[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 16th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23142 41 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 2874)
---------------------------------------
Vector Time (GMT): 2011/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6549086
37 A = 6776820
67 meter
Y = 725654
65 meter E =
0032684
Z = -1513952
26 I = 51
55996
XDOT = 760
738081 Wp = 152
60483
YDOT = -5018
035159 meter/sec RA = 343
16943 deg
ZDOT = -5773
788750 TA = 44
00747
MA = 43
74772
Ha = 222
890 n
mi
Hp = 201
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21486503
84 X = -6549359
54
Y = 2380756
74 feet Y = 652417
42 meter
Z = -4967034
98 Z = -1545768
26
XDOT = 2495
859847 XDOT = 844
842187
YDOT = -16463
369944 feet/sec YDOT = -5009
057135 meter/sec
ZDOT = -18942
876475 ZDOT = -5769
889436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1364084
37 X = 415772
92
Y = -21544570
71 feet Y = -6566785
15 meter
Z = -5097061
25 Z = -1553584
27
XDOT = 14194
352519 XDOT = 4326
438648
YDOT = 5317
555345 feet/sec YDOT = 1620
790869 meter/sec
ZDOT = -18926
494501 ZDOT = -5768
795524
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 11346
52912317
00016717 00000-0 10270-3 0 9002
2 25544 51
6414 343
5391 0024740 156
6278 203
6007 15
58086873 28754
Satellite: ISS
Catalog Number: 25544
Epoch time: 11346
52912317 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 343
5391 deg
Eccentricity:
0024740
Arg of perigee: 156
6278 deg
Mean anomaly: 203
6007 deg
Mean motion: 15
58086873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2875
Checksum: 310
Coasting Arc #2 (Orbit 2890)
---------------------------------------
Vector Time (GMT): 2011/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5307862
70 A = 6770734
38 meter
Y = 1299121
95 meter E =
0031575
Z = 4000205
82 I = 51
51120
XDOT = -4226
828399 Wp = 143
12091
YDOT = 5056
735729 meter/sec RA = 338
15817 deg
ZDOT = 3925
413692 TA = 265
87309
MA = 266
23404
Ha = 222
645 n
mi
Hp = 201
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17414247
70 X = 5273508
98
Y = 4262211
13 feet Y = 1358285
20 meter
Z = 13124034
84 Z = 4025908
00
XDOT = -13867
547241 XDOT = -4302
128532
YDOT = 16590
340317 feet/sec YDOT = 5009
047271 meter/sec
ZDOT = 12878
653844 ZDOT = 3904
697520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6913023
24 X = -2107089
48
Y = 16458094
81 feet Y = 5016427
30 meter
Z = 13228907
06 Z = 4032170
87
XDOT = -13014
272214 XDOT = -3966
750171
YDOT = -15856
907368 feet/sec YDOT = -4833
185366 meter/sec
ZDOT = 12793
577728 ZDOT = 3899
482491
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 11347
55531066
00016717 00000-0 10270-3 0 9015
2 25544 51
6410 338
3929 0024587 160
6925 199
5167 15
58156026 28918
Satellite: ISS
Catalog Number: 25544
Epoch time: 11347
55531066 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 338
3929 deg
Eccentricity:
0024587
Arg of perigee: 160
6925 deg
Mean anomaly: 199
5167 deg
Mean motion: 15
58156026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2891
Checksum: 327
Coasting Arc #3 (Orbit 2905)
---------------------------------------
Vector Time (GMT): 2011/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2655959
64 A = 6765791
56 meter
Y = -3350061
13 meter E =
0030817
Z = -5260107
00 I = 51
46693
XDOT = 6499
408837 Wp = 135
65603
YDOT = -3982
669853 meter/sec RA = 333
11256 deg
ZDOT = -769
537239 TA = 127
10764
MA = 126
82562
Ha = 222
541 n
mi
Hp = 201
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8713778
36 X = -2592748
72
Y = -10991014
19 feet Y = -3379407
77 meter
Z = -17257568
89 Z = -5272856
34
XDOT = 21323
519808 XDOT = 6547
