[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 20th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
172/13:59:39
523 -1
9 4
3 4
4
N/A 3
2 -0
5 221
4
000/00:09:19
045 2
2 -0
1 209
4
Coasting Arc #1 (Orbit 1821)
---------------------------------------
Vector Time (GMT): 2012/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 190237
50 A = 6778597
44 meter
Y = -6049503
85 meter E =
0023267
Z = 3033348
87 I = 51
95834
XDOT = 5368
501861 Wp = 87
92945
YDOT = -2338
154418 meter/sec RA = 114
88932 deg
ZDOT = -4966
197448 TA = 57
39628
MA = 57
17189
Ha = 221
133 n
mi
Hp = 207
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 624138
80 X = 243134
79
Y = -19847453
59 feet Y = -6047081
25 meter
Z = 9951932
00 Z = 3034400
51
XDOT = 17613
195081 XDOT = 5418
373304
YDOT = -7671
110295 feet/sec YDOT = -2277
840821 meter/sec
ZDOT = -16293
298715 ZDOT = -4939
996694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19769945
46 X = -6025879
38
Y = -1833691
35 feet Y = -558909
12 meter
Z = 9956844
19 Z = 3034846
11
XDOT = -6655
453143 XDOT = -2028
582118
YDOT = -16725
685748 feet/sec YDOT = -5097
989016 meter/sec
ZDOT = -16185
088855 ZDOT = -4933
215083
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 12170
53839858
00016717 00000-0 10270-3 0 9007
2 25544 51
6360 115
6401 0010491 77
1756 283
0569 15
56476536 18223
Satellite: ISS
Catalog Number: 25544
Epoch time: 12170
53839858 = yrday
fracday
Element set: 900
Inclination: 51
6360 deg
RA of node: 115
6401 deg
Eccentricity:
0010491
Arg of perigee: 77
1756 deg
Mean anomaly: 283
0569 deg
Mean motion: 15
56476536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1822
Checksum: 314
Coasting Arc #2 (Orbit 1836)
---------------------------------------
Vector Time (GMT): 2012/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1736877
63 A = 6782219
46 meter
Y = 6508134
57 meter E =
0019521
Z = -748310
78 I = 51
98264
XDOT = -4761
185326 Wp = 60
48636
YDOT = -596
899154 meter/sec RA = 109
92509 deg
ZDOT = 5985
868686 TA = 291
45713
MA = 291
66520
Ha = 221
091 n
mi
Hp = 207
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5698417
42 X = -1805888
71
Y = 21352147
53 feet Y = 6488325
99 meter
Z = -2455087
85 Z = -756914
95
XDOT = -15620
686765 XDOT = -4783
234780
YDOT = -1958
330559 feet/sec YDOT = -650
265992 meter/sec
ZDOT = 19638
676792 ZDOT = 5962
685420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21062036
41 X = 6419708
70
Y = 6678191
50 feet Y = 2035512
77 meter
Z = -2491184
92 Z = -759313
16
XDOT = -2205
913014 XDOT = -672
362287
YDOT = 14095
228649 feet/sec YDOT = 4296
225692 meter/sec
ZDOT = 19543
174730 ZDOT = 5956
759658
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 12171
50146811
00016717 00000-0 10270-3 0 9016
2 25544 51
6361 110
8219 0010431 80
7859 279
4474 15
56491649 18378
Satellite: ISS
Catalog Number: 25544
Epoch time: 12171
50146811 = yrday
fracday
Element set: 901
Inclination: 51
6361 deg
RA of node: 110
8219 deg
Eccentricity:
0010431
Arg of perigee: 80
7859 deg
Mean anomaly: 279
4474 deg
Mean motion: 15
56491649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1837
Checksum: 308
Coasting Arc #3 (Orbit 1852)
---------------------------------------
Vector Time (GMT): 2012/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2996545
95 A = 6781041
62 meter
Y = -5816468
76 meter E =
0015761
Z = -1781931
10 I = 51
98975
