[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 3rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 315)
---------------------------------------
Vector Time (GMT): 2011/182/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3569277
52 A = 6763750
43 meter
Y = 3253834
33 meter E =
0004701
Z = 4739633
76 I = 51
97389
XDOT = -2455
623150 Wp = 240
37278
YDOT = -6722
833469 meter/sec RA = 87
52450 deg
ZDOT = 2765
860476 TA = 182
39405
MA = 182
39630
Ha = 210
445 n
mi
Hp = 208
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11710228
08 X = -3628421
20
Y = 10675309
49 feet Y = 3213588
94 meter
Z = 15549979
53 Z = 4722151
39
XDOT = -8056
506396 XDOT = -2393
700478
YDOT = -22056
540254 feet/sec YDOT = -6749
948019 meter/sec
ZDOT = 9074
345394 ZDOT = 2754
080399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14989102
94 X = 4568678
57
Y = 5350406
63 feet Y = 1630803
94 meter
Z = 15478807
44 Z = 4717940
51
XDOT = -15206
909183 XDOT = -4635
065919
YDOT = 16485
065186 feet/sec YDOT = 5024
647869 meter/sec
ZDOT = 9026
867504 ZDOT = 2751
389215
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 11182
60780787
00016717 00000-0 10270-3 0 9003
2 25544 51
6414 88
0160 0011101 276
7601 83
2291 15
59676876 3164
Satellite: ISS
Catalog Number: 25544
Epoch time: 11182
60780787 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 88
0160 deg
Eccentricity:
0011101
Arg of perigee: 276
7601 deg
Mean anomaly: 83
2291 deg
Mean motion: 15
59676876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 316
Checksum: 301
Coasting Arc #2 (Orbit 330)
---------------------------------------
Vector Time (GMT): 2011/183/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4224778
61 A = 6761602
64 meter
Y = 782730
95 meter E =
0002951
Z = -5223467
93 I = 51
96447
XDOT = 62
723953 Wp = 93
99914
YDOT = 7583
022500 meter/sec RA = 82
49011 deg
ZDOT = 1187
413321 TA = 187
32579
MA = 187
33011
Ha = 210
792 n
mi
Hp = 208
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13860822
22 X = 4241086
18
Y = 2568014
92 feet Y = 830067
04 meter
Z = -17137361
98 Z = -5202904
57
XDOT = 205
787249 XDOT = -27
843667
YDOT = 24878
682743 feet/sec YDOT = 7583
217328 meter/sec
ZDOT = 3895
712997 ZDOT = 1187
499310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4574238
61 X = -1394227
93
Y = -13440516
10 feet Y = -4096669
31 meter
Z = -17053889
19 Z = -5198025
43
XDOT = 20645
571716 XDOT = 6292
770259
YDOT = -11967
746840 feet/sec YDOT = -3647
769237 meter/sec
ZDOT = 3895
648500 ZDOT = 1187
393663
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 11183
56889630
00016717 00000-0 10270-3 0 9017
2 25544 51
6412 83
1843 0011261 280
4610 79
5277 15
59712521 3312
Satellite: ISS
Catalog Number: 25544
Epoch time: 11183
56889630 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 83
1843 deg
Eccentricity:
0011261
Arg of perigee: 280
4610 deg
Mean anomaly: 79
5277 deg
Mean motion: 15
59712521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 331
Checksum: 293
Coasting Arc #3 (Orbit 346)
---------------------------------------
Vector Time (GMT): 2011/184/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3742113
85 A = 6768151
96 meter
Y = -4477744
80 meter E =
0003269
Z = 3430075
48 I = 51
98147
XDOT = 2460
566186 Wp = 28
09097
YDOT = -5604
601993 meter/sec RA = 77
47132 deg
ZDOT = -4627
449347 TA = 111
87681
MA = 111
84204
Ha = 211
055 n
mi
Hp = 208
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12277276
41 X = -3708427
08
Y = -14690763
79 feet Y = -4519403
54 meter
Z = 11253528
49 Z = 3411977
82
XDOT = 8072
723708 XDOT = 2545
533925
YDOT = -18387
801813 feet/sec YDOT = -5576
610695 meter/sec
ZDOT = -15181
