[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 27th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 67 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 2397)
---------------------------------------
Vector Time (GMT): 2012/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 522645
94 A = 6783318
13 meter
Y = 5960486
00 meter E =
0012058
Z = 3184994
03 I = 51
32068
XDOT = -5187
539427 Wp = 91
18584
YDOT = 3016
763707 meter/sec RA = 290
21196 deg
ZDOT = -4778
938880 TA = 51
80740
MA = 51
69887
Ha = 219
796 n
mi
Hp = 214
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1714717
64 X = 440483
82
Y = 19555400
27 feet Y = 5965871
01 meter
Z = 10449455
47 Z = 3187333
71
XDOT = -17019
486308 XDOT = -5197
673085
YDOT = 9897
518723 feet/sec YDOT = 2958
696982 meter/sec
ZDOT = -15678
933333 ZDOT = -4804
164033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15545014
63 X = 4738120
46
Y = -11979893
96 feet Y = -3651471
68 meter
Z = 10458475
84 Z = 3187743
44
XDOT = 16611
793960 XDOT = 5063
274799
YDOT = 7732
265892 feet/sec YDOT = 2356
794644 meter/sec
ZDOT = -15783
259987 ZDOT = -4810
737644
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 12207
53875278
00016717 00000-0 10270-3 0 9004
2 25544 51
6425 290
7458 0000953 306
8616 53
2450 15
54713219 23986
Satellite: ISS
Catalog Number: 25544
Epoch time: 12207
53875278 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 290
7458 deg
Eccentricity:
0000953
Arg of perigee: 306
8616 deg
Mean anomaly: 53
2450 deg
Mean motion: 15
54713219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2398
Checksum: 314
Coasting Arc #2 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2012/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 549720
05 A = 6786745
73 meter
Y = -6592377
56 meter E =
0008525
Z = -1497879
65 I = 51
32228
XDOT = 5004
159947 Wp = 29
49887
YDOT = -882
757247 meter/sec RA = 285
20978 deg
ZDOT = 5742
915429 TA = 314
06890
MA = 314
13906
Ha = 219
822 n
mi
Hp = 214
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1803543
46 X = 630672
84
Y = -21628535
29 feet Y = -6585777
51 meter
Z = -4914303
32 Z = -1495012
95
XDOT = 16417
847595 XDOT = 4985
761535
YDOT = -2896
185195 feet/sec YDOT = -826
900877 meter/sec
ZDOT = 18841
586053 ZDOT = 5767
180560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18996836
61 X = -5790235
80
Y = 10501870
87 feet Y = 3200970
24 meter
Z = -4901794
76 Z = -1494067
04
XDOT = -10704
724659 XDOT = -3262
800076
YDOT = -10555
276685 feet/sec YDOT = -3217
248334 meter/sec
ZDOT = 18941
730602 ZDOT = 5773
439488
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 12208
50291646
00016717 00000-0 10270-3 0 9014
2 25544 51
6425 285
9348 0001194 314
1887 45
9168 15
54690338 24138
Satellite: ISS
Catalog Number: 25544
Epoch time: 12208
50291646 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 285
9348 deg
Eccentricity:
0001194
Arg of perigee: 314
1887 deg
Mean anomaly: 45
9168 deg
Mean motion: 15
54690338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2413
Checksum: 316
Coasting Arc #3 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2012/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1528884
66 A = 6787477
18 meter
Y = 6594928
04 meter E =
0010172
Z = -418631
08 I = 51
31746
XDOT = -4595
955382 Wp = 137
60581
YDOT = -1438
439815 meter/sec RA = 280
21426 deg
ZDOT = -5967
887467 TA = 46
92902
MA = 46
84391
Ha = 219
813 n
mi
Hp = 213
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5016025
77 X = -1600483
26
Y = 21636903
03 feet Y = 6577430
81 meter
Z = -1373461
54 Z = -426231
62
XDOT = -15078
593774 XDOT = -4550
538367
YDOT = -4719
