[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 25th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 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
243/07:34:03
641 0
3 1
0 1
0
N/A 0
9 -0
1 227
5
000/00:02:07
282 -0
3 -0
0 220
3
Coasting Arc #1 (Orbit 483)
---------------------------------------
Vector Time (GMT): 2013/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2578699
24 A = 6795122
34 meter
Y = -5255961
74 meter E =
0011507
Z = 3444514
93 I = 51
85979
XDOT = 6125
706892 Wp = 68
55705
YDOT = -21
319070 meter/sec RA = 143
64974 deg
ZDOT = -4602
013340 TA = 71
29595
MA = 71
17109
Ha = 226
925 n
mi
Hp = 220
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8460299
34 X = 2620548
70
Y = -17243968
95 feet Y = -5226890
88 meter
Z = 11300902
00 Z = 3457143
75
XDOT = 20097
463557 XDOT = 6147
844920
YDOT = -69
944457 feet/sec YDOT = 47
305962 meter/sec
ZDOT = -15098
468962 ZDOT = -4572
202007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16044179
24 X = -4890265
83
Y = 10502419
99 feet Y = 3201137
61 meter
Z = 11354514
67 Z = 3460856
07
XDOT = -16605
504173 XDOT = -5061
357672
YDOT = -9121
258714 feet/sec YDOT = -2780
159656 meter/sec
ZDOT = -14973
430463 ZDOT = -4563
901605
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 13233
53951829
00016717 00000-0 10270-3 0 9001
2 25544 51
6500 144
5224 0004414 338
6605 21
4361 15
50404946 4846
Satellite: ISS
Catalog Number: 25544
Epoch time: 13233
53951829 = yrday
fracday
Element set: 900
Inclination: 51
6500 deg
RA of node: 144
5224 deg
Eccentricity:
0004414
Arg of perigee: 338
6605 deg
Mean anomaly: 21
4361 deg
Mean motion: 15
50404946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 484
Checksum: 281
Coasting Arc #2 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2013/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2581674
25 A = 6796018
06 meter
Y = 5479752
05 meter E =
0006225
Z = -3076946
06 I = 51
88792
XDOT = -5862
801636 Wp = 28
51625
YDOT = 1
225800 meter/sec RA = 138
70876 deg
ZDOT = 4930
729067 TA = 296
34231
MA = 296
40622
Ha = 226
963 n
mi
Hp = 220
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8470059
87 X = -2627811
41
Y = 17978189
13 feet Y = 5450623
92 meter
Z = -10094967
40 Z = -3089599
90
XDOT = -19234
913504 XDOT = -5886
331399
YDOT = 4
021654 feet/sec YDOT = -64
466952 meter/sec
ZDOT = 16176
932636 ZDOT = 4902
191381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16241703
49 X = 4950471
22
Y = -11405093
33 feet Y = -3476272
45 meter
Z = -10148718
11 Z = -3093329
28
XDOT = 15939
127657 XDOT = 4858
246110
YDOT = 8437
520821 feet/sec YDOT = 2571
756346 meter/sec
ZDOT = 16057
230829 ZDOT = 4894
243957
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 13234
50635601
00016717 00000-0 10270-3 0 9017
2 25544 51
6505 139
7298 0004473 341
7365 18
3625 15
50444185 4994
Satellite: ISS
Catalog Number: 25544
Epoch time: 13234
50635601 = yrday
fracday
Element set: 901
Inclination: 51
6505 deg
RA of node: 139
7298 deg
Eccentricity:
0004473
Arg of perigee: 341
7365 deg
Mean anomaly: 18
3625 deg
Mean motion: 15
50444185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 305
Coasting Arc #3 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2013/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2583934
44 A = 6797090
37 meter
Y = -5697784
01 meter E =
0012199
Z = 2648473
05 I = 51
