[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 1st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 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
243/07:18:42
647 1
2 1
6 1
6
N/A 0
1 -0
3 227
7
000/00:03:25
294 -1
1 -0
1 220
3
256/03:26:12
480 1
3 1
5 1
5
N/A 0
6 0
0 227
7
000/00:03:20
961 -0
3 0
0 219
8
Coasting Arc #1 (Orbit 623)
---------------------------------------
Vector Time (GMT): 2013/242/11:22:36
808
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3691292
81 A = 6793773
44 meter
Y = -4294186
07 meter E =
0008547
Z = -3764115
92 I = 51
99950
XDOT = 2430
899914 Wp = 46
43938
YDOT = 5851
524342 meter/sec RA = 99
39375 deg
ZDOT = -4292
050991 TA = 178
18927
MA = 178
18617
Ha = 227
414 n
mi
Hp = 219
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12110540
72 X = 3757321
86
Y = -14088536
98 feet Y = -4252538
63 meter
Z = -12349461
68 Z = -3746023
61
XDOT = 7975
393418 XDOT = 2386
135631
YDOT = 19197
914509 feet/sec YDOT = 5878
457774 meter/sec
ZDOT = -14081
532123 ZDOT = -4280
350941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17737698
24 X = -5406450
42
Y = 5692966
00 feet Y = 1735216
04 meter
Z = -12272957
01 Z = -3740797
30
XDOT = 3515
936227 XDOT = 1071
657362
YDOT = -19295
625647 feet/sec YDOT = -5881
306697 meter/sec
ZDOT = -14033
219214 ZDOT = -4277
325216
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
49831255
00016717 00000-0 10270-3 0 9006
2 25544 51
6489 100
1127 0004739 6
2106 353
9103 15
50577954 6249
Satellite: ISS
Catalog Number: 25544
Epoch time: 13242
49831255 = yrday
fracday
Element set: 900
Inclination: 51
6489 deg
RA of node: 100
1127 deg
Eccentricity:
0004739
Arg of perigee: 6
2106 deg
Mean anomaly: 353
9103 deg
Mean motion: 15
50577954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 624
Checksum: 289
Coasting Arc #2 (Orbit 636)
---------------------------------------
Vector Time (GMT): 2013/243/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1410746
91 A = 6800003
30 meter
Y = -6570540
59 meter E =
0008106
Z = -1025923
70 I = 52
02044
XDOT = 4472
487120 Wp = 120
73388
YDOT = 1879
475655 meter/sec RA = 95
27287 deg
ZDOT = -5925
727593 TA = 70
30395
MA = 70
21652
Ha = 227
689 n
mi
Hp = 220
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4628434
76 X = 1489098
89
Y = -21556891
68 feet Y = -6554326
67 meter
Z = -3365891
41 Z = -1018879
93
XDOT = 14673
514172 XDOT = 4479
923250
YDOT = 6166
258709 feet/sec YDOT = 1929
531189 meter/sec
ZDOT = -19441
363494 ZDOT = -5903
982922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21466116
94 X = -6542872
44
Y = -5052908
43 feet Y = -1540126
49 meter
Z = -3335438
82 Z = -1016641
75
XDOT = 6072
810404 XDOT = 1850
992611
YDOT = -13110
324181 feet/sec YDOT = -3996
026810 meter/sec
ZDOT = -19350
359750 ZDOT = -5897
989652
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
33615027
00016717 00000-0 10270-3 0 9018
2 25544 51
6481 95
9579 0003546 15
2231 344
9026 15
50312512 6372
Satellite: ISS
Catalog Number: 25544
Epoch time: 13243
33615027 = yrday
fracday
Element set: 901
Inclination: 51
6481 deg
RA of node: 95
9579 deg
Eccentricity:
0003546
Arg of perigee: 15
2231 deg
Mean anomaly: 344
9026 deg
Mean motion: 15
50312512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 637
Checksum: 284
Coasting Arc #3 (Orbit 652)
---------------------------------------
Vector Time (GMT): 2013/244/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1169423
