[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 20th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 3507)
---------------------------------------
Vector Time (GMT): 2013/170/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4092242
43 A = 6790409
49 meter
Y = 2232577
05 meter E =
0014170
Z = 4925643
27 I = 51
98726
XDOT = -1116
034841 Wp = 93
75705
YDOT = -7220
392622 meter/sec RA = 95
70374 deg
ZDOT = 2338
796542 TA = 333
44133
MA = 333
51387
Ha = 230
395 n
mi
Hp = 217
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13425992
22 X = -4140831
14
Y = 7324727
86 feet Y = 2186542
79 meter
Z = 16160246
96 Z = 4905645
54
XDOT = -3661
531629 XDOT = -1046
573267
YDOT = -23688
952171 feet/sec YDOT = -7232
484709 meter/sec
ZDOT = 7673
217002 ZDOT = 2333
542796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11899252
95 X = 3626892
30
Y = 9748007
17 feet Y = 2971192
59 meter
Z = 16076275
15 Z = 4900048
66
XDOT = -19812
804746 XDOT = -6038
942887
YDOT = 11528
844669 feet/sec YDOT = 3513
991855 meter/sec
ZDOT = 7652
267860 ZDOT = 2332
411244
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 13170
62219970
00016717 00000-0 10270-3 0 9005
2 25544 51
6486 96
2699 0008780 73
1495 287
0618 15
50266851 35082
Satellite: ISS
Catalog Number: 25544
Epoch time: 13170
62219970 = yrday
fracday
Element set: 900
Inclination: 51
6486 deg
RA of node: 96
2699 deg
Eccentricity:
0008780
Arg of perigee: 73
1495 deg
Mean anomaly: 287
0618 deg
Mean motion: 15
50266851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3508
Checksum: 331
Coasting Arc #2 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2013/171/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4010983
99 A = 6789704
43 meter
Y = -2060440
95 meter E =
0021788
Z = -5095808
48 I = 51
98813
XDOT = 1365
869713 Wp = 75
98817
YDOT = 7285
645582 meter/sec RA = 90
76865 deg
ZDOT = -1872
374229 TA = 175
91114
MA = 175
89331
Ha = 230
216 n
mi
Hp = 217
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13159396
29 X = 4058480
49
Y = -6759976
86 feet Y = -2015321
33 meter
Z = -16718531
76 Z = -5076208
19
XDOT = 4481
199846 XDOT = 1293
394117
YDOT = 23903
036687 feet/sec YDOT = 7300
514621 meter/sec
ZDOT = -6142
960069 ZDOT = -1865
913932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11442468
00 X = -3487664
25
Y = -9522701
30 feet Y = -2902519
36 meter
Z = -16636237
20 Z = -5070725
10
XDOT = 19490
395559 XDOT = 5940
672566
YDOT = -12742
365150 feet/sec YDOT = -3883
872898 meter/sec
ZDOT = -6116
988591 ZDOT = -1864
458122
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 13171
58913530
00016717 00000-0 10270-3 0 9015
2 25544 51
6496 91
4779 0008751 75
9314 284
2809 15
50292523 35230
Satellite: ISS
Catalog Number: 25544
Epoch time: 13171
58913530 = yrday
fracday
Element set: 901
Inclination: 51
6496 deg
RA of node: 91
4779 deg
Eccentricity:
0008751
Arg of perigee: 75
9314 deg
Mean anomaly: 284
2809 deg
Mean motion: 15
50292523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 319
Coasting Arc #3 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2013/172/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3934869
46 A = 6789170
65 meter
Y = 1874956
89 meter E =
0012266
Z = 5194880
11 I = 51
98623
XDOT = -1640
938185 Wp = 94
64579
YDOT = -7359
929991 meter/sec RA = 85
83348 deg
ZDOT = 1409
621514 TA = 341
84501
MA = 341
88876
Ha = 230
356 n
mi
Hp = 217
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12909676
71 X = -3980778
69
Y = 6151433
37 feet Y = 1830697
18 meter
Z = 17043569
92 Z = 5175653
51
XDOT = -5383
655461 XDOT = -1565
363509
YDOT = -24146
751939 feet/sec YDOT = -7377
857660 meter/sec
ZDOT = 4624
742501 ZDOT = 1401
