[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 9th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
166/13:46:01
000 0
0 0
0 0
0
N/A 0
0 0
0 230
1
000/00:00:00
000 0
0 0
0 216
1
170/12:58:26
030 -0
1 3
2 3
2
N/A 3
1 0
0 229
9
000/00:06:52
060 -0
3 -0
1 217
8
Coasting Arc #1 (Orbit 3319)
---------------------------------------
Vector Time (GMT): 2013/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3593302
96 A = 6794296
30 meter
Y = 4631720
15 meter E =
0014438
Z = -3437373
86 I = 51
79078
XDOT = -5987
707983 Wp = 57
65560
YDOT = -1239
923705 meter/sec RA = 155
29349 deg
ZDOT = 4610
245131 TA = 262
27315
MA = 262
43711
Ha = 229
928 n
mi
Hp = 216
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11789051
69 X = -3628130
78
Y = 15195932
26 feet Y = 4591343
30 meter
Z = -11277473
29 Z = -3454913
96
XDOT = -19644
711231 XDOT = -5995
793426
YDOT = -4067
991158 feet/sec YDOT = -1306
927862 meter/sec
ZDOT = 15125
476152 ZDOT = 4581
137261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11706309
53 X = 3568083
15
Y = 15204882
27 feet Y = 4634448
12 meter
Z = -11351359
97 Z = -3459894
52
XDOT = -7854
452516 XDOT = -2394
037127
YDOT = 17195
852369 feet/sec YDOT = 5241
295802 meter/sec
ZDOT = 15004
000765 ZDOT = 4573
219433
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 13158
50724933
00016717 00000-0 10270-3 0 9008
2 25544 51
6443 156
3513 0010730 42
0310 318
1662 15
50686270 33205
Satellite: ISS
Catalog Number: 25544
Epoch time: 13158
50724933 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 156
3513 deg
Eccentricity:
0010730
Arg of perigee: 42
0310 deg
Mean anomaly: 318
1662 deg
Mean motion: 15
50686270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3320
Checksum: 267
Coasting Arc #2 (Orbit 3335)
---------------------------------------
Vector Time (GMT): 2013/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3780431
52 A = 6795482
22 meter
Y = -4813853
27 meter E =
0021445
Z = 2941493
99 I = 51
82207
XDOT = 5634
337489 Wp = 74
49633
YDOT = 1334
866776 meter/sec RA = 150
34525 deg
ZDOT = -5020
665637 TA = 72
06717
MA = 71
83349
Ha = 229
889 n
mi
Hp = 216
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12402990
56 X = 3819691
00
Y = -15793481
86 feet Y = -4771359
01 meter
Z = 9650570
85 Z = 2959953
81
XDOT = 18485
359216 XDOT = 5643
381188
YDOT = 4379
484173 feet/sec YDOT = 1397
924773 meter/sec
ZDOT = -16472
000120 ZDOT = -4993
272151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12397956
50 X = -3778897
14
Y = -15749661
61 feet Y = -4800496
86 meter
Z = 9728339
82 Z = 2965197
98
XDOT = 7531
174903 XDOT = 2295
502110
YDOT = -16104
888528 feet/sec YDOT = -4908
770023 meter/sec
ZDOT = -16357
687012 ZDOT = -4985
823001
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 13159
53835184
00016717 00000-0 10270-3 0 9014
2 25544 51
6436 151
2363 0010724 44
9759 315
2258 15
50742741 33367
Satellite: ISS
Catalog Number: 25544
Epoch time: 13159
53835184 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 151
2363 deg
Eccentricity:
0010724
Arg of perigee: 44
9759 deg
Mean anomaly: 315
2258 deg
Mean motion: 15
50742741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3336
Checksum: 305
Coasting Arc #3 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2013/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3856325
63 A = 6796589
72 meter
Y = 5018183
90 meter E =
0016121
Z = -2471192
33 I = 51
85183
XDOT = -5292