XDOT = 3644
823487 Wp = 108
06754
YDOT = 3609
266251 meter/sec RA = 104
96700 deg
ZDOT = -5697
876932 TA = 91
41434
MA = 91
23378
Ha = 221
058 n
mi
Hp = 207
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9831187
50 X = 3070020
36
Y = -19082902
76 feet Y = -5782548
41 meter
Z = -5846230
64 Z = -1767196
59
XDOT = 11958
082306 XDOT = 3631
871914
YDOT = 11841
424709 feet/sec YDOT = 3649
953467 meter/sec
ZDOT = -18693
821954 ZDOT = -5680
201470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18781859
23 X = -5724710
69
Y = -10429013
38 feet Y = -3178763
28 meter
Z = -5784918
48 Z = -1763243
15
XDOT = 11432
985380 XDOT = 3484
773944
YDOT = -10345
344545 feet/sec YDOT = -3153
261017 meter/sec
ZDOT = -18621
312171 ZDOT = -5675
775950
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 12172
52872483
00016717 00000-0 10270-3 0 9021
2 25544 51
6374 105
6815 0010406 84
5108 275
7233 15
56525281 18537
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
52872483 = yrday
fracday
Element set: 902
Inclination: 51
6374 deg
RA of node: 105
6815 deg
Eccentricity:
0010406
Arg of perigee: 84
5108 deg
Mean anomaly: 275
7233 deg
Mean motion: 15
56525281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1853
Checksum: 302
Coasting Arc #4 (Orbit 1853)
---------------------------------------
Vector Time (GMT): 2012/172/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1063477
29 A = 6780409
82 meter
Y = 5884998
82 meter E =
0012564
Z = -3201304
92 I = 51
98229
XDOT = -4809
956870 Wp = 72
77690
YDOT = 3490
999958 meter/sec RA = 104
49618 deg
ZDOT = 4838
906938 TA = 250
42135
MA = 250
55704
Ha = 221
412 n
mi
Hp = 209
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3489098
73 X = 1013142
13
Y = 19307738
90 feet Y = 5896610
37 meter
Z = -10502968
88 Z = -3196259
89
XDOT = -15780
698393 XDOT = -4872
142660
YDOT = 11453
411936 feet/sec YDOT = 3436
863531 meter/sec
ZDOT = 15875
678932 ZDOT = 4815
390028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15062575
55 X = 4591073
03
Y = -12589905
21 feet Y = -3837403
11 meter
Z = -10482750
17 Z = -3195142
25
XDOT = 16864
363757 XDOT = 5140
258073
YDOT = 7091
596079 feet/sec YDOT = 2161
518485 meter/sec
ZDOT = 15778
389979 ZDOT = 4809
253266
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 12172
59292692
00016717 00000-0 10270-3 0 9037
2 25544 51
6393 105
3599 0008052 68
8238 291
3775 15
55705415 18541
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
59292692 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 105
3599 deg
Eccentricity:
0008052
Arg of perigee: 68
8238 deg
Mean anomaly: 291
3775 deg
Mean motion: 15
55705415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1854
Checksum: 332
Coasting Arc #5 (Orbit 1869)
---------------------------------------
Vector Time (GMT): 2012/173/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 226499
57 A = 6784239
41 meter
Y = -6679318
68 meter E =
0019833
Z = 1130452
62 I = 52
00168
XDOT = 4821
872951 Wp = 104
86975
YDOT = -849
891660 meter/sec RA = 99
53581 deg
ZDOT = -5906
583339 TA = 62
91163
MA = 62
70943
Ha = 221
429 n
mi
Hp = 209
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 743108
84 X = 295680
81
Y = -21913775
20 feet Y = -6676399
18 meter
Z = 3708834
06 Z = 1131719
93
XDOT = 15819
793145 XDOT = 4859
710866
YDOT = -2788
358465 feet/sec YDOT = -795
758006 meter/sec
ZDOT = -19378
554263 ZDOT = -5883