832315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10948006
13 X = 3336952
27
Y = 9348040
45 feet Y = 2849282
73 meter
Z = 16962855
37 Z = 5170278
32
XDOT = -19122
853122 XDOT = -5828
645631
YDOT = 14038
122750 feet/sec YDOT = 4278
819814 meter/sec
ZDOT = 4593
236824 ZDOT = 1400
018584
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 13172
62052537
00016717 00000-0 10270-3 0 9023
2 25544 51
6499 86
3665 0008705 79
8826 280
3306 15
50295318 35391
Satellite: ISS
Catalog Number: 25544
Epoch time: 13172
62052537 = yrday
fracday
Element set: 902
Inclination: 51
6499 deg
RA of node: 86
3665 deg
Eccentricity:
0008705
Arg of perigee: 79
8826 deg
Mean anomaly: 280
3306 deg
Mean motion: 15
50295318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 328
Coasting Arc #4 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2013/173/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3925851
36 A = 6788753
94 meter
Y = -1678637
81 meter E =
0023048
Z = -5298080
66 I = 51
98213
XDOT = 1903
762378 Wp = 82
77769
YDOT = 7346
995719 meter/sec RA = 80
89747 deg
ZDOT = -917
744409 TA = 178
46111
MA = 178
45401
Ha = 230
155 n
mi
Hp = 217
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12880089
76 X = 3970067
17
Y = -5507341
88 feet Y = -1634488
31 meter
Z = -17382154
40 Z = -5278902
07
XDOT = 6245
939562 XDOT = 1825
923356
YDOT = 24104
316664 feet/sec YDOT = 7367
849729 meter/sec
ZDOT = -3010
972469 ZDOT = -908
683866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10512678
31 X = -3204264
35
Y = -9407602
51 feet Y = -2867437
25 meter
Z = -17301659
69 Z = -5273545
87
XDOT = 18459
330397 XDOT = 5626
403905
YDOT = -15161
554691 feet/sec YDOT = -4621
241870 meter/sec
ZDOT = -2974
157450 ZDOT = -906
523191
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 13173
58744586
00016717 00000-0 10270-3 0 9032
2 25544 51
6502 81
5744 0008631 82
6466 277
5666 15
50317227 35549
Satellite: ISS
Catalog Number: 25544
Epoch time: 13173
58744586 = yrday
fracday
Element set: 903
Inclination: 51
6502 deg
RA of node: 81
5744 deg
Eccentricity:
0008631
Arg of perigee: 82
6466 deg
Mean anomaly: 277
5666 deg
Mean motion: 15
50317227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 325
Coasting Arc #5 (Orbit 3569)
---------------------------------------
Vector Time (GMT): 2013/174/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3926307
12 A = 6788496
51 meter
Y = 1474300
89 meter E =
0011101
Z = 5328455
23 I = 51
97582
XDOT = -2178
793702 Wp = 91
37391
YDOT = -7342
959487 meter/sec RA = 75
96138 deg
ZDOT = 425
203076 TA = 354
58524
MA = 354
59724
Ha = 230
291 n
mi
Hp = 217
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12881585
05 X = -3968385
34
Y = 4836945
16 feet Y = 1430158
24 meter
Z = 17481808
51 Z = 5309279
71
XDOT = -7148
273301 XDOT = -2098
586721
YDOT = -24091
074433 feet/sec YDOT = -7366
875745 meter/sec
ZDOT = 1395
023214 ZDOT = 414
812264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10072248
22 X = 3070021
26
Y = 9523014
06 feet Y = 2902614
69 meter
Z = 17401348
21 Z = 5303930
93
XDOT = -17768
696593 XDOT = -5415
898722
YDOT = 16315
654820 feet/sec YDOT = 4973
011589 meter/sec
ZDOT = 1352
649535 ZDOT = 412
287578
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 13174
61881979
00016717 00000-0 10270-3 0 9046
2 25544 51
6504 76
4633 0008598 86
6020 273
6114 15
50322559 35700
Satellite: ISS
Catalog Number: 25544
Epoch time: 13174
61881979 = yrday
fracday
Element set: 904
Inclination: 51
6504 deg
RA of node: 76
4633 deg
Eccentricity:
0008598
Arg of perigee: 86
6020 deg
Mean anomaly: 273
6114 deg
Mean motion: 15
50322559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3570
Checksum: 320
Coasting Arc #6 (Orbit 3584)