76 A = 6799508
88 meter
Y = 6530439
70 meter E =
0016686
Z = 1447592
82 I = 52
02047
XDOT = -4528
270321 Wp = 52
46215
YDOT = -2108
136219 meter/sec RA = 90
34438 deg
ZDOT = 5816
316810 TA = 323
22926
MA = 323
34361
Ha = 227
755 n
mi
Hp = 220
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3836692
14 X = -1249393
58
Y = 21425327
09 feet Y = 6516915
40 meter
Z = 4749320
28 Z = 1441717
37
XDOT = -14856
529924 XDOT = -4532
613852
YDOT = -6916
457411 feet/sec YDOT = -2158
798204 meter/sec
ZDOT = 19082
404232 ZDOT = 5794
308728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21419622
50 X = 6528700
94
Y = 3899573
62 feet Y = 1188590
04 meter
Z = 4723768
43 Z = 1439804
62
XDOT = -6654
029296 XDOT = -2028
148129
YDOT = 13401
958153 feet/sec YDOT = 4084
916845 meter/sec
ZDOT = 18990
323761 ZDOT = 5788
250682
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
36750430
00016717 00000-0 10270-3 0 9021
2 25544 51
6477 90
8462 0003658 18
2184 341
9097 15
50335215 6534
Satellite: ISS
Catalog Number: 25544
Epoch time: 13244
36750430 = yrday
fracday
Element set: 902
Inclination: 51
6477 deg
RA of node: 90
8462 deg
Eccentricity:
0003658
Arg of perigee: 18
2184 deg
Mean anomaly: 341
9097 deg
Mean motion: 15
50335215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 653
Checksum: 299
Coasting Arc #4 (Orbit 667)
---------------------------------------
Vector Time (GMT): 2013/245/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 974464
35 A = 6798779
15 meter
Y = -6453409
05 meter E =
0006099
Z = -1904744
00 I = 52
01824
XDOT = 4608
517173 Wp = 110
05268
YDOT = 2356
336327 meter/sec RA = 85
41541 deg
ZDOT = -5642
393226 TA = 90
76753
MA = 90
69764
Ha = 227
712 n
mi
Hp = 220
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3197061
53 X = 1055807
97
Y = -21172601
86 feet Y = -6442057
28 meter
Z = -6249160
11 Z = -1899812
21
XDOT = 15119
806997 XDOT = 4609
234433
YDOT = 7730
762227 feet/sec YDOT = 2407
875329 meter/sec
ZDOT = -18511
788800 ZDOT = -5620
004188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21221093
41 X = -6468189
27
Y = -2904273
75 feet Y = -885222
64 meter
Z = -6227572
79 Z = -1898164
19
XDOT = 7278
372093 XDOT = 2218
447814
YDOT = -13806
008053 feet/sec YDOT = -4208
071255 meter/sec
ZDOT = -18418
142328 ZDOT = -5613
849782
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
33438254
00016717 00000-0 10270-3 0 9037
2 25544 51
6484 86
0537 0003597 20
7013 339
4282 15
50360556 6683
Satellite: ISS
Catalog Number: 25544
Epoch time: 13245
33438254 = yrday
fracday
Element set: 903
Inclination: 51
6484 deg
RA of node: 86
0537 deg
Eccentricity:
0003597
Arg of perigee: 20
7013 deg
Mean anomaly: 339
4282 deg
Mean motion: 15
50360556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 668
Checksum: 304
Coasting Arc #5 (Orbit 683)
---------------------------------------
Vector Time (GMT): 2013/246/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -773758
64 A = 6797982
35 meter
Y = 6334014
23 meter E =
0016509
Z = 2317844
86 I = 52
01197
XDOT = -4743
166353 Wp = 62
76241
YDOT = -2579
750355 meter/sec RA = 80
48541 deg
ZDOT = 5444
000964 TA = 322
90749
MA = 323
02147
Ha = 227
799 n
mi
Hp = 219
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2538578
20 X = -855788
78
Y = 20780886
59 feet Y = 6324903
11 meter
Z = 7604477
89 Z = 2313886
28
XDOT = -15561
569400 XDOT = -4740
411632
YDOT = -8463
747885 feet/sec YDOT = -2632
