[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 10th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 123 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 362 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2013/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4682825
90 A = 6786419
75 meter
Y = -2689664
55 meter E =
0010748
Z = -4108048
27 I = 51
31069
XDOT = 513
131838 Wp = 29
73103
YDOT = -6647
975011 meter/sec RA = 247
40403 deg
ZDOT = 3781
128203 TA = 279
40389
MA = 279
52538
Ha = 225
884 n
mi
Hp = 215
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15363602
03 X = -4632446
08
Y = -8824358
78 feet Y = -2741749
57 meter
Z = -13477848
64 Z = -4130673
91
XDOT = 1683
503404 XDOT = 569
065452
YDOT = -21810
941636 feet/sec YDOT = -6641
923734 meter/sec
ZDOT = 12405
276256 ZDOT = 3783
757409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12593115
68 X = -3838381
66
Y = -12360594
56 feet Y = -3767509
22 meter
Z = -13571702
87 Z = -4136655
04
XDOT = 6099
679042 XDOT = 1859
182172
YDOT = -19799
979869 feet/sec YDOT = -6035
033864 meter/sec
ZDOT = 12416
945682 ZDOT = 3784
685044
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 13067
50911542
00016717 00000-0 10270-3 0 9001
2 25544 51
6427 248
2980 0011995 351
1177 8
9761 15
52636348 19071
Satellite: ISS
Catalog Number: 25544
Epoch time: 13067
50911542 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 248
2980 deg
Eccentricity:
0011995
Arg of perigee: 351
1177 deg
Mean anomaly: 8
9761 deg
Mean motion: 15
52636348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 316
Coasting Arc #2 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2013/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4780288
39 A = 6789167
04 meter
Y = 3597741
34 meter E =
0016164
Z = 3211885
43 I = 51
33252
XDOT = -1216
886735 Wp = 45
56119
YDOT = 5883
432217 meter/sec RA = 242
40768 deg
ZDOT = -4753
141933 TA = 97
15274
MA = 96
96892
Ha = 226
076 n
mi
Hp = 215
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15683360
87 X = 4724100
24
Y = 11803613
31 feet Y = 3650883
75 meter
Z = 10537681
87 Z = 3234970
28
XDOT = -3992
410547 XDOT = -1259
497060
YDOT = 19302
599137 feet/sec YDOT = 5869
585412 meter/sec
ZDOT = -15594
297679 ZDOT = -4759
157536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12438460
13 X = 3791242
65
Y = 15117942
83 feet Y = 4607948
97 meter
Z = 10633360
19 Z = 3241048
19
XDOT = -7183
015772 XDOT = -2189
383207
YDOT = 16955
786653 feet/sec YDOT = 5168
123772 meter/sec
ZDOT = -15619
964160 ZDOT = -4760
965076
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 13068
53893141
00016717 00000-0 10270-3 0 9010
2 25544 51
6425 243
1752 0012090 354
2956 5
8057 15
52659059 19232
Satellite: ISS
Catalog Number: 25544
Epoch time: 13068
53893141 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 243
1752 deg
Eccentricity:
0012090
Arg of perigee: 354
2956 deg
Mean anomaly: 5
8057 deg
Mean motion: 15
52659059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 306
Coasting Arc #3 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2013/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4795829
63 A = 6791504
46 meter
Y = -4274247
25 meter E =
0016944
Z = -2175278
15 I = 51
35597
XDOT = 1989
771252 Wp = 13
55131
YDOT = -5001
582633 meter/sec RA = 237
41688 deg
ZDOT = 5465
669705 TA = 322
20387
MA = 322
32274
Ha = 226
113 n
mi
Hp = 215
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15734349
19 X = -4737110
92
Y = -14023120
90 feet Y = -4327549
22 meter
Z = -7136739
33 Z = -2198432
26
XDOT = 6528
120905 XDOT = 2019
001829
YDOT = -16409
391842 feet/sec YDOT = -4979
167581 meter/sec
