[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 8th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
345/16:37:50
586 1
9 3
1 3
1
N/A -2
5 -0
3 226
4
000/00:07:41
172 0
4 0
2 221
1
347/15:02:13
546 1
5 3
4 3
4
N/A -3
0 -0
3 226
3
000/00:08:27
092 0
4 0
2 223
0
Coasting Arc #1 (Orbit 2143)
---------------------------------------
Vector Time (GMT): 2013/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4703506
46 A = 6790135
72 meter
Y = 1752616
68 meter E =
0009644
Z = 4566995
09 I = 51
48440
XDOT = -4866
489455 Wp = 112
08489
YDOT = 5074
515747 meter/sec RA = 334
03874 deg
ZDOT = 3055
831188 TA = 307
24442
MA = 307
33235
Ha = 226
570 n
mi
Hp = 219
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15431451
63 X = 4661373
51
Y = 5750054
73 feet Y = 1804978
35 meter
Z = 14983579
68 Z = 4589742
10
XDOT = -15966
172753 XDOT = -4937
716526
YDOT = 16648
673709 feet/sec YDOT = 5019
697073 meter/sec
ZDOT = 10025
692873 ZDOT = 3032
017601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9614340
92 X = -2930451
11
Y = 13262377
26 feet Y = 4042372
59 meter
Z = 15078935
21 Z = 4596059
45
XDOT = -10833
468757 XDOT = -3302
041277
YDOT = -19169
977165 feet/sec YDOT = -5843
009040 meter/sec
ZDOT = 9924
648894 ZDOT = 3025
032983
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 13340
55375771
00016717 00000-0 10270-3 0 9008
2 25544 51
6469 334
3128 0001173 101
3337 258
7946 15
50784374 21443
Satellite: ISS
Catalog Number: 25544
Epoch time: 13340
55375771 = yrday
fracday
Element set: 900
Inclination: 51
6469 deg
RA of node: 334
3128 deg
Eccentricity:
0001173
Arg of perigee: 101
3337 deg
Mean anomaly: 258
7946 deg
Mean motion: 15
50784374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2144
Checksum: 305
Coasting Arc #2 (Orbit 2158)
---------------------------------------
Vector Time (GMT): 2013/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4358474
17 A = 6788964
73 meter
Y = -1900428
02 meter E =
0012944
Z = -4857982
72 I = 51
45322
XDOT = 5001
035543 Wp = 75
17373
YDOT = -5256
963131 meter/sec RA = 329
06376 deg
ZDOT = -2432
515252 TA = 170
85756
MA = 170
83397
Ha = 226
671 n
mi
Hp = 219
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14299455
95 X = -4313300
49
Y = -6235000
08 feet Y = -1948914
40 meter
Z = -15938263
52 Z = -4879046
16
XDOT = 16407
596925 XDOT = 5071
264869
YDOT = -17247
254366 feet/sec YDOT = -5200
645551 meter/sec
ZDOT = -7980
693085 ZDOT = -2408
050413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9571600
09 X = 2917423
71
Y = -12203000
68 feet Y = -3719474
61 meter
Z = -16026514
18 Z = -4884881
52
XDOT = 11723
791161 XDOT = 3573
411546
YDOT = 19531
191174 feet/sec YDOT = 5953
107070 meter/sec
ZDOT = -7876
885106 ZDOT = -2400
874580
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 13341
52036018
00016717 00000-0 10270-3 0 9015
2 25544 51
6469 329
5183 0001249 103
8282 256
3008 15
50802342 21595
Satellite: ISS
Catalog Number: 25544
Epoch time: 13341
52036018 = yrday
fracday
Element set: 901
Inclination: 51
6469 deg
RA of node: 329
5183 deg
Eccentricity:
0001249
Arg of perigee: 103
8282 deg
Mean anomaly: 256
3008 deg
Mean motion: 15
50802342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2159
Checksum: 284
Coasting Arc #3 (Orbit 2174)
---------------------------------------
Vector Time (GMT): 2013/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4008350
17 A = 6787974
37 meter
Y = 2082929
80 meter E =
0006362
Z = 5062807