125083 Wp = 49
57011
YDOT = -1450
546733 meter/sec RA = 145
40152 deg
ZDOT = 5345
927111 TA = 282
88075
MA = 283
06079
Ha = 229
990 n
mi
Hp = 216
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12651986
98 X = -3900148
99
Y = 16463857
94 feet Y = 4974815
36 meter
Z = -8107586
38 Z = -2490031
82
XDOT = -17362
615101 XDOT = -5301
480623
YDOT = -4759
011590 feet/sec YDOT = -1509
779699 meter/sec
ZDOT = 17539
130940 ZDOT = 5320
195377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13263628
74 X = 4042754
04
Y = 15934672
66 feet Y = 4856888
23 meter
Z = -8186984
17 Z = -2495392
78
XDOT = -7346
664614 XDOT = -2239
263374
YDOT = 15016
115449 feet/sec YDOT = 4576
911989 meter/sec
ZDOT = 17431
764760 ZDOT = 5313
201899
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 13160
50500056
00016717 00000-0 10270-3 0 9021
2 25544 51
6436 146
4428 0010785 49
1956 311
0129 15
50730102 33514
Satellite: ISS
Catalog Number: 25544
Epoch time: 13160
50500056 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 146
4428 deg
Eccentricity:
0010785
Arg of perigee: 49
1956 deg
Mean anomaly: 311
0129 deg
Mean motion: 15
50730102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 269
Coasting Arc #4 (Orbit 3366)
---------------------------------------
Vector Time (GMT): 2013/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3951154
41 A = 6797547
74 meter
Y = -5190539
88 meter E =
0021312
Z = 1895566
92 I = 51
88036
XDOT = 4920
522247 Wp = 86
89991
YDOT = 1668
454677 meter/sec RA = 140
45903 deg
ZDOT = -5632
053233 TA = 72
32571
MA = 72
09313
Ha = 229
967 n
mi
Hp = 216
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12963105
03 X = 3999694
32
Y = -17029330
32 feet Y = -5146084
45 meter
Z = 6219051
57 Z = 1914878
47
XDOT = 16143
445692 XDOT = 4928
858560
YDOT = 5473
932666 feet/sec YDOT = 1723
526474 meter/sec
ZDOT = -18477
864939 ZDOT = -5608
129243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14023350
69 X = -4274317
29
Y = -16135880
01 feet Y = -4918216
23 meter
Z = 6300460
10 Z = 1920380
24
XDOT = 7507
199723 XDOT = 2288
194475
YDOT = -13770
763103 feet/sec YDOT = -4197
328594 meter/sec
ZDOT = -18378
071677 ZDOT = -5601
636247
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 13161
53607932
00016717 00000-0 10270-3 0 9037
2 25544 51
6439 141
3278 0010757 51
7644 308
4473 15
50773204 33675
Satellite: ISS
Catalog Number: 25544
Epoch time: 13161
53607932 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 141
3278 deg
Eccentricity:
0010757
Arg of perigee: 51
7644 deg
Mean anomaly: 308
4473 deg
Mean motion: 15
50773204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3367
Checksum: 306
Coasting Arc #5 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2013/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3937325
30 A = 6798267
08 meter
Y = 5364260
14 meter E =
0019143
Z = -1363230
49 I = 51
90592
XDOT = -4590
239781 Wp = 48
34979
YDOT = -1902
989022 meter/sec RA = 135
52031 deg
ZDOT = 5834
631054 TA = 296
87544
MA = 297
07098
Ha = 230
010 n
mi
Hp = 216
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12917733
92 X = -3990394
78
Y = 17599278
68 feet Y = 5319933
94 meter
Z = -4472540
98 Z = -1382485
83
XDOT = -15059
841800 XDOT = -4596
962027
YDOT = -6243
402303 feet/sec YDOT = -1954
358352 meter/sec
ZDOT = 19142
490335 ZDOT = 5812
315507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14865269
10 X = 4530934
02
Y = 15965375
