[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 8th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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 392)
---------------------------------------
Vector Time (GMT): 2011/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4831496
51 A = 6765438
14 meter
Y = -2182302
30 meter E =
0007626
Z = 4208432
23 I = 51
94261
XDOT = -199
113904 Wp = 357
09987
YDOT = -6715
660671 meter/sec RA = 62
73231 deg
ZDOT = -3703
898130 TA = 130
75039
MA = 130
68416
Ha = 211
848 n
mi
Hp = 208
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15851366
49 X = -4827178
03
Y = -7159784
46 feet Y = -2236307
27 meter
Z = 13807192
34 Z = 4184971
41
XDOT = -653
260841 XDOT = -106
010658
YDOT = -22033
007450 feet/sec YDOT = -6717
366381 meter/sec
ZDOT = -12151
896753 ZDOT = -3704
639875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3291299
71 X = -1003188
15
Y = 17155600
71 feet Y = 5229027
10 meter
Z = 13712024
06 Z = 4179424
93
XDOT = -20054
807090 XDOT = -6112
705201
YDOT = 5886
116467 feet/sec YDOT = 1794
088299 meter/sec
ZDOT = -12154
526440 ZDOT = -3704
699659
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 11187
54128726
00016717 00000-0 10270-3 0 9000
2 25544 51
6401 63
2151 0011411 295
8925 64
1054 15
59801685 3938
Satellite: ISS
Catalog Number: 25544
Epoch time: 11187
54128726 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 63
2151 deg
Eccentricity:
0011411
Arg of perigee: 295
8925 deg
Mean anomaly: 64
1054 deg
Mean motion: 15
59801685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 393
Checksum: 292
Coasting Arc #2 (Orbit 407)
---------------------------------------
Vector Time (GMT): 2011/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4324097
47 A = 6772327
10 meter
Y = 5053937
50 meter E =
0013579
Z = -1224922
88 I = 51
95057
XDOT = -2952
713736 Wp = 341
08562
YDOT = 3954
564026 meter/sec RA = 57
73749 deg
ZDOT = 5887
228425 TA = 5
61759
MA = 5
60237
Ha = 212
149 n
mi
Hp = 207
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14186671
48 X = 4273212
39
Y = 16581159
79 feet Y = 5102007
79 meter
Z = -4018775
85 Z = -1204039
73
XDOT = -9687
381023 XDOT = -3025
313825
YDOT = 12974
291423 feet/sec YDOT = 3921
138520 meter/sec
ZDOT = 19315
053888 ZDOT = 5872
708279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12551113
67 X = 3825579
45
Y = -17870039
23 feet Y = -5446787
96 meter
Z = -3934248
45 Z = -1199158
93
XDOT = 13693
656506 XDOT = 4173
826503
YDOT = 5374
309425 feet/sec YDOT = 1638
089513 meter/sec
ZDOT = 19255
846438 ZDOT = 5869
181994
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 11188
50232640
00016717 00000-0 10270-3 0 9019
2 25544 51
6399 58
3821 0011451 299
2555 60
7456 15
59784158 4084
Satellite: ISS
Catalog Number: 25544
Epoch time: 11188
50232640 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 58
3821 deg
Eccentricity:
0011451
Arg of perigee: 299
2555 deg
Mean anomaly: 60
7456 deg
Mean motion: 15
59784158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 408
Checksum: 317
Coasting Arc #3 (Orbit 423)
---------------------------------------
Vector Time (GMT): 2011/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2258920
29 A = 6770679
11 meter
Y = -5952410
57 meter E =
0006003
Z = -2302646
77 I = 51
92777
XDOT = 5404
983562 Wp = 289
37118
YDOT = 60
880259 meter/sec RA = 52
76078 deg
ZDOT = -5446
259537 TA = 276
22565
MA = 276
29403
Ha = 212
307 n
mi
Hp = 207
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7411155
82 X = -2181005
61
Y = -19528906
08 feet Y = -5977235
31 meter
Z = -7554615
40 Z = -2313431
92
XDOT = 17732
885703 XDOT = 5430
357887
YDOT = 199
738384 feet/sec YDOT = 121
464520 meter/sec
