[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 20th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 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
295/11:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 220
6
297/11:20:09
350 -2
0 2
0 2
0
N/A -0
1 0
0 228
5
000/00:04:14
699 -0
2 0
0 221
7
301/09:00:02
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 221
5
Coasting Arc #1 (Orbit 1383)
---------------------------------------
Vector Time (GMT): 2013/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2775372
25 A = 6797716
66 meter
Y = -5268301
31 meter E =
0014565
Z = 3263322
93 I = 51
43937
XDOT = 6031
790487 Wp = 78
68172
YDOT = -241
365311 meter/sec RA = 216
31507 deg
ZDOT = 4725
072216 TA = 319
24174
MA = 319
35062
Ha = 228
680 n
mi
Hp = 220
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9105552
00 X = -2732107
37
Y = -17284453
10 feet Y = -5299095
03 meter
Z = 10706440
07 Z = 3249945
77
XDOT = 19789
338869 XDOT = 6011
087536
YDOT = -791
880943 feet/sec YDOT = -174
029243 meter/sec
ZDOT = 15502
205432 ZDOT = 4754
324515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15884422
81 X = 4841572
07
Y = 11425109
25 feet Y = 3482373
30 meter
Z = 10650973
95 Z = 3246416
86
XDOT = -16467
354344 XDOT = -5019
249604
YDOT = 8281
841585 feet/sec YDOT = 2524
305315 meter/sec
ZDOT = 15624
982563 ZDOT = 4762
494685
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 13291
55776510
00016717 00000-0 10270-3 0 9009
2 25544 51
6495 217
0472 0002784 34
3586 325
7744 15
49724060 13841
Satellite: ISS
Catalog Number: 25544
Epoch time: 13291
55776510 = yrday
fracday
Element set: 900
Inclination: 51
6495 deg
RA of node: 217
0472 deg
Eccentricity:
0002784
Arg of perigee: 34
3586 deg
Mean anomaly: 325
7744 deg
Mean motion: 15
49724060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1384
Checksum: 314
Coasting Arc #2 (Orbit 1398)
---------------------------------------
Vector Time (GMT): 2013/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2951035
31 A = 6796985
51 meter
Y = 5043440
88 meter E =
0007085
Z = -3480084
65 I = 51
46349
XDOT = -6150
585916 Wp = 70
53423
YDOT = 477
186645 meter/sec RA = 211
34998 deg
ZDOT = -4529
258861 TA = 150
32155
MA = 150
28133
Ha = 228
636 n
mi
Hp = 220
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9681874
36 X = 2911324
84
Y = 16546722
04 feet Y = 5076218
88 meter
Z = -11417600
57 Z = -3465845
35
XDOT = -20179
087652 XDOT = -6133
462324
YDOT = 1565
572982 feet/sec YDOT = 408
502206 meter/sec
ZDOT = -14859
773166 ZDOT = -4559
097049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16256168
64 X = -4954880
20
Y = -10228202
65 feet Y = -3117556
17 meter
Z = -11358483
88 Z = -3462065
89
XDOT = 16384
606200 XDOT = 4994
027970
YDOT = -9419
070177 feet/sec YDOT = -2870
932590 meter/sec
ZDOT = -14985
048081 ZDOT = -4567
442655
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 13292
52502770
00016717 00000-0 10270-3 0 9013
2 25544 51
6502 212
2576 0002822 37
3329 322
8017 15
49767835 13997
Satellite: ISS
Catalog Number: 25544
Epoch time: 13292
52502770 = yrday
fracday
Element set: 901
Inclination: 51
6502 deg
RA of node: 212
2576 deg
Eccentricity:
0002822
Arg of perigee: 37
3329 deg
Mean anomaly: 322
8017 deg
Mean motion: 15
49767835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1399
Checksum: 304
Coasting Arc #3 (Orbit 1414)
---------------------------------------
Vector Time (GMT): 2013/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3109698