---------------------------------------
Vector Time (GMT): 2013/175/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3993136
07 A = 6788422
25 meter
Y = -1278577
68 meter E =
0023346
Z = -5358935
63 I = 51
96665
XDOT = 2427
107600 Wp = 90
13425
YDOT = 7248
935546 meter/sec RA = 71
02359 deg
ZDOT = 79
261585 TA = 180
61851
MA = 180
62140
Ha = 230
085 n
mi
Hp = 217
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13100840
12 X = 4033168
63
Y = -4194808
66 feet Y = -1233699
21 meter
Z = -17581809
82 Z = -5339440
49
XDOT = 7962
951442 XDOT = 2345
483019
YDOT = 23782
596935 feet/sec YDOT = 7275
620593 meter/sec
ZDOT = 260
044569 ZDOT = 90
855060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9763626
68 X = -2975953
41
Y = -9837116
38 feet Y = -2998353
07 meter
Z = -17500034
39 Z = -5334010
48
XDOT = 16808
211967 XDOT = 5123
143008
YDOT = -17228
171358 feet/sec YDOT = -5251
146630 meter/sec
ZDOT = 307
460196 ZDOT = 93
713868
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 13175
58572532
00016717 00000-0 10270-3 0 9056
2 25544 51
6497 71
6706 0008507 89
5483 270
6643 15
50338680 35856
Satellite: ISS
Catalog Number: 25544
Epoch time: 13175
58572532 = yrday
fracday
Element set: 905
Inclination: 51
6497 deg
RA of node: 71
6706 deg
Eccentricity:
0008507
Arg of perigee: 89
5483 deg
Mean anomaly: 270
6643 deg
Mean motion: 15
50338680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3585
Checksum: 336
Coasting Arc #7 (Orbit 3600)
---------------------------------------
Vector Time (GMT): 2013/176/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4070337
79 A = 6788489
14 meter
Y = 1080572
63 meter E =
0011118
Z = 5314815
26 I = 51
95614
XDOT = -2673
589463 Wp = 86
17128
YDOT = -7165
979957 meter/sec RA = 66
08587 deg
ZDOT = -588
841216 TA = 9
43260
MA = 9
41174
Ha = 230
205 n
mi
Hp = 217
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13354126
59 X = -4107936
06
Y = 3545185
79 feet Y = 1034844
57 meter
Z = 17437057
94 Z = 5294951
00
XDOT = -8771
618973 XDOT = -2590
398824
YDOT = -23510
432929 feet/sec YDOT = -7195
412494 meter/sec
ZDOT = -1931
893752 ZDOT = -601
628050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9477649
97 X = 2888787
71
Y = 10196719
64 feet Y = 3107960
15 meter
Z = 17353762
95 Z = 5289426
95
XDOT = -15854
348722 XDOT = -4832
405490
YDOT = 18123
394868 feet/sec YDOT = 5524
010756 meter/sec
ZDOT = -1984
312835 ZDOT = -604
818552
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 13176
61708312
00016717 00000-0 10270-3 0 9069
2 25544 51
6497 66
5591 0008467 93
4750 266
7370 15
50347438 36010
Satellite: ISS
Catalog Number: 25544
Epoch time: 13176
61708312 = yrday
fracday
Element set: 906
Inclination: 51
6497 deg
RA of node: 66
5591 deg
Eccentricity:
0008467
Arg of perigee: 93
4750 deg
Mean anomaly: 266
7370 deg
Mean motion: 15
50347438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3601
Checksum: 323
Coasting Arc #8 (Orbit 3615)
---------------------------------------
Vector Time (GMT): 2013/177/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4207965
14 A = 6788772
04 meter
Y = -910458
44 meter E =
0022606
Z = -5268763
47 I = 51
94257
XDOT = 2879
650435 Wp = 97
61662
YDOT = 6997
556577 meter/sec RA = 61
14583 deg
ZDOT = 1091
773298 TA = 182
82612
MA = 182
83891
Ha = 230
011 n
mi
Hp = 217
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13805659
92 X = 4243427
22
Y = -2987068
36 feet Y = -863203
42 meter
Z = -17285969
40 Z = -5248235
80
XDOT = 9447
672032 XDOT = 2795
884754
YDOT = 22957
862785 feet/sec YDOT = 7029
290158 meter/sec
ZDOT = 3581
933394 ZDOT = 1105
559553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9383489
01 X = -2860087
45
Y = -10697495