199037
YDOT = -13066
502142 feet/sec YDOT = -3909
722193 meter/sec
ZDOT = -2524
728473 ZDOT = -737
847613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12081049
02 X = 3682303
74
Y = -6999332
09 feet Y = -2133396
42 meter
Z = -17309350
51 Z = -5275890
04
XDOT = 9466
372868 XDOT = 2885
350450
YDOT = 22065
246341 feet/sec YDOT = 6725
487085 meter/sec
ZDOT = -2394
927106 ZDOT = -729
973782
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 11348
51733803
00016717 00000-0 10270-3 0 9026
2 25544 51
6410 333
5667 0024575 163
9749 196
2188 15
58167565 29065
Satellite: ISS
Catalog Number: 25544
Epoch time: 11348
51733803 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 333
5667 deg
Eccentricity:
0024575
Arg of perigee: 163
9749 deg
Mean anomaly: 196
2188 deg
Mean motion: 15
58167565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2906
Checksum: 335
Coasting Arc #4 (Orbit 2921)
---------------------------------------
Vector Time (GMT): 2011/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -468145
68 A = 6767725
00 meter
Y = 4765653
62 meter E =
0023451
Z = 4763751
61 I = 51
44712
XDOT = -6979
423476 Wp = 149
56026
YDOT = 1904
440820 meter/sec RA = 328
05922 deg
ZDOT = -2605
341533 TA = 326
03931
MA = 326
18920
Ha = 222
287 n
mi
Hp = 202
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1535911
01 X = -544542
65
Y = 15635346
51 feet Y = 4759991
01 meter
Z = 15629106
33 Z = 4761292
16
XDOT = -22898
370984 XDOT = -6987
544393
YDOT = 6248
165421 feet/sec YDOT = 1826
347412 meter/sec
ZDOT = -8547
708443 ZDOT = -2639
266923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15321173
52 X = -4669893
69
Y = -3523026
77 feet Y = -1073818
56 meter
Z = 15618641
82 Z = 4760562
03
XDOT = -3675
046586 XDOT = -1120
154200
YDOT = -22319
913980 feet/sec YDOT = -6803
109781 meter/sec
ZDOT = -8686
455271 ZDOT = -2647
631567
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 11349
54347310
00016717 00000-0 10270-3 0 9035
2 25544 51
6408 328
4201 0024441 167
9763 192
1980 15
58226930 29226
Satellite: ISS
Catalog Number: 25544
Epoch time: 11349
54347310 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 328
4201 deg
Eccentricity:
0024441
Arg of perigee: 167
9763 deg
Mean anomaly: 192
1980 deg
Mean motion: 15
58226930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2922
Checksum: 305
Coasting Arc #5 (Orbit 2936)
---------------------------------------
Vector Time (GMT): 2011/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3359164
35 A = 6774259
45 meter
Y = -5238084
62 meter E =
0022780
Z = -2715689
84 I = 51
44405
XDOT = 5594
461695 Wp = 159
58443
YDOT = 917
936572 meter/sec RA = 323
02716 deg
ZDOT = 5141
668269 TA = 169
65225
MA = 169
60528
Ha = 222
142 n
mi
Hp = 202
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11020880
42 X = 3430680
25
Y = -17185316
99 feet Y = -5200120
36 meter
Z = -8909743
58 Z = -2699197
70
XDOT = 18354
533119 XDOT = 5558
804187
YDOT = 3011
602927 feet/sec YDOT = 980
297604 meter/sec
ZDOT = 16868
990385 ZDOT = 5168
759466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15931551
51 X = 4855936
90
Y = 12813450
72 feet Y = 3905539
78 meter
Z = -8841923
05 Z = -2695018
14
XDOT = -3973
048537 XDOT = -1210
985194
YDOT = 16674
531261 feet/sec YDOT = 5082
397128 meter/sec
ZDOT = 16979
572360 ZDOT = 5175
373655
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 11350
50545011
00016717 00000-0 10270-3 0 9042
2 25544 51
6407 323
5946 0024455 171
1479 189
0112 15
58258678 29375
Satellite: ISS
Catalog Number: 25544
Epoch time: 11350
50545011 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 323
5946 deg
Eccentricity:
0024455
Arg of perigee: 171