ZDOT = 17931
987222 ZDOT = 5475
407347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12287126
50 X = -3745116
16
Y = -17084088
32 feet Y = -5207230
12 meter
Z = -7232645
52 Z = -2204510
35
XDOT = 8567
237023 XDOT = 2611
293845
YDOT = -13736
676158 feet/sec YDOT = -4186
938893 meter/sec
ZDOT = 17973
040421 ZDOT = 5478
182720
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 13069
50437302
00016717 00000-0 10270-3 0 9022
2 25544 51
6429 238
3722 0012003 358
7630 1
3490 15
52672250 19387
Satellite: ISS
Catalog Number: 25544
Epoch time: 13069
50437302 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 238
3722 deg
Eccentricity:
0012003
Arg of perigee: 358
7630 deg
Mean anomaly: 1
3490 deg
Mean motion: 15
52672250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 283
Coasting Arc #4 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2013/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4688566
05 A = 6792963
89 meter
Y = 4820462
57 meter E =
0012486
Z = 972853
28 I = 51
37847
XDOT = -2862
508680 Wp = 68
56901
YDOT = 3984
254496 meter/sec RA = 232
43171 deg
ZDOT = -5880
711239 TA = 100
87107
MA = 100
73054
Ha = 226
292 n
mi
Hp = 215
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15382434
56 X = 4629588
35
Y = 15815165
91 feet Y = 4872563
45 meter
Z = 3191775
85 Z = 995485
66
XDOT = -9391
432676 XDOT = -2878
282168
YDOT = 13071
701103 feet/sec YDOT = 3952
155065 meter/sec
ZDOT = -19293
672045 ZDOT = -5894
655767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11900946
58 X = 3627408
52
Y = 18560694
86 feet Y = 5657299
79 meter
Z = 3285464
25 Z = 1001409
50
XDOT = -10338
503614 XDOT = -3151
175902
YDOT = 10091
520295 feet/sec YDOT = 3075
895386 meter/sec
ZDOT = -19352
121359 ZDOT = -5898
526590
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 13070
53416138
00016717 00000-0 10270-3 0 9032
2 25544 51
6427 233
2490 0012224 1
9863 358
1335 15
52731384 19544
Satellite: ISS
Catalog Number: 25544
Epoch time: 13070
53416138 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 233
2490 deg
Eccentricity:
0012224
Arg of perigee: 1
9863 deg
Mean anomaly: 358
1335 deg
Mean motion: 15
52731384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 290
Coasting Arc #5 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2013/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4433525
22 A = 6793402
82 meter
Y = -5122596
33 meter E =
0022945
Z = 248003
10 I = 51
40057
XDOT = 3771
788824 Wp = 27
78044
YDOT = -2964
460347 meter/sec RA = 227
44978 deg
ZDOT = 5992
053599 TA = 334
90250
MA = 335
01385
Ha = 226
327 n
mi
Hp = 214
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14545686
42 X = -4377118
47
Y = -16806418
42 feet Y = -5171859
38 meter
Z = 813658
46 Z = 226603
40
XDOT = 12374
635248 XDOT = 3775
550182
YDOT = -9725
919774 feet/sec YDOT = -2922
259893 meter/sec
ZDOT = 19658
968501 ZDOT = 6010
386041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11239218
06 X = -3425713
67
Y = -19179387
60 feet Y = -5845877
34 meter
Z = 725122
13 Z = 221017
22
XDOT = 12423
427435 XDOT = 3786
660682
YDOT = -6505
677427 feet/sec YDOT = -1982
930480 meter/sec
ZDOT = 19735
572803 ZDOT = 6015
402590
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 13071
56393828
00016717 00000-0 10270-3 0 9047
2 25544 51
6440 228
1261 0012005 6
6846 353
4464 15
52724971 19701
Satellite: ISS
Catalog Number: 25544
Epoch time: 13071
56393828 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 228
1261 deg
Eccentricity:
0012005
Arg of perigee: 6
6846 deg
Mean anomaly: 353
4464 deg
Mean motion: 15
52724971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 302
