[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 11th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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
200/03:16:13
873 6
8 7
7 7
7
N/A -1
3 -0
1 219
3
000/00:18:27
746 3
3 0
1 215
4
Coasting Arc #1 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2012/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6773021
12 A = 6783559
03 meter
Y = -100559
42 meter E =
0018824
Z = -77523
65 I = 51
66255
XDOT = 129
739408 Wp = 137
82004
YDOT = -4760
307175 meter/sec RA =
33204 deg
ZDOT = -6020
350528 TA = 43
01593
MA = 42
86892
Ha = 219
978 n
mi
Hp = 209
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22221197
91 X = -6771016
67
Y = -329919
37 feet Y = -176288
33 meter
Z = -254342
70 Z = -110421
67
XDOT = 425
654227 XDOT = 212
205855
YDOT = -15617
805691 feet/sec YDOT = -4758
394697 meter/sec
ZDOT = -19751
806194 ZDOT = -6019
520394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6920479
67 X = 2109362
20
Y = 21116582
19 feet Y = 6436334
25 meter
Z = -389988
67 Z = -118868
55
XDOT = -13406
439410 XDOT = -4086
282732
YDOT = 4062
937838 feet/sec YDOT = 1238
383453 meter/sec
ZDOT = -19747
825174 ZDOT = -6019
137113
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 12193
53193679
00016717 00000-0 10270-3 0 9006
2 25544 51
6376
6954 0006971 143
1088 217
0547 15
56115048 21805
Satellite: ISS
Catalog Number: 25544
Epoch time: 12193
53193679 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node:
6954 deg
Eccentricity:
0006971
Arg of perigee: 143
1088 deg
Mean anomaly: 217
0547 deg
Mean motion: 15
56115048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 305
Coasting Arc #2 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2012/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6214033
46 A = 6781195
24 meter
Y = 1354902
40 meter E =
0017259
Z = 2341409
21 I = 51
62406
XDOT = -3034
358596 Wp = 96
94393
YDOT = 4532
519450 meter/sec RA = 355
35027 deg
ZDOT = 5394
100163 TA = 289
20366
MA = 289
39034
Ha = 220
009 n
mi
Hp = 209
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20387248
87 X = 6187046
83
Y = 4445217
86 feet Y = 1424240
44 meter
Z = 7681788
76 Z = 2371531
18
XDOT = -9955
244737 XDOT = -3111
019849
YDOT = 14870
470636 feet/sec YDOT = 4498
158162 meter/sec
ZDOT = 17697
179012 ZDOT = 5379
173716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2772487
89 X = -845054
31
Y = -20634727
80 feet Y = -6289465
03 meter
Z = 7805836
05 Z = 2379218
83
XDOT = 15910
435973 XDOT = 4849
500885
YDOT = 4577
563026 feet/sec YDOT = 1395
241210 meter/sec
ZDOT = 17635
097346 ZDOT = 5375
177671
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 12194
55947486
00016717 00000-0 10270-3 0 9013
2 25544 51
6375 355
5571 0007236 147
8898 212
2698 15
56102862 21967
Satellite: ISS
Catalog Number: 25544
Epoch time: 12194
55947486 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 355
5571 deg
Eccentricity:
0007236
Arg of perigee: 147
8898 deg
Mean anomaly: 212
2698 deg
Mean motion: 15
56102862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 344
Coasting Arc #3 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2012/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4658294
82 A = 6775944
08 meter
Y = -2583657
02 meter E =
0011663
Z = -4195274
21 I = 51
57726
XDOT = 5472
773127 Wp = 106
81071
YDOT = -3897
887049 meter/sec RA = 350
35165 deg
ZDOT = -3688
068049 TA = 125
35123
MA = 125
24217
Ha = 219
879 n
mi
Hp = 209
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15283119
48 X = -4608678
02
Y = -8476565
03 feet Y = -2635471
04 meter
Z = -13764022
99 Z = -4217783
69
XDOT = 17955
292412 XDOT = 5533
869070
YDOT = -12788
343337 feet/sec YDOT = -3836
345060 meter/sec
ZDOT = -12099
960792 ZDOT = -3661
333744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2477453
62 X = -755127
86
Y = 17225937
77 feet Y = 5250465
83 meter
