[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 3rd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 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
345/16:37:49
310 1
8 3
0 3
1
N/A -2
4 -0
3 226
5
000/00:09:38
621 0
4 0
2 221
1
347/15:02:18
115 1
5 3
3 3
3
N/A -3
0 -0
3 226
5
000/00:10:36
231 0
4 0
3 223
1
Coasting Arc #1 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2013/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5856921
82 A = 6795581
38 meter
Y = 1734397
58 meter E =
0014457
Z = 2963291
86 I = 51
62198
XDOT = -3831
272323 Wp = 83
12101
YDOT = 4382
377946 meter/sec RA = 353
90134 deg
ZDOT = 4988
269722 TA = 310
71206
MA = 310
83754
Ha = 226
854 n
mi
Hp = 219
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19215622
78 X = 5822696
95
Y = 5690280
77 feet Y = 1799701
78 meter
Z = 9722086
17 Z = 2991661
85
XDOT = -12569
791086 XDOT = -3904
224431
YDOT = 14377
880401 feet/sec YDOT = 4339
125877 meter/sec
ZDOT = 16365
714310 ZDOT = 4969
480568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11709865
51 X = -3569167
01
Y = 16191680
74 feet Y = 4935224
29 meter
Z = 9841084
18 Z = 2999562
46
XDOT = -8194
383937 XDOT = -2497
648224
YDOT = -15862
440351 feet/sec YDOT = -4834
871819 meter/sec
ZDOT = 16285
922401 ZDOT = 4963
949148
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 13336
55831216
00016717 00000-0 10270-3 0 9004
2 25544 51
6488 354
1261 0001338 89
1858 270
9446 15
50677729 20823
Satellite: ISS
Catalog Number: 25544
Epoch time: 13336
55831216 = yrday
fracday
Element set: 900
Inclination: 51
6488 deg
RA of node: 354
1261 deg
Eccentricity:
0001338
Arg of perigee: 89
1858 deg
Mean anomaly: 270
9446 deg
Mean motion: 15
50677729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2082
Checksum: 321
Coasting Arc #2 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2013/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5615639
04 A = 6794195
90 meter
Y = -1681906
20 meter E =
0006226
Z = -3440232
56 I = 51
58727
XDOT = 4154
187650 Wp = 88
42439
YDOT = -4513
588341 meter/sec RA = 348
94017 deg
ZDOT = -4581
418959 TA = 131
81266
MA = 131
75946
Ha = 226
807 n
mi
Hp = 219
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18424012
60 X = -5579702
26
Y = -5518064
95 feet Y = -1744502
56 meter
Z = -11286852
22 Z = -3467426
11
XDOT = 13629
224572 XDOT = 4226
606459
YDOT = -14808
360699 feet/sec YDOT = -4466
728180 meter/sec
ZDOT = -15030
902098 ZDOT = -4561
062554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11014104
74 X = 3357099
13
Y = -15684227
67 feet Y = -4780552
59 meter
Z = -11400912
82 Z = -3474998
23
XDOT = 8595
286924 XDOT = 2619
843454
YDOT = 16882
577599 feet/sec YDOT = 5145
809652 meter/sec
ZDOT = -14944
493004 ZDOT = -4555
081468
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 13337
52497555
00016717 00000-0 10270-3 0 9017
2 25544 51
6489 349
3320 0001238 94
4434 265
6858 15
50707666 20972
Satellite: ISS
Catalog Number: 25544
Epoch time: 13337
52497555 = yrday
fracday
Element set: 901
Inclination: 51
6489 deg
RA of node: 349
3320 deg
Eccentricity:
0001238
Arg of perigee: 94
4434 deg
Mean anomaly: 265
6858 deg
Mean motion: 15
50707666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2097
Checksum: 333
Coasting Arc #3 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2013/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5344812