775592 meter/sec
ZDOT = 17860
895550 ZDOT = 5420
966305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20855164
05 X = 6356654
00
Y = 1901968
48 feet Y = 579719
99 meter
Z = 7586986
17 Z = 2312513
39
XDOT = -7804
523459 XDOT = -2378
818750
YDOT = 14420
810659 feet/sec YDOT = 4395
463089 meter/sec
ZDOT = 17764
570529 ZDOT = 5414
641097
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
36570369
00016717 00000-0 10270-3 0 9046
2 25544 51
6480 80
9414 0003740 24
1735 335
9591 15
50383989 6842
Satellite: ISS
Catalog Number: 25544
Epoch time: 13246
36570369 = yrday
fracday
Element set: 904
Inclination: 51
6480 deg
RA of node: 80
9414 deg
Eccentricity:
0003740
Arg of perigee: 24
1735 deg
Mean anomaly: 335
9591 deg
Mean motion: 15
50383989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 684
Checksum: 322
Coasting Arc #6 (Orbit 698)
---------------------------------------
Vector Time (GMT): 2013/247/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 630755
23 A = 6796963
84 meter
Y = -6183471
75 meter E =
0005676
Z = -2756489
89 I = 52
00336
XDOT = 4896
203972 Wp = 82
37736
YDOT = 2802
438485 meter/sec RA = 75
55441 deg
ZDOT = -5174
550331 TA = 128
58275
MA = 128
53189
Ha = 227
716 n
mi
Hp = 219
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2069406
93 X = 713243
42
Y = -20286980
81 feet Y = -6175957
31 meter
Z = -9043601
99 Z = -2753224
78
XDOT = 16063
661325 XDOT = 4889
638873
YDOT = 9194
351985 feet/sec YDOT = 2857
153710 meter/sec
ZDOT = -16976
871164 ZDOT = -5150
781522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20368593
54 X = -6208347
31
Y = -1108002
69 feet Y = -337719
22 meter
Z = -9029036
49 Z = -2752050
32
XDOT = 8291
946847 XDOT = 2527
385399
YDOT = -15123
091302 feet/sec YDOT = -4609
518229 meter/sec
ZDOT = -16877
497941 ZDOT = -5144
261373
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
33255039
00016717 00000-0 10270-3 0 9059
2 25544 51
6485 76
1485 0003641 25
4697 334
6633 15
50409642 6997
Satellite: ISS
Catalog Number: 25544
Epoch time: 13247
33255039 = yrday
fracday
Element set: 905
Inclination: 51
6485 deg
RA of node: 76
1485 deg
Eccentricity:
0003641
Arg of perigee: 25
4697 deg
Mean anomaly: 334
6633 deg
Mean motion: 15
50409642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 699
Checksum: 320
Coasting Arc #7 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2013/248/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -497090
98 A = 6795921
38 meter
Y = 5994454
30 meter E =
0015362
Z = 3145002
71 I = 51
99131
XDOT = -5098
312199 Wp = 73
29473
YDOT = -2992
874025 meter/sec RA = 70
62169 deg
ZDOT = 4883
289028 TA = 322
72492
MA = 322
83144
Ha = 227
822 n
mi
Hp = 219
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1630875
91 X = -579362
77
Y = 19666844
82 feet Y = 5988435
87 meter
Z = 10318250
35 Z = 3142387
37
XDOT = -16726
746059 XDOT = -5088
187804
YDOT = -9819
140503 feet/sec YDOT = -3049
829412 meter/sec
ZDOT = 16021
289463 ZDOT = 4858
547043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19737065
19 X = 6015857
47
Y = 369501
90 feet Y = 112624
18 meter
Z = 10306432
85 Z = 3141400
73
XDOT = -8638
168145 XDOT = -2632
913651
YDOT = 16008
350389 feet/sec YDOT = 4879
345199 meter/sec
ZDOT = 15917
862614 ZDOT = 4851
764525
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
36383784
00016717 00000-0 10270-3 0 9063
2 25544 51
6483 71
0357 0003820 29
4530 330
6835 15
50434591 7156
Satellite: ISS