Z = -13856533
33 Z = -4223471
36
XDOT = -17137
519020 XDOT = -5223
515797
YDOT = -12077
982969 feet/sec YDOT = -3681
369209 meter/sec
ZDOT = -11989
265556 ZDOT = -3654
328141
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 12195
52277715
00016717 00000-0 10270-3 0 9023
2 25544 51
6383 350
7403 0007167 150
2227 209
9336 15
56128925 22112
Satellite: ISS
Catalog Number: 25544
Epoch time: 12195
52277715 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 350
7403 deg
Eccentricity:
0007167
Arg of perigee: 150
2227 deg
Mean anomaly: 209
9336 deg
Mean motion: 15
56128925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 299
Coasting Arc #4 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2012/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2434071
61 A = 6772003
20 meter
Y = 3615854
91 meter E =
0010827
Z = 5178747
49 I = 51
53375
XDOT = -7001
236402 Wp = 143
08037
YDOT = 2877
209388 meter/sec RA = 345
33114 deg
ZDOT = 1271
896818 TA = 294
64480
MA = 294
75754
Ha = 219
730 n
mi
Hp = 210
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7985799
23 X = 2368300
44
Y = 11863041
03 feet Y = 3642705
78 meter
Z = 16990641
38 Z = 5190412
75
XDOT = -22969
935702 XDOT = -7039
068149
YDOT = 9439
663346 feet/sec YDOT = 2798
705526 meter/sec
ZDOT = 4172
889823 ZDOT = 1237
793809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8057284
71 X = 2455860
38
Y = -11745749
56 feet Y = -3580104
47 meter
Z = 17038314
38 Z = 5193278
22
XDOT = 16495
504411 XDOT = 5027
829744
YDOT = 17211
026395 feet/sec YDOT = 5245
920845 meter/sec
ZDOT = 4031
931908 ZDOT = 1228
932846
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 12196
55028487
00016717 00000-0 10270-3 0 9038
2 25544 51
6379 345
6012 0007087 154
6715 205
4787 15
56138732 22272
Satellite: ISS
Catalog Number: 25544
Epoch time: 12196
55028487 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 345
6012 deg
Eccentricity:
0007087
Arg of perigee: 154
6715 deg
Mean anomaly: 205
4787 deg
Mean motion: 15
56138732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 324
Coasting Arc #5 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2012/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 136764
77 A = 6772143
81 meter
Y = -4405488
36 meter E =
0018689
Z = -5157526
47 I = 51
50610
XDOT = 7385
325968 Wp = 119
42572
YDOT = -1442
295725 meter/sec RA = 340
30178 deg
ZDOT = 1422
736879 TA = 164
33439
MA = 164
27648
Ha = 219
717 n
mi
Hp = 210
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 448703
30 X = 211071
56
Y = -14453701
97 feet Y = -4403542
79 meter
Z = -16921018
60 Z = -5156682
20
XDOT = 24230
072075 XDOT = 7393
993846
YDOT = -4731
941354 feet/sec YDOT = -1359
660161 meter/sec
ZDOT = 4667
771913 ZDOT = 1458
635014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13526917
31 X = -4123004
40
Y = 5125301
46 feet Y = 1562191
89 meter
Z = -16917018
02 Z = -5156307
09
XDOT = -13415
964965 XDOT = -4089
186121
YDOT = -19456
845493 feet/sec YDOT = -5930
446506 meter/sec
ZDOT = 4815
962365 ZDOT = 1467
905329
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 12197
51355916
00016717 00000-0 10270-3 0 9046
2 25544 51
6390 340
7849 0007164 157
8488 202
2977 15
56168805 22424
Satellite: ISS
Catalog Number: 25544
Epoch time: 12197
51355916 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 340
7849 deg
Eccentricity:
0007164
Arg of perigee: 157
8488 deg
Mean anomaly: 202
2977 deg
Mean motion: 15
56168805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 334
Coasting Arc #6 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2012/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2572310
56 A = 6776408
91 meter
Y = 4752942
44 meter E =
0013445
Z = 4073946
32 I = 51
49172
XDOT = -6644
840445 Wp = 108
98958
YDOT = -301
902087 meter/sec RA = 335
27775 deg
ZDOT = -3837
305037 TA = 20
72378
MA = 20
66932
Ha = 219
674 n
mi
Hp = 210