920430 ZDOT = -4615
290577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6487363
25 X = -1977348
32
Y = 18058450
93 feet Y = 5504215
84 meter
Z = 11180269
59 Z = 3407746
17
XDOT = -18682
549419 XDOT = -5694
441063
YDOT = 2666
425604 feet/sec YDOT = 812
726524 meter/sec
ZDOT = -15132
227417 ZDOT = -4612
302917
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 11184
59405248
00016717 00000-0 10270-3 0 9021
2 25544 51
6412 78
0309 0011278 284
8804 75
1103 15
59725816 3471
Satellite: ISS
Catalog Number: 25544
Epoch time: 11184
59405248 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 78
0309 deg
Eccentricity:
0011278
Arg of perigee: 284
8804 deg
Mean anomaly: 75
1103 deg
Mean motion: 15
59725816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 347
Checksum: 306
Coasting Arc #4 (Orbit 361)
---------------------------------------
Vector Time (GMT): 2011/185/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2129555
59 A = 6773099
63 meter
Y = 6419731
40 meter E =
0012278
Z = -127096
70 I = 51
98995
XDOT = -4453
683180 Wp = 348
31826
YDOT = 1598
929109 meter/sec RA = 72
48977 deg
ZDOT = 6049
879088 TA = 10
31539
MA = 10
29022
Ha = 211
388 n
mi
Hp = 208
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6986730
93 X = 2058228
04
Y = 21062110
89 feet Y = 6443146
59 meter
Z = -416983
94 Z = -116923
99
XDOT = -14611
821458 XDOT = -4500
620358
YDOT = 5245
830411 feet/sec YDOT = 1548
862141 meter/sec
ZDOT = 19848
684673 ZDOT = 6028
129694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14400018
25 X = 4389125
56
Y = -16884871
39 feet Y = -5146508
80 meter
Z = -376021
79 Z = -114611
44
XDOT = 10884
823573 XDOT = 3317
694225
YDOT = 8835
634802 feet/sec YDOT = 2693
101488 meter/sec
ZDOT = 19760
255139 ZDOT = 6022
925766
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 11185
55513095
00016717 00000-0 10270-3 0 9039
2 25544 51
6406 73
1981 0011371 288
0407 71
9509 15
59727247 3626
Satellite: ISS
Catalog Number: 25544
Epoch time: 11185
55513095 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 73
1981 deg
Eccentricity:
0011371
Arg of perigee: 288
0407 deg
Mean anomaly: 71
9509 deg
Mean motion: 15
59727247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 362
Checksum: 309
Coasting Arc #5 (Orbit 377)
---------------------------------------
Vector Time (GMT): 2011/186/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 270259
09 A = 6768734
17 meter
Y = -5943887
80 meter E =
0007089
Z = -3225554
32 I = 51
96423
XDOT = 5254
618434 Wp = 299
56070
YDOT = 2855
285262 meter/sec RA = 67
51053 deg
ZDOT = -4809
994369 TA = 277
67443
MA = 277
75493
Ha = 211
673 n
mi
Hp = 208
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 886676
80 X = 352373
60
Y = -19500944
21 feet Y = -5940406
14 meter
Z = -10582527
30 Z = -3224042
57
XDOT = 17239
561790 XDOT = 5245
665235
YDOT = 9367
733798 feet/sec YDOT = 2913
996029 meter/sec
ZDOT = -15780
821420 ZDOT = -4784
489316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17013509
02 X = -5185717
55
Y = 9578649
31 feet Y = 2919572
31 meter
Z = -10576052
81 Z = -3223580
90
XDOT = -601
646590 XDOT = -183
381881
YDOT = -18419
479767 feet/sec YDOT = -5614
257433 meter/sec
ZDOT = -15677
385432 ZDOT = -4778
467080
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 11186
58027578
00016717 00000-0 10270-3 0 9040
2 25544 51
6398 68
0443 0011493 291
5979 68
3951 15
59704548 3787
Satellite: ISS
Catalog Number: 25544
Epoch time: 11186
58027578 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 68
0443 deg
Eccentricity:
0011493
Arg of perigee: 291
5979 deg
Mean anomaly: 68
3951 deg
Mean motion: 15
59704548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 378