Catalog Number: 25544
Epoch time: 13248
36383784 = yrday
fracday
Element set: 906
Inclination: 51
6483 deg
RA of node: 71
0357 deg
Eccentricity:
0003820
Arg of perigee: 29
4530 deg
Mean anomaly: 330
6835 deg
Mean motion: 15
50434591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 303
Coasting Arc #8 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2013/249/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 429993
74 A = 6794710
13 meter
Y = -5785213
70 meter E =
0007885
Z = -3547212
25 I = 51
97685
XDOT = 5306
102844 Wp = 61
95220
YDOT = 3162
627904 meter/sec RA = 65
68764 deg
ZDOT = -4518
832255 TA = 159
51700
MA = 159
48537
Ha = 227
706 n
mi
Hp = 219
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1410740
61 X = 511884
62
Y = -18980359
92 feet Y = -5779947
80 meter
Z = -11637835
46 Z = -3544923
76
XDOT = 17408
473898 XDOT = 5292
294444
YDOT = 10376
075800 feet/sec YDOT = 3221
886349 meter/sec
ZDOT = -14825
565142 ZDOT = -4493
089747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19038684
93 X = -5802991
17
Y = 123342
86 feet Y = 37594
90 meter
Z = -11627412
80 Z = -3544035
42
XDOT = 8870
870031 XDOT = 2703
841185
YDOT = -16924
618760 feet/sec YDOT = -5158
623798 meter/sec
ZDOT = -14717
969399 ZDOT = -4486
037073
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
33065221
00016717 00000-0 10270-3 0 9075
2 25544 51
6487 66
2427 0003697 29
6516 330
4844 15
50463324 7303
Satellite: ISS
Catalog Number: 25544
Epoch time: 13249
33065221 = yrday
fracday
Element set: 907
Inclination: 51
6487 deg
RA of node: 66
2427 deg
Eccentricity:
0003697
Arg of perigee: 29
6516 deg
Mean anomaly: 330
4844 deg
Mean motion: 15
50463324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 730
Checksum: 302
Coasting Arc #9 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2013/250/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -385846
99 A = 6793545
15 meter
Y = 5545134
41 meter E =
0013332
Z = 3893068
83 I = 51
95975
XDOT = -5553
408099 Wp = 83
29168
YDOT = -3296
435432 meter/sec RA = 60
75142 deg
ZDOT = 4134
309336 TA = 323
46043
MA = 323
55132
Ha = 227
833 n
mi
Hp = 219
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1265902
18 X = -466736
68
Y = 18192698
18 feet Y = 5540367
82 meter
Z = 12772535
52 Z = 3890997
26
XDOT = -18219
842844 XDOT = -5536
217233
YDOT = -10815
076875 feet/sec YDOT = -3358
440538 meter/sec
ZDOT = 13564
007009 ZDOT = 4107
373572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18236253
93 X = 5558410
20
Y = -507973
83 feet Y = -154830
42 meter
Z = 12763049
96 Z = 3890177
63
XDOT = -8937
892165 XDOT = -2724
269532
YDOT = 17976
789451 feet/sec YDOT = 5479
325425 meter/sec
ZDOT = 13451
430576 ZDOT = 4099
996040
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
36190525
00016717 00000-0 10270-3 0 9087
2 25544 51
6488 61
1296 0003896 34
1485 325
9915 15
50484617 7462
Satellite: ISS
Catalog Number: 25544
Epoch time: 13250
36190525 = yrday
fracday
Element set: 908
Inclination: 51
6488 deg
RA of node: 61
1296 deg
Eccentricity:
0003896
Arg of perigee: 34
1485 deg
Mean anomaly: 325
9915 deg
Mean motion: 15
50484617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 746
Checksum: 323
Coasting Arc #10 (Orbit 760)
---------------------------------------
Vector Time (GMT): 2013/251/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 412558
99 A = 6792274
89 meter
Y = -5300390
70 meter E =
0011305
Z = -4239626
77 I = 51