92 A = 6792875
38 meter
Y = 1643224
85 meter E =
0012498
Z = 3847569
97 I = 51
55202
XDOT = -4431
068461 Wp = 97
68647
YDOT = 4691
336198 meter/sec RA = 343
97558 deg
ZDOT = 4138
607933 TA = 308
68214
MA = 308
79388
Ha = 226
721 n
mi
Hp = 219
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17535475
47 X = 5307350
16
Y = 5391157
64 feet Y = 1702784
08 meter
Z = 12623261
04 Z = 3873443
99
XDOT = -14537
626183 XDOT = -4503
303101
YDOT = 15391
522959 feet/sec YDOT = 4641
380848 meter/sec
ZDOT = 13578
110017 ZDOT = 4116
907049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10354126
55 X = -3155937
77
Y = 15053172
46 feet Y = 4588206
96 meter
Z = 12731781
58 Z = 3880647
03
XDOT = -9232
296005 XDOT = -2814
003822
YDOT = -17792
885609 feet/sec YDOT = -5423
271534 meter/sec
ZDOT = 13486
013708 ZDOT = 4110
536978
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 13338
55607145
00016717 00000-0 10270-3 0 9020
2 25544 51
6481 344
2182 0001266 93
6506 266
4790 15
50725794 21131
Satellite: ISS
Catalog Number: 25544
Epoch time: 13338
55607145 = yrday
fracday
Element set: 902
Inclination: 51
6481 deg
RA of node: 344
2182 deg
Eccentricity:
0001266
Arg of perigee: 93
6506 deg
Mean anomaly: 266
4790 deg
Mean motion: 15
50725794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 305
Coasting Arc #4 (Orbit 2127)
---------------------------------------
Vector Time (GMT): 2013/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5037692
47 A = 6791488
03 meter
Y = -1679832
89 meter E =
0009387
Z = -4243292
81 I = 51
51815
XDOT = 4667
330365 Wp = 72
86411
YDOT = -4870
486297 meter/sec RA = 339
00745 deg
ZDOT = -3616
925141 TA = 160
02281
MA = 159
98604
Ha = 226
766 n
mi
Hp = 219
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16527862
43 X = -4997920
95
Y = -5511262
76 feet Y = -1735944
80 meter
Z = -13921564
35 Z = -4267669
11
XDOT = 15312
763665 XDOT = 4739
016435
YDOT = -15979
285752 feet/sec YDOT = -4817
892075 meter/sec
ZDOT = -11866
552300 ZDOT = -3594
077930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9922732
92 X = 3024449
00
Y = -14220657
66 feet Y = -4334456
45 meter
Z = -14023782
47 Z = -4274448
90
XDOT = 9958
859465 XDOT = 3035
460365
YDOT = 18543
003979 feet/sec YDOT = 5651
907613 meter/sec
ZDOT = -11769
604379 ZDOT = -3587
375415
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 13339
52271123
00016717 00000-0 10270-3 0 9032
2 25544 51
6481 339
4239 0001255 96
8668 263
2626 15
50742714 21282
Satellite: ISS
Catalog Number: 25544
Epoch time: 13339
52271123 = yrday
fracday
Element set: 903
Inclination: 51
6481 deg
RA of node: 339
4239 deg
Eccentricity:
0001255
Arg of perigee: 96
8668 deg
Mean anomaly: 263
2626 deg
Mean motion: 15
50742714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2128
Checksum: 308
Coasting Arc #5 (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 = 4713017
96 A = 6790210
40 meter
Y = 1742485
53 meter E =
0009657
Z = 4561092
56 I = 51
48517
XDOT = -4854
597177 Wp = 111
42164
YDOT = 5079
053553 meter/sec RA = 334
03632 deg
ZDOT = 3067
234475 TA = 307
78171
MA = 307
86913
Ha = 226
604 n
mi
Hp = 219
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15462657
34 X = 4671026
26
Y = 5716816
03 feet Y = 1794954
35 meter
Z = 14964214
45 Z = 4583886
12
XDOT = -15927
156092 XDOT = -4925
931268
YDOT = 16663
561524 feet/sec YDOT = 5024
367267 meter/sec