067297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19256469
51 X = -5869371
91
Y = 10483817
13 feet Y = 3195467
46 meter
Z = 3714722
65 Z = 1132247
46
XDOT = -9717
001365 XDOT = -2961
742016
YDOT = -10921
804181 feet/sec YDOT = -3328
965914 meter/sec
ZDOT = -19281
519233 ZDOT = -5877
007062
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 12173
62071512
00016717 00000-0 10270-3 0 9049
2 25544 51
6394 100
2234 0007997 73
2881 286
9150 15
55694688 18707
Satellite: ISS
Catalog Number: 25544
Epoch time: 12173
62071512 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 100
2234 deg
Eccentricity:
0007997
Arg of perigee: 73
2881 deg
Mean anomaly: 286
9150 deg
Mean motion: 15
55694688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1870
Checksum: 320
Coasting Arc #6 (Orbit 1885)
---------------------------------------
Vector Time (GMT): 2012/174/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1375251
61 A = 6784166
08 meter
Y = 6544734
12 meter E =
0021336
Z = 1085573
18 I = 52
00617
XDOT = -4483
962589 Wp = 63
55022
YDOT = -1937
528724 meter/sec RA = 94
58261 deg
ZDOT = 5920
314798 TA = 308
18063
MA = 308
37262
Ha = 221
364 n
mi
Hp = 209
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4511980
33 X = -1453607
37
Y = 21472224
81 feet Y = 6528916
94 meter
Z = 3561591
79 Z = 1078702
92
XDOT = -14711
163350 XDOT = -4490
722766
YDOT = -6356
721536 feet/sec YDOT = -1987
709793 meter/sec
ZDOT = 19423
604980 ZDOT = 5898
515421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20685552
28 X = 6304956
34
Y = -7329934
49 feet Y = -2234164
03 meter
Z = 3532609
25 Z = 1076739
30
XDOT = 1776
484218 XDOT = 541
472390
YDOT = 14459
100869 feet/sec YDOT = 4407
133945 meter/sec
ZDOT = 19333
919525 ZDOT = 5892
978671
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 12174
64848467
00016717 00000-0 10270-3 0 9054
2 25544 51
6396 95
0869 0007959 75
4365 284
7671 15
55739120 18865
Satellite: ISS
Catalog Number: 25544
Epoch time: 12174
64848467 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 95
0869 deg
Eccentricity:
0007959
Arg of perigee: 75
4365 deg
Mean anomaly: 284
7671 deg
Mean motion: 15
55739120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1886
Checksum: 363
Coasting Arc #7 (Orbit 1900)
---------------------------------------
Vector Time (GMT): 2012/175/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2446883
43 A = 6780364
97 meter
Y = -5473521
34 meter E =
0012045
Z = -3177386
80 I = 51
99520
XDOT = 3826
545037 Wp = 87
81234
YDOT = 4522
154806 meter/sec RA = 89
62268 deg
ZDOT = -4858
691495 TA = 128
64859
MA = 128
54074
Ha = 221
272 n
mi
Hp = 209
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8027832
76 X = 2523342
48
Y = -17957747
18 feet Y = -5445730
89 meter
Z = -10424497
39 Z = -3165315
01
XDOT = 12554
281619 XDOT = 3799
295172
YDOT = 14836
465898 feet/sec YDOT = 4564
793825 meter/sec
ZDOT = -15940
588895 ZDOT = -4840
168136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19497363
06 X = -5942796
26
Y = 2797567
16 feet Y = 852698
47 meter
Z = -10374168
88 Z = -3162046
68
XDOT = 5944
718171 XDOT = 1811
950098
YDOT = -17211
252214 feet/sec YDOT = -5245
989675 meter/sec
ZDOT = -15864
669376 ZDOT = -4835
551226
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 12175
61200272
00016717 00000-0 10270-3 0 9069
2 25544 51
6397 90
2713 0007734 79
4867 280
7158 15