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8439339
11 X = -2645057
83
Y = 15593643
19 feet Y = 4723769
95 meter
Z = 13365965
62 Z = 4061274
26
XDOT = -21800
657627 XDOT = -6622
330114
YDOT = -990
492411 feet/sec YDOT = -376
082414 meter/sec
ZDOT = -12589
583454 ZDOT = -3869
530362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17710100
62 X = 5398038
67
Y = 1464720
73 feet Y = 446446
88 meter
Z = 13313155
84 Z = 4057849
90
XDOT = 8010
080271 XDOT = 2441
472466
YDOT = 18967
521463 feet/sec YDOT = 5781
300542 meter/sec
ZDOT = -12722
425384 ZDOT = -3877
795257
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 12198
54103764
00016717 00000-0 10270-3 0 9053
2 25544 51
6388 335
6455 0007136 161
6820 198
4592 15
56161391 22588
Satellite: ISS
Catalog Number: 25544
Epoch time: 12198
54103764 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 335
6455 deg
Eccentricity:
0007136
Arg of perigee: 161
6820 deg
Mean anomaly: 198
4592 deg
Mean motion: 15
56161391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 325
Coasting Arc #7 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2012/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4504487
46 A = 6781309
16 meter
Y = -4577184
28 meter E =
0006339
Z = -2187495
10 I = 51
48260
XDOT = 4896
387670 Wp = 109
00480
YDOT = 2212
384526 meter/sec RA = 330
27217 deg
ZDOT = 5464
334162 TA = 226
65822
MA = 226
71106
Ha = 219
442 n
mi
Hp = 210
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14778502
16 X = 4565961
88
Y = -15017008
81 feet Y = -4526468
29 meter
Z = -7176821
20 Z = -2165464
14
XDOT = 16064
264009 XDOT = 4844
740328
YDOT = 7258
479415 feet/sec YDOT = 2266
849453 meter/sec
ZDOT = 17927
605519 ZDOT = 5487
995085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19863344
42 X = -6054347
38
Y = -7117968
04 feet Y = -2169556
66 meter
Z = -7085444
34 Z = -2159643
43
XDOT = -654
624661 XDOT = -199
529597
YDOT = -16079
499980 feet/sec YDOT = -4901
031594 meter/sec
ZDOT = 18024
911976 ZDOT = 5493
993170
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 12199
50428352
00016717 00000-0 10270-3 0 9064
2 25544 51
6401 330
8285 0006988 165
2082 194
9277 15
56206032 22736
Satellite: ISS
Catalog Number: 25544
Epoch time: 12199
50428352 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 330
8285 deg
Eccentricity:
0006988
Arg of perigee: 165
2082 deg
Mean anomaly: 194
9277 deg
Mean motion: 15
56206032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 314
Coasting Arc #8 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2012/200/03:25:27
746
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4463846
95 A = 6786384
13 meter
Y = -4728834
31 meter E =
0002846
Z = -1935097
93 I = 51
46887
XDOT = 4762
922394 Wp = 9
06003
YDOT = 2212
470265 meter/sec RA = 327
05636 deg
ZDOT = 5584
239450 TA = 329
55711
MA = 329
57364
Ha = 219
301 n
mi
Hp = 215
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14645167
16 X = 4525794
09
Y = -15514548
27 feet Y = -4678570
19 meter
Z = -6348746
48 Z = -1913263
27
XDOT = 15626
385806 XDOT = 4710
701604
YDOT = 7258
760713 feet/sec YDOT = 2265
439519 meter/sec
ZDOT = 18320
995571 ZDOT = 5607
250558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17816208
30 X = 5430380
29
Y = -11785873
53 feet Y = -3592334
25 meter
Z = -6258164
10 Z = -1907488
42
XDOT = 12607
164903 XDOT = 3842
663863
YDOT = 9286
082180 feet/sec YDOT = 2830
397848 meter/sec
ZDOT = 18415
624991 ZDOT = 5613
082497
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 12200
14643992
00016717 00000-0 10270-3 0 9077
2 25544 51
6418 327
6214 0004772 236
5012 123
5686 15
54609517 22830
Satellite: ISS
Catalog Number: 25544
Epoch time: 12200
14643992 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 327
6214 deg
Eccentricity:
0004772
Arg of perigee: 236
5012 deg
Mean anomaly: 123
5686 deg
Mean motion: 15
54609517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2283
