[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 5th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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) : 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 2070)
---------------------------------------
Vector Time (GMT): 2012/186/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5692593
42 A = 6784138
55 meter
Y = 3668570
99 meter E =
0015046
Z = -349626
64 I = 51
86084
XDOT = -2316
937289 Wp = 70
28261
YDOT = 4148
356031 meter/sec RA = 35
12284 deg
ZDOT = 6018
854779 TA = 285
95886
MA = 286
12457
Ha = 220
764 n
mi
Hp = 209
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18676487
59 X = 5652846
00
Y = 12035994
07 feet Y = 3732006
91 meter
Z = -1147069
04 Z = -322068
69
XDOT = -7601
500293 XDOT = -2392
390599
YDOT = 13610
091964 feet/sec YDOT = 4122
023753 meter/sec
ZDOT = 19746
898882 ZDOT = 6007
416784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3698228
36 X = 1127220
00
Y = -21914524
92 feet Y = -6679547
20 meter
Z = -1033834
48 Z = -315112
75
XDOT = 13954
989220 XDOT = 4253
480714
YDOT = 1462
608830 feet/sec YDOT = 445
803171 meter/sec
ZDOT = 19699
241681 ZDOT = 6004
328864
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 12186
53139893
00016717 00000-0 10270-3 0 9006
2 25544 51
6372 35
6995 0007243 118
1501 242
0385 15
55899561 20714
Satellite: ISS
Catalog Number: 25544
Epoch time: 12186
53139893 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 35
6995 deg
Eccentricity:
0007243
Arg of perigee: 118
1501 deg
Mean anomaly: 242
0385 deg
Mean motion: 15
55899561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2071
Checksum: 314
Coasting Arc #2 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2012/187/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4676733
16 A = 6782423
51 meter
Y = -4499514
70 meter E =
0013847
Z = -1960392
76 I = 51
82964
XDOT = 4646
429521 Wp = 130
12426
YDOT = -2400
453833 meter/sec RA = 30
15721 deg
ZDOT = -5609
825877 TA = 71
45669
MA = 71
30631
Ha = 220
644 n
mi
Hp = 209
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15343612
74 X = -4616548
12
Y = -14762187
32 feet Y = -4551476
04 meter
Z = -6431734
77 Z = -1982966
13
XDOT = 15244
191343 XDOT = 4700
177309
YDOT = -7875
504701 feet/sec YDOT = -2348
193286 meter/sec
ZDOT = -18404
940542 ZDOT = -5587
123932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7192844
94 X = -2192379
14
Y = 20010300
66 feet Y = 6099139
64 meter
Z = -6524315
10 Z = -1988611
24
XDOT = -12019
635333 XDOT = -3663
584850
YDOT = -10254
113124 feet/sec YDOT = -3125
453680 meter/sec
ZDOT = -18311
028012 ZDOT = -5581
201338
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 12187
55904734
00016717 00000-0 10270-3 0 9014
2 25544 51
6369 30
5616 0007249 121
7058 238
4803 15
55926005 20872
Satellite: ISS
Catalog Number: 25544
Epoch time: 12187
55904734 = yrday
fracday
Element set: 901
Inclination: 51
6369 deg
RA of node: 30
5616 deg
Eccentricity:
0007249
Arg of perigee: 121
7058 deg
Mean anomaly: 238
4803 deg
Mean motion: 15
55926005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 310
Coasting Arc #3 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2012/188/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2943998
39 A = 6777675
95 meter
Y = 4731399
67 meter E =
0017965
Z = 3848045
59 I = 51
78674
XDOT = -6423
584156 Wp = 108
91503
YDOT = 597
736430 meter/sec RA = 25
17611 deg
ZDOT = 4157
971407 TA = 297
40387
MA = 297
58651
Ha = 220
526 n
mi
Hp = 209
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9658787
37 X = 2872179
51
Y = 15522964
80 feet Y = 4763919
29 meter
Z = 12624821
50 Z = 3862173
24
XDOT = -21074
751168 XDOT = -6449