55752829 19018
Satellite: ISS
Catalog Number: 25544
Epoch time: 12175
61200272 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 90
2713 deg
Eccentricity:
0007734
Arg of perigee: 79
4867 deg
Mean anomaly: 280
7158 deg
Mean motion: 15
55752829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1901
Checksum: 321
Coasting Arc #8 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2012/176/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3312396
48 A = 6775373
73 meter
Y = 3631645
63 meter E =
0015522
Z = 4651157
05 I = 51
97747
XDOT = -2922
950017 Wp = 99
21084
YDOT = -6459
253695 meter/sec RA = 84
64569 deg
ZDOT = 2951
015824 TA = 321
53780
MA = 321
64833
Ha = 221
387 n
mi
Hp = 209
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10867442
52 X = -3375354
18
Y = 11914847
86 feet Y = 3594251
86 meter
Z = 15259701
61 Z = 4634913
16
XDOT = -9589
731027 XDOT = -2864
839326
YDOT = -21191
777216 feet/sec YDOT = -6491
615323 meter/sec
ZDOT = 9681
810446 ZDOT = 2936
956867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15981590
12 X = 4871188
67
Y = 2589333
17 feet Y = 789228
75 meter
Z = 15192351
06 Z = 4630628
60
XDOT = -12189
417664 XDOT = -3715
334504
YDOT = 18556
169610 feet/sec YDOT = 5655
920497 meter/sec
ZDOT = 9624
498465 ZDOT = 2933
547132
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 12176
63973953
00016717 00000-0 10270-3 0 9076
2 25544 51
6396 85
1344 0007906 82
7136 277
4916 15
55786960 19172
Satellite: ISS
Catalog Number: 25544
Epoch time: 12176
63973953 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 85
1344 deg
Eccentricity:
0007906
Arg of perigee: 82
7136 deg
Mean anomaly: 277
4916 deg
Mean motion: 15
55786960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 352
Coasting Arc #9 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2012/177/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4004533
18 A = 6772455
31 meter
Y = -1278817
68 meter E =
0022486
Z = -5329257
13 I = 51
96376
XDOT = 1738
908815 Wp = 86
07500
YDOT = 7439
028452 meter/sec RA = 79
65262 deg
ZDOT = -478
664309 TA = 179
37261
MA = 179
36979
Ha = 221
128 n
mi
Hp = 209
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13138232
22 X = 4044423
74
Y = -4195596
05 feet Y = -1233812
98 meter
Z = -17484439
40 Z = -5309706
62
XDOT = 5705
081415 XDOT = 1657
920066
YDOT = 24406
261325 feet/sec YDOT = 7458
021218 meter/sec
ZDOT = -1570
420962 ZDOT = -470
412857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10944185
45 X = -3335787
72
Y = -8559095
96 feet Y = -2608812
45 meter
Z = -17403691
41 Z = -5304645
14
XDOT = 16288
156851 XDOT = 4964
630208
YDOT = -17703
049306 feet/sec YDOT = -5395
889429 meter/sec
ZDOT = -1537
163104 ZDOT = -468
527314
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 12177
60322555
00016717 00000-0 10270-3 0 9081
2 25544 51
6391 80
3178 0007713 85
8130 274
3905 15
55840811 19320
Satellite: ISS
Catalog Number: 25544
Epoch time: 12177
60322555 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 80
3178 deg
Eccentricity:
0007713
Arg of perigee: 85
8130 deg
Mean anomaly: 274
3905 deg
Mean motion: 15
55840811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1932
Checksum: 305
Coasting Arc #10 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2012/178/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4391684
49 A = 6773681
38 meter
Y = -1218388
16 meter E =
0013158
