[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 28th 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) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
243/07:34:29
793 0
4 1
3 1
4
N/A 1
2 -0
2 227
5
000/00:02:59
586 -0
4 -0
0 220
5
Coasting Arc #1 (Orbit 560)
---------------------------------------
Vector Time (GMT): 2013/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2358027
33 A = 6799083
24 meter
Y = 6249289
33 meter E =
0012820
Z = -1232441
12 I = 51
97623
XDOT = -4872
540839 Wp = 23
64450
YDOT = -686
028233 meter/sec RA = 118
96856 deg
ZDOT = 5876
534187 TA = 323
03840
MA = 323
12666
Ha = 227
170 n
mi
Hp = 220
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7736310
13 X = -2421746
15
Y = 20502917
76 feet Y = 6222564
04 meter
Z = -4043442
00 Z = -1244051
26
XDOT = -15986
026374 XDOT = -4893
053898
YDOT = -2250
748795 feet/sec YDOT = -740
630462 meter/sec
ZDOT = 19279
967805 ZDOT = 5852
814116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15896649
93 X = 4845298
90
Y = -15070295
29 feet Y = -4593426
00 meter
Z = -4092954
32 Z = -1247532
48
XDOT = 12403
576939 XDOT = 3780
610251
YDOT = 7903
079561 feet/sec YDOT = 2408
858650 meter/sec
ZDOT = 19180
538786 ZDOT = 5846
228222
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 13238
50242642
00016717 00000-0 10270-3 0 9009
2 25544 51
6495 119
9224 0004665 354
4570 5
6529 15
50553341 5610
Satellite: ISS
Catalog Number: 25544
Epoch time: 13238
50242642 = yrday
fracday
Element set: 900
Inclination: 51
6495 deg
RA of node: 119
9224 deg
Eccentricity:
0004665
Arg of perigee: 354
4570 deg
Mean anomaly: 5
6529 deg
Mean motion: 15
50553341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 561
Checksum: 293
Coasting Arc #2 (Orbit 576)
---------------------------------------
Vector Time (GMT): 2013/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2247135
20 A = 6799616
73 meter
Y = -6376072
09 meter E =
0010931
Z = 697213
63 I = 51
99164
XDOT = 4679
951421 Wp = 108
76049
YDOT = 987
085905 meter/sec RA = 114
03711 deg
ZDOT = -5983
440911 TA = 63
75839
MA = 63
64608
Ha = 227
278 n
mi
Hp = 220
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7372490
81 X = 2314879
96
Y = -20918871
69 feet Y = -6350564
39 meter
Z = 2287446
28 Z = 708294
77
XDOT = 15354
171329 XDOT = 4697
631605
YDOT = 3238
470817 feet/sec YDOT = 1039
518707 meter/sec
ZDOT = -19630
711650 ZDOT = -5960
663317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15490439
56 X = -4721485
98
Y = 15867588
25 feet Y = 4836440
90 meter
Z = 2334769
70 Z = 711637
80
XDOT = -11511
990334 XDOT = -3508
854654
YDOT = -8329
324996 feet/sec YDOT = -2538
778259 meter/sec
ZDOT = -19535
270649 ZDOT = -5954
350494
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 13239
53363866
00016717 00000-0 10270-3 0 9016
2 25544 51
6494 114
8098 0004532 358
3882 1
7254 15
50522327 5773
Satellite: ISS
Catalog Number: 25544
Epoch time: 13239
53363866 = yrday
fracday
Element set: 901
Inclination: 51
6494 deg
RA of node: 114
8098 deg
Eccentricity:
0004532
Arg of perigee: 358
3882 deg
Mean anomaly: 1
7254 deg
Mean motion: 15
50522327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 577
Checksum: 313
Coasting Arc #3 (Orbit 591)
---------------------------------------
Vector Time (GMT): 2013/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2083674
85 A = 6799625
62 meter
Y = 6460624
58 meter E =
0015464