Checksum: 301
Coasting Arc #9 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2012/201/03:25:27
746
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5303050
85 A = 6788009
36 meter
Y = 4224387
66 meter E =
0011862
Z = 90730
21 I = 51
44927
XDOT = -3044
576681 Wp = 156
63682
YDOT = -3687
594037 meter/sec RA = 322
07034 deg
ZDOT = -5998
538806 TA = 22
38280
MA = 22
33109
Ha = 219
197 n
mi
Hp = 215
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17398460
81 X = -5350335
43
Y = 13859539
55 feet Y = 4164821
26 meter
Z = 297671
28 Z = 64854
35
XDOT = -9988
768639 XDOT = -2973
975998
YDOT = -12098
405632 feet/sec YDOT = -3721
244961 meter/sec
ZDOT = -19680
245427 ZDOT = -6013
157861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19919560
39 X = -6071482
01
Y = 9902358
87 feet Y = 3018238
98 meter
Z = 190488
34 Z = 58060
85
XDOT = -6389
371276 XDOT = -1947
480365
YDOT = -12447
598013 feet/sec YDOT = -3794
027874 meter/sec
ZDOT = -19740
105347 ZDOT = -6016
784110
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 12201
17495678
00016717 00000-0 10270-3 0 9088
2 25544 51
6420 322
4903 0004830 239
7800 120
2875 15
54582915 22999
Satellite: ISS
Catalog Number: 25544
Epoch time: 12201
17495678 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 322
4903 deg
Eccentricity:
0004830
Arg of perigee: 239
7800 deg
Mean anomaly: 120
2875 deg
Mean motion: 15
54582915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 311
Coasting Arc #10 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2012/202/03:25:27
746
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5639520
17 A = 6786523
32 meter
Y = -3334786
08 meter E =
0009237
Z = 1752656
28 I = 51
42144
XDOT = 1212
660411 Wp = 64
37491
YDOT = 5033
978275 meter/sec RA = 317
08220 deg
ZDOT = 5656
800398 TA = 314
92844
MA = 315
00335
Ha = 218
922 n
mi
Hp = 215
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18502362
76 X = 5667877
46
Y = -10940899
21 feet Y = -3271563
07 meter
Z = 5750184
65 Z = 1780120
82
XDOT = 3978
544656 XDOT = 1128
800420
YDOT = 16515
676756 feet/sec YDOT = 5047
069595 meter/sec
ZDOT = 18559
056424 ZDOT = 5662
488093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20230211
48 X = 6166168
46
Y = -7173533
52 feet Y = -2186493
02 meter
Z = 5863811
67 Z = 1787289
80
XDOT = 83
933557 XDOT = 25
582948
YDOT = 15477
014047 feet/sec YDOT = 4717
393882 meter/sec
ZDOT = 18581
941993 ZDOT = 5663
775920
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 12202
20345874
00016717 00000-0 10270-3 0 9096
2 25544 51
6420 317
3585 0004721 247
1840 112
8814 15
54628347 23153
Satellite: ISS
Catalog Number: 25544
Epoch time: 12202
20345874 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 317
3585 deg
Eccentricity:
0004721
Arg of perigee: 247
1840 deg
Mean anomaly: 112
8814 deg
Mean motion: 15
54628347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 293
Coasting Arc #11 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2012/203/03:25:27
746
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5502372
24 A = 6782851
56 meter
Y = 2044671
58 meter E =
0001553
Z = -3397210
40 I = 51
38764
XDOT = 568
078399 Wp = 170
21706
YDOT = -6108
262425 meter/sec RA = 312
08533 deg
ZDOT = -4598
279999 TA = 49
65270
MA = 49
63913
Ha = 218
674 n
mi
Hp = 215
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18052402
35 X = -5508324
68
Y = 6708240
09 feet Y = 1983107
59 meter
Z = -11145703
40 Z = -3423954
45
XDOT = 1863
774274 XDOT = 658
676973
YDOT = -20040
231053 feet/sec YDOT = -6101
402936 meter/sec
ZDOT = -15086
220469 ZDOT = -4595
300721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18883620
03 X = -5755727
39
Y = 3438467
29 feet Y = 1048044
83 meter
Z = -11256209
72 Z = -3430892
72
XDOT = 5702
497151 XDOT = 1738
121132
YDOT = -18007
354523 feet/sec YDOT = -5488
641659 meter/sec
ZDOT = -15073
257125 ZDOT = -4594
328772