Coasting Arc #6 (Orbit 1984)
---------------------------------------
Vector Time (GMT): 2013/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3999847
08 A = 6792355
71 meter
Y = 5286378
11 meter E =
0009044
Z = -1502737
59 I = 51
41892
XDOT = -4686
129945 Wp = 53
36593
YDOT = 1919
136134 meter/sec RA = 222
46891 deg
ZDOT = -5740
737958 TA = 143
06203
MA = 142
99972
Ha = 226
493 n
mi
Hp = 214
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13122857
89 X = 3947736
26
Y = 17343760
22 feet Y = 5330815
33 meter
Z = -4930241
45 Z = -1483434
14
XDOT = -15374
442076 XDOT = -4679
355010
YDOT = 6296
378393 feet/sec YDOT = 1866
769911 meter/sec
ZDOT = -18834
442118 ZDOT = -5763
486484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10100422
37 X = 3078608
74
Y = 19281530
34 feet Y = 5877010
45 meter
Z = -4850438
55 Z = -1478413
67
XDOT = -14683
571778 XDOT = -4475
552678
YDOT = 2945
791760 feet/sec YDOT = 897
877329 meter/sec
ZDOT = -18929
321264 ZDOT = -5769
657121
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 13072
52933939
00016717 00000-0 10270-3 0 9058
2 25544 51
6440 223
3233 0012235 10
1106 350
0290 15
52766992 19856
Satellite: ISS
Catalog Number: 25544
Epoch time: 13072
52933939 = yrday
fracday
Element set: 905
Inclination: 51
6440 deg
RA of node: 223
3233 deg
Eccentricity:
0012235
Arg of perigee: 10
1106 deg
Mean anomaly: 350
0290 deg
Mean motion: 15
52766992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1985
Checksum: 288
Coasting Arc #7 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2013/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3377238
88 A = 6790329
33 meter
Y = -5246276
75 meter E =
0021786
Z = 2643575
90 I = 51
43667
XDOT = 5566
353331 Wp = 47
92620
YDOT = -956
040268 meter/sec RA = 217
48681 deg
ZDOT = 5200
647675 TA = 342
00305
MA = 342
08006
Ha = 226
508 n
mi
Hp = 214
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11080180
05 X = -3331164
65
Y = -17212194
07 feet Y = -5283785
19 meter
Z = 8673149
29 Z = 2627282
23
XDOT = 18262
314078 XDOT = 5551
366960
YDOT = -3136
615053 feet/sec YDOT = -893
876883 meter/sec
ZDOT = 17062
492371 ZDOT = 5227
652210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8453029
15 X = -2576483
29
Y = -18674553
62 feet Y = -5692003
94 meter
Z = 8605863
04 Z = 2623067
06
XDOT = 17059
305983 XDOT = 5199
676464
YDOT = 213
070021 feet/sec YDOT = 64
943743 meter/sec
ZDOT = 17174
993390 ZDOT = 5234
937985
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 13073
55908680
00016717 00000-0 10270-3 0 9068
2 25544 51
6451 218
2007 0012034 13
8441 346
3039 15
52783295 20013
Satellite: ISS
Catalog Number: 25544
Epoch time: 13073
55908680 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 218
2007 deg
Eccentricity:
0012034
Arg of perigee: 13
8441 deg
Mean anomaly: 346
3039 deg
Mean motion: 15
52783295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 285
Coasting Arc #8 (Orbit 2015)
---------------------------------------
Vector Time (GMT): 2013/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2572735
25 A = 6787597
95 meter
Y = 5109152
21 meter E =
0015464
Z = -3672937
83 I = 51
45270
XDOT = -6310
946505 Wp = 36
23565
YDOT = 66
058907 meter/sec RA = 212
50169 deg
ZDOT = -4325
809536 TA = 187
46044
MA = 187
48347
Ha = 226
652 n
mi
Hp = 214
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8440732
43 X = 2533254
55
Y = 16762310
40 feet Y = 5137700
96 meter
Z = -12050320
96 Z = -3660536
22
XDOT = -20705
205069 XDOT = -6290
202524
YDOT = 216
728699 feet/sec YDOT = -4
398604 meter/sec
ZDOT = -14192
288505 ZDOT = -4356
417172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6236382