Z = 5001302
55 I = 51
96211
XDOT = -334
645744 Wp = 74
75840
YDOT = -7383
372741 meter/sec RA = 74
65689 deg
ZDOT = -2084
629349 TA = 35
44670
MA = 35
35933
Ha = 221
161 n
mi
Hp = 209
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14408413
69 X = -4402028
98
Y = -3997336
47 feet Y = -1267556
97 meter
Z = 16408472
92 Z = 4979942
74
XDOT = -1097
919108 XDOT = -241
931846
YDOT = -24223
663847 feet/sec YDOT = -7386
596381 meter/sec
ZDOT = -6839
335136 ZDOT = -2086
030491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5141048
19 X = 1566991
49
Y = 14143168
86 feet Y = 4310837
87 meter
Z = 16320522
84 Z = 4974495
36
XDOT = -18108
719811 XDOT = -5519
537798
YDOT = 14510
708189 feet/sec YDOT = 4422
863856 meter/sec
ZDOT = -6844
341556 ZDOT = -2086
155306
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 12178
63092763
00016717 00000-0 10270-3 0 9091
2 25544 51
6393 75
1807 0007583 89
5146 270
6876 15
55883395 19483
Satellite: ISS
Catalog Number: 25544
Epoch time: 12178
63092763 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 75
1807 deg
Eccentricity:
0007583
Arg of perigee: 89
5146 deg
Mean anomaly: 270
6876 deg
Mean motion: 15
55883395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1948
Checksum: 358
Coasting Arc #11 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2012/179/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4442702
37 A = 6778233
43 meter
Y = 3452798
16 meter E =
0013420
Z = -3792460
37 I = 51
96743
XDOT = -1234
135644 Wp = 97
22725
YDOT = 6249
224814 meter/sec RA = 69
67130 deg
ZDOT = 4255
019484 TA = 217
57165
MA = 217
66549
Ha = 221
026 n
mi
Hp = 209
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14575795
17 X = 4422185
23
Y = 11328077
95 feet Y = 3502364
86 meter
Z = -12442455
27 Z = -3770927
37
XDOT = -4049
001456 XDOT = -1324
593997
YDOT = 20502
706082 feet/sec YDOT = 6234
917755 meter/sec
ZDOT = 13960
037676 ZDOT = 4248
804973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 435096
41 X = 132617
38
Y = -18514385
81 feet Y = -5643184
79 meter
Z = -12354030
00 Z = -3765508
35
XDOT = 17612
244601 XDOT = 5368
212155
YDOT = -8858
874441 feet/sec YDOT = -2700
184930 meter/sec
ZDOT = 13933
748822 ZDOT = 4247
006641
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 12179
59438455
00016717 00000-0 10270-3 0 9101
2 25544 51
6385 70
3639 0007535 93
2030 266
9985 15
55877533 19638
Satellite: ISS
Catalog Number: 25544
Epoch time: 12179
59438455 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 70
3639 deg
Eccentricity:
0007535
Arg of perigee: 93
2030 deg
Mean anomaly: 266
9985 deg
Mean motion: 15
55877533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 343
Coasting Arc #12 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2012/180/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4011885
90 A = 6782775
41 meter
Y = -5142824
03 meter E =
0021303
Z = 1828033
21 I = 51
97181
XDOT = 2885
282253 Wp = 107
82086
YDOT = -4285
695434 meter/sec RA = 64
70374 deg
ZDOT = -5677
036734 TA = 52
14409
MA = 51
95154
Ha = 220
996 n
mi
Hp = 209
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13162355
31 X = -3962959
83
Y = -16872782
24 feet Y = -5187414
07 meter
Z = 5997484
30 Z = 1808661
81
XDOT = 9466
149124 XDOT = 2960
569225
YDOT = -14060
680558 feet/sec YDOT = -4253
008818 meter/sec
ZDOT = -18625
448601 ZDOT = -5662
837713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5406060