Z = -186553
69 I = 52
00389
XDOT = -4542
196084 Wp = 31
86090
YDOT = -1297
530297 meter/sec RA = 109
10562 deg
ZDOT = 6037
936159 TA = 326
14139
MA = 326
24003
Ha = 227
286 n
mi
Hp = 220
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6836203
58 X = -2154857
88
Y = 21196274
86 feet Y = 6436925
59 meter
Z = -612052
79 Z = -196849
04
XDOT = -14902
218122 XDOT = -4556
679722
YDOT = -4256
989162 feet/sec YDOT = -1348
404803 meter/sec
ZDOT = 19809
501835 ZDOT = 6015
835569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14847233
32 X = 4525436
72
Y = -16598781
46 feet Y = -5059308
59 meter
Z = -656104
07 Z = -199980
52
XDOT = 10794
090956 XDOT = 3290
038923
YDOT = 8904
762125 feet/sec YDOT = 2714
171496 meter/sec
ZDOT = 19716
937391 ZDOT = 6009
722517
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 13240
50038785
00016717 00000-0 10270-3 0 9025
2 25544 51
6493 110
0161 0004739
3297 359
7857 15
50587988 5920
Satellite: ISS
Catalog Number: 25544
Epoch time: 13240
50038785 = yrday
fracday
Element set: 902
Inclination: 51
6493 deg
RA of node: 110
0161 deg
Eccentricity:
0004739
Arg of perigee:
3297 deg
Mean anomaly: 359
7857 deg
Mean motion: 15
50587988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 592
Checksum: 319
Coasting Arc #4 (Orbit 607)
---------------------------------------
Vector Time (GMT): 2013/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1939760
34 A = 6799680
77 meter
Y = -6504430
93 meter E =
0008808
Z = -368454
63 I = 52
01280
XDOT = 4432
335093 Wp = 115
21549
YDOT = 1656
396180 meter/sec RA = 104
17610 deg
ZDOT = -6022
358944 TA = 68
72811
MA = 68
63407
Ha = 227
369 n
mi
Hp = 220
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6364043
13 X = 2014139
98
Y = -21339996
49 feet Y = -6482323
43 meter
Z = -1208840
66 Z = -358850
67
XDOT = 14541
781802 XDOT = 4442
738246
YDOT = 5434
370668 feet/sec YDOT = 1706
019349 meter/sec
ZDOT = -19758
395484 ZDOT = -6000
802012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14191298
42 X = -4325507
76
Y = 17163955
90 feet Y = 5231573
76 meter
Z = -1167671
94 Z = -355906
41
XDOT = -10131
446376 XDOT = -3088
064856
YDOT = -9688
005842 feet/sec YDOT = -2952
904181 meter/sec
ZDOT = -19668
155755 ZDOT = -5994
853874
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 13241
53157866
00016717 00000-0 10270-3 0 9032
2 25544 51
6492 104
9036 0004612 3
7350 356
3834 15
50554262 6084
Satellite: ISS
Catalog Number: 25544
Epoch time: 13241
53157866 = yrday
fracday
Element set: 903
Inclination: 51
6492 deg
RA of node: 104
9036 deg
Eccentricity:
0004612
Arg of perigee: 3
7350 deg
Mean anomaly: 356
3834 deg
Mean motion: 15
50554262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 608
Checksum: 290
Coasting Arc #5 (Orbit 623)
---------------------------------------
Vector Time (GMT): 2013/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1760001
60 A = 6799215
50 meter
Y = 6497057
13 meter E =
0016938
Z = 887951
58 I = 52
01801
XDOT = -4386
639861 Wp = 42
42461
YDOT = -2010
066359 meter/sec RA = 99
24544 deg
ZDOT = 5958
914688 TA = 327
12634
MA = 327
23158
Ha = 227
377 n
mi
Hp = 219
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5774283
45 X = -1836835
69
Y = 21315804
24 feet Y = 6476946
11 meter
Z = 2913226
98 Z = 879214
90
XDOT = -14391
863061 XDOT = -4392
783335
YDOT = -6594
705902 feet/sec YDOT = -2059
154701 meter/sec
ZDOT = 19550