ZDOT = -17868
305566 ZDOT = -5419
940612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16892411
17 X = -5148806
92
Y = 12259341
84 feet Y = 3736647
39 meter
Z = -7598065
52 Z = -2315890
37
XDOT = -3623
267013 XDOT = -1104
371786
YDOT = -16027
919674 feet/sec YDOT = -4885
309917 meter/sec
ZDOT = -17761
409786 ZDOT = -5413
677703
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 11189
52742399
00016717 00000-0 10270-3 0 9020
2 25544 51
6396 53
2282 0011511 302
3137 57
6903 15
59773754 4245
Satellite: ISS
Catalog Number: 25544
Epoch time: 11189
52742399 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 53
2282 deg
Eccentricity:
0011511
Arg of perigee: 302
3137 deg
Mean anomaly: 57
6903 deg
Mean motion: 15
59773754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 424
Checksum: 309
Coasting Arc #4 (Orbit 439)
---------------------------------------
Vector Time (GMT): 2011/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -852760
75 A = 6763069
44 meter
Y = 4676211
13 meter E =
0004380
Z = 4812015
69 I = 51
88322
XDOT = -6165
104181 Wp = 319
45165
YDOT = -3775
499437 meter/sec RA = 47
74959 deg
ZDOT = 2580
958753 TA = 105
27236
MA = 105
22394
Ha = 212
631 n
mi
Hp = 207
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2797771
49 X = -928363
50
Y = 15341900
03 feet Y = 4666251
71 meter
Z = 15787453
05 Z = 4807689
95
XDOT = -20226
719755 XDOT = -6134
965400
YDOT = -12386
809178 feet/sec YDOT = -3844
273197 meter/sec
ZDOT = 8467
712443 ZDOT = 2551
081491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15538088
05 X = 4736009
24
Y = -1527339
58 feet Y = -465533
10 meter
Z = 15769595
72 Z = 4806572
78
XDOT = -6312
435398 XDOT = -1924
030309
YDOT = 21804
613197 feet/sec YDOT = 6646
046102 meter/sec
ZDOT = 8346
592555 ZDOT = 2544
041411
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 11190
55251139
00016717 00000-0 10270-3 0 9033
2 25544 51
6396 48
0727 0011485 307
3057 52
7051 15
59783609 4405
Satellite: ISS
Catalog Number: 25544
Epoch time: 11190
55251139 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 48
0727 deg
Eccentricity:
0011485
Arg of perigee: 307
3057 deg
Mean anomaly: 52
7051 deg
Mean motion: 15
59783609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 440
Checksum: 302
Coasting Arc #5 (Orbit 454)
---------------------------------------
Vector Time (GMT): 2011/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3926457
75 A = 6761457
79 meter
Y = -1900361
54 meter E =
0006763
Z = -5169164
17 I = 51
85614
XDOT = 4719
361536 Wp = 44
18430
YDOT = 5882
122517 meter/sec RA = 42
70598 deg
ZDOT = 1428
174501 TA = 239
46790
MA = 239
53468
Ha = 212
765 n
mi
Hp = 207
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12882079
23 X = 3972526
90
Y = -6234781
97 feet Y = -1856195
13 meter
Z = -16959200
04 Z = -5149977
90
XDOT = 15483
469607 XDOT = 4646
297963
YDOT = 19298
302221 feet/sec YDOT = 5934
488550 meter/sec
ZDOT = 4685
611880 ZDOT = 1450
924499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9810236
41 X = -2990160
06
Y = -10546134
82 feet Y = -3214461
89 meter
Z = -16881150
42 Z = -5145374
65
XDOT = 13068
948242 XDOT = 3983
415424
YDOT = -19773
685654 feet/sec YDOT = -6027
019387 meter/sec
ZDOT = 4777
644575 ZDOT = 1456
226067
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 11191
51351880
00016717 00000-0 10270-3 0 9045
2 25544 51
6386 43
2396 0011572 310
2818 49
7325 15
59842886 4557
Satellite: ISS
Catalog Number: 25544
Epoch time: 11191
51351880 = yrday
fracday
Element set: 904
Inclination: 51
6386 deg
RA of node: 43
2396 deg
Eccentricity:
0011572
Arg of perigee: 310
2818 deg
Mean anomaly: 49
7325 deg
Mean motion: 15
59842886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 455