35 X = 1900849
34
Y = 17735771
73 feet Y = 5405863
22 meter
Z = -11999216
04 Z = -3657361
05
XDOT = -19173
258528 XDOT = -5844
009199
YDOT = -2952
567489 feet/sec YDOT = -899
942571 meter/sec
ZDOT = -14319
705795 ZDOT = -4364
646326
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 13074
52446259
00016717 00000-0 10270-3 0 9076
2 25544 51
6454 213
3986 0012191 17
3503 342
8063 15
52783416 20169
Satellite: ISS
Catalog Number: 25544
Epoch time: 13074
52446259 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 213
3986 deg
Eccentricity:
0012191
Arg of perigee: 17
3503 deg
Mean anomaly: 342
8063 deg
Mean motion: 15
52783416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2016
Checksum: 299
Coasting Arc #9 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2013/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1584244
07 A = 6784644
04 meter
Y = -4837933
35 meter E =
0015121
Z = 4469549
31 I = 51
47035
XDOT = 6928
984247 Wp = 58
02854
YDOT = 712
018225 meter/sec RA = 207
51195 deg
ZDOT = 3226
538830 TA = 359
47127
MA = 359
47287
Ha = 226
656 n
mi
Hp = 214
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5197651
16 X = -1551739
40
Y = -15872484
74 feet Y = -4855467
16 meter
Z = 14663875
69 Z = 4461932
65
XDOT = 22732
887949 XDOT = 6904
833668
YDOT = 2336
017797 feet/sec YDOT = 789
367789 meter/sec
ZDOT = 10585
757316 ZDOT = 3260
140484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3436705
36 X = -1047507
79
Y = -16372384
44 feet Y = -4990302
78 meter
Z = 14632658
11 Z = 4460034
19
XDOT = 21056
888083 XDOT = 6418
139488
YDOT = 5166
327184 feet/sec YDOT = 1574
696526 meter/sec
ZDOT = 10725
571180 ZDOT = 3269
154096
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 13075
55418052
00016717 00000-0 10270-3 0 9081
2 25544 51
6460 208
2756 0012154 20
7918 339
3726 15
52833255 20323
Satellite: ISS
Catalog Number: 25544
Epoch time: 13075
55418052 = yrday
fracday
Element set: 908
Inclination: 51
6460 deg
RA of node: 208
2756 deg
Eccentricity:
0012154
Arg of perigee: 20
7918 deg
Mean anomaly: 339
3726 deg
Mean motion: 15
52833255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 298
Coasting Arc #10 (Orbit 2046)
---------------------------------------
Vector Time (GMT): 2013/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 481647
59 A = 6782444
11 meter
Y = 4538301
98 meter E =
0022686
Z = -5036770
51 I = 51
49066
XDOT = -7278
478072 Wp = 50
78659
YDOT = -1365
513466 meter/sec RA = 202
51988 deg
ZDOT = -1918
177306 TA = 200
47826
MA = 200
56936
Ha = 226
800 n
mi
Hp = 213
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1580208
64 X = 455330
79
Y = 14889442
20 feet Y = 4543540
46 meter
Z = -16524837
63 Z = -5034495
05
XDOT = -23879
521232 XDOT = -7253
349674
YDOT = -4480
031057 feet/sec YDOT = -1446
765662 meter/sec
ZDOT = -6293
232630 ZDOT = -1953
474306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 224764
10 X = 68508
10
Y = 14981316
56 feet Y = 4566305
29 meter
Z = -16515823
99 Z = -5034023
15
XDOT = -22198
415199 XDOT = -6766
076953
YDOT = -6796
366402 feet/sec YDOT = -2071
532479 meter/sec
ZDOT = -6440
052984 ZDOT = -1962
928149
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 13076
51952942
00016717 00000-0 10270-3 0 9090
2 25544 51
6461 203
4740 0012305 24
2601 335
9128 15
52825224 20471
Satellite: ISS
Catalog Number: 25544
Epoch time: 13076
51952942 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 203
4740 deg
Eccentricity:
0012305
Arg of perigee: 24
2601 deg
Mean anomaly: 335
9128 deg
Mean motion: 15
52825224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 285