988866
YDOT = 1961
077526 feet/sec YDOT = 525
755821 meter/sec
ZDOT = 13641
638476 ZDOT = 4126
702427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9971368
59 X = 3039273
15
Y = -15276311
79 feet Y = -4656219
83 meter
Z = 12682540
52 Z = 3865638
35
XDOT = 9664
182319 XDOT = 2945
642771
YDOT = 17584
794575 feet/sec YDOT = 5359
845386 meter/sec
ZDOT = 13512
602471 ZDOT = 4118
641233
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 12188
58668441
00016717 00000-0 10270-3 0 9021
2 25544 51
6365 25
4229 0007195 126
5903 233
5914 15
55953285 21031
Satellite: ISS
Catalog Number: 25544
Epoch time: 12188
58668441 = yrday
fracday
Element set: 902
Inclination: 51
6365 deg
RA of node: 25
4229 deg
Eccentricity:
0007195
Arg of perigee: 126
5903 deg
Mean anomaly: 233
5914 deg
Mean motion: 15
55953285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 316
Coasting Arc #4 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2012/189/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -624233
26 A = 6773158
09 meter
Y = -4478586
07 meter E =
0018548
Z = -5058206
54 I = 51
74349
XDOT = 7337
806194 Wp = 94
31401
YDOT = 1106
361501 meter/sec RA = 20
17511 deg
ZDOT = -1892
481507 TA = 157
38427
MA = 157
30243
Ha = 220
595 n
mi
Hp = 209
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2048009
38 X = -549535
17
Y = -14693523
85 feet Y = -4485148
50 meter
Z = -16595165
82 Z = -5061057
97
XDOT = 24074
167303 XDOT = 7334
082369
YDOT = 3629
794950 feet/sec YDOT = 1188
396755 meter/sec
ZDOT = -6208
928828 ZDOT = -1856
844292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12329961
16 X = -3758172
16
Y = 8227566
21 feet Y = 2507762
18 meter
Z = -16606406
19 Z = -5061632
61
XDOT = -6776
048800 XDOT = -2065
339674
YDOT = -22341
740969 feet/sec YDOT = -6809
762647 meter/sec
ZDOT = -6062
078556 ZDOT = -1847
721544
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 12189
55008587
00016717 00000-0 10270-3 0 9039
2 25544 51
6364 20
6058 0007401 129
1252 231
0561 15
55959947 21181
Satellite: ISS
Catalog Number: 25544
Epoch time: 12189
55008587 = yrday
fracday
Element set: 903
Inclination: 51
6364 deg
RA of node: 20
6058 deg
Eccentricity:
0007401
Arg of perigee: 129
1252 deg
Mean anomaly: 231
0561 deg
Mean motion: 15
55959947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 304
Coasting Arc #5 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2012/190/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1857246
00 A = 6772278
98 meter
Y = 3810452
33 meter E =
0008928
Z = 5274110
91 I = 51
71123
XDOT = -7212
817298 Wp = 112
98529
YDOT = -2535
577107 meter/sec RA = 15
16139 deg
ZDOT = -710
495885 TA = 343
77074
MA = 343
79931
Ha = 220
643 n
mi
Hp = 209
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6093326
78 X = -1925337
33
Y = 12501484
02 feet Y = 3789302
31 meter
Z = 17303513
49 Z = 5264923
53
XDOT = -23664
098748 XDOT = -7180
476499
YDOT = -8318
822528 feet/sec YDOT = -2616
054420 meter/sec
ZDOT = -2331
023245 ZDOT = -745
456617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13953659
85 X = 4253075
52
Y = -190303
91 feet Y = -58004
63 meter
Z = 17265180
98 Z = 5262427
16
XDOT = 3377
162778 XDOT = 1029
359215
YDOT = 23822
002151 feet/sec YDOT = 7260
946256 meter/sec
ZDOT = -2474
911379 ZDOT = -754
352988
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 12190
57770354
00016717 00000-0 10270-3 0 9042
2 25544 51
6364 15
4675 0007393 133
0024 227
1750 15
55933118 21345
Satellite: ISS
Catalog Number: 25544
Epoch time: 12190
57770354 = yrday
fracday
Element set: 904
Inclination: 51
6364 deg
RA of node: 15
4675 deg
Eccentricity:
0007393
Arg of perigee: 133
0024 deg
Mean anomaly: 227