Checksum: 316
Coasting Arc #6 (Orbit 470)
---------------------------------------
Vector Time (GMT): 2011/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5816226
26 A = 6768334
34 meter
Y = -1307212
59 meter E =
0008528
Z = 3209792
52 I = 51
85724
XDOT = -1354
180307 Wp = 30
53842
YDOT = -5819
944461 meter/sec RA = 37
68077 deg
ZDOT = -4811
262808 TA = 112
39122
MA = 112
30085
Ha = 212
901 n
mi
Hp = 207
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19082107
17 X = -5816768
96
Y = -4288755
20 feet Y = -1372256
75 meter
Z = 10530815
34 Z = 3181535
94
XDOT = -4442
848776 XDOT = -1265
627838
YDOT = -19094
305976 feet/sec YDOT = -5834
591784 meter/sec
ZDOT = -15784
982965 ZDOT = -4817
627272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1927107
73 X = 587382
44
Y = 19524571
10 feet Y = 5951089
27 meter
Z = 10416126
24 Z = 3174835
28
XDOT = -15347
115340 XDOT = -4677
800756
YDOT = 9972
062803 feet/sec YDOT = 3039
484742 meter/sec
ZDOT = -15810
457837 ZDOT = -4819
027549
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 11192
53858322
00016717 00000-0 10270-3 0 9052
2 25544 51
6392 38
0855 0011813 314
1786 45
8399 15
59889935 4713
Satellite: ISS
Catalog Number: 25544
Epoch time: 11192
53858322 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 38
0855 deg
Eccentricity:
0011813
Arg of perigee: 314
1786 deg
Mean anomaly: 45
8399 deg
Mean motion: 15
59889935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 471
Checksum: 339
Coasting Arc #7 (Orbit 486)
---------------------------------------
Vector Time (GMT): 2011/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5605868
24 A = 6772729
79 meter
Y = 3775040
16 meter E =
0017153
Z = 189946
69 I = 51
84559
XDOT = -2794
070584 Wp = 4
33436
YDOT = 3844
341829 meter/sec RA = 32
69145 deg
ZDOT = 6039
044624 TA = 357
71309
MA = 357
72093
Ha = 213
105 n
mi
Hp = 206
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18391956
18 X = 5562315
66
Y = 12385302
35 feet Y = 3837484
83 meter
Z = 623184
67 Z = 217074
57
XDOT = -9166
898240 XDOT = -2866
187334
YDOT = 12612
670044 feet/sec YDOT = 3812
692526 meter/sec
ZDOT = 19813
138530 ZDOT = 6025
296703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5631431
74 X = 1716460
39
Y = -21442892
15 feet Y = -6535793
53 meter
Z = 733129
17 Z = 223457
77
XDOT = 13406
039272 XDOT = 4086
160770
YDOT = 4198
028541 feet/sec YDOT = 1279
559099 meter/sec
ZDOT = 19757
041680 ZDOT = 6021
946304
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 11193
56363968
00016717 00000-0 10270-3 0 9064
2 25544 51
6377 32
9296 0011668 317
8467 42
1790 15
59852264 4879
Satellite: ISS
Catalog Number: 25544
Epoch time: 11193
56363968 = yrday
fracday
Element set: 906
Inclination: 51
6377 deg
RA of node: 32
9296 deg
Eccentricity:
0011668
Arg of perigee: 317
8467 deg
Mean anomaly: 42
1790 deg
Mean motion: 15
59852264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 487
Checksum: 347
Coasting Arc #8 (Orbit 501)
---------------------------------------
Vector Time (GMT): 2011/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3225376
74 A = 6767347
80 meter
Y = -4810679
24 meter E =
0009821
Z = -3507738
40 I = 51
80118
XDOT = 6137
524287 Wp = 347
30745
YDOT = -803
585451 meter/sec RA = 27
69834 deg
ZDOT = -4529
636857 TA = 233
93031
MA = 234
02132
Ha = 213
239 n
mi
Hp = 206
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10581944
68 X = -3154303
40
Y = -15783068
36 feet Y = -4846349
35 meter
Z = -11508328
08 Z = -3523235
23
XDOT = 20136
234538 XDOT = 6168
057764
YDOT = -2636
435208 feet/sec YDOT = -734
780403 meter/sec
ZDOT = -14861
013312 ZDOT = -4499
747237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11173979