20 feet Y = 4866246
36 meter
Z = -4553751
38 Z = -1387983
42
XDOT = -7816
901272 XDOT = -2382
591508
YDOT = 12651
806836 feet/sec YDOT = 3856
270724 meter/sec
ZDOT = 19049
441875 ZDOT = 5806
269884
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 13162
50270515
00016717 00000-0 10270-3 0 9049
2 25544 51
6439 136
5344 0010777 56
2487 303
9690 15
50778432 33828
Satellite: ISS
Catalog Number: 25544
Epoch time: 13162
50270515 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 136
5344 deg
Eccentricity:
0010777
Arg of perigee: 56
2487 deg
Mean anomaly: 303
9690 deg
Mean motion: 15
50778432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 311
Coasting Arc #6 (Orbit 3397)
---------------------------------------
Vector Time (GMT): 2013/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3943392
51 A = 6798778
12 meter
Y = -5485326
42 meter E =
0019933
Z = 732285
25 I = 51
92991
XDOT = 4244
628536 Wp = 97
12234
YDOT = 2235
841995 meter/sec RA = 130
58267 deg
ZDOT = -5972
715787 TA = 75
00997
MA = 74
78942
Ha = 230
016 n
mi
Hp = 216
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12937639
48 X = 4000880
30
Y = -17996477
76 feet Y = -5440907
57 meter
Z = 2402510
66 Z = 751580
82
XDOT = 13925
946641 XDOT = 4248
325166
YDOT = 7335
439615 feet/sec YDOT = 2283
329512 meter/sec
ZDOT = -19595
524235 ZDOT = -5952
086552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15523624
13 X = -4731600
63
Y = -15807435
88 feet Y = -4818106
45 meter
Z = 2483918
18 Z = 757098
26
XDOT = 8473
500093 XDOT = 2582
722828
YDOT = -11455
237470 feet/sec YDOT = -3491
556381 meter/sec
ZDOT = -19509
562116 ZDOT = -5946
514533
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 13163
53375965
00016717 00000-0 10270-3 0 9059
2 25544 51
6448 131
4196 0010743 58
7821 301
4382 15
50800561 33986
Satellite: ISS
Catalog Number: 25544
Epoch time: 13163
53375965 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 131
4196 deg
Eccentricity:
0010743
Arg of perigee: 58
7821 deg
Mean anomaly: 301
4382 deg
Mean motion: 15
50800561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3398
Checksum: 309
Coasting Arc #7 (Orbit 3412)
---------------------------------------
Vector Time (GMT): 2013/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3852415
44 A = 6798943
36 meter
Y = 5589366
82 meter E =
0022113
Z = -162184
63 I = 51
94983
XDOT = -3965
707382 Wp = 53
36136
YDOT = -2575
087293 meter/sec RA = 125
64765 deg
ZDOT = 6034
721843 TA = 304
90055
MA = 305
10817
Ha = 230
001 n
mi
Hp = 216
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12639158
25 X = -3913842
77
Y = 18337817
65 feet Y = 5545943
24 meter
Z = -532101
82 Z = -181047
87
XDOT = -13010
850991 XDOT = -3965
932419
YDOT = -8448
449123 feet/sec YDOT = -2619
436250 meter/sec
ZDOT = 19798
956178 ZDOT = 6015
456018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16174806
84 X = 4930081
12
Y = 15307136
35 feet Y = 4665615
16 meter
Z = -611727
21 Z = -186454
45
XDOT = -9251
149366 XDOT = -2819
750327
YDOT = 10497
264891 feet/sec YDOT = 3199
566339 meter/sec
ZDOT = 19718
734186 ZDOT = 6010
270180
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 13164
50036181
00016717 00000-0 10270-3 0 9062
2 25544 51
6447 126
6261 0010706 63
0303 297
1940 15
50822467 34135
Satellite: ISS
Catalog Number: 25544
Epoch time: 13164
50036181 = yrday
fracday
Element set: 906
Inclination: 51
6447 deg
RA of node: 126
6261 deg
Eccentricity:
0010706
Arg of perigee: 63
0303 deg
Mean anomaly: 297
1940 deg
Mean motion: 15
50822467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3413
Checksum: 281
Coasting Arc #8 (Orbit 3428)
---------------------------------------
Vector Time (GMT): 2013/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3788923
58 A = 6798829
27 meter
Y = -5621595
14 meter E =
0017559
Z = -493853
62 I = 51
96764
XDOT = 3686
033785 Wp = 102
95238
YDOT = 2996
028702 meter/sec RA = 120
71320 deg
ZDOT = -6007
712239 TA = 82
34019
MA = 82
14081
Ha = 230
021 n
mi
Hp = 216
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12430851
64 X = 3853902
87
Y = -18443553
62 feet Y = -5578861
64 meter
Z = -1620254
67 Z = -475290
11
XDOT = 12093
286695 XDOT = 3681
441366
YDOT = 9829
490493 feet/sec YDOT = 3037
223152 meter/sec
ZDOT = -19710
341993 ZDOT = -5989
816725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16567312
28 X = -5049716
78
Y = -14847989
00 feet Y = -4525667
05 meter
Z = -1541867
23 Z = -469961
13
XDOT = 10324
632083 XDOT = 3146
947859
YDOT = -9546
770278 feet/sec YDOT = -2909
855581 meter/sec
ZDOT = -19635
902995 ZDOT = -5985
023233
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 13165
53139127
00016717 00000-0 10270-3 0 9071
2 25544 51
6457 121
5114 0010683 65
8226 294
4041 15
50832026 34296
Satellite: ISS
Catalog Number: 25544
Epoch time: 13165
53139127 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 121
5114 deg
Eccentricity:
0010683
Arg of perigee: 65
8226 deg
Mean anomaly: 294
4041 deg
Mean motion: 15
50832026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3429
Checksum: 291
Coasting Arc #9 (Orbit 3444)
---------------------------------------
Vector Time (GMT): 2013/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3647377
77 A = 6798398
79 meter
Y = 5623507
47 meter E =
0024045
Z = 1072622
32 I = 51
98105
XDOT = -3490
160147 Wp = 62
43255
YDOT = -3409
440719 meter/sec RA = 115
78002 deg
ZDOT = 5916
476548 TA = 309
13816
MA = 309
35163
Ha = 229
996 n
mi
Hp = 216
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11966462
52 X = -3715200
48
Y = 18449827
66 feet Y = 5582340
88 meter
Z = 3519102
09 Z = 1054739
42
XDOT = -11450
656650 XDOT = -3480
516283
YDOT = -11185
829130 feet/sec YDOT = -3448
416471 meter/sec
ZDOT = 19411
012298 ZDOT = 5899
544801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16880873
15 X = 5145290
14
Y = 14112212
13 feet Y = 4301402
26 meter
Z = 3443549
92 Z = 1049594
01
XDOT = -11460
976676 XDOT = -3493
305691
YDOT = 8916
202350 feet/sec YDOT = 2717
658476 meter/sec
ZDOT = 19340
658289 ZDOT = 5895
032647
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 13166
56240728
00016717 00000-0 10270-3 0 9086
2 25544 51
6455 116
3979 0010632 69
8789 290
3505 15
50856992 34453
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166
56240728 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 116
3979 deg
Eccentricity:
0010632
Arg of perigee: 69
8789 deg
Mean anomaly: 290
3505 deg
Mean motion: 15
50856992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3445
Checksum: 343
Coasting Arc #10 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2013/166/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 922037
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4683229
72 A = 6789342
20 meter
Y = 1179432
19 meter E =
0016857
Z = 4757414
95 I = 51
95336
XDOT = 1002
164418 Wp = 89
97038
YDOT = -7098