1750 deg
Mean motion: 15
55933118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 291
Coasting Arc #6 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2012/191/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4169840
86 A = 6775390
07 meter
Y = -2877350
81 meter E =
0016526
Z = -4515643
77 I = 51
69301
XDOT = 5947
956902 Wp = 121
48551
YDOT = 3621
064541 meter/sec RA = 10
14972 deg
ZDOT = 3185
315700 TA = 180
52637
MA = 180
52811
Ha = 220
470 n
mi
Hp = 209
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13680580
23 X = 4223641
83
Y = -9440127
34 feet Y = -2830419
90 meter
Z = -14815104
22 Z = -4495256
60
XDOT = 19514
294299 XDOT = 5891
549958
YDOT = 11880
133010 feet/sec YDOT = 3687
262654 meter/sec
ZDOT = 10450
510827 ZDOT = 3214
073591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14819724
75 X = -4517052
10
Y = -7690514
00 feet Y = -2344068
67 meter
Z = -14730694
00 Z = -4489915
53
XDOT = 742
690592 XDOT = 226
372092
YDOT = -21673
717715 feet/sec YDOT = -6606
149160 meter/sec
ZDOT = 10568
685088 ZDOT = 3221
335215
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 12191
54108357
00016717 00000-0 10270-3 0 9059
2 25544 51
6370 10
6503 0007449 136
6277 223
5464 15
55988312 21494
Satellite: ISS
Catalog Number: 25544
Epoch time: 12191
54108357 = yrday
fracday
Element set: 905
Inclination: 51
6370 deg
RA of node: 10
6503 deg
Eccentricity:
0007449
Arg of perigee: 136
6277 deg
Mean anomaly: 223
5464 deg
Mean motion: 15
55988312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 307
Coasting Arc #7 (Orbit 2164)
---------------------------------------
Vector Time (GMT): 2012/192/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5885817
99 A = 6780519
94 meter
Y = 1736927
78 meter E =
0019506
Z = 2857769
57 I = 51
67966
XDOT = -3762
270554 Wp = 113
53061
YDOT = -4366
513499 meter/sec RA = 5
15332 deg
ZDOT = -5075
016580 TA = 33
91659
MA = 33
79201
Ha = 220
422 n
mi
Hp = 209
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19310426
48 X = -5918685
53
Y = 5698581
96 feet Y = 1670924
91 meter
Z = 9375884
43 Z = 2829097
04
XDOT = -12343
407331 XDOT = -3688
510571
YDOT = -14325
831690 feet/sec YDOT = -4408
172714 meter/sec
ZDOT = -16650
316864 ZDOT = -5093
114592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14404976
17 X = 4390636
74
Y = 14144610
97 feet Y = 4311277
42 meter
Z = 9257443
37 Z = 2821668
74
XDOT = -5525
816747 XDOT = -1684
268945
YDOT = 16616
426538 feet/sec YDOT = 5064
686809 meter/sec
ZDOT = -16724
438606 ZDOT = -5097
608887
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 12192
56867877
00016717 00000-0 10270-3 0 9062
2 25544 51
6367 5
5124 0007318 140
9431 219
2252 15
55996448 21651
Satellite: ISS
Catalog Number: 25544
Epoch time: 12192
56867877 = yrday
fracday
Element set: 906
Inclination: 51
6367 deg
RA of node: 5
5124 deg
Eccentricity:
0007318
Arg of perigee: 140
9431 deg
Mean anomaly: 219
2252 deg
Mean motion: 15
55996448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2165
Checksum: 327
Coasting Arc #8 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2012/193/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6727804
35 A = 6783633
12 meter
Y = -523899
80 meter E =
0011531
Z = -687931
69 I = 51
66112
XDOT = 968
337278 Wp = 79
06783
YDOT = 4719
017595 meter/sec RA =
17166 deg
ZDOT = 5963
287682 TA = 273
50298
MA = 273
63486
Ha = 220
313 n
mi
Hp = 209
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22072848
92 X = 6736504
48
Y = -1718831
37 feet Y = -448616
61 meter
Z = -2256993
73 Z = -655227
39
XDOT = 3176
959575 XDOT = 886
528125
YDOT = 15482
341191 feet/sec YDOT = 4729
388170 meter/sec
ZDOT = 19564
592132 ZDOT = 5967