62 A = 6796404
40 meter
Y = -4796706
62 meter E =
0013727
Z = 3662999
66 I = 51
48792
XDOT = 6274
835995 Wp = 85
14618
YDOT = -743
155574 meter/sec RA = 206
38652 deg
ZDOT = 4340
923799 TA = 318
44419
MA = 318
54846
Ha = 228
686 n
mi
Hp = 220
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10202423
31 X = -3073623
99
Y = -15737226
44 feet Y = -4831279
27 meter
Z = 12017715
41 Z = 3647980
62
XDOT = 20586
732268 XDOT = 6261
592182
YDOT = -2438
174457 feet/sec YDOT = -673
060094 meter/sec
ZDOT = 14241
875982 ZDOT = 4371
375053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16507658
75 X = 5031534
39
Y = 8985736
05 feet Y = 2738852
35 meter
Z = 11955290
51 Z = 3643972
55
XDOT = -16238
989817 XDOT = -4949
644096
YDOT = 10657
256963 feet/sec YDOT = 3248
331922 meter/sec
ZDOT = 14369
769014 ZDOT = 4379
905596
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 13293
55675707
00016717 00000-0 10270-3 0 9029
2 25544 51
6498 207
1487 0002795 41
1084 319
0276 15
49776584 14150
Satellite: ISS
Catalog Number: 25544
Epoch time: 13293
55675707 = yrday
fracday
Element set: 902
Inclination: 51
6498 deg
RA of node: 207
1487 deg
Eccentricity:
0002795
Arg of perigee: 41
1084 deg
Mean anomaly: 319
0276 deg
Mean motion: 15
49776584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1415
Checksum: 333
Coasting Arc #4 (Orbit 1429)
---------------------------------------
Vector Time (GMT): 2013/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936557
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3216793
15 A = 6795617
44 meter
Y = 4571268
78 meter E =
0008732
Z = -3874572
78 I = 51
51433
XDOT = -6376
402131 Wp = 65
98178
YDOT = 1007
419262 meter/sec RA = 201
42433 deg
ZDOT = -4109
201833 TA = 160
71970
MA = 160
68664
Ha = 228
596 n
mi
Hp = 220
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10553783
30 X = 3184259
23
Y = 14997600
97 feet Y = 4607058
88 meter
Z = -12711852
94 Z = -3859024
78
XDOT = -20919
954499 XDOT = -6367
231514
YDOT = 3305
181306 feet/sec YDOT = 936
165320 meter/sec
ZDOT = -13481
633311 ZDOT = -4140
156369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16608293
03 X = -5062207
72
Y = -7881318
37 feet Y = -2402225
84 meter
Z = -12647173
81 Z = -3854858
58
XDOT = 15983
749881 XDOT = 4871
846964
YDOT = -11860
338999 feet/sec YDOT = -3615
031327 meter/sec
ZDOT = -13611
685952 ZDOT = -4148
841878
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 13294
52398537
00016717 00000-0 10270-3 0 9031
2 25544 51
6503 202
3590 0002791 43
3076 316
8294 15
49822854 14304
Satellite: ISS
Catalog Number: 25544
Epoch time: 13294
52398537 = yrday
fracday
Element set: 903
Inclination: 51
6503 deg
RA of node: 202
3590 deg
Eccentricity:
0002791
Arg of perigee: 43
3076 deg
Mean anomaly: 316
8294 deg
Mean motion: 15
49822854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1430
Checksum: 309
Coasting Arc #5 (Orbit 1444)
---------------------------------------
Vector Time (GMT): 2013/295/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 927096
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3687832
34 A = 6791684
44 meter
Y = 2957803
13 meter E =
0013568
Z = -4888609
13 I = 51
52933
XDOT = -6196
838684 Wp = 97
07542
YDOT = -3807
065344 meter/sec RA = 196
52316 deg
ZDOT = 2375
348631 TA = 196
26509
MA = 196
30868
Ha = 228
568 n
mi
Hp = 220
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12099187
48 X = -3696884
98
Y = 9704078
50 feet Y = 2916512
61 meter
Z = -16038743