91338
XDOT = 5593
093298 Wp = 83
54217
YDOT = 92
732013 meter/sec RA = 133
77057 deg
ZDOT = -5235
279721 TA = 66
76864
MA = 66
64023
Ha = 227
075 n
mi
Hp = 220
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8477475
20 X = 2634590
83
Y = -18693517
09 feet Y = -5668605
36 meter
Z = 8689216
04 Z = 2661148
94
XDOT = 18350
043630 XDOT = 5617
071968
YDOT = 304
238889 feet/sec YDOT = 155
411177 meter/sec
ZDOT = -17176
114571 ZDOT = -5208
051027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16402725
19 X = -4999550
64
Y = 12301485
96 feet Y = 3749492
92 meter
Z = 8743093
95 Z = 2664895
03
XDOT = -15118
552213 XDOT = -4608
134715
YDOT = -7981
459570 feet/sec YDOT = -2432
748877 meter/sec
ZDOT = -17061
908602 ZDOT = -5200
469742
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 13235
53763816
00016717 00000-0 10270-3 0 9022
2 25544 51
6500 134
6179 0004446 345
6755 14
4269 15
50435793 5152
Satellite: ISS
Catalog Number: 25544
Epoch time: 13235
53763816 = yrday
fracday
Element set: 902
Inclination: 51
6500 deg
RA of node: 134
6179 deg
Eccentricity:
0004446
Arg of perigee: 345
6755 deg
Mean anomaly: 14
4269 deg
Mean motion: 15
50435793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 308
Coasting Arc #4 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2013/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2517946
39 A = 6797825
04 meter
Y = 5904613
36 meter E =
0009397
Z = -2223554
41 I = 51
93733
XDOT = -5342
537835 Wp = 20
16580
YDOT = -217
180791 meter/sec RA = 128
83365 deg
ZDOT = 5488
625566 TA = 315
26914
MA = 315
34488
Ha = 227
088 n
mi
Hp = 220
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8260978
99 X = -2572984
58
Y = 19372091
08 feet Y = 5876148
18 meter
Z = -7295126
01 Z = -2235920
42
XDOT = -17528
011270 XDOT = -5366
374286
YDOT = -712
535402 feet/sec YDOT = -277
057291 meter/sec
ZDOT = 18007
301727 ZDOT = 5462
614292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16322449
20 X = 4975082
52
Y = -13278890
04 feet Y = -4047405
69 meter
Z = -7347739
89 Z = -2239591
12
XDOT = 14289
837681 XDOT = 4355
542525
YDOT = 7689
200231 feet/sec YDOT = 2343
668230 meter/sec
ZDOT = 17898
212281 ZDOT = 5455
375103
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 13236
50445184
00016717 00000-0 10270-3 0 9036
2 25544 51
6505 129
8249 0004564 348
0333 12
0709 15
50483313 5302
Satellite: ISS
Catalog Number: 25544
Epoch time: 13236
50445184 = yrday
fracday
Element set: 903
Inclination: 51
6505 deg
RA of node: 129
8249 deg
Eccentricity:
0004564
Arg of perigee: 348
0333 deg
Mean anomaly: 12
0709 deg
Mean motion: 15
50483313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 282
Coasting Arc #5 (Orbit 545)
---------------------------------------
Vector Time (GMT): 2013/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2454028
21 A = 6798702
63 meter
Y = -6092944
80 meter E =
0012078
Z = 1739835
72 I = 51
95818
XDOT = 5097
783182 Wp = 97
06109
YDOT = 415
276950 meter/sec RA = 123
89927 deg
ZDOT = -5703
630880 TA = 63
96674
MA = 63
84244
Ha = 227
207 n
mi
Hp = 220
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8051273
64 X = 2513526
84
Y = -19989976
38 feet Y = -6065169
51 meter
Z = 5708122
43 Z = 1751902
04
XDOT = 16725
010439 XDOT = 5120
467165
YDOT = 1362
457185 feet/sec YDOT = 472
410050 meter/sec
ZDOT = -18712
699736 ZDOT = -5678