Checksum: 351
Coasting Arc #6 (Orbit 393)
---------------------------------------
Vector Time (GMT): 2011/187/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2838920
07 A = 6761836
49 meter
Y = 3315355
02 meter E =
0006933
Z = 5169543
30 I = 51
92858
XDOT = -4451
812800 Wp = 289
69320
YDOT = -6077
774009 meter/sec RA = 62
49070 deg
ZDOT = 1456
914422 TA = 146
37268
MA = 146
32866
Ha = 212
060 n
mi
Hp = 208
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9314042
21 X = -2900894
39
Y = 10877149
02 feet Y = 3283261
51 meter
Z = 16960443
91 Z = 5155601
77
XDOT = -14605
685038 XDOT = -4390
596421
YDOT = -19940
203440 feet/sec YDOT = -6127
214740 meter/sec
ZDOT = 4779
902960 ZDOT = 1435
435937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14256535
15 X = 4345391
91
Y = 1933650
84 feet Y = 589376
78 meter
Z = 16903627
15 Z = 5152225
56
XDOT = -8549
154864 XDOT = -2605
782402
YDOT = 22117
297205 feet/sec YDOT = 6741
352188 meter/sec
ZDOT = 4693
009044 ZDOT = 1430
429157
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
60541565
00016717 00000-0 10270-3 0 9052
2 25544 51
6398 62
8892 0011376 296
1228 63
8757 15
59705222 3947
Satellite: ISS
Catalog Number: 25544
Epoch time: 11187
60541565 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 62
8892 deg
Eccentricity:
0011376
Arg of perigee: 296
1228 deg
Mean anomaly: 63
8757 deg
Mean motion: 15
59705222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 394
Checksum: 333
Coasting Arc #7 (Orbit 408)
---------------------------------------
Vector Time (GMT): 2011/188/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4715675
35 A = 6763167
15 meter
Y = 345135
58 meter E =
0002264
Z = -4835704
88 I = 51
91743
XDOT = 2081
712612 Wp = 25
62826
YDOT = 6943
487984 meter/sec RA = 57
45100 deg
ZDOT = 2528
044378 TA = 269
08985
MA = 269
11578
Ha = 212
269 n
mi
Hp = 207
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15471375
81 X = 4734956
27
Y = 1132334
59 feet Y = 397977
38 meter
Z = -15865173
48 Z = -4812749
45
XDOT = 6829
765788 XDOT = 1991
633790
YDOT = 22780
472387 feet/sec YDOT = 6966
263072 meter/sec
ZDOT = 8294
108851 ZDOT = 2537
939088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7799722
49 X = -2377355
41
Y = -13518844
28 feet Y = -4120543
74 meter
Z = -15771954
82 Z = -4807291
83
XDOT = 14064
106887 XDOT = 4286
739779
YDOT = -17827
813616 feet/sec YDOT = -5433
917590 meter/sec
ZDOT = 8333
893454 ZDOT = 2540
170725
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
56647723
00016717 00000-0 10270-3 0 9062
2 25544 51
6388 58
0560 0011491 299
3286 60
6722 15
59747472 4099
Satellite: ISS
Catalog Number: 25544
Epoch time: 11188
56647723 = yrday
fracday
Element set: 906
Inclination: 51
6388 deg
RA of node: 58
0560 deg
Eccentricity:
0011491
Arg of perigee: 299
3286 deg
Mean anomaly: 60
6722 deg
Mean motion: 15
59747472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 409
Checksum: 335
Coasting Arc #8 (Orbit 424)
---------------------------------------
Vector Time (GMT): 2011/189/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5169204
37 A = 6770587
07 meter
Y = -3674008
23 meter E =
0004284
Z = 2372248
65 I = 51
92626
XDOT = 1274
921663 Wp = 55
16890
YDOT = -5291
326372 meter/sec RA = 52
44249 deg
ZDOT = -5407
539020 TA = 98
40436
MA = 98
35579
Ha = 212
411 n
mi
Hp = 207
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16959331
92 X = -5139260
61
Y = -12053832
78 feet Y = -3731646
24 meter
Z = 7782968
01 Z = 2347209
12
XDOT = 4182
813855 XDOT = 1360
264262
YDOT = -17359
994660 feet/sec YDOT = -5276
591674 meter/sec
ZDOT = -17741
269752 ZDOT = -5401
138743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -73592