ZDOT = 10063
105234 ZDOT = 3043
478400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9590602
47 X = -2923215
63
Y = 13301399
11 feet Y = 4054266
45 meter
Z = 15059767
52 Z = 4590217
14
XDOT = -10855
269678 XDOT = -3308
686198
YDOT = -19138
265662 feet/sec YDOT = -5833
343374 meter/sec
ZDOT = 9962
302331 ZDOT = 3036
509750
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
55378103
00016717 00000-0 10270-3 0 9044
2 25544 51
6476 334
3101 0001178 96
7662 263
3623 15
50766588 21446
Satellite: ISS
Catalog Number: 25544
Epoch time: 13340
55378103 = yrday
fracday
Element set: 904
Inclination: 51
6476 deg
RA of node: 334
3101 deg
Eccentricity:
0001178
Arg of perigee: 96
7662 deg
Mean anomaly: 263
3623 deg
Mean motion: 15
50766588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2144
Checksum: 304
Coasting Arc #6 (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 = -4374326
95 A = 6789066
92 meter
Y = -1883644
48 meter E =
0012941
Z = -4850414
00 I = 51
45403
XDOT = 4983
389876 Wp = 74
69781
YDOT = -5264
621656 meter/sec RA = 329
06164 deg
ZDOT = -2451
892677 TA = 171
13003
MA = 171
10714
Ha = 226
717 n
mi
Hp = 219
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14351466
36 X = -4329376
53
Y = -6179935
97 feet Y = -1932309
38 meter
Z = -15913431
75 Z = -4871554
99
XDOT = 16349
704316 XDOT = 5053
800283
YDOT = -17272
380760 feet/sec YDOT = -5208
500387 meter/sec
ZDOT = -8044
267314 ZDOT = -2427
513119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9531235
68 X = 2905120
64
Y = -12267219
74 feet Y = -3739048
58 meter
Z = -16002011
50 Z = -4877413
10
XDOT = 11757
748208 XDOT = 3583
761654
YDOT = 19484
694912 feet/sec YDOT = 5938
935009 meter/sec
ZDOT = -7940
816654 ZDOT = -2420
360916
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
52039687
00016717 00000-0 10270-3 0 9054
2 25544 51
6476 329
5158 0001252 99
3102 260
8191 15
50777975 21595
Satellite: ISS
Catalog Number: 25544
Epoch time: 13341
52039687 = yrday
fracday
Element set: 905
Inclination: 51
6476 deg
RA of node: 329
5158 deg
Eccentricity:
0001252
Arg of perigee: 99
3102 deg
Mean anomaly: 260
8191 deg
Mean motion: 15
50777975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2159
Checksum: 323
Coasting Arc #7 (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 = 4032131
67 A = 6788099
41 meter
Y = 2057291
76 meter E =
0006404
Z = 5054494
04 I = 51
42475
XDOT = -5067
408072 Wp = 119
88553
YDOT = 5458
520592 meter/sec RA = 324
08460 deg
ZDOT = 1815
833080 TA = 312
45118
MA = 312
50531
Ha = 226
519 n
mi
Hp = 219
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13228778
45 X = 3984273
54
Y = 6749644
88 feet Y = 2102113
82 meter
Z = 16582985
71 Z = 5073965
62
XDOT = -16625
354567 XDOT = -5136
890663
YDOT = 17908
532127 feet/sec YDOT = 5401
465031 meter/sec
ZDOT = 5957
457611 ZDOT = 1791
047524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9611631
00 X = -2929625
13
Y = 11201079
85 feet Y = 3414089
14 meter
Z = 16664515
00 Z = 5079344
17
XDOT = -12738
438151 XDOT = -3882
675948
YDOT = -19661
224607 feet/sec YDOT = -5992
741260 meter/sec
ZDOT = 5852
274374 ZDOT = 1783
773229
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
55144062
00016717 00000-0 10270-3 0 9063
2 25544 51
6473 324
4023 0001125 99
0964 261
0314 15
50803082 21756
Satellite: ISS
Catalog Number: 25544
Epoch time: 13342
55144062 = yrday