290730 feet/sec YDOT = -1489
580168 meter/sec
ZDOT = -19579
683291 ZDOT = -5990
104113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20629816
42 X = 6287968
04
Y = -8224218
36 feet Y = -2506741
75 meter
Z = -1405485
90 Z = -428392
10
XDOT = 4052
206095 XDOT = 1235
112418
YDOT = 13475
816972 feet/sec YDOT = 4107
429013 meter/sec
ZDOT = -19671
143331 ZDOT = -5995
764487
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 12209
53134886
00016717 00000-0 10270-3 0 9021
2 25544 51
6417 280
8031 0001034 320
7308 39
3770 15
54738519 24293
Satellite: ISS
Catalog Number: 25544
Epoch time: 12209
53134886 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 280
8031 deg
Eccentricity:
0001034
Arg of perigee: 320
7308 deg
Mean anomaly: 39
3770 deg
Mean motion: 15
54738519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 298
Coasting Arc #4 (Orbit 2444)
---------------------------------------
Vector Time (GMT): 2012/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2355258
66 A = 6785335
23 meter
Y = -5943147
09 meter E =
0013618
Z = 2253814
05 I = 51
30629
XDOT = 4021
835124 Wp = 67
46073
YDOT = 3655
484823 meter/sec RA = 275
21573 deg
ZDOT = 5415
289244 TA = 317
75344
MA = 317
85828
Ha = 219
795 n
mi
Hp = 213
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7727226
56 X = 2410592
67
Y = -19498514
06 feet Y = -5916499
97 meter
Z = 7394403
07 Z = 2265389
47
XDOT = 13194
997126 XDOT = 3954
353790
YDOT = 11993
060443 feet/sec YDOT = 3700
081591 meter/sec
ZDOT = 17766
696996 ZDOT = 5434
663465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20312102
81 X = -6191128
94
Y = 5157835
05 feet Y = 1572108
12 meter
Z = 7442747
80 Z = 2268549
53
XDOT = 2464
236320 XDOT = 751
099230
YDOT = -16146
902240 feet/sec YDOT = -4921
575803 meter/sec
ZDOT = 17846
214423 ZDOT = 5439
526156
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 12210
55977002
00016717 00000-0 10270-3 0 9031
2 25544 51
6420 275
6710 0001110 327
6244 32
4841 15
54752555 24450
Satellite: ISS
Catalog Number: 25544
Epoch time: 12210
55977002 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 275
6710 deg
Eccentricity:
0001110
Arg of perigee: 327
6244 deg
Mean anomaly: 32
4841 deg
Mean motion: 15
54752555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2445
Checksum: 275
Coasting Arc #5 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2012/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3082188
94 A = 6781227
98 meter
Y = 4680803
49 meter E =
0006114
Z = -3824724
53 I = 51
29029
XDOT = -3294
205658 Wp = 64
95840
YDOT = -5546
044582 meter/sec RA = 270
20714 deg
ZDOT = -4135
404262 TA = 161
29286
MA = 161
27037
Ha = 219
852 n
mi
Hp = 213
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10112168
43 X = -3115722
16
Y = 15356966
82 feet Y = 4646149
48 meter
Z = -12548308
83 Z = -3839778
39
XDOT = -10807
761346 XDOT = -3211
855213
YDOT = -18195
684324 feet/sec YDOT = -5582
421517 meter/sec
ZDOT = -13567
599285 ZDOT = -4151
207768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18308793
90 X = 5580520
38
Y = -1143035
24 feet Y = -348397
14 meter
Z = -12610867
18 Z = -3843792
32
XDOT = -8250
969108 XDOT = -2514
895384
YDOT = 18143
692056 feet/sec YDOT = 5530
197339 meter/sec
ZDOT = -13632
209299 ZDOT = -4155
097394
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 12211
52390646
00016717 00000-0 10270-3 0 9043
2 25544 51
6414 270
8599 0001126 333
8096 26
3000 15
54761108 24606
Satellite: ISS
Catalog Number: 25544
Epoch time: 12211
52390646 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 270
8599 deg
Eccentricity:
0001126
Arg of perigee: 333
8096 deg
Mean anomaly: 26
3000 deg