26 I = 51
42390
XDOT = -5091
534875 Wp = 120
81402
YDOT = 5446
031782 meter/sec RA = 324
08633 deg
ZDOT = 1785
630260 TA = 311
82513
MA = 311
87944
Ha = 226
464 n
mi
Hp = 219
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13150755
16 X = 3960166
73
Y = 6833759
18 feet Y = 2127484
10 meter
Z = 16610260
04 Z = 5082162
52
XDOT = -16704
510744 XDOT = -5160
729303
YDOT = 17867
558341 feet/sec YDOT = 5388
708033 meter/sec
ZDOT = 5858
366994 ZDOT = 1760
728197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9675314
19 X = -2949035
77
Y = 11105507
98 feet Y = 3384958
83 meter
Z = 16691295
71 Z = 5087506
93
XDOT = -12687
324307 XDOT = -3867
096449
YDOT = -19723
468724 feet/sec YDOT = -6011
713267 meter/sec
ZDOT = 5752
695962 ZDOT = 1753
421729
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 13342
55138533
00016717 00000-0 10270-3 0 9025
2 25544 51
6466 324
4045 0001122 104
4191 255
7085 15
50833795 21751
Satellite: ISS
Catalog Number: 25544
Epoch time: 13342
55138533 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node: 324
4045 deg
Eccentricity:
0001122
Arg of perigee: 104
4191 deg
Mean anomaly: 255
7085 deg
Mean motion: 15
50833795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2175
Checksum: 290
Coasting Arc #4 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2013/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3667313
52 A = 6787283
25 meter
Y = -2340418
77 meter E =
0015369
Z = -5223202
47 I = 51
39725
XDOT = 5116
410942 Wp = 83
42439
YDOT = -5583
813301 meter/sec RA = 319
10536 deg
ZDOT = -1091
383206 TA = 176
06538
MA = 176
05328
Ha = 226
579 n
mi
Hp = 219
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12031868
50 X = -3615496
91
Y = -7678539
26 feet Y = -2381139
10 meter
Z = -17136491
06 Z = -5240892
22
XDOT = 16786
125137 XDOT = 5183
771772
YDOT = -18319
597444 feet/sec YDOT = -5526
221662 meter/sec
ZDOT = -3580
653562 ZDOT = -1066
364649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10066381
02 X = 3068232
93
Y = -9992625
69 feet Y = -3045752
31 meter
Z = -17210478
07 Z = -5245753
72
XDOT = 13544
636833 XDOT = 4128
405307
YDOT = 19622
846880 feet/sec YDOT = 5981
043729 meter/sec
ZDOT = -3474
477815 ZDOT = -1059
020838
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 13343
51795497
00016717 00000-0 10270-3 0 9031
2 25544 51
6466 319
6098 0001208 107
1104 253
0180 15
50852519 21903
Satellite: ISS
Catalog Number: 25544
Epoch time: 13343
51795497 = yrday
fracday
Element set: 903
Inclination: 51
6466 deg
RA of node: 319
6098 deg
Eccentricity:
0001208
Arg of perigee: 107
1104 deg
Mean anomaly: 253
0180 deg
Mean motion: 15
50852519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 298
Coasting Arc #5 (Orbit 2205)
---------------------------------------
Vector Time (GMT): 2013/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3335228
93 A = 6786847
81 meter
Y = 2631967
77 meter E =
0003686
Z = 5289454
60 I = 51
37323
XDOT = -5107
802393 Wp = 106
04014
YDOT = 5704
137959 meter/sec RA = 314
12270 deg
ZDOT = 381
159067 TA = 340
30387
MA = 340
31810
Ha = 226
380 n
mi
Hp = 219
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10942352
12 X = 3279854
92
Y = 8635064
86 feet Y = 2668954
64 meter
Z = 17353853
67 Z = 5305522
51
XDOT = -16757
881868 XDOT = -5173
059281
YDOT = 18714
363381 feet/sec YDOT = 5646
654373 meter/sec
ZDOT = 1250
521873 ZDOT = 356
187367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10614133
15 X = -3235187
78