fracday
Element set: 906
Inclination: 51
6473 deg
RA of node: 324
4023 deg
Eccentricity:
0001125
Arg of perigee: 99
0964 deg
Mean anomaly: 261
0314 deg
Mean motion: 15
50803082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2175
Checksum: 273
Coasting Arc #8 (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 = -3701161
56 A = 6787423
99 meter
Y = -2303295
54 meter E =
0015359
Z = -5216002
69 I = 51
39810
XDOT = 5085
369288 Wp = 82
74294
YDOT = -5603
312874 meter/sec RA = 319
10409 deg
ZDOT = -1135
126572 TA = 176
31986
MA = 176
30855
Ha = 226
646 n
mi
Hp = 219
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12142918
51 X = -3649792
53
Y = -7556743
91 feet Y = -2344396
90 meter
Z = -17112869
71 Z = -5233857
95
XDOT = 16684
282441 XDOT = 5153
162968
YDOT = -18383
572420 feet/sec YDOT = -5546
065940 meter/sec
ZDOT = -3724
168544 ZDOT = -1110
257763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9971368
21 X = 3039273
03
Y = -10127427
28 feet Y = -3086839
84 meter
Z = -17187559
19 Z = -5238768
04
XDOT = 13619
019418 XDOT = 4151
077119
YDOT = 19544
964875 feet/sec YDOT = 5957
305294 meter/sec
ZDOT = -3618
619168 ZDOT = -1102
955123
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
51803181
00016717 00000-0 10270-3 0 9075
2 25544 51
6473 319
6077 0001209 101
8837 258
2450 15
50815052 21901
Satellite: ISS
Catalog Number: 25544
Epoch time: 13343
51803181 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 319
6077 deg
Eccentricity:
0001209
Arg of perigee: 101
8837 deg
Mean anomaly: 258
2450 deg
Mean motion: 15
50815052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 290
Coasting Arc #9 (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 = 3380381
22 A = 6786990
81 meter
Y = 2581202
63 meter E =
0003746
Z = 5285948
27 I = 51
37403
XDOT = -5069
712748 Wp = 105
85508
YDOT = 5733
670283 meter/sec RA = 314
12198 deg
ZDOT = 441
000833 TA = 339
91487
MA = 339
92961
Ha = 226
458 n
mi
Hp = 219
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11090489
58 X = 3325588
56
Y = 8468512
55 feet Y = 2618697
67 meter
Z = 17342349
98 Z = 5302236
95
XDOT = -16632
915840 XDOT = -5135
593400
YDOT = 18811
254210 feet/sec YDOT = 5676
609151 meter/sec
ZDOT = 1446
853126 ZDOT = 416
212656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10480291
56 X = -3194392
87
Y = 9083672
07 feet Y = 2768703
25 meter
Z = 17410403
70 Z = 5306691
05
XDOT = -14473
714068 XDOT = -4411
588048
YDOT = -19278
441771 feet/sec YDOT = -5876
069052 meter/sec
ZDOT = 1341
628604 ZDOT = 408
928398
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
54904931
00016717 00000-0 10270-3 0 9085
2 25544 51
6472 314
4940 0001104 102
0021 258
1254 15
50839811 22062
Satellite: ISS
Catalog Number: 25544
Epoch time: 13344
54904931 = yrday
fracday
Element set: 908
Inclination: 51
6472 deg
RA of node: 314
4940 deg
Eccentricity:
0001104
Arg of perigee: 102
0021 deg
Mean anomaly: 258
1254 deg
Mean motion: 15
50839811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2206
Checksum: 271
Coasting Arc #10 (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 = -3095182
36 A = 6786935
55 meter
Y = -2915504
08 meter E =
0015906
Z = -5303661
41 I = 51
35328
XDOT = 4992
215631 Wp = 92
93681
YDOT = -5792
120168 meter/sec RA = 309
13705 deg
ZDOT = 270
499518 TA = 179
65815
MA = 179
65706
Ha = 226
552 n
mi
Hp = 219