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 12203
16766698
00016717 00000-0 10270-3 0 9105
2 25544 51
6419 312
5482 0004926 251
0286 109
0333 15
54638702 23306
Satellite: ISS
Catalog Number: 25544
Epoch time: 12203
16766698 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 312
5482 deg
Eccentricity:
0004926
Arg of perigee: 251
0286 deg
Mean anomaly: 109
0333 deg
Mean motion: 15
54638702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 295
Coasting Arc #12 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2012/204/03:25:27
746
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4957352
41 A = 6778686
05 meter
Y = -459457
94 meter E =
0005544
Z = 4600135
35 I = 51
35402
XDOT = -2128
773453 Wp = 147
10747
YDOT = 6745
604115 meter/sec RA = 307
07385 deg
ZDOT = 2961
571183 TA = 273
22523
MA = 273
28866
Ha = 218
533 n
mi
Hp = 215
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16264279
57 X = 4939775
72
Y = -1507407
93 feet Y = -404120
25 meter
Z = 15092307
58 Z = 4624174
79
XDOT = -6984
164872 XDOT = -2218
432349
YDOT = 22131
247095 feet/sec YDOT = 6721
297388 meter/sec
ZDOT = 9716
440888 ZDOT = 2951
012452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16205572
85 X = 4939458
60
Y = 1084003
96 feet Y = 330404
41 meter
Z = 15191483
17 Z = 4630364
07
XDOT = -10393
655345 XDOT = -3167
986149
YDOT = 19548
722291 feet/sec YDOT = 5958
450554 meter/sec
ZDOT = 9672
165105 ZDOT = 2948
075924
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 12204
19614420
00016717 00000-0 10270-3 0 9115
2 25544 51
6417 307
4164 0004688 255
9462 104
1170 15
54659702 23463
Satellite: ISS
Catalog Number: 25544
Epoch time: 12204
19614420 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 307
4164 deg
Eccentricity:
0004688
Arg of perigee: 255
9462 deg
Mean anomaly: 104
1170 deg
Mean motion: 15
54659702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 292
Coasting Arc #13 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2012/205/03:25:27
746
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110744
44 A = 6775921
81 meter
Y = -1322653
84 meter E =
0009623
Z = -5230084
62 I = 51
32667
XDOT = 3381
439069 Wp = 83
81131
YDOT = -6812
032233 meter/sec RA = 302
04962 deg
ZDOT = -935
495641 TA = 177
19461
MA = 177
18921
Ha = 218
388 n
mi
Hp = 215
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13486694
37 X = -4070242
55
Y = -4339415
49 feet Y = -1368396
08 meter
Z = -17159070
27 Z = -5249955
80
XDOT = 11093
960200 XDOT = 3461
905656
YDOT = -22349
187116 feet/sec YDOT = -6773
768932 meter/sec
ZDOT = -3069
211419 ZDOT = -918
873819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12629713
53 X = -3849536
68
Y = -6196619
38 feet Y = -1888729
59 meter
Z = -17240863
93 Z = -5255015
32
XDOT = 13721
463027 XDOT = 4182
301931
YDOT = -19624
082667 feet/sec YDOT = -5981
420397 meter/sec
ZDOT = -2999
939503 ZDOT = -914
381560
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 12205
16032754
00016717 00000-0 10270-3 0 9128
2 25544 51
6407 302
6049 0004831 260
8208 99
2399 15
54715347 23616
Satellite: ISS
Catalog Number: 25544
Epoch time: 12205
16032754 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 302
6049 deg
Eccentricity:
0004831
Arg of perigee: 260
8208 deg
Mean anomaly: 99
2399 deg
Mean motion: 15
54715347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 298
Coasting Arc #14 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2012/206/03:25:27
746
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3071836
40 A = 6776109
03 meter
Y = 3107943
73 meter E =
0002353
Z = 5180424
04 I = 51
31211
XDOT = -4276
185317 Wp = 321
35474
YDOT = 6248
908530 meter/sec RA = 297
02090 deg
ZDOT = -1211
813402 TA = 140
33441
MA = 140
31720
Ha = 218
188 n
mi
Hp = 215
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10078203
43 X = 3011689
38
Y = 10196665
77 feet Y = 3141958
43 meter
Z = 16996141