87 Z = -4906546
82
XDOT = -20330
835576 XDOT = -6165
345737
YDOT = -12490
371862 feet/sec YDOT = -3876
186145 meter/sec
ZDOT = 7793
138553 ZDOT = 2345
320922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7315389
90 X = 2229730
84
Y = -13587177
26 feet Y = -4141371
63 meter
Z = -16114417
99 Z = -4911674
60
XDOT = 22632
073880 XDOT = 6898
256119
YDOT = 3107
126094 feet/sec YDOT = 947
052033 meter/sec
ZDOT = 7667
573396 ZDOT = 2337
076371
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 13295
49119795
00016717 00000-0 10270-3 0 9046
2 25544 51
6497 197
5688 0002765 45
9320 314
2058 15
49836913 14457
Satellite: ISS
Catalog Number: 25544
Epoch time: 13295
49119795 = yrday
fracday
Element set: 904
Inclination: 51
6497 deg
RA of node: 197
5688 deg
Eccentricity:
0002765
Arg of perigee: 45
9320 deg
Mean anomaly: 314
2058 deg
Mean motion: 15
49836913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1445
Checksum: 347
Coasting Arc #6 (Orbit 1460)
---------------------------------------
Vector Time (GMT): 2013/296/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 927096
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3738331
20 A = 6792062
66 meter
Y = -3085496
88 meter E =
0010227
Z = 4752557
09 I = 51
56030
XDOT = 6287
365017 Wp = 58
53372
YDOT = 3463
602478 meter/sec RA = 191
56276 deg
ZDOT = -2687
429927 TA = 58
10822
MA = 58
00876
Ha = 228
428 n
mi
Hp = 220
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12264866
15 X = 3749468
96
Y = -10123021
25 feet Y = -3043630
03 meter
Z = 15592378
91 Z = 4770745
10
XDOT = 20627
837982 XDOT = 6261
222028
YDOT = 11363
525190 feet/sec YDOT = 3533
765521 meter/sec
ZDOT = -8817
027318 ZDOT = -2656
949481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7066204
57 X = -2153779
15
Y = 14162340
92 feet Y = 4316681
51 meter
Z = 15669129
95 Z = 4775950
81
XDOT = -22473
514340 XDOT = -6849
927171
YDOT = -1564
675576 feet/sec YDOT = -476
913116 meter/sec
ZDOT = -8689
502684 ZDOT = -2648
560418
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 13296
52287276
00016717 00000-0 10270-3 0 9052
2 25544 51
6492 192
4595 0002752 48
1955 311
9431 15
49883287 14611
Satellite: ISS
Catalog Number: 25544
Epoch time: 13296
52287276 = yrday
fracday
Element set: 905
Inclination: 51
6492 deg
RA of node: 192
4595 deg
Eccentricity:
0002752
Arg of perigee: 48
1955 deg
Mean anomaly: 311
9431 deg
Mean motion: 15
49883287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1461
Checksum: 337
Coasting Arc #7 (Orbit 1475)
---------------------------------------
Vector Time (GMT): 2013/297/11:22:16
699
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -473041
93 A = 6790795
85 meter
Y = 4199614
86 meter E =
0015465
Z = -5328839
24 I = 51
58314
XDOT = -7599
363709 Wp = 84
63616
YDOT = -875
299279 meter/sec RA = 186
65264 deg
ZDOT = -13
842723 TA = 185
22343
MA = 185
23958
Ha = 228
519 n
mi
Hp = 221
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1551974
83 X = -494081
27
Y = 13778263
97 feet Y = 4194207
17 meter
Z = -17483068
37 Z = -5331188
53
XDOT = -24932
295634 XDOT = -7588
943867
YDOT = -2871
716795 feet/sec YDOT = -960
221938 meter/sec
ZDOT = -45
415757 ZDOT = -50
735065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4003117
30 X = -1220150
15
Y = -13261241
18 feet Y = -4042026
31 meter
Z = -17493467
28 Z = -5332008
83
XDOT = 23132
008261 XDOT = 7050
636118
YDOT = -6712
707928 feet/sec YDOT = -2046
033376 meter/sec
ZDOT = -200
208077 ZDOT = -61