80 X = -22431
09
Y = 20844130
69 feet Y = 6353291
04 meter
Z = 7681485
17 Z = 2341316
68
XDOT = -15147
263385 XDOT = -4616
885880
YDOT = 6486
212382 feet/sec YDOT = 1976
997534 meter/sec
ZDOT = -17714
956937 ZDOT = -5399
518874
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
59160441
00016717 00000-0 10270-3 0 9074
2 25544 51
6395 52
9023 0011678 303
7343 56
2699 15
59788079 4255
Satellite: ISS
Catalog Number: 25544
Epoch time: 11189
59160441 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 52
9023 deg
Eccentricity:
0011678
Arg of perigee: 303
7343 deg
Mean anomaly: 56
2699 deg
Mean motion: 15
59788079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 425
Checksum: 333
Coasting Arc #9 (Orbit 440)
---------------------------------------
Vector Time (GMT): 2011/190/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3807002
82 A = 6772441
20 meter
Y = 5471701
13 meter E =
0014406
Z = 1140760
25 I = 51
91184
XDOT = -4523
835383 Wp = 9
13005
YDOT = 1916
886479 meter/sec RA = 47
46289 deg
ZDOT = 5906
460868 TA = 3
24565
MA = 3
23632
Ha = 212
602 n
mi
Hp = 207
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12490166
73 X = 3739992
66
Y = 17951775
35 feet Y = 5513898
53 meter
Z = 3742651
73 Z = 1159092
55
XDOT = -14841
979603 XDOT = -4573
626583
YDOT = 6288
997634 feet/sec YDOT = 1866
019040 meter/sec
ZDOT = 19378
152454 ZDOT = 5884
363445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7154993
70 X = 2180842
08
Y = -20652269
63 feet Y = -6294811
78 meter
Z = 3816774
80 Z = 1163352
96
XDOT = 12391
256263 XDOT = 3776
854909
YDOT = 7855
448415 feet/sec YDOT = 2394
340677 meter/sec
ZDOT = 19288
281534 ZDOT = 5879
068212
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
61672788
00016717 00000-0 10270-3 0 9082
2 25544 51
6384 47
7469 0011525 306
8265 53
1833 15
59758255 4414
Satellite: ISS
Catalog Number: 25544
Epoch time: 11190
61672788 = yrday
fracday
Element set: 908
Inclination: 51
6384 deg
RA of node: 47
7469 deg
Eccentricity:
0011525
Arg of perigee: 306
8265 deg
Mean anomaly: 53
1833 deg
Mean motion: 15
59758255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 441
Checksum: 330
Coasting Arc #10 (Orbit 455)
---------------------------------------
Vector Time (GMT): 2011/191/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -937151
22 A = 6765634
19 meter
Y = -5268877
46 meter E =
0010186
Z = -4145108
91 I = 51
86739
XDOT = 6414
004412 Wp = 351
74775
YDOT = 1844
240754 meter/sec RA = 42
46632 deg
ZDOT = -3783
357461 TA = 239
37551
MA = 239
47599
Ha = 212
809 n
mi
Hp = 207
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3074643
10 X = -858027
85
Y = -17286343
36 feet Y = -5278914
21 meter
Z = -13599438
69 Z = -4149470
20
XDOT = 21043
321562 XDOT = 6411
283841
YDOT = 6050
658643 feet/sec YDOT = 1915
951422 meter/sec
ZDOT = -12412
590094 ZDOT = -3752
204671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11983130
00 X = -3652458
02
Y = 12814158
11 feet Y = 3905755
39 meter
Z = -13616819
65 Z = -4150406
63
XDOT = -6977
490338 XDOT = -2126
739055
YDOT = -19619
000492 feet/sec YDOT = -5979
871350 meter/sec
ZDOT = -12286
172273 ZDOT = -3744
825309
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
57777570
00016717 00000-0 10270-3 0 9094
2 25544 51
6377 42
9151 0011479 310
9335 49
0827 15
59769857 4566
Satellite: ISS
Catalog Number: 25544
Epoch time: 11191
57777570 = yrday
fracday
Element set: 909
Inclination: 51
6377 deg
RA of node: 42
9151 deg
Eccentricity:
0011479
Arg of perigee: 310
9335 deg
Mean anomaly: 49
0827 deg
Mean motion: 15
59769857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 456
Checksum: 344
Coasting Arc #11 (Orbit 471)