245038 ZDOT = 5937
590149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13347862
80 X = 4068428
58
Y = -17599935
56 feet Y = -5364460
36 meter
Z = 2875687
45 Z = 876509
53
XDOT = 9707
998582 XDOT = 2958
997968
YDOT = 10571
590921 feet/sec YDOT = 3222
220913 meter/sec
ZDOT = 19461
024512 ZDOT = 5931
720271
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 13242
56275589
00016717 00000-0 10270-3 0 9040
2 25544 51
6487 99
7898 0004758 6
3555 353
7655 15
50624621 6249
Satellite: ISS
Catalog Number: 25544
Epoch time: 13242
56275589 = yrday
fracday
Element set: 904
Inclination: 51
6487 deg
RA of node: 99
7898 deg
Eccentricity:
0004758
Arg of perigee: 6
3555 deg
Mean anomaly: 353
7655 deg
Mean motion: 15
50624621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 624
Checksum: 343
Coasting Arc #6 (Orbit 635)
---------------------------------------
Vector Time (GMT): 2013/243/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4149093
89 A = 6789508
68 meter
Y = -1801721
62 meter E =
0014621
Z = -5076232
95 I = 51
98678
XDOT = 837
532873 Wp = 59
28943
YDOT = 7357
858083 meter/sec RA = 95
22241 deg
ZDOT = -1923
841337 TA = 192
08186
MA = 192
11696
Ha = 227
488 n
mi
Hp = 220
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13612512
77 X = 4193591
44
Y = -5911160
17 feet Y = -1755075
22 meter
Z = -16654307
59 Z = -5055969
12
XDOT = 2747
811263 XDOT = 764
538839
YDOT = 24139
954339 feet/sec YDOT = 7366
815698 meter/sec
ZDOT = -6311
815411 ZDOT = -1919
950312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6582028
14 X = -2006202
18
Y = -13407191
39 feet Y = -4086511
94 meter
Z = -16569019
42 Z = -5050237
12
XDOT = 22994
874773 XDOT = 7008
837831
YDOT = -3494
747696 feet/sec YDOT = -1065
199098 meter/sec
ZDOT = -6296
483432 ZDOT = -1919
168150
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 13243
33613691
00016717 00000-0 10270-3 0 9057
2 25544 51
6488 95
9549 0004281
5582 359
5572 15
50382334 6365
Satellite: ISS
Catalog Number: 25544
Epoch time: 13243
33613691 = yrday
fracday
Element set: 905
Inclination: 51
6488 deg
RA of node: 95
9549 deg
Eccentricity:
0004281
Arg of perigee:
5582 deg
Mean anomaly: 359
5572 deg
Mean motion: 15
50382334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 636
Checksum: 316
Coasting Arc #7 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2013/244/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4070215
52 A = 6788851
68 meter
Y = 1573280
64 meter E =
0004179
Z = 5196989
04 I = 51
98651
XDOT = -1071
708280 Wp = 66
55335
YDOT = -7456
614043 meter/sec RA = 90
28627 deg
ZDOT = 1418
703379 TA = 9
86481
MA = 9
85660
Ha = 227
609 n
mi
Hp = 220
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13353725
45 X = -4112751
01
Y = 5161681
89 feet Y = 1527527
34 meter
Z = 17050488
97 Z = 5177113
16
XDOT = -3516
103281 XDOT = -995
138726
YDOT = -24463
956833 feet/sec YDOT = -7468
170368 meter/sec
ZDOT = 4654
538645 ZDOT = 1413
683544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6046835
90 X = 1843075
58
Y = 13086089
76 feet Y = 3988640
16 meter
Z = 16966854
38 Z = 5171497
22
XDOT = -23219
365079 XDOT = -7077
262476
YDOT = 4723
417021 feet/sec YDOT = 1439
697508 meter/sec
ZDOT = 4634
489347 ZDOT = 1412
592353
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 13244
36746163
00016717 00000-0 10270-3 0 9063
2 25544 51
6485 90
8431 0004240 2
2234 357
8935 15
50409625 6529