023422
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 13297
49005254
00016717 00000-0 10270-3 0 9064
2 25544 51
6497 187
6689 0001543 20
8488 339
2725 15
49524532 14761
Satellite: ISS
Catalog Number: 25544
Epoch time: 13297
49005254 = yrday
fracday
Element set: 906
Inclination: 51
6497 deg
RA of node: 187
6689 deg
Eccentricity:
0001543
Arg of perigee: 20
8488 deg
Mean anomaly: 339
2725 deg
Mean motion: 15
49524532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1476
Checksum: 339
Coasting Arc #8 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2013/298/11:22:16
699
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 346047
98 A = 6790659
52 meter
Y = -4204877
95 meter E =
0003371
Z = 5318444
97 I = 51
61363
XDOT = 7651
718734 Wp = 60
16393
YDOT = 381
235204 meter/sec RA = 181
69860 deg
ZDOT = -194
718420 TA = 31
70377
MA = 31
68347
Ha = 228
406 n
mi
Hp = 221
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1135328
02 X = 367206
15
Y = -13795531
33 feet Y = -4200889
70 meter
Z = 17448966
45 Z = 5320177
63
XDOT = 25104
064089 XDOT = 7647
832885
YDOT = 1250
771668 feet/sec YDOT = 466
779856 meter/sec
ZDOT = -638
839959 ZDOT = -157
555923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4618721
00 X = 1407786
16
Y = 13038420
63 feet Y = 3974110
61 meter
Z = 17456777
72 Z = 5320825
85
XDOT = -22532
102828 XDOT = -6867
784942
YDOT = 8635
812877 feet/sec YDOT = 2632
195765 meter/sec
ZDOT = -482
831009 ZDOT = -147
166892
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 13298
52194484
00016717 00000-0 10270-3 0 9074
2 25544 51
6495 182
5607 0001486 19
3324 340
7882 15
49568604 14928
Satellite: ISS
Catalog Number: 25544
Epoch time: 13298
52194484 = yrday
fracday
Element set: 907
Inclination: 51
6495 deg
RA of node: 182
5607 deg
Eccentricity:
0001486
Arg of perigee: 19
3324 deg
Mean anomaly: 340
7882 deg
Mean motion: 15
49568604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 336
Coasting Arc #9 (Orbit 1506)
---------------------------------------
Vector Time (GMT): 2013/299/11:22:16
699
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -221836
37 A = 6790677
68 meter
Y = 4229961
71 meter E =
0015373
Z = -5320958
09 I = 51
64492
XDOT = -7638
077505 Wp = 87
76882
YDOT = 110
765178 meter/sec RA = 176
74626 deg
ZDOT = 408
099341 TA = 186
12263
MA = 186
14144
Ha = 228
451 n
mi
Hp = 221
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -727809
60 X = -243272
09
Y = 13877827
13 feet Y = 4227360
88 meter
Z = -17457211
58 Z = -5322088
04
XDOT = -25059
309401 XDOT = -7640
730887
YDOT = 363
402816 feet/sec YDOT = 25
336520 meter/sec
ZDOT = 1338
908599 ZDOT = 370
987255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5246900
19 X = -1599255
18
Y = -12861155
53 feet Y = -3920080
21 meter
Z = -17462495
40 Z = -5322568
60
XDOT = 21674
739438 XDOT = 6606
460581
YDOT = -10441
666032 feet/sec YDOT = -3182
619807 meter/sec
ZDOT = 1183
030211 ZDOT = 360
587608
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 13299
48932936
00016717 00000-0 10270-3 0 9083
2 25544 51
6499 177
7716 0001560 22
6620 337
4599 15
49579035 15073
Satellite: ISS
Catalog Number: 25544
Epoch time: 13299
48932936 = yrday
fracday
Element set: 908
Inclination: 51
6499 deg
RA of node: 177
7716 deg
Eccentricity:
0001560
Arg of perigee: 22
6620 deg
Mean anomaly: 337
4599 deg
Mean motion: 15
49579035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1507
Checksum: 350
Coasting Arc #10 (Orbit 1522)