37 X = -3405828
91
Y = 15322516
76 feet Y = 4670303
11 meter
Z = -11570958
48 Z = -3526828
15
XDOT = -8351
850055 XDOT = -2545
643897
YDOT = -17250
307275 feet/sec YDOT = -5257
893658 meter/sec
ZDOT = -14739
544395 ZDOT = -4492
613132
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 11194
52461840
00016717 00000-0 10270-3 0 9070
2 25544 51
6368 28
0972 0011653 321
7022 38
3306 15
59883698 5024
Satellite: ISS
Catalog Number: 25544
Epoch time: 11194
52461840 = yrday
fracday
Element set: 907
Inclination: 51
6368 deg
RA of node: 28
0972 deg
Eccentricity:
0011653
Arg of perigee: 321
7022 deg
Mean anomaly: 38
3306 deg
Mean motion: 15
59883698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 502
Checksum: 308
Coasting Arc #9 (Orbit 517)
---------------------------------------
Vector Time (GMT): 2011/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -585975
32 A = 6761032
24 meter
Y = 4232755
25 meter E =
0008552
Z = 5241521
30 I = 51
75221
XDOT = -7286
864803 Wp = 334
66203
YDOT = -2208
073339 meter/sec RA = 22
66091 deg
ZDOT = 976
621616 TA = 106
06222
MA = 105
96803
Ha = 213
515 n
mi
Hp = 206
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1922491
20 X = -658725
07
Y = 13886992
27 feet Y = 4225794
89 meter
Z = 17196592
18 Z = 5238498
68
XDOT = -23907
036755 XDOT = -7266
376274
YDOT = -7244
335103 feet/sec YDOT = -2289
445097 meter/sec
ZDOT = 3204
139160 ZDOT = 941
272173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13679537
11 X = 4169522
91
Y = -3137935
22 feet Y = -956442
66 meter
Z = 17184031
44 Z = 5237692
78
XDOT = 1677
646818 XDOT = 511
346750
YDOT = 23928
179422 feet/sec YDOT = 7293
309088 meter/sec
ZDOT = 3060
688161 ZDOT = 932
897751
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 11195
54965360
00016717 00000-0 10270-3 0 9080
2 25544 51
6367 22
9408 0011598 325
7058 34
3348 15
59847498 5188
Satellite: ISS
Catalog Number: 25544
Epoch time: 11195
54965360 = yrday
fracday
Element set: 908
Inclination: 51
6367 deg
RA of node: 22
9408 deg
Eccentricity:
0011598
Arg of perigee: 325
7058 deg
Mean anomaly: 34
3348 deg
Mean motion: 15
59847498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 518
Checksum: 342
Coasting Arc #10 (Orbit 532)
---------------------------------------
Vector Time (GMT): 2011/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4311822
91 A = 6763613
64 meter
Y = -2441430
69 meter E =
0007305
Z = -4603568
87 I = 51
73254
XDOT = 5622
940969 Wp = 28
89063
YDOT = 4274
179675 meter/sec RA = 17
60886 deg
ZDOT = 3008
086806 TA = 271
00623
MA = 271
08993
Ha = 213
590 n
mi
Hp = 206
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14146400
61 X = 4361165
76
Y = -8009943
21 feet Y = -2392936
70 meter
Z = -15103572
41 Z = -4582503
04
XDOT = 18447
969057 XDOT = 5560
115967
YDOT = 14022
899196 feet/sec YDOT = 4336
707110 meter/sec
ZDOT = 9869
051201 ZDOT = 3035
250425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12796961
71 X = -3900513
93
Y = -10153825
29 feet Y = -3094885
95 meter
Z = -15017834
16 Z = -4577435
85
XDOT = 5293
826109 XDOT = 1613
558198
YDOT = -21391
088618 feet/sec YDOT = -6520
003811 meter/sec
ZDOT = 9979
114148 ZDOT = 3041
633992
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 11196
51061137
00016717 00000-0 10270-3 0 9098
2 25544 51
6362 18
1069 0011514 328
9254 31
1219 15
59911247 5337
Satellite: ISS
Catalog Number: 25544
Epoch time: 11196
51061137 = yrday
fracday
Element set: 909
Inclination: 51
6362 deg
RA of node: 18
1069 deg
Eccentricity:
0011514
Arg of perigee: 328
9254 deg
Mean anomaly: 31
1219 deg
Mean motion: 15
59911247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 533
Checksum: 289
Coasting Arc #11 (Orbit 548)