09 feet Y = -3260596
50 meter
Z = -17199921
33 Z = -5242536
02
XDOT = 14685
040086 XDOT = 4476
000218
YDOT = -18725
623429 feet/sec YDOT = -5707
570021 meter/sec
ZDOT = 3638
557460 ZDOT = 1109
032314
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 13177
58397388
00016717 00000-0 10270-3 0 9074
2 25544 51
6484 61
7656 0008403 96
7127 263
4981 15
50357230 36168
Satellite: ISS
Catalog Number: 25544
Epoch time: 13177
58397388 = yrday
fracday
Element set: 907
Inclination: 51
6484 deg
RA of node: 61
7656 deg
Eccentricity:
0008403
Arg of perigee: 96
7127 deg
Mean anomaly: 263
4981 deg
Mean motion: 15
50357230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3616
Checksum: 336
Coasting Arc #9 (Orbit 3631)
---------------------------------------
Vector Time (GMT): 2013/178/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4353183
83 A = 6789177
50 meter
Y = 743251
02 meter E =
0012345
Z = 5146336
39 I = 51
92863
XDOT = -3069
779793 Wp = 83
48705
YDOT = -6844
792561 meter/sec RA = 56
20626 deg
ZDOT = -1603
461608 TA = 21
93700
MA = 21
88420
Ha = 230
105 n
mi
Hp = 217
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14282099
19 X = -4386170
71
Y = 2438487
59 feet Y = 694386
03 meter
Z = 16884305
75 Z = 5125109
21
XDOT = -10071
456013 XDOT = -2985
222596
YDOT = -22456
668506 feet/sec YDOT = -6878
647835 meter/sec
ZDOT = -5260
700815 ZDOT = -1618
169434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9329390
44 X = 2843598
21
Y = 11219753
82 feet Y = 3419780
96 meter
Z = 16795355
26 Z = 5119224
28
XDOT = -13569
591381 XDOT = -4136
011453
YDOT = 19271
849732 feet/sec YDOT = 5874
059798 meter/sec
ZDOT = -5321
200231 ZDOT = -1621
901831
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 13178
61531576
00016717 00000-0 10270-3 0 9089
2 25544 51
6486 56
6539 0008331 100
6130 259
5959 15
50369355 36322
Satellite: ISS
Catalog Number: 25544
Epoch time: 13178
61531576 = yrday
fracday
Element set: 908
Inclination: 51
6486 deg
RA of node: 56
6539 deg
Eccentricity:
0008331
Arg of perigee: 100
6130 deg
Mean anomaly: 259
5959 deg
Mean motion: 15
50369355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3632
Checksum: 325
Coasting Arc #10 (Orbit 3646)
---------------------------------------
Vector Time (GMT): 2013/179/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4548023
21 A = 6789785
76 meter
Y = -621113
66 meter E =
0020876
Z = -5022214
96 I = 51
91151
XDOT = 3209
052349 Wp = 104
67858
YDOT = 6617
973506 meter/sec RA = 51
26427 deg
ZDOT = 2089
716457 TA = 185
62883
MA = 185
65233
Ha = 229
939 n
mi
Hp = 217
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14921335
99 X = 4579026
97
Y = -2037774
48 feet Y = -570081
01 meter
Z = -16477083
21 Z = -5000046
01
XDOT = 10528
386971 XDOT = 3124
659043
YDOT = 21712
511504 feet/sec YDOT = 6653
387108 meter/sec
ZDOT = 6856
025122 ZDOT = 2105
101194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9506795
51 X = -2897671
27
Y = -11809806
37 feet Y = -3599628
98 meter
Z = -16384211
18 Z = -4993907
57
XDOT = 12313
229150 XDOT = 3753
072245
YDOT = -19501
854304 feet/sec YDOT = -5944
165192 meter/sec
ZDOT = 6919
385324 ZDOT = 2109
028647
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 13179
58219217
00016717 00000-0 10270-3 0 9092
2 25544 51
6473 51
8599 0008346 104
1253 256
0826 15
50374580 36479
Satellite: ISS
Catalog Number: 25544
Epoch time: 13179
58219217 = yrday
fracday
Element set: 909
Inclination: 51
6473 deg
RA of node: 51
8599 deg
Eccentricity:
0008346
Arg of perigee: 104
1253 deg
Mean anomaly: 256
0826 deg
Mean motion: 15
50374580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3647
Checksum: 325
Coasting Arc #11 (Orbit 3662)