94006
XDOT = 5787
810039 Wp = 58
42462
YDOT = 3392
851162 meter/sec RA = 55
81342 deg
ZDOT = -3680
004534 TA = 173
93492
MA = 173
92122
Ha = 227
691 n
mi
Hp = 219
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1353540
00 X = 492393
48
Y = -17389733
28 feet Y = -5295331
32 meter
Z = -13909536
66 Z = -4237428
07
XDOT = 18988
878080 XDOT = 5767
316786
YDOT = 11131
401451 feet/sec YDOT = 3457
459120 meter/sec
ZDOT = -12073
505689 ZDOT = -3651
937972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17438832
89 X = -5315356
26
Y = 632357
93 feet Y = 192742
70 meter
Z = -13899544
42 Z = -4236581
14
XDOT = 8837
662890 XDOT = 2693
719649
YDOT = -18977
115057 feet/sec YDOT = -5784
224669 meter/sec
ZDOT = -11956
206929 ZDOT = -3644
251872
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
32868650
00016717 00000-0 10270-3 0 9096
2 25544 51
6488 56
3364 0003770 33
9121 326
2271 15
50522050 7619
Satellite: ISS
Catalog Number: 25544
Epoch time: 13251
32868650 = yrday
fracday
Element set: 909
Inclination: 51
6488 deg
RA of node: 56
3364 deg
Eccentricity:
0003770
Arg of perigee: 33
9121 deg
Mean anomaly: 326
2271 deg
Mean motion: 15
50522050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 761
Checksum: 289
Coasting Arc #11 (Orbit 776)
---------------------------------------
Vector Time (GMT): 2013/252/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -472850
96 A = 6791156
40 meter
Y = 5035308
44 meter E =
0010661
Z = 4523239
29 I = 51
91868
XDOT = -6048
621187 Wp = 91
16984
YDOT = -3454
323037 meter/sec RA = 50
87315 deg
ZDOT = 3206
345328 TA = 326
70859
MA = 326
77560
Ha = 227
834 n
mi
Hp = 219
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1551348
28 X = -551094
53
Y = 16520040
82 feet Y = 5029583
70 meter
Z = 14840023
92 Z = 4520751
65
XDOT = -19844
557700 XDOT = -6025
120285
YDOT = -11333
080830 feet/sec YDOT = -3521
830832 meter/sec
ZDOT = 10519
505668 ZDOT = 3177
018951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16591405
05 X = 5057060
26
Y = -612581
68 feet Y = -186714
90 meter
Z = 14828848
99 Z = 4519833
17
XDOT = -8571
795667 XDOT = -2612
683319
YDOT = 20052
708100 feet/sec YDOT = 6112
065429 meter/sec
ZDOT = 10396
938678 ZDOT = 3168
986909
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
35990429
00016717 00000-0 10270-3 0 9102
2 25544 51
6491 51
2234 0003952 38
7080 321
4354 15
50534104 7771
Satellite: ISS
Catalog Number: 25544
Epoch time: 13252
35990429 = yrday
fracday
Element set: 910
Inclination: 51
6491 deg
RA of node: 51
2234 deg
Eccentricity:
0003952
Arg of perigee: 38
7080 deg
Mean anomaly: 321
4354 deg
Mean motion: 15
50534104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 777
Checksum: 287
Coasting Arc #12 (Orbit 791)
---------------------------------------
Vector Time (GMT): 2013/253/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 601954
83 A = 6789999
66 meter
Y = -4784281
86 meter E =
0014628
Z = -4794514
15 I = 51
89449
XDOT = 6274
111642 Wp = 63
02813
YDOT = 3467
814051 meter/sec RA = 45
93035 deg
ZDOT = -2672
522886 TA = 180
61594
MA = 180
61774
Ha = 227
681 n
mi
Hp = 219
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1974917
41 X = 678699
58
Y = -15696462
78 feet Y = -4777121
72 meter
Z = -15730033
29 Z = -4791403
07
XDOT = 20584
355780 XDOT = 6247
849955
YDOT = 11377
342688 feet/sec YDOT = 3537
828088 meter/sec
ZDOT = -8768
119706 ZDOT = -2642
107704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15830061