811344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16193031
80 X = -4935636
09
Y = 14199244
08 feet Y = 4327929
60 meter
Z = 5759515
00 Z = 1755500
17
XDOT = -13366
978564 XDOT = -4074
255066
YDOT = -7653
045666 feet/sec YDOT = -2332
648319 meter/sec
ZDOT = -18608
629028 ZDOT = -5671
910128
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 13237
53570914
00016717 00000-0 10270-3 0 9041
2 25544 51
6501 124
7126 0004486 352
1218 7
9862 15
50464160 5466
Satellite: ISS
Catalog Number: 25544
Epoch time: 13237
53570914 = yrday
fracday
Element set: 904
Inclination: 51
6501 deg
RA of node: 124
7126 deg
Eccentricity:
0004486
Arg of perigee: 352
1218 deg
Mean anomaly: 7
9862 deg
Mean motion: 15
50464160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 546
Checksum: 291
Coasting Arc #6 (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 = -2327152
02 A = 6799137
33 meter
Y = 6253623
08 meter E =
0012705
Z = -1269272
08 I = 51
97684
XDOT = -4891
189710 Wp = 23
30971
YDOT = -635
807310 meter/sec RA = 118
96567 deg
ZDOT = 5866
540639 TA = 322
96791
MA = 323
05553
Ha = 227
211 n
mi
Hp = 220
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7635013
19 X = -2390742
68
Y = 20517136
10 feet Y = 6227243
77 meter
Z = -4164278
47 Z = -1280731
92
XDOT = -16047
210334 XDOT = -4912
214419
YDOT = -2085
981989 feet/sec YDOT = -690
620944 meter/sec
ZDOT = 19247
180575 ZDOT = 5842
728729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15811078
33 X = 4819216
68
Y = -15127676
41 feet Y = -4610915
77 meter
Z = -4213160
77 Z = -1284171
40
XDOT = 12526
252868 XDOT = 3818
001874
YDOT = 7787
778529 feet/sec YDOT = 2373
714896 meter/sec
ZDOT = 19147
359795 ZDOT = 5836
115265
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
50249901
00016717 00000-0 10270-3 0 9059
2 25544 51
6504 119
9193 0004671 353
9785 6
1309 15
50521360 5613
Satellite: ISS
Catalog Number: 25544
Epoch time: 13238
50249901 = yrday
fracday
Element set: 905
Inclination: 51
6504 deg
RA of node: 119
9193 deg
Eccentricity:
0004671
Arg of perigee: 353
9785 deg
Mean anomaly: 6
1309 deg
Mean motion: 15
50521360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 561
Checksum: 296
Coasting Arc #7 (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 = 2209406
71 A = 6799671
48 meter
Y = -6383882
56 meter E =
0010984
Z = 744984
50 I = 51
99228
XDOT = 4702
507860 Wp = 108
31251
YDOT = 922
072384 meter/sec RA = 114
03441 deg
ZDOT = -5976
118556 TA = 63
69065
MA = 63
57786
Ha = 227
313 n
mi
Hp = 220
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7248709
66 X = 2277009
55
Y = -20944496
59 feet Y = -6358797
56 meter
Z = 2444174
86 Z = 755882
01
XDOT = 15428
175394 XDOT = 4720
877793
YDOT = 3025
171864 feet/sec YDOT = 974
761283 meter/sec
ZDOT = -19606
688176 ZDOT = -5953
229708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15388110
09 X = -4690295
96
Y = 15943401
70 feet Y = 4859548
84 meter
Z = 2490728
84 Z = 759174
15
XDOT = -11663
345571 XDOT = -3554
987730
YDOT = -8174
498632 feet/sec YDOT = -2491
587183 meter/sec
ZDOT = -19510
771915 ZDOT = -5946
883280
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
53373155
00016717 00000-0 10270-3 0 9063
2 25544 51
6502 114
8069 0004538 357
8902 2
2229 15
50493505 5777
Satellite: ISS
Catalog Number: 25544
Epoch time: 13239
53373155 = yrday
fracday
Element set: 906
Inclination: 51
6502 deg
RA of node: 114
8069 deg