Mean motion: 15
54761108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2460
Checksum: 283
Coasting Arc #6 (Orbit 2475)
---------------------------------------
Vector Time (GMT): 2012/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3670156
80 A = 6777207
62 meter
Y = -2950432
20 meter E =
0005815
Z = 4870210
53 I = 51
27809
XDOT = 2449
551117 Wp = 114
06327
YDOT = 6889
418712 meter/sec RA = 265
18559 deg
ZDOT = 2323
196735 TA = 313
07468
MA = 313
12334
Ha = 219
706 n
mi
Hp = 213
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12041196
85 X = 3679218
41
Y = -9679895
66 feet Y = -2909340
08 meter
Z = 15978381
00 Z = 4888061
36
XDOT = 8036
585031 XDOT = 2361
044804
YDOT = 22603
079765 feet/sec YDOT = 6916
315997 meter/sec
ZDOT = 7622
036533 ZDOT = 2334
882097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14963202
24 X = -4560784
04
Y = -3525011
07 feet Y = -1074423
37 meter
Z = 16052300
04 Z = 4892741
05
XDOT = 12733
418277 XDOT = 3881
145891
YDOT = -19058
488282 feet/sec YDOT = -5809
027228 meter/sec
ZDOT = 7669
541615 ZDOT = 2337
676284
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 12212
55230723
00016717 00000-0 10270-3 0 9057
2 25544 51
6414 265
7282 0001224 338
3011 21
8090 15
54798432 24760
Satellite: ISS
Catalog Number: 25544
Epoch time: 12212
55230723 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 265
7282 deg
Eccentricity:
0001224
Arg of perigee: 338
3011 deg
Mean anomaly: 21
8090 deg
Mean motion: 15
54798432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2476
Checksum: 281
Coasting Arc #7 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2012/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4143116
39 A = 6775469
83 meter
Y = 938655
12 meter E =
0014617
Z = -5290971
56 I = 51
27538
XDOT = -1458
976670 Wp = 83
58809
YDOT = -7516
257531 meter/sec RA = 260
15410 deg
ZDOT = -189
829534 TA = 184
58463
MA = 184
59803
Ha = 219
906 n
mi
Hp = 213
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13592901
55 X = -4127602
94
Y = 3079577
18 feet Y = 892411
45 meter
Z = -17358830
58 Z = -5311060
41
XDOT = -4786
668864 XDOT = -1373
897768
YDOT = -24659
637570 feet/sec YDOT = -7532
096995 meter/sec
ZDOT = -622
800310 ZDOT = -196
711054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10836139
11 X = 3302855
20
Y = 8598954
65 feet Y = 2620961
38 meter
Z = -17441784
18 Z = -5316255
82
XDOT = -15624
924095 XDOT = -4762
476864
YDOT = 18363
098010 feet/sec YDOT = 5597
072273 meter/sec
ZDOT = -650
446686 ZDOT = -198
256150
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 12213
51642560
00016717 00000-0 10270-3 0 9061
2 25544 51
6411 260
9167 0001293 345
1467 14
9648 15
54781387 24913
Satellite: ISS
Catalog Number: 25544
Epoch time: 12213
51642560 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 260
9167 deg
Eccentricity:
0001293
Arg of perigee: 345
1467 deg
Mean anomaly: 14
9648 deg
Mean motion: 15
54781387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 308
Coasting Arc #8 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2012/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4439914
92 A = 6776567
19 meter
Y = 1138361
37 meter E =
0006535
Z = 4988664
65 I = 51
28517
XDOT = 328
444177 Wp = 45
35012
YDOT = 7405
507912 meter/sec RA = 255
12244 deg
ZDOT = -1976
060121 TA = 63
95935
MA = 63
89209
Ha = 219
735 n
mi
Hp = 213
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14566650
02 X = 4402622
35
Y = 3734781
39 feet Y = 1187802
40 meter
Z = 16367009
99 Z = 5010142
51
XDOT = 1077
572760 XDOT = 255
208865
YDOT = 24296
285800 feet/sec YDOT = 7408
771433 meter/sec
ZDOT = -6483
136880 ZDOT = -1974