291414 meter/sec RA = 115
42770 deg
ZDOT = 2737
963832 TA = 333
04517
MA = 333
13263
Ha = 230
095 n
mi
Hp = 216
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15364926
92 X = -4719180
55
Y = 3869528
20 feet Y = 1126859
95 meter
Z = 15608316
75 Z = 4734577
01
XDOT = 3287
941005 XDOT = 1068
164276
YDOT = -23288
357656 feet/sec YDOT = -7086
715782 meter/sec
ZDOT = 8982
820970 ZDOT = 2742
991972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8855030
04 X = 2699013
16
Y = 13252177
21 feet Y = 4039263
61 meter
Z = 15512640
70 Z = 4728252
89
XDOT = -22048
252309 XDOT = -6720
307304
YDOT = 4159
493153 feet/sec YDOT = 1267
813513 meter/sec
ZDOT = 9004
809958 ZDOT = 2744
666075
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 13166
62684498
00016717 00000-0 10270-3 0 9090
2 25544 51
6469 116
0789 0010594 70
1514 290
0778 15
50869321 34462
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166
62684498 = yrday
fracday
Element set: 909
Inclination: 51
6469 deg
RA of node: 116
0789 deg
Eccentricity:
0010594
Arg of perigee: 70
1514 deg
Mean anomaly: 290
0778 deg
Mean motion: 15
50869321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 336
Coasting Arc #11 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2013/167/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 922037
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4506805
97 A = 6788259
89 meter
Y = -815174
88 meter E =
0023292
Z = -5031796
92 I = 51
96275
XDOT = -993
099496 Wp = 74
13297
YDOT = 7291
457720 meter/sec RA = 110
48477 deg
ZDOT = -2072
526445 TA = 175
74414
MA = 175
72430
Ha = 229
981 n
mi
Hp = 216
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14786108
82 X = 4540029
65
Y = -2674458
27 feet Y = -764590
77 meter
Z = -16508520
08 Z = -5009822
56
XDOT = -3258
200446 XDOT = -1064
492539
YDOT = 23922
105381 feet/sec YDOT = 7279
953238 meter/sec
ZDOT = -6799
627444 ZDOT = -2077
523682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7761233
88 X = -2365624
09
Y = -12983635
12 feet Y = -3957411
98 meter
Z = -16416499
15 Z = -5003748
94
XDOT = 22569
109885 XDOT = 6879
064693
YDOT = -4873
488834 feet/sec YDOT = -1485
439397 meter/sec
ZDOT = -6821
524237 ZDOT = -2079
200588
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 13167
59341070
00016717 00000-0 10270-3 0 9105
2 25544 51
6475 111
2839 0010696 73
2548 286
9776 15
50883396 34613
Satellite: ISS
Catalog Number: 25544
Epoch time: 13167
59341070 = yrday
fracday
Element set: 910
Inclination: 51
6475 deg
RA of node: 111
2839 deg
Eccentricity:
0010696
Arg of perigee: 73
2548 deg
Mean anomaly: 286
9776 deg
Mean motion: 15
50883396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 332
Coasting Arc #12 (Orbit 3476)
---------------------------------------
Vector Time (GMT): 2013/168/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 922037
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4334006
71 A = 6787357
60 meter
Y = 420429
06 meter E =
0013924
Z = 5194572
67 I = 51
96967
XDOT = 949
646014 Wp = 90
90863
YDOT = -7485
883209 meter/sec RA = 105
54216 deg
ZDOT = 1394
768652 TA = 345
73040
MA = 345
76969
Ha = 230
046 n
mi
Hp = 215
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14219182
12 X = -4363619
91
Y = 1379360
43 feet Y = 371797
46 meter
Z = 17042561
25 Z = 5173446
42
XDOT = 3115
636530 XDOT = 1026
508746
YDOT = -24559
984281 feet/sec YDOT = -7474
834018 meter/sec
ZDOT = 4576
012637 ZDOT = 1399