Satellite: ISS
Catalog Number: 25544
Epoch time: 13244
36746163 = yrday
fracday
Element set: 906
Inclination: 51
6485 deg
RA of node: 90
8431 deg
Eccentricity:
0004240
Arg of perigee: 2
2234 deg
Mean anomaly: 357
8935 deg
Mean motion: 15
50409625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 296
Coasting Arc #8 (Orbit 666)
---------------------------------------
Vector Time (GMT): 2013/245/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4044709
74 A = 6788451
37 meter
Y = -1345901
07 meter E =
0016037
Z = -5296759
63 I = 51
98498
XDOT = 1311
753996 Wp = 67
74954
YDOT = 7484
033981 meter/sec RA = 85
34931 deg
ZDOT = -896
274098 TA = 193
67750
MA = 193
72101
Ha = 227
594 n
mi
Hp = 220
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13270045
09 X = 4085189
16
Y = -4415685
94 feet Y = -1300444
58 meter
Z = -17377820
30 Z = -5277012
65
XDOT = 4303
654843 XDOT = 1232
322196
YDOT = 24553
917260 feet/sec YDOT = 7498
258659 meter/sec
ZDOT = -2940
531818 ZDOT = -890
095231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5520850
37 X = -1682755
19
Y = -12961200
56 feet Y = -3950573
93 meter
Z = -17294753
79 Z = -5271440
95
XDOT = 23160
834102 XDOT = 7059
422234
YDOT = -5958
535756 feet/sec YDOT = -1816
161699 meter/sec
ZDOT = -2915
627672 ZDOT = -888
683314
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 13245
33432032
00016717 00000-0 10270-3 0 9079
2 25544 51
6491 86
0505 0004368 6
8319 353
2891 15
50415849 6672
Satellite: ISS
Catalog Number: 25544
Epoch time: 13245
33432032 = yrday
fracday
Element set: 907
Inclination: 51
6491 deg
RA of node: 86
0505 deg
Eccentricity:
0004368
Arg of perigee: 6
8319 deg
Mean anomaly: 353
2891 deg
Mean motion: 15
50415849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 667
Checksum: 305
Coasting Arc #9 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2013/246/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4047657
98 A = 6788122
41 meter
Y = 1088360
51 meter E =
0004768
Z = 5336663
32 I = 51
98041
XDOT = -1549
869448 Wp = 40
69257
YDOT = -7498
644347 meter/sec RA = 80
41172 deg
ZDOT = 357
096610 TA = 45
93700
MA = 45
89774
Ha = 227
704 n
mi
Hp = 220
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13279717
78 X = -4085451
16
Y = 3570736
58 feet Y = 1042886
17 meter
Z = 17508737
93 Z = 5316908
54
XDOT = -5084
873518 XDOT = -1467
637433
YDOT = -24601
851531 feet/sec YDOT = -7515
516155 meter/sec
ZDOT = 1171
576806 ZDOT = 349
767952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4903401
75 X = 1494556
85
Y = 12959922
20 feet Y = 3950184
29 meter
Z = 17425671
75 Z = 5311344
75
XDOT = -23018
127596 XDOT = -7015
925291
YDOT = 7188
417355 feet/sec YDOT = 2191
029610 meter/sec
ZDOT = 1141
854562 ZDOT = 348
037270
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 13246
36562338
00016717 00000-0 10270-3 0 9087
2 25544 51
6487 80
9382 0004351 8
4721 351
6502 15
50447005 6838
Satellite: ISS
Catalog Number: 25544
Epoch time: 13246
36562338 = yrday
fracday
Element set: 908
Inclination: 51
6487 deg
RA of node: 80
9382 deg
Eccentricity:
0004351
Arg of perigee: 8
4721 deg
Mean anomaly: 351
6502 deg
Mean motion: 15
50447005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 683
Checksum: 299
Coasting Arc #10 (Orbit 697)
---------------------------------------
Vector Time (GMT): 2013/247/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4103529
07 A = 6788103