641967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6364856
79 X = -1940008
35
Y = -13517398
71 feet Y = -4120103
13 meter
Z = 16455498
50 Z = 5015635
94
XDOT = 16995
625075 XDOT = 5180
266523
YDOT = -15912
956954 feet/sec YDOT = -4850
269280 meter/sec
ZDOT = -6477
998159 ZDOT = -1974
493839
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 12214
54480642
00016717 00000-0 10270-3 0 9077
2 25544 51
6403 255
7848 0001366 351
1166 8
9962 15
54840994 25076
Satellite: ISS
Catalog Number: 25544
Epoch time: 12214
54480642 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 255
7848 deg
Eccentricity:
0001366
Arg of perigee: 351
1166 deg
Mean anomaly: 8
9962 deg
Mean motion: 15
54840994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 317
Coasting Arc #9 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2012/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4534921
06 A = 6780250
49 meter
Y = -3026140
37 meter E =
0006980
Z = -4037643
64 I = 51
30666
XDOT = 927
088312 Wp = 97
27501
YDOT = -6547
864444 meter/sec RA = 250
09864 deg
ZDOT = 3871
139045 TA = 213
03776
MA = 213
08139
Ha = 219
936 n
mi
Hp = 213
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14878349
92 X = -4481131
62
Y = -9928282
04 feet Y = -3076551
74 meter
Z = -13246862
34 Z = -4059543
01
XDOT = 3041
628319 XDOT = 981
434333
YDOT = -21482
494896 feet/sec YDOT = -6537
193473 meter/sec
ZDOT = 12700
587418 ZDOT = 3875
774395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2115244
15 X = 644726
42
Y = 17693719
77 feet Y = 5393045
79 meter
Z = -13336921
14 Z = -4065093
56
XDOT = -16932
715479 XDOT = -5161
091678
YDOT = 11600
370979 feet/sec YDOT = 3535
793074 meter/sec
ZDOT = 12720
324249 ZDOT = 3877
154831
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 12215
50890629
00016717 00000-0 10270-3 0 9085
2 25544 51
6407 250
9729 0001431 2
4503 357
6657 15
54841487 25229
Satellite: ISS
Catalog Number: 25544
Epoch time: 12215
50890629 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 250
9729 deg
Eccentricity:
0001431
Arg of perigee: 2
4503 deg
Mean anomaly: 357
6657 deg
Mean motion: 15
54841487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 308
Coasting Arc #10 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2012/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4336757
22 A = 6784463
46 meter
Y = 4564549
58 meter E =
0013548
Z = 2512459
70 I = 51
33126
XDOT = -2286
960398 Wp = 97
96057
YDOT = 5085
192643 meter/sec RA = 245
08866 deg
ZDOT = -5268
497345 TA = 53
70036
MA = 53
57532
Ha = 219
939 n
mi
Hp = 213
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14228206
09 X = 4273188
49
Y = 14975556
38 feet Y = 4612690
41 meter
Z = 8242978
01 Z = 2533372
67
XDOT = -7503
150912 XDOT = -2318
061526
YDOT = 16683
702898 feet/sec YDOT = 5059
444650 meter/sec
ZDOT = -17285
096277 ZDOT = -5279
682467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1762857
13 X = 537318
85
Y = -20546985
71 feet Y = -6262721
24 meter
Z = 8328837
65 Z = 2538629
72
XDOT = 15881
873753 XDOT = 4840
795120
YDOT = -5692
620629 feet/sec YDOT = -1735
110768 meter/sec
ZDOT = -17331
707944 ZDOT = -5282
704581
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 12216
53726805
00016717 00000-0 10270-3 0 9094
2 25544 51
6397 245
8401 0001497 6
1346 353
9825 15
54862592 25388
Satellite: ISS
Catalog Number: 25544
Epoch time: 12216
53726805 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 245
8401 deg
Eccentricity:
0001497
Arg of perigee: 6
1346 deg
Mean anomaly: 353
9825 deg
Mean motion: 15
54862592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2538
Checksum: 326