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10154797
77 X = -3036586
54
Y = -9565302
12 feet Y = -2949788
55 meter
Z = -17400463
96 Z = -5318555
44
XDOT = 16378
660206 XDOT = 5055
299343
YDOT = -19003
018923 feet/sec YDOT = -5735
941321 meter/sec
ZDOT = 887
465611 ZDOT = 294
904452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11231186
57 X = 3423265
67
Y = -8143049
47 feet Y = -2482001
48 meter
Z = -17462596
08 Z = -5322599
28
XDOT = 15121
999264 XDOT = 4609
185376
YDOT = 18730
797342 feet/sec YDOT = 5709
147030 meter/sec
ZDOT = 991
081964 ZDOT = 302
081783
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
51561536
00016717 00000-0 10270-3 0 9094
2 25544 51
6474 309
6992 0001128 104
9733 255
1543 15
50854904 22219
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
51561536 = yrday
fracday
Element set: 909
Inclination: 51
6474 deg
RA of node: 309
6992 deg
Eccentricity:
0001128
Arg of perigee: 104
9733 deg
Mean anomaly: 255
1543 deg
Mean motion: 15
50854904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2221
Checksum: 307
Coasting Arc #11 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2013/345/16:42:38
621
Vector Time (MET): N/A
Weight (LBS) : 901645
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1775189
42 A = 6789836
04 meter
Y = -4231345
53 meter E =
0011413
Z = -5015127
48 I = 51
35713
XDOT = 5699
057613 Wp = 106
88494
YDOT = -4716
137899 meter/sec RA = 308
14671 deg
ZDOT = 1962
275822 TA = 182
27645
MA = 182
28165
Ha = 226
488 n
mi
Hp = 221
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5824112
28 X = -1703379
30
Y = -13882367
22 feet Y = -4250795
10 meter
Z = -16453830
32 Z = -5023577
02
XDOT = 18697
695582 XDOT = 5741
838656
YDOT = -15472
893369 feet/sec YDOT = -4652
168285 meter/sec
ZDOT = 6437
912801 ZDOT = 1990
065290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1883566
47 X = 574111
06
Y = -14897849
93 feet Y = -4540864
66 meter
Z = -16488637
92 Z = -5025736
84
XDOT = 22778
602317 XDOT = 6942
917986
YDOT = -4373
926301 feet/sec YDOT = -1333
172737 meter/sec
ZDOT = 6555
576358 ZDOT = 1998
139674
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
70892758
00016717 00000-0 10270-3 0 9100
2 25544 51
6508 308
7409 0001450 265
9759 94
1226 15
50303085 22245
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
70892758 = yrday
fracday
Element set: 910
Inclination: 51
6508 deg
RA of node: 308
7409 deg
Eccentricity:
0001450
Arg of perigee: 265
9759 deg
Mean anomaly: 94
1226 deg
Mean motion: 15
50303085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 309
Coasting Arc #12 (Orbit 2239)
---------------------------------------
Vector Time (GMT): 2013/346/16:42:38
621
Vector Time (MET): N/A
Weight (LBS) : 901645
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1728510
32 A = 6790379
08 meter
Y = 4434054
71 meter E =
0005848
Z = 4841044
98 I = 51
34101
XDOT = -5460
737883 Wp = 51
56932
YDOT = 4793
873475 meter/sec RA = 303
16772 deg
ZDOT = -2435
503833 TA = 62
47525
MA = 62
41584
Ha = 226
321 n
mi
Hp = 221
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5670965
62 X = 1655282
55
Y = 14547423
59 feet Y = 4452974
31 meter
Z = 15882693
52 Z = 4849264
39
XDOT = -17915
806702 XDOT = -5502
107043
YDOT = 15727
931349 feet/sec YDOT = 4732
576850 meter/sec
ZDOT = -7990
498141 ZDOT = -2462
132102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2076846
37 X = -633022
77