Y = 8905370
40 feet Y = 2714356
90 meter
Z = 17420970
35 Z = 5309911
76
XDOT = -14367
187024 XDOT = -4379
118605
YDOT = -19370
738360 feet/sec YDOT = -5904
201052 meter/sec
ZDOT = 1144
530671 ZDOT = 348
852949
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 13344
54894510
00016717 00000-0 10270-3 0 9042
2 25544 51
6464 314
4959 0001103 108
1021 252
0250 15
50883670 22060
Satellite: ISS
Catalog Number: 25544
Epoch time: 13344
54894510 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 314
4959 deg
Eccentricity:
0001103
Arg of perigee: 108
1021 deg
Mean anomaly: 252
0250 deg
Mean motion: 15
50883670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2206
Checksum: 276
Coasting Arc #6 (Orbit 2220)
---------------------------------------
Vector Time (GMT): 2013/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3037172
16 A = 6786805
40 meter
Y = -2982196
02 meter E =
0015851
Z = -5299900
48 I = 51
35257
XDOT = 5037
200398 Wp = 93
93147
YDOT = -5749
021226 meter/sec RA = 309
13719 deg
ZDOT = 348
121982 TA = 179
40910
MA = 179
40723
Ha = 226
461 n
mi
Hp = 219
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9964475
59 X = -2977853
16
Y = -9784107
69 feet Y = -3015827
73 meter
Z = -17388124
95 Z = -5314510
95
XDOT = 16526
248026 XDOT = 5099
421754
YDOT = -18861
618195 feet/sec YDOT = -5692
344156 meter/sec
ZDOT = 1142
132487 ZDOT = 372
743357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11411829
76 X = 3478325
71
Y = -7916255
98 feet Y = -2412874
82 meter
Z = -17449053
24 Z = -5318471
43
XDOT = 14972
966337 XDOT = 4563
760140
YDOT = 18835
531171 feet/sec YDOT = 5741
069901 meter/sec
ZDOT = 1246
651623 ZDOT = 379
979415
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 13345
51548134
00016717 00000-0 10270-3 0 9059
2 25544 51
6466 309
7007 0001127 111
2355 248
8917 15
50905544 22219
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
51548134 = yrday
fracday
Element set: 905
Inclination: 51
6466 deg
RA of node: 309
7007 deg
Eccentricity:
0001127
Arg of perigee: 111
2355 deg
Mean anomaly: 248
8917 deg
Mean motion: 15
50905544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2221
Checksum: 292
Coasting Arc #7 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2013/345/16:41:41
172
Vector Time (MET): N/A
Weight (LBS) : 901651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2031062
84 A = 6789333
81 meter
Y = -4012105
13 meter E =
0011924
Z = -5097335
00 I = 51
35519
XDOT = 5589
993119 Wp = 105
11926
YDOT = -4952
704662 meter/sec RA = 308
15280 deg
ZDOT = 1671
138447 TA = 181
11454
MA = 181
11720
Ha = 226
390 n
mi
Hp = 221
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6663591
99 X = -1961285
95
Y = -13163074
56 feet Y = -4034427
41 meter
Z = -16723540
02 Z = -5107032
49
XDOT = 18339
872438 XDOT = 5636
841889
YDOT = -16249
031043 feet/sec YDOT = -4889
931921 meter/sec
ZDOT = 5482
737687 ZDOT = 1698
407956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 861349
76 X = 262539
41
Y = -14682829
13 feet Y = -4475326
32 meter
Z = -16763632
85 Z = -5109555
29
XDOT = 22892
871282 XDOT = 6977
747167
YDOT = -5047
754922 feet/sec YDOT = -1538
555700 meter/sec
ZDOT = 5598
255226 ZDOT = 1706
348193
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 13345
70878708
00016717 00000-0 10270-3 0 9064
2 25544 51
6500 308
7423 0001521 262
3770 97
7208 15
50352664 22242
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
70878708 = yrday
fracday
Element set: 906