47 X = -4825002
74
Y = 348109
37 feet Y = 106103
74 meter
Z = -15716270
66 Z = -4790319
30
XDOT = 8118
103388 XDOT = 2474
397913
YDOT = -20978
901695 feet/sec YDOT = -6394
369237 meter/sec
ZDOT = -8640
994562 ZDOT = -2633
775143
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
32665158
00016717 00000-0 10270-3 0 9119
2 25544 51
6485 46
4299 0003842 38
9168 321
2259 15
50582562 7928
Satellite: ISS
Catalog Number: 25544
Epoch time: 13253
32665158 = yrday
fracday
Element set: 911
Inclination: 51
6485 deg
RA of node: 46
4299 deg
Eccentricity:
0003842
Arg of perigee: 38
9168 deg
Mean anomaly: 321
2259 deg
Mean motion: 15
50582562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 792
Checksum: 321
Coasting Arc #13 (Orbit 807)
---------------------------------------
Vector Time (GMT): 2013/254/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -770931
07 A = 6789109
99 meter
Y = 4524901
73 meter E =
0007839
Z = 4995668
00 I = 51
86972
XDOT = -6510
299363 Wp = 92
93312
YDOT = -3452
625886 meter/sec RA = 40
98544 deg
ZDOT = 2119
343575 TA = 336
47768
MA = 336
51351
Ha = 227
825 n
mi
Hp = 219
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2529301
42 X = -845739
96
Y = 14845478
11 feet Y = 4515862
74 meter
Z = 16389986
87 Z = 4991740
85
XDOT = -21359
249878 XDOT = -6481
502737
YDOT = -11327
512750 feet/sec YDOT = -3525
267035 meter/sec
ZDOT = 6953
226951 ZDOT = 2087
787129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15077869
05 X = 4595734
49
Y = 74373
50 feet Y = 22669
04 meter
Z = 16372830
82 Z = 4990438
83
XDOT = -7526
869255 XDOT = -2294
189749
YDOT = 21913
797501 feet/sec YDOT = 6679
325478 meter/sec
ZDOT = 6821
317668 ZDOT = 2079
137625
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 13254
35783289
00016717 00000-0 10270-3 0 9120
2 25544 51
6488 41
3169 0003971 43
5936 316
5528 15
50585168 8088
Satellite: ISS
Catalog Number: 25544
Epoch time: 13254
35783289 = yrday
fracday
Element set: 912
Inclination: 51
6488 deg
RA of node: 41
3169 deg
Eccentricity:
0003971
Arg of perigee: 43
5936 deg
Mean anomaly: 316
5528 deg
Mean motion: 15
50585168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 808
Checksum: 332
Coasting Arc #14 (Orbit 822)
---------------------------------------
Vector Time (GMT): 2013/255/07:20:25
294
Vector Time (MET): N/A
Weight (LBS) : 957312
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 999195
78 A = 6788256
86 meter
Y = -4299173
83 meter E =
0017080
Z = -5172644
11 I = 51
84222
XDOT = 6688
131461 Wp = 71
06774
YDOT = 3387
064639 meter/sec RA = 36
03718 deg
ZDOT = -1521
891251 TA = 184
26924
MA = 184
28382
Ha = 227
673 n
mi
Hp = 219
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3278201
37 X = 1072323
19
Y = -14104901
02 feet Y = -4287591
59 meter
Z = -16970617
17 Z = -5167612
24
XDOT = 21942
688519 XDOT = 6657
152439
YDOT = 11112
416793 feet/sec YDOT = 3461
682276 meter/sec
ZDOT = -4993
081531 ZDOT = -1489
476251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14489775
01 X = -4416483
42
Y = -692443
26 feet Y = -211056
70 meter
Z = -16948853
24 Z = -5166010
47
XDOT = 6767
077530 XDOT = 2062
605231
YDOT = -22603
968702 feet/sec YDOT = -6889
689660 meter/sec
ZDOT = -4857
564799 ZDOT = -1480
585751
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 13255
32454539
00016717 00000-0 10270-3 0 9132
2 25544 51
6475 36
5227 0003896 44
9136 315
2330 15
50641728 8237