---------------------------------------
Vector Time (GMT): 2013/300/11:22:16
699
Vector Time (MET): N/A
Weight (LBS) : 926908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 116023
75 A = 6790622
54 meter
Y = -4245895
17 meter E =
0004120
Z = 5295684
34 I = 51
67597
XDOT = 7614
502808 Wp = 51
79274
YDOT = -589
429726 meter/sec RA = 171
79599 deg
ZDOT = -636
585316 TA = 44
30159
MA = 44
26863
Ha = 228
372 n
mi
Hp = 221
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 380655
35 X = 137768
29
Y = -13930102
28 feet Y = -4244475
83 meter
Z = 17374292
45 Z = 5296301
05
XDOT = 24981
964592 XDOT = 7623
620413
YDOT = -1933
824559 feet/sec YDOT = -504
228568 meter/sec
ZDOT = -2088
534501 ZDOT = -599
572037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5802308
95 X = 1768543
77
Y = 12665585
93 feet Y = 3860470
59 meter
Z = 17377423
00 Z = 5296638
53
XDOT = -20752
084935 XDOT = -6325
235488
YDOT = 12171
685545 feet/sec YDOT = 3709
929754 meter/sec
ZDOT = -1932
993038 ZDOT = -589
176278
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 13300
52118742
00016717 00000-0 10270-3 0 9093
2 25544 51
6500 172
6632 0001522 22
6079 337
5138 15
49618231 15233
Satellite: ISS
Catalog Number: 25544
Epoch time: 13300
52118742 = yrday
fracday
Element set: 909
Inclination: 51
6500 deg
RA of node: 172
6632 deg
Eccentricity:
0001522
Arg of perigee: 22
6079 deg
Mean anomaly: 337
5138 deg
Mean motion: 15
49618231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1523
Checksum: 280
Coasting Arc #11 (Orbit 1536)
---------------------------------------
Vector Time (GMT): 2013/301/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1279966
56 A = 6790474
18 meter
Y = -4018077
12 meter E =
0003206
Z = 5319584
00 I = 51
70185
XDOT = 7410
266112 Wp = 79
41869
YDOT = -1928
313785 meter/sec RA = 167
34590 deg
ZDOT = 326
895164 TA = 7
46818
MA = 7
46340
Ha = 228
392 n
mi
Hp = 221
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4199365
34 X = -1260781
89
Y = -13182667
72 feet Y = -4032282
89 meter
Z = 17452703
42 Z = 5313412
83
XDOT = 24311
896693 XDOT = 7429
690197
YDOT = -6326
488795 feet/sec YDOT = -1845
338844 meter/sec
ZDOT = 1072
490694 ZDOT = 362
941417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2207469
31 X = 672836
64
Y = 13690537
98 feet Y = 4172875
98 meter
Z = 17427291
91 Z = 5311838
58
XDOT = -23994
220561 XDOT = -7313
438427
YDOT = 2312
263487 feet/sec YDOT = 704
777911 meter/sec
ZDOT = 1224
154602 ZDOT = 373
122323
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 13301
42405000
00016717 00000-0 10270-3 0 9101
2 25544 51
6489 168
1931 0001504 25
6343 334
4882 15
49645170 15377
Satellite: ISS
Catalog Number: 25544
Epoch time: 13301
42405000 = yrday
fracday
Element set: 910
Inclination: 51
6489 deg
RA of node: 168
1931 deg
Eccentricity:
0001504
Arg of perigee: 25
6343 deg
Mean anomaly: 334
4882 deg
Mean motion: 15
49645170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1537
Checksum: 282
Coasting Arc #12 (Orbit 1551)
---------------------------------------
Vector Time (GMT): 2013/302/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1365419
86 A = 6790436
38 meter
Y = 3985444
81 meter E =
0015770
Z = -5339187
94 I = 51
73229
XDOT = -7270
635951 Wp = 84
43942
YDOT = 2376
306764 meter/sec RA = 162
39878 deg
ZDOT = -84
287749 TA = 184
74896
MA = 184
76394
Ha = 228
427 n
mi
Hp = 221
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4479723
95 X = 1346689
02
Y = 13075606
34 feet Y = 4000608
64 meter