Inclination: 51
6500 deg
RA of node: 308
7423 deg
Eccentricity:
0001521
Arg of perigee: 262
3770 deg
Mean anomaly: 97
7208 deg
Mean motion: 15
50352664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 300
Coasting Arc #8 (Orbit 2239)
---------------------------------------
Vector Time (GMT): 2013/346/16:41:41
172
Vector Time (MET): N/A
Weight (LBS) : 901651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1958479
26 A = 6789803
99 meter
Y = 4225265
99 meter E =
0005092
Z = 4938796
10 I = 51
33888
XDOT = -5361
296050 Wp = 48
13528
YDOT = 5027
727437 meter/sec RA = 303
17294 deg
ZDOT = -2170
542494 TA = 63
15738
MA = 63
10532
Ha = 226
194 n
mi
Hp = 221
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6425456
89 X = 1887094
26
Y = 13862421
24 feet Y = 4246767
55 meter
Z = 16203399
28 Z = 4948137
15
XDOT = -17589
553970 XDOT = -5406
574731
YDOT = 16495
168758 feet/sec YDOT = 4967
520961 meter/sec
ZDOT = -7121
202407 ZDOT = -2196
697161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1151884
58 X = -351094
42
Y = 15194581
27 feet Y = 4631308
37 meter
Z = 16241958
90 Z = 4950549
07
XDOT = -22218
905003 XDOT = -6772
322245
YDOT = 6062
902676 feet/sec YDOT = 1847
972736 meter/sec
ZDOT = -7232
040864 ZDOT = -2204
326055
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 13346
74012381
00016717 00000-0 10270-3 0 9077
2 25544 51
6499 303
6304 0001610 268
7780 91
3186 15
50410365 22407
Satellite: ISS
Catalog Number: 25544
Epoch time: 13346
74012381 = yrday
fracday
Element set: 907
Inclination: 51
6499 deg
RA of node: 303
6304 deg
Eccentricity:
0001610
Arg of perigee: 268
7780 deg
Mean anomaly: 91
3186 deg
Mean motion: 15
50410365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2240
Checksum: 288
Coasting Arc #9 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2013/347/15:06:27
092
Vector Time (MET): N/A
Weight (LBS) : 901284
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2622520
22 A = 6791153
18 meter
Y = -3683198
89 meter E =
0009127
Z = -5075470
05 I = 51
32155
XDOT = 4722
633426 Wp = 108
41900
YDOT = -5765
716541 meter/sec RA = 298
52593 deg
ZDOT = 1743
656253 TA = 178
54846
MA = 178
54581
Ha = 226
337 n
mi
Hp = 222
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8604068
95 X = -2556483
44
Y = -12083985
85 feet Y = -3712156
00 meter
Z = -16651804
62 Z = -5088050
00
XDOT = 15494
204154 XDOT = 4778
285651
YDOT = -18916
392852 feet/sec YDOT = -5712
593997 meter/sec
ZDOT = 5720
656999 ZDOT = 1766
733400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4227230
53 X = 1288459
87
Y = -14157669
08 feet Y = -4315257
54 meter
Z = -16704078
61 Z = -5091403
16
XDOT = 23392
738121 XDOT = 7130
106579
YDOT = 118
514434 feet/sec YDOT = 36
123200 meter/sec
ZDOT = 5818
677634 ZDOT = 1773
532943
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 13347
64253222
00016717 00000-0 10270-3 0 9089
2 25544 51
6496 299
1559 0004210 271
7177 88
3492 15
49756445 22549
Satellite: ISS
Catalog Number: 25544
Epoch time: 13347
64253222 = yrday
fracday
Element set: 908
Inclination: 51
6496 deg
RA of node: 299
1559 deg
Eccentricity:
0004210
Arg of perigee: 271
7177 deg
Mean anomaly: 88
3492 deg
Mean motion: 15
49756445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 332
Coasting Arc #10 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2013/348/15:06:27
092
Vector Time (MET): N/A
Weight (LBS) : 901284
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2736903
47 A = 6791359