Satellite: ISS
Catalog Number: 25544
Epoch time: 13255
32454539 = yrday
fracday
Element set: 913
Inclination: 51
6475 deg
RA of node: 36
5227 deg
Eccentricity:
0003896
Arg of perigee: 44
9136 deg
Mean anomaly: 315
2330 deg
Mean motion: 15
50641728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 823
Checksum: 303
Coasting Arc #15 (Orbit 835)
---------------------------------------
Vector Time (GMT): 2013/256/03:27:52
961
Vector Time (MET): N/A
Weight (LBS) : 957165
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1106629
12 A = 6788618
12 meter
Y = -4175111
57 meter E =
0016654
Z = -5251879
63 I = 51
82180
XDOT = 6846
692098 Wp = 74
47898
YDOT = 3223
763411 meter/sec RA = 31
88868 deg
ZDOT = -1118
756605 TA = 184
79130
MA = 184
80726
Ha = 227
730 n
mi
Hp = 219
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3630672
98 X = 1178746
08
Y = -13697872
60 feet Y = -4162333
57 meter
Z = -17230576
21 Z = -5246328
35
XDOT = 22462
900583 XDOT = 6815
569020
YDOT = 10576
651612 feet/sec YDOT = 3300
153394 meter/sec
ZDOT = -3670
461301 ZDOT = -1085
571770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6706489
09 X = -2044137
87
Y = -12516410
34 feet Y = -3815001
87 meter
Z = -17206647
93 Z = -5244586
29
XDOT = 22685
447552 XDOT = 6914
524414
YDOT = -7293
872855 feet/sec YDOT = -2223
172446 meter/sec
ZDOT = -3531
692172 ZDOT = -1076
459774
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 13256
16235306
00016717 00000-0 10270-3 0 9145
2 25544 51
6495 32
3693 0003033 40
8245 319
3132 15
50400548 8361
Satellite: ISS
Catalog Number: 25544
Epoch time: 13256
16235306 = yrday
fracday
Element set: 914
Inclination: 51
6495 deg
RA of node: 32
3693 deg
Eccentricity:
0003033
Arg of perigee: 40
8245 deg
Mean anomaly: 319
3132 deg
Mean motion: 15
50400548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 836
Checksum: 280
Coasting Arc #16 (Orbit 851)
---------------------------------------
Vector Time (GMT): 2013/257/03:27:52
961
Vector Time (MET): N/A
Weight (LBS) : 957165
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1301353
09 A = 6788202
92 meter
Y = 4023445
93 meter E =
0004720
Z = 5306133
03 I = 51
79397
XDOT = -7011
762379 Wp = 75
95379
YDOT = -3043
512818 meter/sec RA = 26
93958 deg
ZDOT = 588
796522 TA = 8
44125
MA = 8
43331
Ha = 227
722 n
mi
Hp = 219
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4269531
15 X = -1372023
07
Y = 13200281
91 feet Y = 4008498
53 meter
Z = 17408572
94 Z = 5299639
32
XDOT = -23004
469747 XDOT = -6980
068221
YDOT = -9985
278275 feet/sec YDOT = -3121
745552 meter/sec
ZDOT = 1931
747118 ZDOT = 554
811330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6115474
17 X = 1863996
53
Y = 12491862
31 feet Y = 3807519
63 meter
Z = 17380710
64 Z = 5297640
60
XDOT = -22515
005258 XDOT = -6862
573603
YDOT = 8535
499542 feet/sec YDOT = 2601
620260 meter/sec
ZDOT = 1789
594289 ZDOT = 545
468339
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 13257
19366280
00016717 00000-0 10270-3 0 9156
2 25544 51
6492 27
2571 0002960 42
3176 317
8203 15
50439156 8521
Satellite: ISS
Catalog Number: 25544
Epoch time: 13257
19366280 = yrday
fracday
Element set: 915
Inclination: 51
6492 deg
RA of node: 27
2571 deg
Eccentricity:
0002960
Arg of perigee: 42
3176 deg
Mean anomaly: 317
8203 deg
Mean motion: 15
50439156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 852
Checksum: 301
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