Coasting Arc #11 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2013/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 745706
15 A = 6781068
50 meter
Y = -4171390
62 meter E =
0012912
Z = 5286050
63 I = 51
51580
XDOT = 7410
483851 Wp = 40
37231
YDOT = 1932
579169 meter/sec RA = 197
52407 deg
ZDOT = 488
632035 TA = 45
01414
MA = 44
90956
Ha = 226
763 n
mi
Hp = 213
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2446542
50 X = 766617
97
Y = -13685664
76 feet Y = -4162934
29 meter
Z = 17342685
81 Z = 5289724
34
XDOT = 24312
611060 XDOT = 7385
948937
YDOT = 6340
482839 feet/sec YDOT = 2015
310722 meter/sec
ZDOT = 1603
123476 ZDOT = 524
571648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3429675
56 X = 1045365
11
Y = -13452688
62 feet Y = -4100379
49 meter
Z = 17358405
33 Z = 5290841
94
XDOT = 22734
371826 XDOT = 6929
436533
YDOT = 8019
431113 feet/sec YDOT = 2444
322603 meter/sec
ZDOT = 1752
578662 ZDOT = 534
185976
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 13077
54921839
00016717 00000-0 10270-3 0 9107
2 25544 51
6465 198
3503 0012350 27
6939 332
4868 15
52879686 20637
Satellite: ISS
Catalog Number: 25544
Epoch time: 13077
54921839 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 198
3503 deg
Eccentricity:
0012350
Arg of perigee: 27
6939 deg
Mean anomaly: 332
4868 deg
Mean motion: 15
52879686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 338
Coasting Arc #12 (Orbit 2077)
---------------------------------------
Vector Time (GMT): 2013/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1959550
86 A = 6781236
05 meter
Y = 3837795
77 meter E =
0022666
Z = -5253000
56 I = 51
54602
XDOT = -7207
964514 Wp = 67
43272
YDOT = -2382
860048 meter/sec RA = 192
53136 deg
ZDOT = 959
739120 TA = 211
71505
MA = 211
85179
Ha = 226
904 n
mi
Hp = 213
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6428972
63 X = -1976802
73
Y = 12591193
48 feet Y = 3815785
95 meter
Z = -17234253
79 Z = -5262562
05
XDOT = -23648
177539 XDOT = -7185
445283
YDOT = -7817
782310 feet/sec YDOT = -2463
338053 meter/sec
ZDOT = 3148
750393 ZDOT = 924
778536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7103844
73 X = -2165251
87
Y = 12166255
72 feet Y = 3708274
74 meter
Z = -17274459
70 Z = -5265255
32
XDOT = -22239
935766 XDOT = -6778
732421
YDOT = -8776
325945 feet/sec YDOT = -2675
024148 meter/sec
ZDOT = 3003
399967 ZDOT = 915
436310
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 13078
51453988
00016717 00000-0 10270-3 0 9111
2 25544 51
6465 193
5488 0012473 31
6400 328
5499 15
52891350 20784
Satellite: ISS
Catalog Number: 25544
Epoch time: 13078
51453988 = yrday
fracday
Element set: 911
Inclination: 51
6465 deg
RA of node: 193
5488 deg
Eccentricity:
0012473
Arg of perigee: 31
6400 deg
Mean anomaly: 328
5499 deg
Mean motion: 15
52891350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 329
Coasting Arc #13 (Orbit 2093)
---------------------------------------
Vector Time (GMT): 2013/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3193196
61 A = 6782793
15 meter
Y = -3471732
21 meter E =
0018996
Z = 4867826
31 I = 51
58174
XDOT = 6726
791167 Wp = 43
94021
YDOT = 2804
950529 meter/sec RA = 187
53997 deg
ZDOT = -2393
142086 TA = 69
62616
MA = 69
42221
Ha = 226
951 n
mi
Hp = 213
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10476366
84 X = 3208134
51
Y = -11390197
54 feet Y = -3435939
94 meter
Z = 15970558
75 Z = 4883375
04
XDOT = 22069
524827 XDOT = 6706
550822
YDOT = 9202
593598 feet/sec YDOT = 2880
060367 meter/sec
ZDOT = -7851
516030 ZDOT = -2360
513562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10889258
15 X = 3319045
88
Y = -10900964
67 feet Y = -3322614
03 meter