---------------------------------------
Vector Time (GMT): 2013/180/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4744177
22 A = 6790505
06 meter
Y = 505327
70 meter E =
0014382
Z = 4820101
66 I = 51
89461
XDOT = -3319
241314 Wp = 85
56307
YDOT = -6413
839214 meter/sec RA = 46
32298 deg
ZDOT = -2586
829247 TA = 29
85344
MA = 29
77148
Ha = 230
003 n
mi
Hp = 217
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15564885
88 X = -4772889
93
Y = 1657899
26 feet Y = 452114
37 meter
Z = 15813981
81 Z = 4796985
29
XDOT = -10889
899325 XDOT = -3234
707632
YDOT = -21042
779573 feet/sec YDOT = -6450
484198 meter/sec
ZDOT = -8486
972596 ZDOT = -2602
748945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9726352
33 X = 2964592
19
Y = 12388104
11 feet Y = 3775894
13 meter
Z = 15717164
83 Z = 4790591
84
XDOT = -11167
744843 XDOT = -3403
928628
YDOT = 19651
461926 feet/sec YDOT = 5989
765595 meter/sec
ZDOT = -8552
594275 ZDOT = -2606
830735
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 13180
61351854
00016717 00000-0 10270-3 0 9104
2 25544 51
6478 46
7481 0008237 108
0462 252
1587 15
50388223 36639
Satellite: ISS
Catalog Number: 25544
Epoch time: 13180
61351854 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 46
7481 deg
Eccentricity:
0008237
Arg of perigee: 108
0462 deg
Mean anomaly: 252
1587 deg
Mean motion: 15
50388223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3663
Checksum: 307
Coasting Arc #12 (Orbit 3677)
---------------------------------------
Vector Time (GMT): 2013/181/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4975370
83 A = 6791360
59 meter
Y = -447912
61 meter E =
0018342
Z = -4618926
07 I = 51
87450
XDOT = 3373
541729 Wp = 110
49019
YDOT = 6152
509384 meter/sec RA = 41
37942 deg
ZDOT = 3040
792640 TA = 189
85422
MA = 189
89024
Ha = 229
872 n
mi
Hp = 217
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16323395
12 X = 5002447
15
Y = -1469529
58 feet Y = -392123
08 meter
Z = -15153956
91 Z = -4594690
49
XDOT = 11068
050293 XDOT = 3289
720994
YDOT = 20185
398240 feet/sec YDOT = 6189
765521 meter/sec
ZDOT = 9976
353805 ZDOT = 3056
977913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10191833
01 X = -3106470
70
Y = -12953953
70 feet Y = -3948365
09 meter
Z = -15052467
54 Z = -4587992
11
XDOT = 9963
930696 XDOT = 3037
006076
YDOT = -19495
847313 feet/sec YDOT = -5942
334261 meter/sec
ZDOT = 10043
117684 ZDOT = 3061
142270
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 13181
58038091
00016717 00000-0 10270-3 0 9117
2 25544 51
6466 41
9543 0008351 111
6797 248
5244 15
50392810 36782
Satellite: ISS
Catalog Number: 25544
Epoch time: 13181
58038091 = yrday
fracday
Element set: 911
Inclination: 51
6466 deg
RA of node: 41
9543 deg
Eccentricity:
0008351
Arg of perigee: 111
6797 deg
Mean anomaly: 248
5244 deg
Mean motion: 15
50392810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3678
Checksum: 313
Coasting Arc #13 (Orbit 3693)
---------------------------------------
Vector Time (GMT): 2013/182/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5198747
31 A = 6792326
46 meter
Y = 397354
22 meter E =
0016745
Z = 4338502
09 I = 51
85466
XDOT = -3387
569571 Wp = 91
67720
YDOT = -5923
055542 meter/sec RA = 36
43636 deg
ZDOT = -3505
595885 TA = 33
90213
MA = 33
79521
Ha = 229
906 n
mi
Hp = 217
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17056257
56 X = -5223879
48
Y = 1303655
57 feet Y = 339077
59 meter
Z = 14233930
74 Z = 4313186
04
XDOT = -11114
073397 XDOT = -3304
055680
YDOT = -19432
596922 feet/sec YDOT = -5960
470183 meter/sec
ZDOT = -11501
298834 ZDOT = -3521
850127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10682937
78 X = 3256159
44
Y = 13472069