---------------------------------------
Vector Time (GMT): 2011/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6511789
34 A = 6770996
50 meter
Y = 48820
60 meter E =
0008700
Z = 1859747
03 I = 51
72905
XDOT = -1654
562705 Wp = 56
40236
YDOT = -4929
025808 meter/sec RA = 12
59152 deg
ZDOT = -5640
282562 TA = 103
12372
MA = 103
02661
Ha = 213
682 n
mi
Hp = 205
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21364138
25 X = -6520885
38
Y = 160172
58 feet Y = -24049
28 meter
Z = 6101532
24 Z = 1828091
46
XDOT = -5428
355332 XDOT = -1571
923635
YDOT = -16171
344513 feet/sec YDOT = -4947
065374 meter/sec
ZDOT = -18504
864048 ZDOT = -5648
120112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8574634
22 X = 2613548
51
Y = 19608173
23 feet Y = 5976571
20 meter
Z = 5972934
34 Z = 1820550
39
XDOT = -11342
011175 XDOT = -3457
045006
YDOT = 10630
468257 feet/sec YDOT = 3240
166725 meter/sec
ZDOT = -18536
377012 ZDOT = -5649
887713
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 11197
53562190
00016717 00000-0 10270-3 0 9108
2 25544 51
6366 12
9516 0011833 332
4342 27
6185 15
59966105 5494
Satellite: ISS
Catalog Number: 25544
Epoch time: 11197
53562190 = yrday
fracday
Element set: 910
Inclination: 51
6366 deg
RA of node: 12
9516 deg
Eccentricity:
0011833
Arg of perigee: 332
4342 deg
Mean anomaly: 27
6185 deg
Mean motion: 15
59966105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 549
Checksum: 306
Coasting Arc #12 (Orbit 564)
---------------------------------------
Vector Time (GMT): 2011/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6157308
91 A = 6771179
32 meter
Y = 2192611
55 meter E =
0018349
Z = 1721034
74 I = 51
69967
XDOT = -3069
491059 Wp = 25
76496
YDOT = 4136
329166 meter/sec RA = 7
59821 deg
ZDOT = 5705
360280 TA = 353
16845
MA = 353
19343
Ha = 213
754 n
mi
Hp = 205
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20201144
71 X = 6123972
81
Y = 7193607
44 feet Y = 2261279
76 meter
Z = 5646439
44 Z = 1750865
47
XDOT = -10070
508724 XDOT = -3143
231085
YDOT = 13570
633746 feet/sec YDOT = 4101
591365 meter/sec
ZDOT = 18718
373621 ZDOT = 5690
270369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1696103
22 X = -516972
26
Y = -21344225
85 feet Y = -6505720
04 meter
Z = 5767475
28 Z = 1757926
46
XDOT = 14995
062973 XDOT = 4570
495194
YDOT = 3855
436590 feet/sec YDOT = 1175
137073 meter/sec
ZDOT = 18656
803849 ZDOT = 5686
593813
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 11198
56062508
00016717 00000-0 10270-3 0 9111
2 25544 51
6364 7
7955 0011529 336
7283 23
3350 15
59938276 5657
Satellite: ISS
Catalog Number: 25544
Epoch time: 11198
56062508 = yrday
fracday
Element set: 911
Inclination: 51
6364 deg
RA of node: 7
7955 deg
Eccentricity:
0011529
Arg of perigee: 336
7283 deg
Mean anomaly: 23
3350 deg
Mean motion: 15
59938276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 565
Checksum: 322
Coasting Arc #13 (Orbit 579)
---------------------------------------
Vector Time (GMT): 2011/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3381460
60 A = 6763591
54 meter
Y = -3735795
25 meter E =
0015385
Z = -4524051
11 I = 51
64545
XDOT = 6641
227235 Wp = 20
68924
YDOT = -2191
097014 meter/sec RA = 2
57863 deg
ZDOT = -3143
777971 TA = 217
73285
MA = 217
84084
Ha = 213
927 n
mi
Hp = 205
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11094030
83 X = -3317458
37
Y = -12256546
11 feet Y = -3773250
58 meter
Z = -14842687
36 Z = -4540322
72
XDOT = 21788
803263 XDOT = 6680
506474
YDOT = -7188
638497 feet/sec YDOT = -2116
610886 meter/sec
ZDOT = -10314
232189 ZDOT = -3111
420390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6415443
51 X = -1955427
18
Y = 15171792
26 feet Y = 4624362