62 meter
Y = 3713044
45 meter E =
0003839
Z = 4985010
18 I = 51
30875
XDOT = -4370
416388 Wp = 11
58379
YDOT = 5954
588958 meter/sec RA = 293
55001 deg
ZDOT = -2031
787123 TA = 98
30271
MA = 98
25918
Ha = 226
167 n
mi
Hp = 223
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8979342
09 X = 2670963
92
Y = 12181904
37 feet Y = 3743281
14 meter
Z = 16355020
28 Z = 4998146
08
XDOT = -14338
636442 XDOT = -4426
807140
YDOT = 19536
053011 feet/sec YDOT = 5905
401051 meter/sec
ZDOT = -6665
968251 ZDOT = -2053
154877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3820343
81 X = -1164440
79
Y = 14582285
93 feet Y = 4444680
75 meter
Z = 16409630
61 Z = 5001655
41
XDOT = -23110
663233 XDOT = -7044
130153
YDOT = 1563
484951 feet/sec YDOT = 476
550213 meter/sec
ZDOT = -6756
831064 ZDOT = -2059
482108
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 13348
67426289
00016717 00000-0 10270-3 0 9099
2 25544 51
6495 294
0468 0004297 276
0830 83
9831 15
49809063 22701
Satellite: ISS
Catalog Number: 25544
Epoch time: 13348
67426289 = yrday
fracday
Element set: 909
Inclination: 51
6495 deg
RA of node: 294
0468 deg
Eccentricity:
0004297
Arg of perigee: 276
0830 deg
Mean anomaly: 83
9831 deg
Mean motion: 15
49809063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 344
Coasting Arc #11 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2013/349/15:06:27
092
Vector Time (MET): N/A
Weight (LBS) : 901284
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2874110
25 A = 6791772
23 meter
Y = -3745715
78 meter E =
0007782
Z = -4889688
62 I = 51
29938
XDOT = 4006
510486 Wp = 110
95396
YDOT = -6097
560977 meter/sec RA = 288
57270 deg
ZDOT = 2316
280605 TA = 181
85746
MA = 181
86036
Ha = 226
281 n
mi
Hp = 222
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9429495
57 X = -2808258
27
Y = -12289093
77 feet Y = -3777487
24 meter
Z = -16042285
49 Z = -4903491
29
XDOT = 13144
719442 XDOT = 4063
145052
YDOT = -20005
121317 feet/sec YDOT = -6052
441189 meter/sec
ZDOT = 7599
345818 ZDOT = 2335
880976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3358803
89 X = 1023763
43
Y = -15060220
81 feet Y = -4590355
30 meter
Z = -16099699
43 Z = -4907188
39
XDOT = 22633
422649 XDOT = 6898
667223
YDOT = -3164
321991 feet/sec YDOT = -964
485343 meter/sec
ZDOT = 7682
798907 ZDOT = 2341
717107
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 13349
64149631
00016717 00000-0 10270-3 0 9102
2 25544 51
6502 289
2566 0004276 279
3709 80
6958 15
49809028 22854
Satellite: ISS
Catalog Number: 25544
Epoch time: 13349
64149631 = yrday
fracday
Element set: 910
Inclination: 51
6502 deg
RA of node: 289
2566 deg
Eccentricity:
0004276
Arg of perigee: 279
3709 deg
Mean anomaly: 80
6958 deg
Mean motion: 15
49809028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 340
Coasting Arc #12 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2013/350/15:06:27
092
Vector Time (MET): N/A
Weight (LBS) : 901284
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3014515
65 A = 6792092
71 meter
Y = 3784878
36 meter E =
0005170
Z = 4766445
36 I = 51
29208
XDOT = -3653
975735 Wp = 26
99984
YDOT = 6206
106450 meter/sec RA = 283
59517 deg
ZDOT = -2611
484084 TA = 88
93268
MA = 88
87345
Ha = 226
186 n
mi
Hp = 222
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9890143
20 X = 2948814
07
Y = 12417579
93 feet Y = 3818220
74 meter
Z = 15637944
10 Z = 4780930
47
XDOT = -11988
109366 XDOT = -3710
416294
YDOT = 20361
241635 feet/sec YDOT = 6164