568062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6571777
86 X = 2003077
89
Y = 12802564
19 feet Y = 3902221
57 meter
Z = 16954136
82 Z = 5167620
90
XDOT = -23030
686354 XDOT = -7019
753201
YDOT = 5719
199788 feet/sec YDOT = 1743
212096 meter/sec
ZDOT = 4597
121925 ZDOT = 1401
202763
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 13168
62439980
00016717 00000-0 10270-3 0 9119
2 25544 51
6472 106
1697 0010531 77
1911 283
0417 15
50915665 34772
Satellite: ISS
Catalog Number: 25544
Epoch time: 13168
62439980 = yrday
fracday
Element set: 911
Inclination: 51
6472 deg
RA of node: 106
1697 deg
Eccentricity:
0010531
Arg of perigee: 77
1911 deg
Mean anomaly: 283
0417 deg
Mean motion: 15
50915665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3477
Checksum: 315
Coasting Arc #13 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2013/169/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 922037
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4234020
75 A = 6786874
55 meter
Y = 16067
93 meter E =
0025204
Z = -5326062
33 I = 51
97619
XDOT = -878
262523 Wp = 82
93492
YDOT = 7563
644386 meter/sec RA = 100
59871 deg
ZDOT = -675
097681 TA = 180
62666
MA = 180
62982
Ha = 229
924 n
mi
Hp = 215
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13891144
19 X = 4259399
20
Y = 52716
29 feet Y = 63557
81 meter
Z = -17473957
76 Z = -5305432
00
XDOT = -2881
438724 XDOT = -959
496082
YDOT = 24815
106253 feet/sec YDOT = 7553
368960 meter/sec
ZDOT = -2214
887405 ZDOT = -679
560854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5344147
22 X = -1628896
07
Y = -12938898
38 feet Y = -3943776
23 meter
Z = -17387664
16 Z = -5299760
04
XDOT = 23061
620032 XDOT = 7029
181786
YDOT = -6520
992043 feet/sec YDOT = -1987
598375 meter/sec
ZDOT = -2234
616878 ZDOT = -681
111224
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 13169
59094216
00016717 00000-0 10270-3 0 9126
2 25544 51
6480 101
3746 0010616 80
3335 279
9015 15
50920587 34927
Satellite: ISS
Catalog Number: 25544
Epoch time: 13169
59094216 = yrday
fracday
Element set: 912
Inclination: 51
6480 deg
RA of node: 101
3746 deg
Eccentricity:
0010616
Arg of perigee: 80
3335 deg
Mean anomaly: 279
9015 deg
Mean motion: 15
50920587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 307
Coasting Arc #14 (Orbit 3506)
---------------------------------------
Vector Time (GMT): 2013/170/13:01:52
060
Vector Time (MET): N/A
Weight (LBS) : 921735
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4005964
86 A = 6788734
00 meter
Y = 1498196
07 meter E =
0022246
Z = -5291350
54 I = 51
98125
XDOT = -1511
475109 Wp = 92
38175
YDOT = 7432
677174 meter/sec RA = 95
79926 deg
ZDOT = 962
783629 TA = 186
80088
MA = 186
83111
Ha = 229
912 n
mi
Hp = 217
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13142929
33 X = 4014618
20
Y = 4915341
45 feet Y = 1543042
27 meter
Z = -17360073
94 Z = -5271868
52
XDOT = -4958
907839 XDOT = -1599
153568
YDOT = 24385
423799 feet/sec YDOT = 7415
284560 meter/sec
ZDOT = 3158
738941 ZDOT = 955
228798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1912451
38 X = 582915
18
Y = -14001973
41 feet Y = -4267801
50 meter
Z = -17278790
76 Z = -5266575
42
XDOT = 23863
573713 XDOT = 7273
617268
YDOT = -587
709161 feet/sec YDOT = -179
133752 meter/sec
ZDOT = 3126
077847 ZDOT = 952
828528
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13170
55747388
00016717 00000-0 10270-3 0 9130
2 25544 51