69 X = -1647767
30
Y = 20728195
08 feet Y = 6317953
86 meter
Z = 5918161
20 Z = 1803855
53
XDOT = -15478
710644 XDOT = -4717
911004
YDOT = 1309
349630 feet/sec YDOT = 399
089767 meter/sec
ZDOT = -18566
435174 ZDOT = -5659
049441
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 12180
62205480
00016717 00000-0 10270-3 0 9118
2 25544 51
6389 65
2266 0007573 96
4752 263
7264 15
55911167 19793
Satellite: ISS
Catalog Number: 25544
Epoch time: 12180
62205480 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 65
2266 deg
Eccentricity:
0007573
Arg of perigee: 96
4752 deg
Mean anomaly: 263
7264 deg
Mean motion: 15
55911167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 325
Coasting Arc #13 (Orbit 1994)
---------------------------------------
Vector Time (GMT): 2012/181/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3117223
19 A = 6784019
11 meter
Y = 6004033
18 meter E =
0018515
Z = 424875
88 I = 51
96136
XDOT = -4383
846595 Wp = 67
82449
YDOT = 1835
572096 meter/sec RA = 59
74573 deg
ZDOT = 6022
183078 TA = 296
74026
MA = 296
92962
Ha = 220
893 n
mi
Hp = 209
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10227110
20 X = 3047789
22
Y = 19698271
60 feet Y = 6038503
62 meter
Z = 1393949
74 Z = 439851
47
XDOT = -14382
698802 XDOT = -4433
301076
YDOT = 6022
218164 feet/sec YDOT = 1786
271854 meter/sec
ZDOT = 19757
818498 ZDOT = 6000
766564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9113920
77 X = 2777923
05
Y = -20233093
77 feet Y = -6167046
98 meter
Z = 1455042
08 Z = 443496
83
XDOT = 12244
756930 XDOT = 3732
201912
YDOT = 6975
807069 feet/sec YDOT = 2126
225995 meter/sec
ZDOT = 19669
302891 ZDOT = 5995
203521
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 12181
64970783
00016717 00000-0 10270-3 0 9127
2 25544 51
6380 60
0885 0007457 101
0271 259
1722 15
55929137 19956
Satellite: ISS
Catalog Number: 25544
Epoch time: 12181
64970783 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 60
0885 deg
Eccentricity:
0007457
Arg of perigee: 101
0271 deg
Mean anomaly: 259
1722 deg
Mean motion: 15
55929137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1995
Checksum: 317
Coasting Arc #14 (Orbit 2009)
---------------------------------------
Vector Time (GMT): 2012/182/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1682261
67 A = 6781022
21 meter
Y = -6004703
73 meter E =
0012144
Z = -2666546
48 I = 51
93476
XDOT = 5550
645793 Wp = 112
33872
YDOT = 758
132282 meter/sec RA = 54
78465 deg
ZDOT = -5232
456256 TA = 97
62090
MA = 97
48295
Ha = 220
826 n
mi
Hp = 209
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5519231
21 X = -1602037
30
Y = -19700471
55 feet Y = -6023066
83 meter
Z = -8748512
08 Z = -2674524
98
XDOT = 18210
780160 XDOT = 5567
173835
YDOT = 2487
310637 feet/sec YDOT = 820
296310 meter/sec
ZDOT = -17166
851235 ZDOT = -5205
451105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11778067
23 X = -3589954
89
Y = 16711753
14 feet Y = 5093742
36 meter
Z = -8780740
04 Z = -2676369
56
XDOT = -8463
110558 XDOT = -2579
556098
YDOT = -14885
687788 feet/sec YDOT = -4537
157638 meter/sec
ZDOT = -17055
573964 ZDOT = -5198
538944
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 12182
61311818
00016717 00000-0 10270-3 0 9134
2 25544 51
6374 55
2721 0007402 104
5453 255
6522 15
55939306 20101
Satellite: ISS
Catalog Number: 25544
Epoch time: 12182