930065 meter/sec
ZDOT = -8567
861167 ZDOT = -2629
371270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2890739
21 X = -881097
31
Y = 15548819
02 feet Y = 4739280
04 meter
Z = 15698228
36 Z = 4784820
00
XDOT = -22045
913693 XDOT = -6719
594494
YDOT = 4647
167168 feet/sec YDOT = 1416
456553 meter/sec
ZDOT = -8644
125436 ZDOT = -2634
729433
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 13350
67319405
00016717 00000-0 10270-3 0 9116
2 25544 51
6503 284
1474 0004363 283
8854 76
1811 15
49864798 23017
Satellite: ISS
Catalog Number: 25544
Epoch time: 13350
67319405 = yrday
fracday
Element set: 911
Inclination: 51
6503 deg
RA of node: 284
1474 deg
Eccentricity:
0004363
Arg of perigee: 283
8854 deg
Mean anomaly: 76
1811 deg
Mean motion: 15
49864798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 317
Coasting Arc #13 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2013/351/15:06:27
092
Vector Time (MET): N/A
Weight (LBS) : 901284
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3181331
94 A = 6792626
61 meter
Y = -3816449
25 meter E =
0006064
Z = -4637794
58 I = 51
28761
XDOT = 3299
532505 Wp = 111
68144
YDOT = -6271
021903 meter/sec RA = 278
61676 deg
ZDOT = 2897
963494 TA = 187
33415
MA = 187
34303
Ha = 226
293 n
mi
Hp = 222
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10437440
75 X = -3115889
96
Y = -12521158
97 feet Y = -3851658
53 meter
Z = -15215861
47 Z = -4653090
66
XDOT = 10825
237878 XDOT = 3355
333713
YDOT = -20574
218843 feet/sec YDOT = -6233
812741 meter/sec
ZDOT = 9507
754246 ZDOT = 2914
127188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2330192
22 X = 710242
59
Y = -16073185
32 feet Y = -4899106
88 meter
Z = -15279559
87 Z = -4657209
85
XDOT = 21300
648493 XDOT = 6492
437661
YDOT = -6013
179473 feet/sec YDOT = -1832
817103 meter/sec
ZDOT = 9576
777111 ZDOT = 2919
001663
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 13351
64039686
00016717 00000-0 10270-3 0 9125
2 25544 51
6504 279
3571 0004382 286
8754 73
1916 15
49860156 23168
Satellite: ISS
Catalog Number: 25544
Epoch time: 13351
64039686 = yrday
fracday
Element set: 912
Inclination: 51
6504 deg
RA of node: 279
3571 deg
Eccentricity:
0004382
Arg of perigee: 286
8754 deg
Mean anomaly: 73
1916 deg
Mean motion: 15
49860156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 327
Coasting Arc #14 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2013/352/15:06:27
092
Vector Time (MET): N/A
Weight (LBS) : 901284
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3351697
33 A = 6793057
86 meter
Y = 3853519
27 meter E =
0006480
Z = 4478159
42 I = 51
28590
XDOT = -2965
911025 Wp = 40
21572
YDOT = 6300
015991 meter/sec RA = 273
63852 deg
ZDOT = -3193
946116 TA = 82
11907
MA = 82
04552
Ha = 226
275 n
mi
Hp = 222
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10996382
30 X = 3286603
70
Y = 12642779
77 feet Y = 3890635
66 meter
Z = 14692124
07 Z = 4494283
90
XDOT = -9730
679215 XDOT = -3020
623497
YDOT = 20669
343801 feet/sec YDOT = 6266
543704 meter/sec
ZDOT = -10478
825841 ZDOT = -3208
486432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1757294
06 X = -535623
23
Y = 16604019
85 feet Y = 5060905
25 meter
Z = 14759310
83 Z = 4498637
94
XDOT = -20474
233877 XDOT = -6240
546486
YDOT = 7224
661731 feet/sec YDOT = 2202
076896 meter/sec
ZDOT = -10541
020153 ZDOT = -3212
902943
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 13352
67206213