Eccentricity:
0004538
Arg of perigee: 357
8902 deg
Mean anomaly: 2
2229 deg
Mean motion: 15
50493505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 577
Checksum: 304
Coasting Arc #8 (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 = -2040016
17 A = 6799693
18 meter
Y = 6472772
51 meter E =
0015346
Z = -244077
27 I = 52
00459
XDOT = -4567
205113 Wp = 31
26787
YDOT = -1218
730472 meter/sec RA = 109
10310 deg
ZDOT = 6035
342889 TA = 326
11813
MA = 326
21607
Ha = 227
317 n
mi
Hp = 220
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6692966
44 X = -2111058
85
Y = 21236130
29 feet Y = 6449562
53 meter
Z = -800778
45 Z = -254160
19
XDOT = -14984
268742 XDOT = -4582
555451
YDOT = -3998
459554 feet/sec YDOT = -1269
889491 meter/sec
ZDOT = 19800
993731 ZDOT = 6013
118701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14731427
12 X = 4490138
99
Y = -16693804
12 feet Y = -5088271
50 meter
Z = -843939
97 Z = -257232
90
XDOT = 10967
030991 XDOT = 3342
751046
YDOT = 8710
210164 feet/sec YDOT = 2654
872058 meter/sec
ZDOT = 19707
900273 ZDOT = 6006
968003
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
50049814
00016717 00000-0 10270-3 0 9075
2 25544 51
6502 110
0134 0004745 359
7907
3241 15
50560992 5929
Satellite: ISS
Catalog Number: 25544
Epoch time: 13240
50049814 = yrday
fracday
Element set: 907
Inclination: 51
6502 deg
RA of node: 110
0134 deg
Eccentricity:
0004745
Arg of perigee: 359
7907 deg
Mean anomaly:
3241 deg
Mean motion: 15
50560992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 592
Checksum: 278
Coasting Arc #9 (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 = 1890799
78 A = 6799768
43 meter
Y = -6522230
91 meter E =
0008939
Z = -302448
51 I = 52
01360
XDOT = 4458
961067 Wp = 115
03598
YDOT = 1565
520502 meter/sec RA = 104
17377 deg
ZDOT = -6027
069037 TA = 68
20028
MA = 68
10519
Ha = 227
395 n
mi
Hp = 220
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6203411
36 X = 1965061
47
Y = -21398395
38 feet Y = -6500671
58 meter
Z = -992285
14 Z = -293082
68
XDOT = 14629
137359 XDOT = 4470
401312
YDOT = 5136
222118 feet/sec YDOT = 1615
447218 meter/sec
ZDOT = -19773
848545 ZDOT = -6005
380238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14064932
35 X = -4286991
38
Y = 17280897
70 feet Y = 5267217
62 meter
Z = -952113
32 Z = -290204
14
XDOT = -10319
746987 XDOT = -3145
458882
YDOT = -9456
805563 feet/sec YDOT = -2882
434336 meter/sec
ZDOT = -19683
043338 ZDOT = -5999
391609
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
53170578
00016717 00000-0 10270-3 0 9082
2 25544 51
6500 104
9011 0004616 3
1878 356
9301 15
50530412 6086
Satellite: ISS
Catalog Number: 25544
Epoch time: 13241
53170578 = yrday
fracday
Element set: 908
Inclination: 51
6500 deg
RA of node: 104
9011 deg
Eccentricity:
0004616
Arg of perigee: 3
1878 deg
Mean anomaly: 356
9301 deg
Mean motion: 15
50530412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 608
Checksum: 272
Coasting Arc #10 (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 = -1706058
56 A = 6799330
58 meter
Y = 6521096
12 meter E =
0016876
Z = 815159
46 I = 52
01892
XDOT = -4413
600099 Wp = 41
60304
YDOT = -1908
539434 meter/sec RA = 99
24331 deg
ZDOT = 5972
243840 TA = 327
15820
MA = 327
26296
Ha = 227
399 n
mi
Hp = 219
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5597304
97 X = -1782811
86
Y = 21394672