61311818 = yrday
fracday
Element set: 913
Inclination: 51
6374 deg
RA of node: 55
2721 deg
Eccentricity:
0007402
Arg of perigee: 104
5453 deg
Mean anomaly: 255
6522 deg
Mean motion: 15
55939306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2010
Checksum: 279
Coasting Arc #15 (Orbit 2025)
---------------------------------------
Vector Time (GMT): 2012/183/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -89695
21 A = 6775966
26 meter
Y = 5182855
79 meter E =
0016919
Z = 4353225
25 I = 51
89930
XDOT = -6134
725636 Wp = 108
04526
YDOT = -3038
648020 meter/sec RA = 49
80547 deg
ZDOT = 3475
181723 TA = 306
76352
MA = 306
91872
Ha = 220
791 n
mi
Hp = 209
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -294275
61 X = -168791
25
Y = 17004120
05 feet Y = 5181409
73 meter
Z = 14282235
07 Z = 4352598
33
XDOT = -20127
052613 XDOT = -6117
172530
YDOT = -9969
317650 feet/sec YDOT = -3107
152803 meter/sec
ZDOT = 11401
514839 ZDOT = 3445
421618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13215087
20 X = 4027958
58
Y = -10708821
65 feet Y = -3264048
84 meter
Z = 14279059
65 Z = 4352257
38
XDOT = 4680
809961 XDOT = 1426
710876
YDOT = 20886
534712 feet/sec YDOT = 6366
215780 meter/sec
ZDOT = 11279
132452 ZDOT = 3437
879571
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 12183
64074007
00016717 00000-0 10270-3 0 9145
2 25544 51
6372 50
1338 0007346 107
9696 252
2259 15
55952637 20269
Satellite: ISS
Catalog Number: 25544
Epoch time: 12183
64074007 = yrday
fracday
Element set: 914
Inclination: 51
6372 deg
RA of node: 50
1338 deg
Eccentricity:
0007346
Arg of perigee: 107
9696 deg
Mean anomaly: 252
2259 deg
Mean motion: 15
55952637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2026
Checksum: 308
Coasting Arc #16 (Orbit 2040)
---------------------------------------
Vector Time (GMT): 2012/184/14:04:19
045
Vector Time (MET): N/A
Weight (LBS) : 923383
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2093525
83 A = 6772264
94 meter
Y = -3741422
53 meter E =
0021177
Z = -5260485
40 I = 51
86574
XDOT = 5919
338124 Wp = 92
16835
YDOT = 4746
233780 meter/sec RA = 44
80717 deg
ZDOT = -1024
274650 TA = 168
06374
MA = 168
01347
Ha = 220
728 n
mi
Hp = 209
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6868523
06 X = 2160761
65
Y = -12275008
31 feet Y = -3717634
52 meter
Z = -17258810
36 Z = -5250152
59
XDOT = 19420
400669 XDOT = 5870
800486
YDOT = 15571
633135 feet/sec YDOT = 4812
156286 meter/sec
ZDOT = -3360
481136 ZDOT = -995
635985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13825787
60 X = -4214100
06
Y = 2860764
58 feet Y = 871961
04 meter
Z = -17215765
92 Z = -5247365
45
XDOT = -919
619517 XDOT = -280
300029
YDOT = -23874
153475 feet/sec YDOT = -7276
841979 meter/sec
ZDOT = -3242
918109 ZDOT = -988
441440
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 12184
60411950
00016717 00000-0 10270-3 0 9155
2 25544 51
6362 45
3164 0007457 112
2978 247
8966 15
55991814 20418
Satellite: ISS
Catalog Number: 25544
Epoch time: 12184
60411950 = yrday
fracday
Element set: 915
Inclination: 51
6362 deg
RA of node: 45
3164 deg
Eccentricity:
0007457
Arg of perigee: 112
2978 deg
Mean anomaly: 247
8966 deg
Mean motion: 15
55991814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2041
Checksum: 317
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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