67 meter
Y = -852557
16 meter E =
0016267
Z = -5353202
68 I = 51
97468
XDOT = 1779
257265 Wp = 75
76896
YDOT = 7438
928788 meter/sec RA = 75
47351 deg
ZDOT = 183
518294 TA = 195
95029
MA = 196
00157
Ha = 227
684 n
mi
Hp = 220
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13463021
87 X = 4138761
68
Y = -2797103
55 feet Y = -806472
45 meter
Z = -17563000
93 Z = -5333182
68
XDOT = 5837
458219 XDOT = 1695
049825
YDOT = 24405
934345 feet/sec YDOT = 7458
354761 meter/sec
ZDOT = 602
094139 ZDOT = 191
956369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4379018
82 X = -1334724
94
Y = -13147228
76 feet Y = -4007275
33 meter
Z = -17478853
45 Z = -5327554
53
XDOT = 22589
277366 XDOT = 6885
211741
YDOT = -8351
040683 feet/sec YDOT = -2545
397200 meter/sec
ZDOT = 636
474774 ZDOT = 193
997511
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 13247
33246148
00016717 00000-0 10270-3 0 9094
2 25544 51
6491 76
1452 0004458 12
3678 347
7582 15
50448743 6981
Satellite: ISS
Catalog Number: 25544
Epoch time: 13247
33246148 = yrday
fracday
Element set: 909
Inclination: 51
6491 deg
RA of node: 76
1452 deg
Eccentricity:
0004458
Arg of perigee: 12
3678 deg
Mean anomaly: 347
7582 deg
Mean motion: 15
50448743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 698
Checksum: 329
Coasting Arc #11 (Orbit 713)
---------------------------------------
Vector Time (GMT): 2013/248/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4190801
26 A = 6788158
74 meter
Y = 593764
62 meter E =
0006978
Z = 5304252
10 I = 51
96652
XDOT = -1988
814650 Wp = 33
49293
YDOT = -7365
630134 meter/sec RA = 70
53446 deg
ZDOT = -740
684179 TA = 63
58963
MA = 63
51803
Ha = 227
782 n
mi
Hp = 219
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13749347
97 X = -4222895
80
Y = 1948046
66 feet Y = 546721
59 meter
Z = 17402401
91 Z = 5283815
72
XDOT = -6524
982447 XDOT = -1902
704735
YDOT = -24165
453196 feet/sec YDOT = -7387
388941 meter/sec
ZDOT = -2430
066203 ZDOT = -750
135563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3801725
97 X = 1158766
08
Y = 13467265
64 feet Y = 4104822
57 meter
Z = 17316543
64 Z = 5278082
50
XDOT = -22083
914196 XDOT = -6731
177047
YDOT = 9434
448092 feet/sec YDOT = 2875
619779 meter/sec
ZDOT = -2468
702430 ZDOT = -752
460501
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 13248
36374238
00016717 00000-0 10270-3 0 9102
2 25544 51
6490 71
0326 0004467 14
2491 345
8785 15
50486032 7144
Satellite: ISS
Catalog Number: 25544
Epoch time: 13248
36374238 = yrday
fracday
Element set: 910
Inclination: 51
6490 deg
RA of node: 71
0326 deg
Eccentricity:
0004467
Arg of perigee: 14
2491 deg
Mean anomaly: 345
8785 deg
Mean motion: 15
50486032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 714
Checksum: 300
Coasting Arc #12 (Orbit 728)
---------------------------------------
Vector Time (GMT): 2013/249/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4324479
16 A = 6788547
73 meter
Y = -377399
75 meter E =
0015259
Z = -5231950
27 I = 51
95677
XDOT = 2175
466016 Wp = 82
54788
YDOT = 7222
978275 meter/sec RA = 65
59486 deg
ZDOT = 1282
239525 TA = 199
70808
MA = 199
76711
Ha = 227
762 n
mi
Hp = 219
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14187923
75 X = 4353793
20
Y = -1238188
16 feet Y = -328877
42 meter
Z = -17165191
16 Z = -5210871
19
XDOT = 7137
355695 XDOT = 2088
306662
YDOT = 23697
435287 feet/sec YDOT = 7246