30 feet Y = 6501588
76 meter
Z = 2674407
68 Z = 806685
02
XDOT = -14480
315286 XDOT = -4420
941615
YDOT = -6261
612315 feet/sec YDOT = -1957
935960 meter/sec
ZDOT = 19593
975854 ZDOT = 5950
785419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13211875
71 X = 4026979
72
Y = -17739835
42 feet Y = -5407101
84 meter
Z = 2637965
43 Z = 804051
86
XDOT = 9904
717449 XDOT = 3018
957878
YDOT = 10305
809894 feet/sec YDOT = 3141
210856 meter/sec
ZDOT = 19504
179799 ZDOT = 5944
874003
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
56289804
00016717 00000-0 10270-3 0 9090
2 25544 51
6495 99
7875 0004765 5
7649 354
3556 15
50602788 6245
Satellite: ISS
Catalog Number: 25544
Epoch time: 13242
56289804 = yrday
fracday
Element set: 909
Inclination: 51
6495 deg
RA of node: 99
7875 deg
Eccentricity:
0004765
Arg of perigee: 5
7649 deg
Mean anomaly: 354
3556 deg
Mean motion: 15
50602788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 624
Checksum: 349
Coasting Arc #11 (Orbit 635)
---------------------------------------
Vector Time (GMT): 2013/243/07:35:07
282
Vector Time (MET): N/A
Weight (LBS) : 957369
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4082967
49 A = 6789938
00 meter
Y = -2278114
08 meter E =
0014173
Z = -4936721
19 I = 51
98951
XDOT = 1178
643681 Wp = 56
20062
YDOT = 7188
749021 meter/sec RA = 95
22706 deg
ZDOT = -2339
691686 TA = 190
94688
MA = 190
97775
Ha = 227
501 n
mi
Hp = 220
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13395562
64 X = 4132119
38
Y = -7474127
55 feet Y = -2232181
11 meter
Z = -16196591
83 Z = -4916767
26
XDOT = 3866
941212 XDOT = 1109
535374
YDOT = 23585
134582 feet/sec YDOT = 7201
542864 meter/sec
ZDOT = -7676
153824 ZDOT = -2334
134149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8082147
55 X = -2463438
57
Y = -13141469
64 feet Y = -4005519
95 meter
Z = -16112539
68 Z = -4911102
09
XDOT = 22423
544042 XDOT = 6834
696224
YDOT = -4395
036351 feet/sec YDOT = -1339
607080 meter/sec
ZDOT = -7653
804842 ZDOT = -2332
879716
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
33628882
00016717 00000-0 10270-3 0 9101
2 25544 51
6496 95
9528 0004408 3
6374 356
4808 15
50434791 6368
Satellite: ISS
Catalog Number: 25544
Epoch time: 13243
33628882 = yrday
fracday
Element set: 910
Inclination: 51
6496 deg
RA of node: 95
9528 deg
Eccentricity:
0004408
Arg of perigee: 3
6374 deg
Mean anomaly: 356
4808 deg
Mean motion: 15
50434791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 636
Checksum: 323
Coasting Arc #12 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2013/244/07:35:07
282
Vector Time (MET): N/A
Weight (LBS) : 957369
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3992862
62 A = 6789144
32 meter
Y = 2034967
68 meter E =
0005064
Z = 5095277
51 I = 51
98873
XDOT = -1392
616140 Wp = 75
82058
YDOT = -7313
373684 meter/sec RA = 90
29083 deg
ZDOT = 1829
217226 TA = 356
54917
MA = 356
55266
Ha = 227
630 n
mi
Hp = 220
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13099942
97 X = -4040072
47
Y = 6676403
13 feet Y = 1990053
24 meter
Z = 16716789
73 Z = 5075766
03
XDOT = -4568
950591 XDOT = -1319
618620
YDOT = -23994
008150 feet/sec YDOT = -7328
538557 meter/sec
ZDOT = 6001
368853 ZDOT = 1822
629787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7492550
33 X = 2283729
34
Y = 12758721
87 feet Y = 3888858
43 meter
Z = 16634621
41 Z = 5070232