6479 96
5798 0008027 83
3865 276
8199 15
50333418 35078
Satellite: ISS
Catalog Number: 25544
Epoch time: 13170
55747388 = yrday
fracday
Element set: 913
Inclination: 51
6479 deg
RA of node: 96
5798 deg
Eccentricity:
0008027
Arg of perigee: 83
3865 deg
Mean anomaly: 276
8199 deg
Mean motion: 15
50333418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3507
Checksum: 352
Coasting Arc #15 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2013/171/13:01:52
060
Vector Time (MET): N/A
Weight (LBS) : 921735
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4024478
05 A = 6788970
88 meter
Y = -1719182
76 meter E =
0012064
Z = 5180830
63 I = 51
98487
XDOT = 1264
391569 Wp = 75
00887
YDOT = -7420
548819 meter/sec RA = 90
86289 deg
ZDOT = -1474
325609 TA = 29
14539
MA = 29
07811
Ha = 229
923 n
mi
Hp = 217
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13203668
16 X = -4030122
01
Y = -5640363
38 feet Y = -1764219
27 meter
Z = 16997475
82 Z = 5161265
92
XDOT = 4148
266301 XDOT = 1354
437726
YDOT = -24345
632609 feet/sec YDOT = -7405
905918 meter/sec
ZDOT = -4837
026277 ZDOT = -1467
965531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2362451
22 X = -720075
13
Y = 14259616
19 feet Y = 4346331
02 meter
Z = 16915877
34 Z = 5155959
41
XDOT = -23607
267970 XDOT = -7195
495277
YDOT = 1817
154618 feet/sec YDOT = 553
868728 meter/sec
ZDOT = -4809
345628 ZDOT = -1465
888547
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13171
58882164
00016717 00000-0 10270-3 0 9147
2 25544 51
6480 91
4680 0007885 86
7335 273
4718 15
50386059 35231
Satellite: ISS
Catalog Number: 25544
Epoch time: 13171
58882164 = yrday
fracday
Element set: 914
Inclination: 51
6480 deg
RA of node: 91
4680 deg
Eccentricity:
0007885
Arg of perigee: 86
7335 deg
Mean anomaly: 273
4718 deg
Mean motion: 15
50386059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 332
Coasting Arc #16 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2013/172/13:01:52
060
Vector Time (MET): N/A
Weight (LBS) : 921735
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4109047
50 A = 6789586
68 meter
Y = 1926405
84 meter E =
0020631
Z = -5068602
08 I = 51
98733
XDOT = -1016
201611 Wp = 99
08098
YDOT = 7320
331116 meter/sec RA = 85
92673 deg
ZDOT = 1962
041455 TA = 189
90521
MA = 189
94594
Ha = 229
824 n
mi
Hp = 217
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13481126
95 X = 4111822
70
Y = 6320229
14 feet Y = 1972372
13 meter
Z = -16629271
93 Z = -5048633
49
XDOT = -3333
994787 XDOT = -1107
514748
YDOT = 24016
834369 feet/sec YDOT = 7308
456435 meter/sec
ZDOT = 6437
143882 ZDOT = 1956
884168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2705834
92 X = 824738
48
Y = -14735219
86 feet Y = -4491295
01 meter
Z = -16546012
15 Z = -5043224
50
XDOT = 23020
544838 XDOT = 7016
662067
YDOT = -2961
973374 feet/sec YDOT = -902
809484 meter/sec
ZDOT = 6414
491207 ZDOT = 1955
136920
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13172
55570109
00016717 00000-0 10270-3 0 9159
2 25544 51
6491 86
6756 0007922 90
3116 269
8943 15
50370947 35387
Satellite: ISS
Catalog Number: 25544
Epoch time: 13172
55570109 = yrday
fracday
Element set: 915
Inclination: 51
6491 deg
RA of node: 86
6756 deg
Eccentricity:
0007922
Arg of perigee: 90
3116 deg
Mean anomaly: 269
8943 deg
Mean motion: 15
50370947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 330
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