818541 meter/sec
ZDOT = 4206
822589 ZDOT = 1292
595090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3397620
21 X = -1035594
64
Y = -13939787
33 feet Y = -4248847
18 meter
Z = -17076667
83 Z = -5204968
35
XDOT = 21325
149291 XDOT = 6499
905504
YDOT = -10382
475049 feet/sec YDOT = -3164
578395 meter/sec
ZDOT = 4249
264321 ZDOT = 1295
175765
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 13249
33055948
00016717 00000-0 10270-3 0 9115
2 25544 51
6492 66
2393 0004540 17
5134 342
6173 15
50481336 7292
Satellite: ISS
Catalog Number: 25544
Epoch time: 13249
33055948 = yrday
fracday
Element set: 911
Inclination: 51
6492 deg
RA of node: 66
2393 deg
Eccentricity:
0004540
Arg of perigee: 17
5134 deg
Mean anomaly: 342
6173 deg
Mean motion: 15
50481336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 729
Checksum: 301
Coasting Arc #13 (Orbit 744)
---------------------------------------
Vector Time (GMT): 2013/250/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4488104
34 A = 6788998
64 meter
Y = 145414
07 meter E =
0009623
Z = 5088605
80 I = 51
94545
XDOT = -2323
634012 Wp = 39
13550
YDOT = -7069
338754 meter/sec RA = 60
65467 deg
ZDOT = -1838
248491 TA = 68
64769
MA = 68
54501
Ha = 227
845 n
mi
Hp = 219
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14724751
77 X = -4514115
88
Y = 477080
28 feet Y = 95080
42 meter
Z = 16694900
93 Z = 5066739
82
XDOT = -7623
471169 XDOT = -2235
480713
YDOT = -23193
368616 feet/sec YDOT = -7094
830439 meter/sec
ZDOT = -6030
998987 ZDOT = -1849
321492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2976911
07 X = 907362
49
Y = 14534109
88 feet Y = 4429996
69 meter
Z = 16603110
79 Z = 5060628
17
XDOT = -20518
746775 XDOT = -6254
114017
YDOT = 11178
692903 feet/sec YDOT = 3407
265597 meter/sec
ZDOT = -6076
462214 ZDOT = -1852
105683
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 13250
36181776
00016717 00000-0 10270-3 0 9120
2 25544 51
6495 61
1266 0004577 19
6436 340
4891 15
50524885 7454
Satellite: ISS
Catalog Number: 25544
Epoch time: 13250
36181776 = yrday
fracday
Element set: 912
Inclination: 51
6495 deg
RA of node: 61
1266 deg
Eccentricity:
0004577
Arg of perigee: 19
6436 deg
Mean anomaly: 340
4891 deg
Mean motion: 15
50524885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 745
Checksum: 318
Coasting Arc #14 (Orbit 759)
---------------------------------------
Vector Time (GMT): 2013/251/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4685804
55 A = 6789761
65 meter
Y = 25817
54 meter E =
0013198
Z = -4924670
30 I = 51
93178
XDOT = 2437
795137 Wp = 86
55931
YDOT = 6859
081620 meter/sec RA = 55
71375 deg
ZDOT = 2361
736071 TA = 206
48529
MA = 206
55280
Ha = 227
835 n
mi
Hp = 219
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15373374
51 X = 4709090
38
Y = 84703
21 feet Y = 78346
81 meter
Z = -16157054
80 Z = -4901850
47
XDOT = 7998
015542 XDOT = 2349
441494
YDOT = 22503
548622 feet/sec YDOT = 6885
848853 meter/sec
ZDOT = 7748
477923 ZDOT = 2373
363290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2794398
85 X = -851732
77
Y = -15219216
57 feet Y = -4638817
21 meter
Z = -16061289
50 Z = -4895481
04
XDOT = 19524
263382 XDOT = 5950
995479
YDOT = -11790
816513 feet/sec YDOT = -3593
840873 meter/sec
ZDOT = 7796
284493 ZDOT = 2376
307514
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 13251
32861351
00016717 00000-0 10270-3 0 9132