793524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12567033
69 X = -3830431
87
Y = -18243506
51 feet Y = -5560620
78 meter
Z = -2122073
54 Z = -646808
01
XDOT = 10530
054572 XDOT = 3209
560633
YDOT = -9496
154788 feet/sec YDOT = -2894
427979 meter/sec
ZDOT = 19582
619217 ZDOT = 5968
782337
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
53204023
00016717 00000-0 10270-3 0 9079
2 25544 51
6377
6957 0007458 143
9084 216
2574 15
56026090 21803
Satellite: ISS
Catalog Number: 25544
Epoch time: 12193
53204023 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node:
6957 deg
Eccentricity:
0007458
Arg of perigee: 143
9084 deg
Mean anomaly: 216
2574 deg
Mean motion: 15
56026090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 296
Coasting Arc #9 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2012/194/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6522213
87 A = 6782487
68 meter
Y = -776385
57 meter E =
0014911
Z = -1667384
10 I = 51
62695
XDOT = 2011
621471 Wp = 143
87106
YDOT = -4709
400991 meter/sec RA = 355
19245 deg
ZDOT = -5713
689498 TA = 54
42008
MA = 54
28120
Ha = 220
074 n
mi
Hp = 209
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21398339
48 X = -6504947
68
Y = -2547196
75 feet Y = -849224
29 meter
Z = -5470420
27 Z = -1699026
74
XDOT = 6599
807975 XDOT = 2091
889148
YDOT = -15450
790654 feet/sec YDOT = -4686
456383 meter/sec
ZDOT = -18745
700452 ZDOT = -5703
722703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8852823
08 X = 2698340
47
Y = 19610230
45 feet Y = 5977198
24 meter
Z = -5600805
91 Z = -1707125
64
XDOT = -15269
268709 XDOT = -4654
073102
YDOT = 1585
729404 feet/sec YDOT = 483
330322 meter/sec
ZDOT = -18704
048864 ZDOT = -5700
994094
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
55961398
00016717 00000-0 10270-3 0 9088
2 25544 51
6375 355
5575 0007272 146
9285 213
2324 15
56056933 21965
Satellite: ISS
Catalog Number: 25544
Epoch time: 12194
55961398 = yrday
fracday
Element set: 908
Inclination: 51
6375 deg
RA of node: 355
5575 deg
Eccentricity:
0007272
Arg of perigee: 146
9285 deg
Mean anomaly: 213
2324 deg
Mean motion: 15
56056933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 337
Coasting Arc #10 (Orbit 2211)
---------------------------------------
Vector Time (GMT): 2012/195/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5337931
67 A = 6777913
84 meter
Y = 2016693
49 meter E =
0016984
Z = 3651304
08 I = 51
58210
XDOT = -4621
932439 Wp = 115
82202
YDOT = 4304
567099 meter/sec RA = 350
19985 deg
ZDOT = 4356
383876 TA = 287
64367
MA = 287
82907
Ha = 219
988 n
mi
Hp = 209
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17512899
17 X = 5297246
73
Y = 6616448
46 feet Y = 2076157
64 meter
Z = 11979344
09 Z = 3677136
82
XDOT = -15163
820338 XDOT = -4690
885710
YDOT = 14122
595470 feet/sec YDOT = 4252
495725 meter/sec
ZDOT = 14292
598019 ZDOT = 4333
763864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3655892
63 X = -1114316
07
Y = -18290867
87 feet Y = -5575056
53 meter
Z = 12085624
27 Z = 3683698
28
XDOT = 18733
097386 XDOT = 5709
848083
YDOT = 5687
017616 feet/sec YDOT = 1733
402969 meter/sec
ZDOT = 14198
819595 ZDOT = 4327
800213
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
58717694
00016717 00000-0 10270-3 0 9091
2 25544 51
6381 350
4196 0007361 151
9525 208
2027 15
56074163 22125
Satellite: ISS
Catalog Number: 25544
Epoch time: 12195
58717694 = yrday
fracday
Element set: 909
Inclination: 51
6381 deg
RA of node: 350
4196 deg
Eccentricity:
0007361
Arg of perigee: 151
9525 deg
Mean anomaly: 208
2027 deg
Mean motion: 15
56074163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2212
Checksum: 310