Y = 15440176
26 feet Y = 4706165
72 meter
Z = 15916500
99 Z = 4851349
50
XDOT = -22089
881006 XDOT = -6732
995731
YDOT = 5400
782181 feet/sec YDOT = 1646
158409 meter/sec
ZDOT = -8103
288257 ZDOT = -2469
882261
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
74029884
00016717 00000-0 10270-3 0 9118
2 25544 51
6507 303
6292 0001531 272
8763 87
2212 15
50354468 22407
Satellite: ISS
Catalog Number: 25544
Epoch time: 13346
74029884 = yrday
fracday
Element set: 911
Inclination: 51
6507 deg
RA of node: 303
6292 deg
Eccentricity:
0001531
Arg of perigee: 272
8763 deg
Mean anomaly: 87
2212 deg
Mean motion: 15
50354468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2240
Checksum: 299
Coasting Arc #13 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2013/347/15:07:36
231
Vector Time (MET): N/A
Weight (LBS) : 901270
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2376868
18 A = 6791743
65 meter
Y = -3971859
53 meter E =
0008588
Z = -4978138
05 I = 51
32372
XDOT = 4884
356154 Wp = 111
24639
YDOT = -5517
769437 meter/sec RA = 298
51991 deg
ZDOT = 2070
166076 TA = 179
02385
MA = 179
02218
Ha = 226
467 n
mi
Hp = 223
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7798123
96 X = -2308094
62
Y = -13031035
19 feet Y = -3998054
30 meter
Z = -16332473
91 Z = -4989518
00
XDOT = 16024
790531 XDOT = 4935
637647
YDOT = -18102
918099 feet/sec YDOT = -5462
862866 meter/sec
ZDOT = 6791
883453 ZDOT = 2094
018267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5397439
86 X = 1645139
67
Y = -14140118
00 feet Y = -4309907
97 meter
Z = -16379652
78 Z = -4992518
17
XDOT = 23085
994958 XDOT = 7036
611263
YDOT = 826
735608 feet/sec YDOT = 251
989013 meter/sec
ZDOT = 6893
121076 ZDOT = 2101
023304
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
64274101
00016717 00000-0 10270-3 0 9123
2 25544 51
6504 299
1551 0004111 272
9133 87
1547 15
49698062 22544
Satellite: ISS
Catalog Number: 25544
Epoch time: 13347
64274101 = yrday
fracday
Element set: 912
Inclination: 51
6504 deg
RA of node: 299
1551 deg
Eccentricity:
0004111
Arg of perigee: 272
9133 deg
Mean anomaly: 87
1547 deg
Mean motion: 15
49698062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 301
Coasting Arc #14 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2013/348/15:07:36
231
Vector Time (MET): N/A
Weight (LBS) : 901270
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2524201
82 A = 6791997
17 meter
Y = 3992126
95 meter E =
0004367
Z = 4880871
39 I = 51
31099
XDOT = -4529
886758 Wp = 22
45168
YDOT = 5720
915626 meter/sec RA = 293
54487 deg
ZDOT = -2331
868555 TA = 90
52617
MA = 90
47612
Ha = 226
337 n
mi
Hp = 223
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8281502
03 X = 2455663
20
Y = 13097529
37 feet Y = 4019970
55 meter
Z = 16013357
57 Z = 4892967
70
XDOT = -14861
833196 XDOT = -4582
194944
YDOT = 18769
408222 feet/sec YDOT = 5669
967272 meter/sec
ZDOT = -7650
487384 ZDOT = -2354
001111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4895766
83 X = -1492229
73
Y = 14647526
46 feet Y = 4464566
07 meter
Z = 16063549
04 Z = 4896169
75
XDOT = -22836
836384 XDOT = -6960
667730
YDOT = 876
963288 feet/sec YDOT = 267
298410 meter/sec
ZDOT = -7744
526773 ZDOT = -2360
531760
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
67451245
00016717 00000-0 10270-3 0 9134
2 25544 51
6503 294
0464 0004182 277
4284 82
6392 15