1479 deg
Mean anomaly: 189
0112 deg
Mean motion: 15
58258678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2937
Checksum: 311
Coasting Arc #6 (Orbit 2952)
---------------------------------------
Vector Time (GMT): 2011/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5159545
49 A = 6777205
35 meter
Y = 4352247
78 meter E =
0034175
Z = -270476
67 I = 51
43132
XDOT = -2918
146465 Wp = 162
79061
YDOT = -3818
792473 meter/sec RA = 318
02024 deg
ZDOT = -6007
905591 TA = 20
14473
MA = 20
01018
Ha = 221
822 n
mi
Hp = 202
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16927642
68 X = -5206515
79
Y = 14279028
17 feet Y = 4294287
97 meter
Z = -887390
66 Z = -295655
57
XDOT = -9573
971341 XDOT = -2846
041825
YDOT = -12528
846696 feet/sec YDOT = -3851
021521 meter/sec
ZDOT = -19710
976347 ZDOT = -6021
906965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12741697
26 X = -3883669
33
Y = -18107761
69 feet Y = -5519245
76 meter
Z = -990611
61 Z = -301938
42
XDOT = 11989
581190 XDOT = 3654
424347
YDOT = -7391
399964 feet/sec YDOT = -2252
898709 meter/sec
ZDOT = -19767
840290 ZDOT = -6025
237720
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 11351
53153211
00016717 00000-0 10270-3 0 9054
2 25544 51
6413 318
4466 0024360 175
2313 184
9078 15
58301658 29539
Satellite: ISS
Catalog Number: 25544
Epoch time: 11351
53153211 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 318
4466 deg
Eccentricity:
0024360
Arg of perigee: 175
2313 deg
Mean anomaly: 184
9078 deg
Mean motion: 15
58301658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2953
Checksum: 297
Coasting Arc #7 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2011/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5558774
55 A = 6772722
16 meter
Y = -2289501
07 meter E =
0027036
Z = 3135061
35 I = 51
39533
XDOT = -289
766274 Wp = 150
34162
YDOT = 5951
314303 meter/sec RA = 313
00932 deg
ZDOT = 4819
005730 TA = 245
93547
MA = 246
21859
Ha = 221
632 n
mi
Hp = 202
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18237449
30 X = 5568733
47
Y = -7511486
45 feet Y = -2227283
92 meter
Z = 10285634
35 Z = 3162090
00
XDOT = -950
676753 XDOT = -379
703418
YDOT = 19525
309392 feet/sec YDOT = 5947
570845 meter/sec
ZDOT = 15810
386253 ZDOT = 4817
379890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6211762
48 X = 1893345
20
Y = 18658876
28 feet Y = 5687225
49 meter
Z = 10396230
20 Z = 3168770
97
XDOT = -18043
339211 XDOT = -5499
609792
YDOT = -2872
377718 feet/sec YDOT = -875
500728 meter/sec
ZDOT = 15803
239310 ZDOT = 4816
827342
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 11352
55758460
00016717 00000-0 10270-3 0 9065
2 25544 51
6412 313
2999 0024500 179
3448 180
7743 15
58385005 29690
Satellite: ISS
Catalog Number: 25544
Epoch time: 11352
55758460 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 313
2999 deg
Eccentricity:
0024500
Arg of perigee: 179
3448 deg
Mean anomaly: 180
7743 deg
Mean motion: 15
58385005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 329
Coasting Arc #8 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2011/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4520926
21 A = 6766257
25 meter
Y = -692058
34 meter E =
0023899
Z = -4989966
47 I = 51
35387
XDOT = 3195
244776 Wp = 151
31304
YDOT = -6684
737032 meter/sec RA = 307
96395 deg
ZDOT = -1992
344623 TA = 99
40225
MA = 99
13199
Ha = 221
348 n
mi
Hp = 202
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14832435
08 X = -4488610
99
Y = -2270532
60 feet Y = -742433
10 meter
Z = -16371281
07 Z = -5011850
80
XDOT = 10483
086537 XDOT = 3279
435854
YDOT = -21931
551941 feet/sec YDOT = -6648
534975 meter/sec