Coasting Arc #11 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2012/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3821285
81 A = 6786951
39 meter
Y = -5561200
49 meter E =
0011853
Z = -674579
68 I = 51
35399
XDOT = 3634
701262 Wp = 36
76197
YDOT = -3210
631022 meter/sec RA = 240
09086 deg
ZDOT = 5942
341274 TA = 315
92039
MA = 316
01482
Ha = 219
953 n
mi
Hp = 213
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12537026
95 X = -3755538
43
Y = -18245408
43 feet Y = -5603564
87 meter
Z = -2213187
93 Z = -692983
27
XDOT = 11924
872907 XDOT = 3641
467089
YDOT = -10533
566346 feet/sec YDOT = -3169
947728 meter/sec
ZDOT = 19495
870322 ZDOT = 5960
014554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4934668
29 X = -1504086
89
Y = 21572701
59 feet Y = 6575359
44 meter
Z = -2288617
34 Z = -697570
57
XDOT = -14171
920126 XDOT = -4319
601254
YDOT = -1187
095528 feet/sec YDOT = -361
826717 meter/sec
ZDOT = 19569
075180 ZDOT = 5964
654115
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 12217
50134864
00016717 00000-0 10270-3 0 9102
2 25544 51
6403 241
0284 0001485 9
5142 350
6039 15
54875130 25531
Satellite: ISS
Catalog Number: 25544
Epoch time: 12217
50134864 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 241
0284 deg
Eccentricity:
0001485
Arg of perigee: 9
5142 deg
Mean anomaly: 350
6039 deg
Mean motion: 15
54875130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 277
Coasting Arc #12 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2012/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2914247
58 A = 6786479
14 meter
Y = 5987193
44 meter E =
0008117
Z = -1295993
23 I = 51
36785
XDOT = -4876
968306 Wp = 134
11593
YDOT = 1122
673414 meter/sec RA = 235
09698 deg
ZDOT = -5808
356519 TA = 60
04002
MA = 59
95946
Ha = 220
047 n
mi
Hp = 213
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9561179
71 X = 2853376
49
Y = 19643023
11 feet Y = 6019442
02 meter
Z = -4251946
29 Z = -1281984
07
XDOT = -16000
552185 XDOT = -4860
944579
YDOT = 3683
311727 feet/sec YDOT = 1068
225682 meter/sec
ZDOT = -19056
287791 ZDOT = -5832
009310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7600320
73 X = 2316577
76
Y = -20493496
45 feet Y = -6246417
72 meter
Z = -4194673
98 Z = -1278536
63
XDOT = 12131
506267 XDOT = 3697
683110
YDOT = 8400
445370 feet/sec YDOT = 2560
455749 meter/sec
ZDOT = -19153
978105 ZDOT = -5838
132526
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 12218
52969093
00016717 00000-0 10270-3 0 9116
2 25544 51
6397 235
8950 0001500 14
4250 345
6946 15
54869325 25694
Satellite: ISS
Catalog Number: 25544
Epoch time: 12218
52969093 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 235
8950 deg
Eccentricity:
0001500
Arg of perigee: 14
4250 deg
Mean anomaly: 345
6946 deg
Mean motion: 15
54869325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 324
Coasting Arc #13 (Orbit 2584)
---------------------------------------
Vector Time (GMT): 2012/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1671291
63 A = 6783178
80 meter
Y = -5810380
80 meter E =
0013801
Z = 3060107
52 I = 51
37465
XDOT = 5845
602853 Wp = 77
91257
YDOT = 901
588903 meter/sec RA = 230
09835 deg
ZDOT = 4888
638227 TA = 317
40027
MA = 317
50723
Ha = 220
068 n
mi
Hp = 213
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5483240
27 X = -1621059
67
Y = -19062929
12 feet Y = -5828789
34 meter
Z = 10039722
82 Z = 3052110
61
XDOT = 19178
487050 XDOT = 5811
339041
YDOT = 2957
968841 feet/sec YDOT = 966
766523 meter/sec
ZDOT = 16038
839327 ZDOT = 4916
952310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9673079
95 X = -2948354
77
Y = 17336205
94 feet Y = 5284075