49741919 22701
Satellite: ISS
Catalog Number: 25544
Epoch time: 13348
67451245 = yrday
fracday
Element set: 913
Inclination: 51
6503 deg
RA of node: 294
0464 deg
Eccentricity:
0004182
Arg of perigee: 277
4284 deg
Mean anomaly: 82
6392 deg
Mean motion: 15
49741919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 319
Coasting Arc #15 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2013/349/15:07:36
231
Vector Time (MET): N/A
Weight (LBS) : 901270
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2694379
34 A = 6792424
66 meter
Y = -4009478
28 meter E =
0007180
Z = -4782010
63 I = 51
30163
XDOT = 4161
643084 Wp = 112
70974
YDOT = -5881
227304 meter/sec RA = 288
56847 deg
ZDOT = 2586
679368 TA = 182
94406
MA = 182
94828
Ha = 226
440 n
mi
Hp = 223
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8839827
22 X = -2626114
34
Y = -13154456
31 feet Y = -4039226
39 meter
Z = -15689011
27 Z = -4794934
35
XDOT = 13653
684660 XDOT = 4214
533497
YDOT = -19295
365172 feet/sec YDOT = -5834
393685 meter/sec
ZDOT = 8486
480866 ZDOT = 2607
024290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4322327
76 X = 1317445
50
Y = -15192521
48 feet Y = -4630680
55 meter
Z = -15742684
48 Z = -4798370
23
XDOT = 22396
167269 XDOT = 6826
351784
YDOT = -2510
329814 feet/sec YDOT = -765
148527 meter/sec
ZDOT = 8573
028601 ZDOT = 2613
059118
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
64178769
00016717 00000-0 10270-3 0 9140
2 25544 51
6510 289
2564 0004185 280
7519 79
3160 15
49737968 22858
Satellite: ISS
Catalog Number: 25544
Epoch time: 13349
64178769 = yrday
fracday
Element set: 914
Inclination: 51
6510 deg
RA of node: 289
2564 deg
Eccentricity:
0004185
Arg of perigee: 280
7519 deg
Mean anomaly: 79
3160 deg
Mean motion: 15
49737968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 352
Coasting Arc #16 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2013/350/15:07:36
231
Vector Time (MET): N/A
Weight (LBS) : 901270
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2865454
88 A = 6792761
52 meter
Y = 4029112
88 meter E =
0005645
Z = 4657433
63 I = 51
29431
XDOT = -3803
100663 Wp = 34
36825
YDOT = 6007
824784 meter/sec RA = 283
59191 deg
ZDOT = -2851
221167 TA = 84
14942
MA = 84
08507
Ha = 226
378 n
mi
Hp = 223
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9401098
69 X = 2797562
85
Y = 13218874
27 feet Y = 4060776
12 meter
Z = 15280294
06 Z = 4671189
32
XDOT = -12477
364381 XDOT = -3856
148328
YDOT = 19710
711233 feet/sec YDOT = 5964
999785 meter/sec
ZDOT = -9354
400155 ZDOT = -2869
824572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3734986
93 X = -1138424
02
Y = 15729544
56 feet Y = 4794365
18 meter
Z = 15337469
82 Z = 4674860
80
XDOT = -21843
751162 XDOT = -6657
975354
YDOT = 4031
686281 feet/sec YDOT = 1228
857979 meter/sec
ZDOT = -9433
643317 ZDOT = -2875
374483
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
67353444
00016717 00000-0 10270-3 0 9151
2 25544 51
6510 284
1477 0004259 285
4405 74
6274 15
49786428 23011
Satellite: ISS
Catalog Number: 25544
Epoch time: 13350
67353444 = yrday
fracday
Element set: 915
Inclination: 51
6510 deg
RA of node: 284
1477 deg
Eccentricity:
0004259
Arg of perigee: 285
4405 deg
Mean anomaly: 74
6274 deg
Mean motion: 15
49786428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 316
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