88 Z = 5195200
74
XDOT = -14029
479387 XDOT = -4339
857431
YDOT = 20501
668407 feet/sec YDOT = 6200
733601 meter/sec
ZDOT = -3975
765754 ZDOT = -1232
741131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8621879
96 X = 2627949
01
Y = 11364059
01 feet Y = 3463765
19 meter
Z = 17056739
57 Z = 5198894
22
XDOT = -15628
015546 XDOT = -4763
419139
YDOT = 17962
217606 feet/sec YDOT = 5474
883926 meter/sec
ZDOT = -4062
722069 ZDOT = -1238
317686
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 12206
18877826
00016717 00000-0 10270-3 0 9139
2 25544 51
6407 297
4732 0004882 264
5906 95
4690 15
54728980 23774
Satellite: ISS
Catalog Number: 25544
Epoch time: 12206
18877826 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 297
4732 deg
Eccentricity:
0004882
Arg of perigee: 264
5906 deg
Mean anomaly: 95
4690 deg
Mean motion: 15
54728980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 347
Coasting Arc #15 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2012/207/03:25:27
746
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1956273
45 A = 6779032
33 meter
Y = -4712679
27 meter E =
0005234
Z = -4468394
45 I = 51
30770
XDOT = 4804
762852 Wp = 130
67354
YDOT = -5036
408543 meter/sec RA = 291
99445 deg
ZDOT = 3207
336343 TA = 171
75413
MA = 171
74553
Ha = 218
231 n
mi
Hp = 215
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6418219
99 X = -1881723
61
Y = -15461546
16 feet Y = -4734138
52 meter
Z = -14660086
78 Z = -4477716
99
XDOT = 15763
657652 XDOT = 4845
143504
YDOT = -16523
650076 feet/sec YDOT = -4982
453053 meter/sec
ZDOT = 10522
757031 ZDOT = 3230
775371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4623859
37 X = -1409352
34
Y = -16054873
74 feet Y = -4893525
51 meter
Z = -14698028
97 Z = -4479959
23
XDOT = 16218
888315 XDOT = 4943
517158
YDOT = -14396
124767 feet/sec YDOT = -4387
938829 meter/sec
ZDOT = 10619
932948 ZDOT = 3236
955563
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
15293942
00016717 00000-0 10270-3 0 9149
2 25544 51
6394 292
6606 0004907 268
7349 91
3242 15
54743529 23922
Satellite: ISS
Catalog Number: 25544
Epoch time: 12207
15293942 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 292
6606 deg
Eccentricity:
0004907
Arg of perigee: 268
7349 deg
Mean anomaly: 91
3242 deg
Mean motion: 15
54743529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 325
Coasting Arc #16 (Orbit 2407)
---------------------------------------
Vector Time (GMT): 2012/208/03:25:27
746
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 833746
07 A = 6783138
48 meter
Y = 5939098
91 meter E =
0007886
Z = 3161613
07 I = 51
31174
XDOT = -5014
529211 Wp = 93
80629
YDOT = 3263
682525 meter/sec RA = 286
98025 deg
ZDOT = -4798
601936 TA = 49
50685
MA = 49
43816
Ha = 218
130 n
mi
Hp = 215
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2735387
38 X = 751913
55
Y = 19485232
66 feet Y = 5947964
64 meter
Z = 10372746
28 Z = 3165464
93
XDOT = -16451
867491 XDOT = -5027
341275
YDOT = 10707
619832 feet/sec YDOT = 3207
535591 meter/sec
ZDOT = -15743
444673 ZDOT = -4822
993107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 892763
92 X = 272114
44
Y = 19647971
51 feet Y = 5988701
72 meter
Z = 10388007
00 Z = 3166264
53
XDOT = -15826
676356 XDOT = -4823
970953
YDOT = 9113
218580 feet/sec YDOT = 2777
709023 meter/sec
ZDOT = -15844
357602 ZDOT = -4829
360197
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
18136438
00016717 00000-0 10270-3 0 9150
2 25544 51
6397 287
5287 0004999 274
7016 85
3566 15
54794933 24087
Satellite: ISS
Catalog Number: 25544
Epoch time: 12208
18136438 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 287
5287 deg
Eccentricity:
0004999
Arg of perigee: 274
7016 deg
Mean anomaly: 85
3566 deg
Mean motion: 15
54794933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2408
Checksum: 351
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list