57 meter
Z = 10007233
03 Z = 3050204
63
XDOT = -10032
103930 XDOT = -3057
785278
YDOT = -14953
468017 feet/sec YDOT = -4557
817052 meter/sec
ZDOT = 16155
590207 ZDOT = 4924
223895
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 12219
55802304
00016717 00000-0 10270-3 0 9122
2 25544 51
6392 230
7623 0001646 17
2496 342
8713 15
54886226 25852
Satellite: ISS
Catalog Number: 25544
Epoch time: 12219
55802304 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 230
7623 deg
Eccentricity:
0001646
Arg of perigee: 17
2496 deg
Mean anomaly: 342
8713 deg
Mean motion: 15
54886226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2585
Checksum: 308
Coasting Arc #14 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2012/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 111566
15 A = 6778735
89 meter
Y = 5132622
57 meter E =
0010330
Z = -4437281
16 I = 51
38040
XDOT = -6379
595788 Wp = 62
80460
YDOT = -2692
449818 meter/sec RA = 225
08803 deg
ZDOT = -3276
033145 TA = 174
01505
MA = 174
00270
Ha = 220
054 n
mi
Hp = 213
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 366030
67 X = 75718
91
Y = 16839312
90 feet Y = 5133669
74 meter
Z = -14558009
05 Z = -4436826
25
XDOT = -20930
432376 XDOT = -6333
100039
YDOT = -8833
496779 feet/sec YDOT = -2763
530452 meter/sec
ZDOT = -10748
140240 ZDOT = -3306
911693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11454448
12 X = 3491315
79
Y = -12350457
20 feet Y = -3764419
35 meter
Z = -14556575
50 Z = -4436844
21
XDOT = 7828
225160 XDOT = 2386
043029
YDOT = 20073
360720 feet/sec YDOT = 6118
360348 meter/sec
ZDOT = -10875
326413 ZDOT = -3314
799491
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 12220
52207435
00016717 00000-0 10270-3 0 9136
2 25544 51
6393 225
9501 0001633 19
5849 340
5366 15
54904599 26008
Satellite: ISS
Catalog Number: 25544
Epoch time: 12220
52207435 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 225
9501 deg
Eccentricity:
0001633
Arg of perigee: 19
5849 deg
Mean anomaly: 340
5366 deg
Mean motion: 15
54904599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 298
Coasting Arc #15 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2012/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1604710
51 A = 6775583
55 meter
Y = -4056419
15 meter E =
0004136
Z = 5181113
87 I = 51
39151
XDOT = 6377
339512 Wp = 101
19117
YDOT = 4087
404712 meter/sec RA = 220
06638 deg
ZDOT = 1223
300098 TA = 337
02717
MA = 337
04566
Ha = 220
005 n
mi
Hp = 213
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5264798
26 X = 1624782
48
Y = -13308461
78 feet Y = -4038362
11 meter
Z = 16998405
08 Z = 5188958
12
XDOT = 20923
029895 XDOT = 6325
216863
YDOT = 13410
120446 feet/sec YDOT = 4158
428639 meter/sec
ZDOT = 4013
451765 ZDOT = 1254
154118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12893741
65 X = -3930012
46
Y = 6121376
81 feet Y = 1865795
65 meter
Z = 17031124
53 Z = 5191086
76
XDOT = -5520
717858 XDOT = -1682
714803
YDOT = -23162
946117 feet/sec YDOT = -7060
065976 meter/sec
ZDOT = 4140
428080 ZDOT = 1262
002479
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 12221
55038619
00016717 00000-0 10270-3 0 9147
2 25544 51
6385 220
8168 0001698 21
9788 338
1438 15
54915059 26165
Satellite: ISS
Catalog Number: 25544
Epoch time: 12221
55038619 = yrday
fracday
Element set: 914
Inclination: 51
6385 deg
RA of node: 220
8168 deg
Eccentricity:
0001698
Arg of perigee: 21
9788 deg
Mean anomaly: 338
1438 deg
Mean motion: 15
54915059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 326
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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