Z = -17517020
79 Z = -5332600
56
XDOT = -23853
792490 XDOT = -7296
258508
YDOT = 7796
282034 feet/sec YDOT = 2294
858614 meter/sec
ZDOT = -276
534611 ZDOT = -119
670857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2735506
80 X = -833782
47
Y = -13583349
54 feet Y = -4140204
94 meter
Z = -17489855
43 Z = -5330907
94
XDOT = 23710
376041 XDOT = 7226
922617
YDOT = -4221
713675 feet/sec YDOT = -1286
778328 meter/sec
ZDOT = -425
484034 ZDOT = -129
687534
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 13302
39138833
00016717 00000-0 10270-3 0 9116
2 25544 51
6496 163
4037 0001626 31
6961 328
4287 15
49648977 15525
Satellite: ISS
Catalog Number: 25544
Epoch time: 13302
39138833 = yrday
fracday
Element set: 911
Inclination: 51
6496 deg
RA of node: 163
4037 deg
Eccentricity:
0001626
Arg of perigee: 31
6961 deg
Mean anomaly: 328
4287 deg
Mean motion: 15
49648977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1552
Checksum: 325
Coasting Arc #13 (Orbit 1567)
---------------------------------------
Vector Time (GMT): 2013/303/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1431372
61 A = 6790277
24 meter
Y = -3953057
36 meter E =
0003561
Z = 5329481
24 I = 51
76106
XDOT = 7127
105757 Wp = 63
68987
YDOT = -2813
148868 meter/sec RA = 157
45374 deg
ZDOT = -170
807665 TA = 27
94566
MA = 27
92655
Ha = 228
356 n
mi
Hp = 221
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4696104
37 X = -1412951
95
Y = -12969348
29 feet Y = -3968960
41 meter
Z = 17485174
66 Z = 5322572
72
XDOT = 23382
892903 XDOT = 7158
863054
YDOT = -9229
491038 feet/sec YDOT = -2733
271485 meter/sec
ZDOT = -560
392603 ZDOT = -136
106772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3196226
18 X = 974209
74
Y = 13455037
19 feet Y = 4101095
33 meter
Z = 17456655
95 Z = 5320788
73
XDOT = -23351
640247 XDOT = -7117
579947
YDOT = 6091
531688 feet/sec YDOT = 1856
698858 meter/sec
ZDOT = -414
240038 ZDOT = -126
260364
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 13303
42319577
00016717 00000-0 10270-3 0 9128
2 25544 51
6493 158
2951 0001547 29
6307 330
4931 15
49698544 15683
Satellite: ISS
Catalog Number: 25544
Epoch time: 13303
42319577 = yrday
fracday
Element set: 912
Inclination: 51
6493 deg
RA of node: 158
2951 deg
Eccentricity:
0001547
Arg of perigee: 29
6307 deg
Mean anomaly: 330
4931 deg
Mean motion: 15
49698544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1568
Checksum: 325
Coasting Arc #14 (Orbit 1582)
---------------------------------------
Vector Time (GMT): 2013/304/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1505019
41 A = 6790316
80 meter
Y = 3946833
05 meter E =
0015665
Z = -5330068
75 I = 51
78965
XDOT = -6925
221434 Wp = 88
22544
YDOT = 3220
884341 meter/sec RA = 152
51009 deg
ZDOT = 431
150195 TA = 185
87870
MA = 185
89710
Ha = 228
358 n
mi
Hp = 221
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4937727
71 X = 1486665
82
Y = 12948927
33 feet Y = 3963560
04 meter
Z = -17487102
21 Z = -5322802
27
XDOT = -22720
542764 XDOT = -6962
817829
YDOT = 10567
205844 feet/sec YDOT = 3143
231932 meter/sec
ZDOT = 1414
534762 ZDOT = 397
415718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3669642
23 X = -1118506
95
Y = -13402936
08 feet Y = -4085214
92 meter
Z = -17457080
17 Z = -5320918
03
XDOT = 22729
009867 XDOT = 6927
802207
YDOT = -7873
597869 feet/sec YDOT = -2399
872631 meter/sec
ZDOT = 1272
376674 ZDOT = 387
820410
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 13304
39050080