00016717 00000-0 10270-3 0 9132
2 25544 51
6504 274
2478 0004463 291
5312 68
5363 15
49918412 23322
Satellite: ISS
Catalog Number: 25544
Epoch time: 13352
67206213 = yrday
fracday
Element set: 913
Inclination: 51
6504 deg
RA of node: 274
2478 deg
Eccentricity:
0004463
Arg of perigee: 291
5312 deg
Mean anomaly: 68
5363 deg
Mean motion: 15
49918412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 298
Coasting Arc #15 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2013/353/15:06:27
092
Vector Time (MET): N/A
Weight (LBS) : 901284
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3548921
72 A = 6793701
04 meter
Y = -3871704
62 meter E =
0004113
Z = -4313387
28 I = 51
28624
XDOT = 2639
888605 Wp = 106
44708
YDOT = -6290
750841 meter/sec RA = 268
65951 deg
ZDOT = 3476
197648 TA = 199
12557
MA = 199
14102
Ha = 226
365 n
mi
Hp = 222
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11643443
96 X = -3484410
56
Y = -12702442
97 feet Y = -3911029
81 meter
Z = -14151533
08 Z = -4330471
20
XDOT = 8661
051854 XDOT = 2693
150654
YDOT = -20638
946330 feet/sec YDOT = -6260
932452 meter/sec
ZDOT = 11404
847928 ZDOT = 3489
150680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1060995
39 X = 323391
39
Y = -17139866
05 feet Y = -5224231
17 meter
Z = -14222763
92 Z = -4335098
44
XDOT = 19538
724013 XDOT = 5955
403079
YDOT = -8295
977366 feet/sec YDOT = -2528
613901 meter/sec
ZDOT = 11460
357046 ZDOT = 3493
116828
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 13353
63923488
00016717 00000-0 10270-3 0 9140
2 25544 51
6497 269
4572 0004485 294
0653 66
0028 15
49908981 23471
Satellite: ISS
Catalog Number: 25544
Epoch time: 13353
63923488 = yrday
fracday
Element set: 914
Inclination: 51
6497 deg
RA of node: 269
4572 deg
Eccentricity:
0004485
Arg of perigee: 294
0653 deg
Mean anomaly: 66
0028 deg
Mean motion: 15
49908981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 345
Coasting Arc #16 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2013/354/15:06:27
092
Vector Time (MET): N/A
Weight (LBS) : 901284
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3748852
85 A = 6794229
09 meter
Y = 3893793
31 meter E =
0007686
Z = 4114538
73 I = 51
29013
XDOT = -2344
517183 Wp = 52
56783
YDOT = 6246
093240 meter/sec RA = 263
68127 deg
ZDOT = -3765
393252 TA = 76
51640
MA = 76
43076
Ha = 226
409 n
mi
Hp = 222
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12299385
99 X = 3685045
81
Y = 12774912
43 feet Y = 3935358
26 meter
Z = 13499142
83 Z = 4132595
52
XDOT = -7691
985507 XDOT = -2395
897022
YDOT = 20492
431889 feet/sec YDOT = 6219
588385 meter/sec
ZDOT = -12353
652401 ZDOT = -3776
906896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -349136
62 X = -106416
84
Y = 17672347
88 feet Y = 5386531
63 meter
Z = 13574474
74 Z = 4137499
90
XDOT = -18560
811266 XDOT = -5657
335274
YDOT = 9184
053694 feet/sec YDOT = 2799
299566 meter/sec
ZDOT = -12403
090961 ZDOT = -3780
462125
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 13354
67086825
00016717 00000-0 10270-3 0 9151
2 25544 51
6496 264
3476 0004582 298
7667 61
3023 15
49968240 23636
Satellite: ISS
Catalog Number: 25544
Epoch time: 13354
67086825 = yrday
fracday
Element set: 915
Inclination: 51
6496 deg
RA of node: 264
3476 deg
Eccentricity:
0004582
Arg of perigee: 298
7667 deg
Mean anomaly: 61
3023 deg
Mean motion: 15
49968240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 341
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