/sec
ZDOT = 10886
870464 ZDOT = 3351
471390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13229093
86 X = 4032227
81
Y = -10288105
59 feet Y = -3135814
58 meter
Z = -14391369
71 Z = -4386489
49
XDOT = 19373
708978 XDOT = 5905
106497
YDOT = 9534
095066 feet/sec YDOT = 2905
992176 meter/sec
ZDOT = 11020
714418 ZDOT = 3359
113755
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 11065
45180159
00016717 00000-0 10270-3 0 9148
2 25544 51
6450 327
8140 0004988 35
6842 324
4653 15
72926476 24737
Satellite: ISS
Catalog Number: 25544
Epoch time: 11065
45180159 = yrday
fracday
Element set: 914
Inclination: 51
6450 deg
RA of node: 327
8140 deg
Eccentricity:
0004988
Arg of perigee: 35
6842 deg
Mean anomaly: 324
4653 deg
Mean motion: 15
72926476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2473
Checksum: 319
Coasting Arc #16 (Orbit 2488)
---------------------------------------
Vector Time (GMT): 2011/066/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5894329
87 A = 6731997
17 meter
Y = 1911053
48 meter E =
0007236
Z = -2639258
54 I = 51
44665
XDOT = 498
279374 Wp = 81
19249
YDOT = -5638
818118 meter/sec RA = 322
19284 deg
ZDOT = -5206
878840 TA = 128
87986
MA = 128
81529
Ha = 193
132 n
mi
Hp = 184
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19338352
58 X = -5902440
66
Y = 6269860
50 feet Y = 1845093
87 meter
Z = -8658984
71 Z = -2667912
76
XDOT = 1634
774848 XDOT = 586
590453
YDOT = -18500
059441 feet/sec YDOT = -5632
752867 meter/sec
ZDOT = -17082
935826 ZDOT = -5204
243089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19186488
44 X = -5848041
68
Y = -6568458
81 feet Y = -2002066
24 meter
Z = -8774682
77 Z = -2674523
31
XDOT = 12019
789048 XDOT = 3663
631702
YDOT = -12351
326724 feet/sec YDOT = -3764
684386 meter/sec
ZDOT = -17072
138396 ZDOT = -5203
587783
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 11066
46831594
00016717 00000-0 10270-3 0 9157
2 25544 51
6454 322
6023 0004960 39
0078 321
1442 15
72971435 24895
Satellite: ISS
Catalog Number: 25544
Epoch time: 11066
46831594 = yrday
fracday
Element set: 915
Inclination: 51
6454 deg
RA of node: 322
6023 deg
Eccentricity:
0004960
Arg of perigee: 39
0078 deg
Mean anomaly: 321
1442 deg
Mean motion: 15
72971435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2489
Checksum: 306
Coasting Arc #17 (Orbit 2504)
---------------------------------------
Vector Time (GMT): 2011/067/10:36:18
165
Vector Time (MET): N/A
Weight (LBS) : 891110
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 345172
86 A = 6725364
64 meter
Y = 4799762
31 meter E =
0012570
Z = 4692691
09 I = 51
40039
XDOT = -6505
522075 Wp = 54
04151
YDOT = 3119
040950 meter/sec RA = 317
00648 deg
ZDOT = -2699
377168 TA = 62
66304
MA = 62
53513
Ha = 193
092 n
mi
Hp = 183
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1132456
88 X = 268679
30
Y = 15747251
69 feet Y = 4803195
02 meter
Z = 15395968
15 Z = 4694181
64
XDOT = -21343
576361 XDOT = -6526
803303
YDOT = 10233
073983 feet/sec YDOT = 3046
172997 meter/sec
ZDOT = -8856
224303 ZDOT = -2731
032722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8396263
77 X = -2559181
20
Y = 13363383
93 feet Y = 4073159
42 meter
Z = 15401849
05 Z = 4694483
59
XDOT = -22270
155389 XDOT = -6787
943363
YDOT = -3591
377008 feet/sec YDOT = -1094
651712 meter/sec
ZDOT = -8984
063167 ZDOT = -2738
342453
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 11067
48480096
00016717 00000-0 10270-3 0 9168
2 25544 51
6447 317
3906 0004956 41
9843 318
1698 15
73025101 25054
Satellite: ISS
Catalog Number: 25544
Epoch time: 11067
48480096 = yrday
fracday
Element set: 916
Inclination: 51
6447 deg
RA of node: 317
3906 deg
Eccentricity:
0004956
Arg of perigee: 41
9843 deg
Mean anomaly: 318
1698 deg
Mean motion: 15
73025101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2505
Checksum: 316
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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