60
XDOT = -22727
083028 XDOT = -6927
214907
YDOT = 5555
379254 feet/sec YDOT = 1693
279597 meter/sec
ZDOT = 5974
720692 ZDOT = 1821
094867
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
36757841
00016717 00000-0 10270-3 0 9114
2 25544 51
6494 90
8409 0004353 5
6448 354
4752 15
50459021 6528
Satellite: ISS
Catalog Number: 25544
Epoch time: 13244
36757841 = yrday
fracday
Element set: 911
Inclination: 51
6494 deg
RA of node: 90
8409 deg
Eccentricity:
0004353
Arg of perigee: 5
6448 deg
Mean anomaly: 354
4752 deg
Mean motion: 15
50459021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 306
Coasting Arc #13 (Orbit 666)
---------------------------------------
Vector Time (GMT): 2013/245/07:35:07
282
Vector Time (MET): N/A
Weight (LBS) : 957369
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3957712
95 A = 6788565
32 meter
Y = -1787184
99 meter E =
0016062
Z = -5231788
26 I = 51
98670
XDOT = 1612
594690 Wp = 64
86879
YDOT = 7366
190469 meter/sec RA = 85
35368 deg
ZDOT = -1292
889527 TA = 192
72525
MA = 192
76585
Ha = 227
592 n
mi
Hp = 220
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12984622
53 X = 4002817
76
Y = -5863467
80 feet Y = -1742675
48 meter
Z = -17164659
65 Z = -5212452
64
XDOT = 5290
664992 XDOT = 1536
384906
YDOT = 24167
291565 feet/sec YDOT = 7383
797328 meter/sec
ZDOT = -4241
763541 ZDOT = -1285
241390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6891613
86 X = -2100563
91
Y = -12580705
07 feet Y = -3834598
90 meter
Z = -17083258
95 Z = -5206977
33
XDOT = 22747
700946 XDOT = 6933
499248
YDOT = -6727
593943 feet/sec YDOT = -2050
570634 meter/sec
ZDOT = -4210
676401 ZDOT = -1283
414167
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
33440207
00016717 00000-0 10270-3 0 9128
2 25544 51
6500 86
0481 0004491 9
8256 350
2981 15
50474214 6674
Satellite: ISS
Catalog Number: 25544
Epoch time: 13245
33440207 = yrday
fracday
Element set: 912
Inclination: 51
6500 deg
RA of node: 86
0481 deg
Eccentricity:
0004491
Arg of perigee: 9
8256 deg
Mean anomaly: 350
2981 deg
Mean motion: 15
50474214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 667
Checksum: 286
Coasting Arc #14 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2013/246/07:35:07
282
Vector Time (MET): N/A
Weight (LBS) : 957369
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3952306
87 A = 6788093
69 meter
Y = 1506773
62 meter E =
0004680
Z = 5305708
84 I = 51
98163
XDOT = -1835
851429 Wp = 50
99882
YDOT = -7406
209818 meter/sec RA = 80
41571 deg
ZDOT = 738
171987 TA = 31
99474
MA = 31
96634
Ha = 227
709 n
mi
Hp = 219
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12966886
05 X = -3994635
55
Y = 4943483
02 feet Y = 1462340
19 meter
Z = 17407181
23 Z = 5286406
21
XDOT = -6023
134608 XDOT = -1756
482918
YDOT = -24298
588643 feet/sec YDOT = -7426
295638 meter/sec
ZDOT = 2421
824105 ZDOT = 729
447110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6189794
26 X = 1886649
29
Y = 12533389
40 feet Y = 3820177
09 meter
Z = 17325954
91 Z = 5280951
06
XDOT = -22684
143160 XDOT = -6914
126835
YDOT = 7915
277699 feet/sec YDOT = 2412
576643 meter/sec
ZDOT = 2386
228795 ZDOT = 727
322537
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
36566633
00016717 00000-0 10270-3 0 9135
2 25544 51
6496 80
9356 0004456 11
7123 348
4131 15
50502634 6830
Satellite: ISS
Catalog Number: 25544
Epoch time: 13246