Coasting Arc #11 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2012/196/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3327223
38 A = 6773125
81 meter
Y = -3201788
06 meter E =
0015648
Z = -4967404
21 I = 51
53678
XDOT = 6494
239583 Wp = 101
32559
YDOT = -3464
184124 meter/sec RA = 345
18665 deg
ZDOT = -2125
735059 TA = 147
96781
MA = 147
87261
Ha = 219
933 n
mi
Hp = 209
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10916087
21 X = -3267042
66
Y = -10504554
01 feet Y = -3238658
00 meter
Z = -16297257
89 Z = -4983421
85
XDOT = 21306
560311 XDOT = 6542
820410
YDOT = -11365
433479 feet/sec YDOT = -3391
289602 meter/sec
ZDOT = -6974
196388 ZDOT = -2094
068973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2902316
24 X = -884625
99
Y = 14796568
46 feet Y = 4509994
07 meter
Z = -16362926
14 Z = -4987419
89
XDOT = -20094
391598 XDOT = -6124
770559
YDOT = -11477
696648 feet/sec YDOT = -3498
401938 meter/sec
ZDOT = -6843
217440 ZDOT = -2085
812676
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
55050801
00016717 00000-0 10270-3 0 9101
2 25544 51
6387 345
6034 0007254 154
4615 205
6898 15
56075792 22279
Satellite: ISS
Catalog Number: 25544
Epoch time: 12196
55050801 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 345
6034 deg
Eccentricity:
0007254
Arg of perigee: 154
4615 deg
Mean anomaly: 205
6898 deg
Mean motion: 15
56075792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 314
Coasting Arc #12 (Orbit 2242)
---------------------------------------
Vector Time (GMT): 2012/197/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 899438
99 A = 6771777
75 meter
Y = 4138838
90 meter E =
0007700
Z = 5278721
84 I = 51
50312
XDOT = -7330
626928 Wp = 135
99936
YDOT = 2223
291517 meter/sec RA = 340
15752 deg
ZDOT = -499
128746 TA = 318
73701
MA = 318
79518
Ha = 219
827 n
mi
Hp = 210
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2950915
34 X = 827448
19
Y = 13578867
80 feet Y = 4148493
74 meter
Z = 17318641
20 Z = 5282916
94
XDOT = -24050
613282 XDOT = -7352
518767
YDOT = 7294
263506 feet/sec YDOT = 2141
193565 meter/sec
ZDOT = -1637
561501 ZDOT = -534
793167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9658145
30 X = 2943802
69
Y = -9961488
14 feet Y = -3036261
59 meter
Z = 17335451
20 Z = 5283845
53
XDOT = 18778
488671 XDOT = 5723
683347
YDOT = 15129
013572 feet/sec YDOT = 4611
323337 meter/sec
ZDOT = -1784
880366 ZDOT = -544
031536
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
57805046
00016717 00000-0 10270-3 0 9114
2 25544 51
6389 340
4646 0007188 157
9842 202
1622 15
56074833 22439
Satellite: ISS
Catalog Number: 25544
Epoch time: 12197
57805046 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 340
4646 deg
Eccentricity:
0007188
Arg of perigee: 157
9842 deg
Mean anomaly: 202
1622 deg
Mean motion: 15
56074833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2243
Checksum: 317
Coasting Arc #13 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2012/198/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1592410
33 A = 6774781
01 meter
Y = -4751074
59 meter E =
0015426
Z = -4574756
77 I = 51
48547
XDOT = 7005
906808 Wp = 131
23211
YDOT = -581
453724 meter/sec RA = 335
13076 deg
ZDOT = 3039
253661 TA = 169
25939
MA = 169
22641
Ha = 219
729 n
mi
Hp = 210
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5224443
33 X = 1667642
34
Y = -15587515
07 feet Y = -4732845
99 meter
Z = -15009044
51 Z = -4566838
93
XDOT = 22985
258558 XDOT = 6997
124218
YDOT = -1907
656574 feet/sec YDOT = -503
158860 meter/sec
ZDOT = 9971
304661 ZDOT = 3073
266227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15815382
71 X = -4820528
65
Y = 4597258