---------------------------------------
Vector Time (GMT): 2011/192/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2557307
96 A = 6761091
61 meter
Y = 3307595
36 meter E =
0009942
Z = 5318417
47 I = 51
82877
XDOT = -6087
425215 Wp = 324
30325
YDOT = -4672
212705 meter/sec RA = 37
42769 deg
ZDOT = -13
497528 TA = 125
87113
MA = 125
77877
Ha = 213
123 n
mi
Hp = 207
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8390117
97 X = -2619939
78
Y = 10851690
80 feet Y = 3278646
88 meter
Z = 17448876
20 Z = 5305842
59
XDOT = -19971
867503 XDOT = -6034
661628
YDOT = -15328
781842 feet/sec YDOT = -4739
990977 meter/sec
ZDOT = -44
283229 ZDOT = -42
942671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13781891
82 X = 4200720
63
Y = -7418
99 feet Y = -2261
31 meter
Z = 17397584
78 Z = 5302783
84
XDOT = 252
191892 XDOT = 76
868089
YDOT = 24169
566614 feet/sec YDOT = 7366
883904 meter/sec
ZDOT = -163
582283 ZDOT = -49
859880
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
60288869
00016717 00000-0 10270-3 0 9109
2 25544 51
6378 37
7600 0011425 314
6389 45
3834 15
59729964 4729
Satellite: ISS
Catalog Number: 25544
Epoch time: 11192
60288869 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 37
7600 deg
Eccentricity:
0011425
Arg of perigee: 314
6389 deg
Mean anomaly: 45
3834 deg
Mean motion: 15
59729964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 472
Checksum: 332
Coasting Arc #12 (Orbit 486)
---------------------------------------
Vector Time (GMT): 2011/193/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5330060
67 A = 6765750
41 meter
Y = -470549
31 meter E =
0005998
Z = -4135952
97 I = 51
81967
XDOT = 3444
858228 Wp = 354
69881
YDOT = 5718
433521 meter/sec RA = 32
38771 deg
ZDOT = 3794
243121 TA = 314
22319
MA = 314
27243
Ha = 213
258 n
mi
Hp = 206
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17487075
67 X = 5355017
76
Y = -1543796
96 feet Y = -410805
05 meter
Z = -13569399
50 Z = -4109999
30
XDOT = 11302
028308 XDOT = 3362
226045
YDOT = 18761
264834 feet/sec YDOT = 5756
493321 meter/sec
ZDOT = 12448
304202 ZDOT = 3810
778356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12271563
33 X = -3740372
50
Y = -12666516
69 feet Y = -3860754
29 meter
Z = -13463945
03 Z = -4103810
45
XDOT = 6567
111168 XDOT = 2001
655484
YDOT = -19646
370472 feet/sec YDOT = -5988
213720 meter/sec
ZDOT = 12515
093503 ZDOT = 3814
600500
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
56392491
00016717 00000-0 10270-3 0 9113
2 25544 51
6374 32
9268 0011361 317
9708 42
0575 15
59779248 4874
Satellite: ISS
Catalog Number: 25544
Epoch time: 11193
56392491 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 32
9268 deg
Eccentricity:
0011361
Arg of perigee: 317
9708 deg
Mean anomaly: 42
0575 deg
Mean motion: 15
59779248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 487
Checksum: 331
Coasting Arc #13 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2011/194/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6282949
39 A = 6772295
88 meter
Y = -2273240
32 meter E =
0004542
Z = 1108294
85 I = 51
81619
XDOT = 712
388630 Wp = 67
72748
YDOT = -4854
271844 meter/sec RA = 27
38651 deg
ZDOT = -5897
167615 TA = 100
25666
MA = 100
20543
Ha = 213
354 n
mi
Hp = 206
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20613351
03 X = -6262446
42
Y = -7458137
54 feet Y = -2343385
64 meter
Z = 3636137
98 Z = 1077822
20
XDOT = 2337
233037 XDOT = 795
263971
YDOT = -15926
088727 feet/sec YDOT = -4845
841066 meter/sec
ZDOT = -19347
662779 ZDOT = -5893
506440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7570176
13 X = 2307389
68
Y = 20593938
35 feet Y = 6277032
41 meter
Z = 3512505