Z = 16035667
60 Z = 4887671
48
XDOT = 20877
151192 XDOT = 6363
355683
YDOT = 9413
024784 feet/sec YDOT = 2869
089954 meter/sec
ZDOT = -7715
903082 ZDOT = -2351
807259
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 13079
54420115
00016717 00000-0 10270-3 0 9122
2 25544 51
6467 188
4249 0012578 35
3794 324
8190 15
52892182 20946
Satellite: ISS
Catalog Number: 25544
Epoch time: 13079
54420115 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 188
4249 deg
Eccentricity:
0012578
Arg of perigee: 35
3794 deg
Mean anomaly: 324
8190 deg
Mean motion: 15
52892182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2094
Checksum: 322
Coasting Arc #14 (Orbit 2108)
---------------------------------------
Vector Time (GMT): 2013/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4265234
67 A = 6785163
25 meter
Y = 3164440
09 meter E =
0016995
Z = -4231767
42 I = 51
62074
XDOT = -5946
007401 Wp = 66
19541
YDOT = -3158
677887 meter/sec RA = 182
55684 deg
ZDOT = 3649
338518 TA = 241
15477
MA = 241
32546
Ha = 226
974 n
mi
Hp = 212
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13993552
06 X = -4279746
50
Y = 10382021
29 feet Y = 3116662
02 meter
Z = -13883751
37 Z = -4252522
91
XDOT = -19507
898296 XDOT = -5927
971823
YDOT = -10363
116426 feet/sec YDOT = -3225
068702 meter/sec
ZDOT = 11972
895401 ZDOT = 3620
497694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14199748
95 X = -4328083
48
Y = 9977776
14 feet Y = 3041226
17 meter
Z = -13970523
63 Z = -4258215
60
XDOT = -18548
441810 XDOT = -5653
565064
YDOT = -9884
317860 feet/sec YDOT = -3012
740084 meter/sec
ZDOT = 11853
078550 ZDOT = 3612
818342
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 13080
50949412
00016717 00000-0 10270-3 0 9137
2 25544 51
6470 183
6228 0012529 38
5373 321
6671 15
52923827 21095
Satellite: ISS
Catalog Number: 25544
Epoch time: 13080
50949412 = yrday
fracday
Element set: 913
Inclination: 51
6470 deg
RA of node: 183
6228 deg
Eccentricity:
0012529
Arg of perigee: 38
5373 deg
Mean anomaly: 321
6671 deg
Mean motion: 15
52923827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2109
Checksum: 306
Coasting Arc #15 (Orbit 2124)
---------------------------------------
Vector Time (GMT): 2013/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5232598
87 A = 6788202
39 meter
Y = -2813527
53 meter E =
0022985
Z = 3275111
11 I = 51
66145
XDOT = 4886
543795 Wp = 67
58703
YDOT = 3538
982873 meter/sec RA = 177
58035 deg
ZDOT = -4731
807890 TA = 74
42487
MA = 74
17127
Ha = 227
089 n
mi
Hp = 212
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17167319
13 X = 5247761
98
Y = -9230733
37 feet Y = -2754928
19 meter
Z = 10745115
20 Z = 3300567
50
XDOT = 16031
967832 XDOT = 4869
592588
YDOT = 11610
836197 feet/sec YDOT = 3593
532003 meter/sec
ZDOT = -15524
304102 ZDOT = -4708
111269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17205642
68 X = 5244279
89
Y = -9032874
30 feet Y = -2753220
09 meter
Z = 10851443
55 Z = 3307520
00
XDOT = 15334
265070 XDOT = 4673
883993
YDOT = 10539
637324 feet/sec YDOT = 3212
481456 meter/sec
ZDOT = -15425
940967 ZDOT = -4701
826807
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 13081
53912672
00016717 00000-0 10270-3 0 9140
2 25544 51
6469 178
4993 0012665 42
6840 317
5293 15
52925431 21255
Satellite: ISS
Catalog Number: 25544
Epoch time: 13081
53912672 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 178
4993 deg
Eccentricity:
0012665
Arg of perigee: 42
6840 deg
Mean anomaly: 317
5293 deg
Mean motion: 15
52925431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2125
Checksum: 319
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