00016717 00000-0 10270-3 0 9137
2 25544 51
6497 153
5055 0001644 33
6272 326
4982 15
49704776 15837
Satellite: ISS
Catalog Number: 25544
Epoch time: 13304
39050080 = yrday
fracday
Element set: 913
Inclination: 51
6497 deg
RA of node: 153
5055 deg
Eccentricity:
0001644
Arg of perigee: 33
6272 deg
Mean anomaly: 326
4982 deg
Mean motion: 15
49704776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1583
Checksum: 308
Coasting Arc #15 (Orbit 1598)
---------------------------------------
Vector Time (GMT): 2013/305/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1560896
93 A = 6790263
11 meter
Y = -3945394
45 meter E =
0004434
Z = 5298616
27 I = 51
81648
XDOT = 6722
233995 Wp = 53
53852
YDOT = -3612
720593 meter/sec RA = 147
56807 deg
ZDOT = -706
807610 TA = 43
21666
MA = 43
18188
Ha = 228
311 n
mi
Hp = 221
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5121052
93 X = -1542402
58
Y = -12944207
51 feet Y = -3962745
57 meter
Z = 17383911
64 Z = 5291078
61
XDOT = 22054
573473 XDOT = 6765
566187
YDOT = -11852
757851 feet/sec YDOT = -3537
306065 meter/sec
ZDOT = -2318
922604 ZDOT = -674
045198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4082045
32 X = 1244207
41
Y = 13349042
84 feet Y = 4068788
26 meter
Z = 17352752
99 Z = 5289119
11
XDOT = -22043
530826 XDOT = -6718
868196
YDOT = 9588
347495 feet/sec YDOT = 2922
528317 meter/sec
ZDOT = -2180
783427 ZDOT = -664
702789
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 13305
42227304
00016717 00000-0 10270-3 0 9148
2 25544 51
6493 148
3965 0001595 32
4032 327
7216 15
49751846 15992
Satellite: ISS
Catalog Number: 25544
Epoch time: 13305
42227304 = yrday
fracday
Element set: 914
Inclination: 51
6493 deg
RA of node: 148
3965 deg
Eccentricity:
0001595
Arg of perigee: 32
4032 deg
Mean anomaly: 327
7216 deg
Mean motion: 15
49751846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 314
Coasting Arc #16 (Orbit 1613)
---------------------------------------
Vector Time (GMT): 2013/306/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893839
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1634377
40 A = 6790401
42 meter
Y = 3967852
05 meter E =
0015212
Z = -5275770
02 I = 51
84223
XDOT = -6466
541481 Wp = 92
05079
YDOT = 3967
615254 meter/sec RA = 142
62724 deg
ZDOT = 982
656022 TA = 187
33992
MA = 187
36222
Ha = 228
284 n
mi
Hp = 221
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5362130
58 X = 1615515
55
Y = 13017887
30 feet Y = 3986022
92 meter
Z = -17308956
75 Z = -5267876
18
XDOT = -21215
687273 XDOT = -6515
201234
YDOT = 13017
110413 feet/sec YDOT = 3895
030257 meter/sec
ZDOT = 3223
937081 ZDOT = 951
122789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4545929
14 X = -1385599
20
Y = -13367180
08 feet Y = -4074316
49 meter
Z = -17276308
72 Z = -5265818
90
XDOT = 21118
986703 XDOT = 6437
067147
YDOT = -11168
829573 feet/sec YDOT = -3404
259254 meter/sec
ZDOT = 3090
899609 ZDOT = 942
106201
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 13306
38954460
00016717 00000-0 10270-3 0 9155
2 25544 51
6491 143
6064 0001659 34
4871 325
6387 15
49759059 16140
Satellite: ISS
Catalog Number: 25544
Epoch time: 13306
38954460 = yrday
fracday
Element set: 915
Inclination: 51
6491 deg
RA of node: 143
6064 deg
Eccentricity:
0001659
Arg of perigee: 34
4871 deg
Mean anomaly: 325
6387 deg
Mean motion: 15
49759059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1614
Checksum: 329
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