2 25544 51
6494 56
3332 0004606 22
7960 337
3395 15
50514184 7605
Satellite: ISS
Catalog Number: 25544
Epoch time: 13251
32861351 = yrday
fracday
Element set: 913
Inclination: 51
6494 deg
RA of node: 56
3332 deg
Eccentricity:
0004606
Arg of perigee: 22
7960 deg
Mean anomaly: 337
3395 deg
Mean motion: 15
50514184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 760
Checksum: 291
Coasting Arc #15 (Orbit 775)
---------------------------------------
Vector Time (GMT): 2013/252/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4907410
13 A = 6790563
20 meter
Y = -206479
99 meter E =
0012160
Z = 4684601
05 I = 51
91731
XDOT = -2495
761375 Wp = 50
09580
YDOT = -6644
022969 meter/sec RA = 50
77264 deg
ZDOT = -2894
737163 TA = 68
64126
MA = 68
51153
Ha = 227
891 n
mi
Hp = 219
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16100426
93 X = -4927493
14
Y = -677427
80 feet Y = -261469
58 meter
Z = 15369426
03 Z = 4660712
41
XDOT = -8188
193489 XDOT = -2407
219036
YDOT = -21797
975621 feet/sec YDOT = -6671
437385 meter/sec
ZDOT = -9497
169170 ZDOT = -2906
645667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2621737
17 X = 799105
49
Y = 15996242
91 feet Y = 4875654
84 meter
Z = 15269204
93 Z = 4654053
66
XDOT = -18531
081897 XDOT = -5648
273762
YDOT = 12189
114859 feet/sec YDOT = 3715
242209 meter/sec
ZDOT = -9546
174141 ZDOT = -2909
673878
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 13252
35984866
00016717 00000-0 10270-3 0 9144
2 25544 51
6499 51
2207 0004666 24
9102 335
2273 15
50562153 7761
Satellite: ISS
Catalog Number: 25544
Epoch time: 13252
35984866 = yrday
fracday
Element set: 914
Inclination: 51
6499 deg
RA of node: 51
2207 deg
Eccentricity:
0004666
Arg of perigee: 24
9102 deg
Mean anomaly: 335
2273 deg
Mean motion: 15
50562153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 776
Checksum: 309
Coasting Arc #16 (Orbit 790)
---------------------------------------
Vector Time (GMT): 2013/253/07:35:59
586
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5146116
22 A = 6791606
97 meter
Y = 312772
20 meter E =
0010623
Z = -4429577
18 I = 51
89968
XDOT = 2513
986822 Wp = 84
55709
YDOT = 6391
422017 meter/sec RA = 45
83038 deg
ZDOT = 3379
902706 TA = 219
53602
MA = 219
61356
Ha = 227
903 n
mi
Hp = 219
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16883583
41 X = 5163754
09
Y = 1026155
51 feet Y = 370417
58 meter
Z = -14532733
54 Z = -4404534
84
XDOT = 8247
988261 XDOT = 2425
910934
YDOT = 20969
232338 feet/sec YDOT = 6419
042838 meter/sec
ZDOT = 11088
919638 ZDOT = 3391
901032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2727053
52 X = -831205
91
Y = -16784328
56 feet Y = -5115863
35 meter
Z = -14427689
40 Z = -4397559
73
XDOT = 17438
386063 XDOT = 5315
220072
YDOT = -12385
166116 feet/sec YDOT = -3774
998632 meter/sec
ZDOT = 11138
326042 ZDOT = 3394
961777
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 13253
32662259
00016717 00000-0 10270-3 0 9152
2 25544 51
6491 46
4271 0004646 28
6258 331
5147 15
50547344 7912
Satellite: ISS
Catalog Number: 25544
Epoch time: 13253
32662259 = yrday
fracday
Element set: 915
Inclination: 51
6491 deg
RA of node: 46
4271 deg
Eccentricity:
0004646
Arg of perigee: 28
6258 deg
Mean anomaly: 331
5147 deg
Mean motion: 15
50547344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 791
Checksum: 308
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