28 meter
Z = -14908541
67 Z = -4544123
50
XDOT = -14690
762594 XDOT = -4477
744439
YDOT = -16252
731781 feet/sec YDOT = -4953
832647 meter/sec
ZDOT = -10182
649913 ZDOT = -3103
671694
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 11199
52155356
00016717 00000-0 10270-3 0 9123
2 25544 51
6373 2
9632 0011539 341
1459 18
9268 15
59975032 5808
Satellite: ISS
Catalog Number: 25544
Epoch time: 11199
52155356 = yrday
fracday
Element set: 912
Inclination: 51
6373 deg
RA of node: 2
9632 deg
Eccentricity:
0011539
Arg of perigee: 341
1459 deg
Mean anomaly: 18
9268 deg
Mean motion: 15
59975032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 580
Checksum: 315
Coasting Arc #14 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2011/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -792966
79 A = 6760787
68 meter
Y = 4194335
47 meter E =
0012857
Z = 5244537
51 I = 51
60477
XDOT = -7620
584357 Wp = 359
31532
YDOT = -350
977080 meter/sec RA = 357
51785 deg
ZDOT = -858
953442 TA = 98
96512
MA = 98
81957
Ha = 214
184 n
mi
Hp = 205
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2601597
07 X = -865286
24
Y = 13760943
15 feet Y = 4185063
31 meter
Z = 17206487
91 Z = 5240509
98
XDOT = -25001
917182 XDOT = -7611
920726
YDOT = -1151
499605 feet/sec YDOT = -436
146595 meter/sec
ZDOT = -2818
088720 ZDOT = -895
952499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13545537
88 X = 4128679
95
Y = -3636246
10 feet Y = -1108327
81 meter
Z = 17189857
69 Z = 5239468
62
XDOT = 9711
089969 XDOT = 2959
940222
YDOT = 21947
517171 feet/sec YDOT = 6689
603234 meter/sec
ZDOT = -2968
353770 ZDOT = -904
754229
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 11200
54653462
00016717 00000-0 10270-3 0 9130
2 25544 51
6369 357
8067 0011487 345
0527 15
0287 15
59929390 5960
Satellite: ISS
Catalog Number: 25544
Epoch time: 11200
54653462 = yrday
fracday
Element set: 913
Inclination: 51
6369 deg
RA of node: 357
8067 deg
Eccentricity:
0011487
Arg of perigee: 345
0527 deg
Mean anomaly: 15
0287 deg
Mean motion: 15
59929390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 324
Coasting Arc #15 (Orbit 610)
---------------------------------------
Vector Time (GMT): 2011/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4588876
77 A = 6766980
63 meter
Y = -3458232
93 meter E =
0011101
Z = -3566376
13 I = 51
59733
XDOT = 5580
857664 Wp = 14
44334
YDOT = 2824
602370 meter/sec RA = 352
46869 deg
ZDOT = 4455
478365 TA = 303
26341
MA = 303
36972
Ha = 214
247 n
mi
Hp = 204
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15055369
99 X = 4644530
88
Y = -11345908
58 feet Y = -3406605
91 meter
Z = -11700709
07 Z = -3543948
76
XDOT = 18309
900472 XDOT = 5527
214071
YDOT = 9267
068142 feet/sec YDOT = 2886
710698 meter/sec
ZDOT = 14617
711172 ZDOT = 4482
459618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16995818
73 X = -5180325
55
Y = -8286407
40 feet Y = -2525696
97 meter
Z = -11609392
66 Z = -3538542
88
XDOT = -666
344412 XDOT = -203
101777
YDOT = -19203
652694 feet/sec YDOT = -5853
273341 meter/sec
ZDOT = 14727
120622 ZDOT = 4488
826366
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 11201
50744123
00016717 00000-0 10270-3 0 9143
2 25544 51
6383 352
9741 0011492 348
2801 11
8085 15
59991620 6110
Satellite: ISS
Catalog Number: 25544
Epoch time: 11201
50744123 = yrday
fracday
Element set: 914
Inclination: 51
6383 deg
RA of node: 352
9741 deg
Eccentricity:
0011492
Arg of perigee: 348
2801 deg
Mean anomaly: 11
8085 deg
Mean motion: 15
59991620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 611
Checksum: 287
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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