05 feet Y = 1401244
25 meter
Z = -14975838
52 Z = -4564635
58
XDOT = -14387
453052 XDOT = -4385
295690
YDOT = -16521
160783 feet/sec YDOT = -5035
649807 meter/sec
ZDOT = 10111
619842 ZDOT = 3082
021728
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
54135999
00016717 00000-0 10270-3 0 9126
2 25544 51
6394 335
6483 0007151 162
2343 197
9062 15
56098378 22580
Satellite: ISS
Catalog Number: 25544
Epoch time: 12198
54135999 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 335
6483 deg
Eccentricity:
0007151
Arg of perigee: 162
2343 deg
Mean anomaly: 197
9062 deg
Mean motion: 15
56098378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 340
Coasting Arc #14 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2012/199/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3716295
44 A = 6779983
20 meter
Y = 4834533
28 meter E =
0017362
Z = 2939598
79 I = 51
47598
XDOT = -5681
300800 Wp = 120
25550
YDOT = -1321
848438 meter/sec RA = 330
11792 deg
ZDOT = -4995
010266 TA = 26
02980
MA = 25
94259
Ha = 219
692 n
mi
Hp = 210
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12192570
34 X = -3784359
66
Y = 15861329
65 feet Y = 4792594
39 meter
Z = 9644352
97 Z = 2921380
79
XDOT = -18639
438319 XDOT = -5641
833116
YDOT = -4336
773092 feet/sec YDOT = -1385
158917 meter/sec
ZDOT = -16387
828957 ZDOT = -5022
513663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20033941
29 X = 6106345
31
Y = 579541
04 feet Y = 176644
11 meter
Z = 9568668
80 Z = 2916530
25
XDOT = 7437
263547 XDOT = 2266
877929
YDOT = 16084
054947 feet/sec YDOT = 4902
419948 meter/sec
ZDOT = -16501
083531 ZDOT = -5029
530260
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
56888075
00016717 00000-0 10270-3 0 9130
2 25544 51
6398 330
5098 0007189 165
6024 194
5336 15
56100889 22740
Satellite: ISS
Catalog Number: 25544
Epoch time: 12199
56888075 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 330
5098 deg
Eccentricity:
0007189
Arg of perigee: 165
6024 deg
Mean anomaly: 194
5336 deg
Mean motion: 15
56100889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2274
Checksum: 344
Coasting Arc #15 (Orbit 2288)
---------------------------------------
Vector Time (GMT): 2012/200/12:44:20
200
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5169847
81 A = 6783300
23 meter
Y = -4327667
13 meter E =
0008207
Z = -745686
56 I = 51
46240
XDOT = 3583
003936 Wp = 81
14527
YDOT = 3267
091942 meter/sec RA = 325
12140 deg
ZDOT = 5937
308291 TA = 270
77558
MA = 270
86962
Ha = 219
473 n
mi
Hp = 210
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16961442
96 X = 5221478
75
Y = -14198382
96 feet Y = -4269565
91 meter
Z = -2446478
23 Z = -720447
26
XDOT = 11755
262257 XDOT = 3517
362776
YDOT = 10718
805583 feet/sec YDOT = 3306
791566 meter/sec
ZDOT = 19479
357911 ZDOT = 5954
555008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21556777
21 X = -6570505
69
Y = -5009063
68 feet Y = -1526762
61 meter
Z = -2341905
04 Z = -713812
65
XDOT = 1190
684323 XDOT = 362
920582
YDOT = -14172
802022 feet/sec YDOT = -4319
870056 meter/sec
ZDOT = 19550
097842 ZDOT = 5958
869822
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
53217032
00016717 00000-0 10270-3 0 9140
2 25544 51
6407 325
6930 0006965 168
8918 191
2391 15
56127450 22893
Satellite: ISS
Catalog Number: 25544
Epoch time: 12200
53217032 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 325
6930 deg
Eccentricity:
0006965
Arg of perigee: 168
8918 deg
Mean anomaly: 191
2391 deg
Mean motion: 15
56127450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2289
Checksum: 307
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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