ZDOT = -6536
563725 ZDOT = -1976
617977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3053275
89 X = 930638
49
Y = -14591131
49 feet Y = -4447376
88 meter
Z = -16460609
98 Z = -5017193
92
XDOT = 20276
084026 XDOT = 6180
150411
YDOT = 11453
470914 feet/sec YDOT = 3491
017935 meter/sec
ZDOT = -6471
761803 ZDOT = -1972
592998
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 11353
51948652
00016717 00000-0 10270-3 0 9077
2 25544 51
6414 308
4726 0024304 182
7495 177
3531 15
58381704 29844
Satellite: ISS
Catalog Number: 25544
Epoch time: 11353
51948652 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 308
4726 deg
Eccentricity:
0024304
Arg of perigee: 182
7495 deg
Mean anomaly: 177
3531 deg
Mean motion: 15
58381704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 325
Coasting Arc #9 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2011/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2535348
35 A = 6765612
57 meter
Y = 3619342
17 meter E =
0021414
Z = 5117279
03 I = 51
33452
XDOT = -5040
041191 Wp = 176
71978
YDOT = 5602
006803 meter/sec RA = 302
89971 deg
ZDOT = -1485
810266 TA = 287
50800
MA = 287
74191
Ha = 221
109 n
mi
Hp = 203
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8318072
01 X = 2469828
73
Y = 11874482
20 feet Y = 3647327
21 meter
Z = 16788973
20 Z = 5129437
01
XDOT = -16535
568213 XDOT = -5095
091508
YDOT = 18379
287412 feet/sec YDOT = 5545
338296 meter/sec
ZDOT = -4874
705596 ZDOT = -1510
428179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12164303
10 X = -3707679
58
Y = 7782270
13 feet Y = 2372035
94 meter
Z = 16838327
48 Z = 5132322
22
XDOT = -17203
689727 XDOT = -5243
684629
YDOT = -16271
437092 feet/sec YDOT = -4959
534026 meter/sec
ZDOT = -4975
731997 ZDOT = -1516
603113
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 11354
54548721
00016717 00000-0 10270-3 0 9085
2 25544 51
6417 303
3257 0024261 186
5830 173
5010 15
58422214 30009
Satellite: ISS
Catalog Number: 25544
Epoch time: 11354
54548721 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 303
3257 deg
Eccentricity:
0024261
Arg of perigee: 186
5830 deg
Mean anomaly: 173
5010 deg
Mean motion: 15
58422214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 278
Coasting Arc #10 (Orbit 3014)
---------------------------------------
Vector Time (GMT): 2011/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -82302
46 A = 6771608
77 meter
Y = -5818274
80 meter E =
0024115
Z = -3488079
64 I = 51
33917
XDOT = 5538
823294 Wp = 178
10975
YDOT = -2786
525448 meter/sec RA = 297
84709 deg
ZDOT = 4494
572221 TA = 140
70951
MA = 140
53428
Ha = 220
938 n
mi
Hp = 203
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -270021
19 X = -290
68
Y = -19088828
08 feet Y = -5818736
20 meter
Z = -11443830
85 Z = -3488280
93
XDOT = 18171
992433 XDOT = 5547
737164
YDOT = -9142
143857 feet/sec YDOT = -2724
537601 meter/sec
ZDOT = 14745
971854 ZDOT = 4521
501323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19089867
42 X = 5818591
59
Y = 160138
65 feet Y = 48810
26 meter
Z = -11444162
31 Z = -3488180
67
XDOT = 8809
514095 XDOT = 2685
139896
YDOT = 16859
933421 feet/sec YDOT = 5138
907707 meter/sec
ZDOT = 14856
203247 ZDOT = 4528
170750
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 11355
50733671
00016717 00000-0 10270-3 0 9093
2 25544 51
6416 298
4984 0024205 190
3231 169
7430 15
58457967 30157
Satellite: ISS
Catalog Number: 25544
Epoch time: 11355
50733671 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 298
4984 deg
Eccentricity:
0024205
Arg of perigee: 190
3231 deg
Mean anomaly: 169
7430 deg
Mean motion: 15
58457967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3015