45 feet Y = 4106286
77 meter
Z = 14127930
11 Z = 4306193
10
XDOT = -8932
360469 XDOT = -2722
583471
YDOT = 19253
424541 feet/sec YDOT = 5868
443800 meter/sec
ZDOT = -11568
377373 ZDOT = -3526
041423
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 13182
61169203
00016717 00000-0 10270-3 0 9123
2 25544 51
6471 36
8424 0008218 115
6436 244
5565 15
50404909 36948
Satellite: ISS
Catalog Number: 25544
Epoch time: 13182
61169203 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 36
8424 deg
Eccentricity:
0008218
Arg of perigee: 115
6436 deg
Mean anomaly: 244
5565 deg
Mean motion: 15
50404909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3694
Checksum: 305
Coasting Arc #14 (Orbit 3708)
---------------------------------------
Vector Time (GMT): 2013/183/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5440409
02 A = 6793315
11 meter
Y = -413320
97 meter E =
0015342
Z = -4063963
30 I = 51
83207
XDOT = 3347
538865 Wp = 113
62779
YDOT = 5656
449513 meter/sec RA = 31
49121 deg
ZDOT = 3911
779583 TA = 196
92607
MA = 196
97731
Ha = 229
803 n
mi
Hp = 217
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17849110
95 X = 5464368
15
Y = -1356039
93 feet Y = -352348
46 meter
Z = -13333212
93 Z = -4037476
12
XDOT = 10982
739057 XDOT = 3265
036054
YDOT = 18557
905226 feet/sec YDOT = 5693
422064 meter/sec
ZDOT = 12833
922517 ZDOT = 3927
841878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11408006
62 X = -3477160
42
Y = -13900793
36 feet Y = -4236961
81 meter
Z = -13222310
77 Z = -4030160
32
XDOT = 7919
195240 XDOT = 2413
770709
YDOT = -18751
630453 feet/sec YDOT = -5715
496962 meter/sec
ZDOT = 12900
230935 ZDOT = 3931
990389
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 13183
57854036
00016717 00000-0 10270-3 0 9135
2 25544 51
6464 32
0488 0008409 119
1813 241
0180 15
50413247 37095
Satellite: ISS
Catalog Number: 25544
Epoch time: 13183
57854036 = yrday
fracday
Element set: 913
Inclination: 51
6464 deg
RA of node: 32
0488 deg
Eccentricity:
0008409
Arg of perigee: 119
1813 deg
Mean anomaly: 241
0180 deg
Mean motion: 15
50413247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3709
Checksum: 294
Coasting Arc #15 (Orbit 3724)
---------------------------------------
Vector Time (GMT): 2013/184/13:40:24
949
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5663286
01 A = 6794416
10 meter
Y = 432822
15 meter E =
0019017
Z = 3709608
26 I = 51
80921
XDOT = -3259
054180 Wp = 100
30448
YDOT = -5432
415598 meter/sec RA = 26
54602 deg
ZDOT = -4326
104072 TA = 35
60892
MA = 35
48218
Ha = 229
810 n
mi
Hp = 217
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18580334
69 X = -5685725
28
Y = 1420020
17 feet Y = 369365
77 meter
Z = 12170630
76 Z = 3682042
09
XDOT = -10692
434975 XDOT = -3177
050484
YDOT = -17822
885820 feet/sec YDOT = -5468
401341 meter/sec
ZDOT = -14193
254830 ZDOT = -4341
737765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12122993
54 X = 3695088
43
Y = 14250419
42 feet Y = 4343527
84 meter
Z = 12055211
39 Z = 3674428
43
XDOT = -7136
925930 XDOT = -2175
335024
YDOT = 18176
375439 feet/sec YDOT = 5540
159234 meter/sec
ZDOT = -14257
797871 ZDOT = -4345
776791
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 13184
60983624
00016717 00000-0 10270-3 0 9147
2 25544 51
6464 26
9366 0008274 123
1637 237
0308 15
50421775 37251
Satellite: ISS
Catalog Number: 25544
Epoch time: 13184
60983624 = yrday
fracday
Element set: 914
Inclination: 51
6464 deg
RA of node: 26
9366 deg
Eccentricity:
0008274
Arg of perigee: 123
1637 deg
Mean anomaly: 237
0308 deg
Mean motion: 15
50421775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3725
Checksum: 312
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