09 Z = 1070611
55
XDOT = -12268
273028 XDOT = -3739
369619
YDOT = 7819
211661 feet/sec YDOT = 2383
295714 meter/sec
ZDOT = -19332
467791 ZDOT = -5892
536183
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
58902394
00016717 00000-0 10270-3 0 9126
2 25544 51
6374 27
7725 0011687 322
1498 37
8835 15
59835689 5031
Satellite: ISS
Catalog Number: 25544
Epoch time: 11194
58902394 = yrday
fracday
Element set: 912
Inclination: 51
6374 deg
RA of node: 27
7725 deg
Eccentricity:
0011687
Arg of perigee: 322
1498 deg
Mean anomaly: 37
8835 deg
Mean motion: 15
59835689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 341
Coasting Arc #14 (Orbit 518)
---------------------------------------
Vector Time (GMT): 2011/195/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4850288
13 A = 6770370
04 meter
Y = 4048251
22 meter E =
0014735
Z = 2406095
47 I = 51
78182
XDOT = -4833
419003 Wp = 27
41865
YDOT = 2591
923180 meter/sec RA = 22
39854 deg
ZDOT = 5382
195362 TA = 359
51819
MA = 359
51961
Ha = 213
436 n
mi
Hp = 206
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15913018
80 X = 4792971
19
Y = 13281664
10 feet Y = 4102169
22 meter
Z = 7894014
03 Z = 2429519
12
XDOT = -15857
673894 XDOT = -4888
188329
YDOT = 8503
684974 feet/sec YDOT = 2537
565839 meter/sec
ZDOT = 17658
121268 ZDOT = 5358
582501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -398828
38 X = -121562
89
Y = -20687210
73 feet Y = -6305461
83 meter
Z = 7988896
94 Z = 2435015
79
XDOT = 15387
468493 XDOT = 4690
100397
YDOT = 6485
706805 feet/sec YDOT = 1976
843434 meter/sec
ZDOT = 17562
027043 ZDOT = 5352
905843
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
61412071
00016717 00000-0 10270-3 0 9130
2 25544 51
6371 22
6170 0011331 325
7747 34
2677 15
59796851 5197
Satellite: ISS
Catalog Number: 25544
Epoch time: 11195
61412071 = yrday
fracday
Element set: 913
Inclination: 51
6371 deg
RA of node: 22
6170 deg
Eccentricity:
0011331
Arg of perigee: 325
7747 deg
Mean anomaly: 34
2677 deg
Mean motion: 15
59796851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 519
Checksum: 301
Coasting Arc #15 (Orbit 533)
---------------------------------------
Vector Time (GMT): 2011/196/13:19:04
039
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1502143
11 A = 6762776
79 meter
Y = -4478818
52 meter E =
0014519
Z = -4849311
57 I = 51
72909
XDOT = 7260
220202 Wp = 22
73018
YDOT = 239
152562 meter/sec RA = 17
37743 deg
ZDOT = -2459
203351 TA = 223
10606
MA = 223
21984
Ha = 213
632 n
mi
Hp = 206
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4928291
05 X = -1428391
95
Y = -14694286
49 feet Y = -4495203
33 meter
Z = -15909814
86 Z = -4856430
32
XDOT = 23819
620085 XDOT = 7268
952431
YDOT = 784
621268 feet/sec YDOT = 320
389943 meter/sec
ZDOT = -8068
252463 ZDOT = -2423
912804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7681017
12 X = -2341174
02
Y = 13427604
27 feet Y = 4092733
78 meter
Z = -15938435
83 Z = -4858035
24
XDOT = -14416
765806 XDOT = -4394
230218
YDOT = -17694
974466 feet/sec YDOT = -5393
428217 meter/sec
ZDOT = -7924
907043 ZDOT = -2415
511667
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
57514233
00016717 00000-0 10270-3 0 9140
2 25544 51
6379 17
7853 0011297 330
2436 29
8076 15
59820281 5340
Satellite: ISS
Catalog Number: 25544
Epoch time: 11196
57514233 = yrday
fracday
Element set: 914
Inclination: 51
6379 deg
RA of node: 17
7853 deg
Eccentricity:
0011297
Arg of perigee: 330
2436 deg
Mean anomaly: 29
8076 deg
Mean motion: 15
59820281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 534
Checksum: 314
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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