Checksum: 324
Coasting Arc #11 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2011/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2127673
54 A = 6776524
84 meter
Y = 6378737
42 meter E =
0032048
Z = 642036
33 I = 51
34382
XDOT = -4760
220767 Wp = 171
73345
YDOT = -986
969598 meter/sec RA = 292
82671 deg
ZDOT = -5963
650646 TA = 1
27542
MA = 1
26727
Ha = 220
671 n
mi
Hp = 203
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6980556
24 X = -2201962
62
Y = 20927616
20 feet Y = 6354529
00 meter
Z = 2106418
39 Z = 631520
48
XDOT = -15617
522200 XDOT = -4719
860073
YDOT = -3238
089232 feet/sec YDOT = -1039
974821 meter/sec
ZDOT = -19565
782959 ZDOT = -5986
677963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20915798
22 X = -6375135
30
Y = -7028798
19 feet Y = -2142377
69 meter
Z = 2062926
16 Z = 628779
89
XDOT = 2753
054951 XDOT = 839
131149
YDOT = -13968
072278 feet/sec YDOT = -4257
468430 meter/sec
ZDOT = -19659
763700 ZDOT = -5992
295976
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 11356
53328408
00016717 00000-0 10270-3 0 9107
2 25544 51
6427 293
3502 0024274 194
0111 166
0374 15
58491892 30313
Satellite: ISS
Catalog Number: 25544
Epoch time: 11356
53328408 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 293
3502 deg
Eccentricity:
0024274
Arg of perigee: 194
0111 deg
Mean anomaly: 166
0374 deg
Mean motion: 15
58491892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3031
Checksum: 294
Coasting Arc #12 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2011/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3697525
55 A = 6773925
05 meter
Y = -5140705
40 meter E =
0020301
Z = 2433246
63 I = 51
32492
XDOT = 2965
204343 Wp = 163
01890
YDOT = 4659
375018 meter/sec RA = 287
81305 deg
ZDOT = 5307
612987 TA = 224
33223
MA = 224
49497
Ha = 220
409 n
mi
Hp = 203
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12130989
34 X = 3742914
89
Y = -16865831
37 feet Y = -5099103
98 meter
Z = 7983092
60 Z = 2451318
64
XDOT = 9728
360707 XDOT = 2887
098552
YDOT = 15286
663445 feet/sec YDOT = 4692
096241 meter/sec
ZDOT = 17413
428435 ZDOT = 5321
828896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17050606
51 X = 5197024
86
Y = 11819597
39 feet Y = 3602613
28 meter
Z = 8057349
01 Z = 2455879
98
XDOT = -14274
793043 XDOT = -4350
956920
YDOT = 8615
215683 feet/sec YDOT = 2625
917740 meter/sec
ZDOT = 17471
113907 ZDOT = 5325
195519
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 11357
55920256
00016717 00000-0 10270-3 0 9110
2 25544 51
6426 288
2018 0024224 198
0247 162
0051 15
58555647 30470
Satellite: ISS
Catalog Number: 25544
Epoch time: 11357
55920256 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 288
2018 deg
Eccentricity:
0024224
Arg of perigee: 198
0247 deg
Mean anomaly: 162
0051 deg
Mean motion: 15
58555647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3047
Checksum: 304
Coasting Arc #13 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2011/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4346452
39 A = 6766891
16 meter
Y = 2232394
12 meter E =
0018922
Z = -4674121
58 I = 51
29424
XDOT = -678
372158 Wp = 175
42486
YDOT = -7123
477917 meter/sec RA = 282
77094 deg
ZDOT = -2790
736587 TA = 66
92513
MA = 66
72576
Ha = 219
980 n
mi
Hp = 203
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14260014
40 X = -4348386
59
Y = 7324127
68 feet Y = 2183779
31 meter
Z = -15335044
56 Z = -4695240
82
XDOT = -2225
630441 XDOT = -585
108821
YDOT = -23370
990541 feet/sec YDOT = -7130
542002 meter/sec
ZDOT = -9155
959931 ZDOT = -2793
806639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7782522
75 X = -2372112
93
Y = -13919905