36566633 = yrday
fracday
Element set: 913
Inclination: 51
6496 deg
RA of node: 80
9356 deg
Eccentricity:
0004456
Arg of perigee: 11
7123 deg
Mean anomaly: 348
4131 deg
Mean motion: 15
50502634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 683
Checksum: 299
Coasting Arc #15 (Orbit 697)
---------------------------------------
Vector Time (GMT): 2013/247/07:35:07
282
Vector Time (MET): N/A
Weight (LBS) : 957369
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4002442
76 A = 6787913
57 meter
Y = -1243153
14 meter E =
0016720
Z = -5353483
64 I = 51
97544
XDOT = 2049
811516 Wp = 73
40826
YDOT = 7368
888689 meter/sec RA = 75
47699 deg
ZDOT = -174
464451 TA = 194
90821
MA = 194
95756
Ha = 227
668 n
mi
Hp = 219
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13131373
90 X = 4042051
98
Y = -4078586
43 feet Y = -1198174
37 meter
Z = -17563922
70 Z = -5333944
02
XDOT = 6725
103400 XDOT = 1968
106135
YDOT = 24176
143993 feet/sec YDOT = 7391
354124 meter/sec
ZDOT = -572
389931 ZDOT = -164
705978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5564111
95 X = -1695941
32
Y = -12688134
34 feet Y = -3867343
35 meter
Z = -17481737
14 Z = -5328433
48
XDOT = 22325
155358 XDOT = 6804
707353
YDOT = -9037
589399 feet/sec YDOT = -2754
657249 meter/sec
ZDOT = -532
457513 ZDOT = -162
293050
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
33246602
00016717 00000-0 10270-3 0 9145
2 25544 51
6500 76
1426 0004574 15
2826 344
8463 15
50512827 6980
Satellite: ISS
Catalog Number: 25544
Epoch time: 13247
33246602 = yrday
fracday
Element set: 914
Inclination: 51
6500 deg
RA of node: 76
1426 deg
Eccentricity:
0004574
Arg of perigee: 15
2826 deg
Mean anomaly: 344
8463 deg
Mean motion: 15
50512827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 698
Checksum: 299
Coasting Arc #16 (Orbit 713)
---------------------------------------
Vector Time (GMT): 2013/248/07:35:07
282
Vector Time (MET): N/A
Weight (LBS) : 957369
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4086388
61 A = 6787846
27 meter
Y = 954648
11 meter E =
0006485
Z = 5332235
43 I = 51
96685
XDOT = -2247
941829 Wp = 36
47668
YDOT = -7317
417048 meter/sec RA = 70
53729 deg
ZDOT = -407
332210 TA = 57
42284
MA = 57
36023
Ha = 227
771 n
mi
Hp = 219
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13406786
79 X = -4122662
33
Y = 3132047
61 feet Y = 908749
32 meter
Z = 17494210
74 Z = 5312296
08
XDOT = -7375
137235 XDOT = -2163
971105
YDOT = -24007
273779 feet/sec YDOT = -7342
085501 meter/sec
ZDOT = -1336
391765 ZDOT = -418
047602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4879246
98 X = 1487194
48
Y = 12987317
01 feet Y = 3958534
22 meter
Z = 17410387
98 Z = 5306686
26
XDOT = -21886
476983 XDOT = -6670
998184
YDOT = 10096
591209 feet/sec YDOT = 3077
441000 meter/sec
ZDOT = -1380
340013 ZDOT = -420
727636
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
36370435
00016717 00000-0 10270-3 0 9152
2 25544 51
6499 71
0297 0004564 17
3029 342
8276 15
50548231 7141
Satellite: ISS
Catalog Number: 25544
Epoch time: 13248
36370435 = yrday
fracday
Element set: 915
Inclination: 51
6499 deg
RA of node: 71
0297 deg
Eccentricity:
0004564
Arg of perigee: 17
3029 deg
Mean anomaly: 342
8276 deg
Mean motion: 15
50548231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 714
Checksum: 307
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