50 feet Y = -4242787
20 meter
Z = -15421511
57 Z = -4700476
73
XDOT = 22273
013246 XDOT = 6788
814437
YDOT = -2365
646389 feet/sec YDOT = -721
049019 meter/sec
ZDOT = -9167
915514 ZDOT = -2794
380649
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 11358
52097697
00016717 00000-0 10270-3 0 9123
2 25544 51
6432 283
3748 0024125 201
5278 158
4865 15
58606972 30624
Satellite: ISS
Catalog Number: 25544
Epoch time: 11358
52097697 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 283
3748 deg
Eccentricity:
0024125
Arg of perigee: 201
5278 deg
Mean anomaly: 158
4865 deg
Mean motion: 15
58606972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 331
Coasting Arc #14 (Orbit 3077)
---------------------------------------
Vector Time (GMT): 2011/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4061495
01 A = 6764355
46 meter
Y = 1342229
66 meter E =
0021829
Z = 5244688
87 I = 51
28032
XDOT = -1583
286930 Wp = 200
56397
YDOT = 7473
814432 meter/sec RA = 277
70247 deg
ZDOT = -707
601663 TA = 256
10321
MA = 256
34612
Ha = 219
717 n
mi
Hp = 203
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13325114
86 X = 4020706
68
Y = 4403640
61 feet Y = 1387418
98 meter
Z = 17206984
47 Z = 5264320
45
XDOT = -5194
510925 XDOT = -1663
305583
YDOT = 24520
388557 feet/sec YDOT = 7455
661838 meter/sec
ZDOT = -2321
527766 ZDOT = -715
486459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3739663
27 X = -1139849
36
Y = 13423954
90 feet Y = 4091621
45 meter
Z = 17287087
81 Z = 5269104
36
XDOT = -23769
249412 XDOT = -7244
867221
YDOT = -3678
060699 feet/sec YDOT = -1121
072901 meter/sec
ZDOT = -2354
348905 ZDOT = -717
605546
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 11359
54684261
00016717 00000-0 10270-3 0 9136
2 25544 51
6430 278
2274 0024187 205
6802 154
3153 15
58657999 30782
Satellite: ISS
Catalog Number: 25544
Epoch time: 11359
54684261 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 278
2274 deg
Eccentricity:
0024187
Arg of perigee: 205
6802 deg
Mean anomaly: 154
3153 deg
Mean motion: 15
58657999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3078
Checksum: 332
Coasting Arc #15 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2011/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2934076
93 A = 6769508
82 meter
Y = -4680186
85 meter E =
0023639
Z = -3926644
88 I = 51
29487
XDOT = 3462
426788 Wp = 192
89612
YDOT = -5547
655288 meter/sec RA = 272
63847 deg
ZDOT = 3997
735640 TA = 119
16391
MA = 118
92717
Ha = 219
528 n
mi
Hp = 203
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9626236
64 X = -2862449
49
Y = -15354943
74 feet Y = -4712596
52 meter
Z = -12882693
18 Z = -3940724
98
XDOT = 11359
667941 XDOT = 3504
784508
YDOT = -18200
968792 feet/sec YDOT = -5508
699971 meter/sec
ZDOT = 13115
930578 ZDOT = 4014
658004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14680873
97 X = 4474730
39
Y = -10556257
05 feet Y = -3217547
15 meter
Z = -12939856
60 Z = -3944068
29
XDOT = 18145
863127 XDOT = 5530
859081
YDOT = 8963
682261 feet/sec YDOT = 2732
130353 meter/sec
ZDOT = 13185
517446 ZDOT = 4018
945717
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 11360
50856837
00016717 00000-0 10270-3 0 9145
2 25544 51
6431 273
3993 0024135 209
0268 150
9547 15
58683926 30939
Satellite: ISS
Catalog Number: 25544
Epoch time: 11360
50856837 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 273
3993 deg
Eccentricity:
0024135
Arg of perigee: 209
0268 deg
Mean anomaly: 150
9547 deg
Mean motion: 15
58683926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 328
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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