[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 4th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 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
311/10:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 221
1
314/23:26:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
9
000/00:00:00
000 0
0 0
0 220
9
Coasting Arc #1 (Orbit 1601)
---------------------------------------
Vector Time (GMT): 2013/305/13:29:29
839
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4729709
88 A = 6792972
01 meter
Y = -1305386
24 meter E =
0009306
Z = 4692391
08 I = 51
82561
XDOT = 4394
481568 Wp = 114
52363
YDOT = -5586
882827 meter/sec RA = 146
67553 deg
ZDOT = 2866
969774 TA = 307
02095
MA = 307
10606
Ha = 228
474 n
mi
Hp = 221
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15517420
85 X = -4737556
22
Y = -4282763
24 feet Y = -1358320
38 meter
Z = 15394983
87 Z = 4669395
00
XDOT = 14417
590447 XDOT = 4442
701370
YDOT = -18329
668069 feet/sec YDOT = -5537
471106 meter/sec
ZDOT = 9406
068813 ZDOT = 2888
435901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10995724
45 X = 3351496
81
Y = -11882220
42 feet Y = -3621700
78 meter
Z = 15298523
49 Z = 4662989
96
XDOT = 8781
438984 XDOT = 2676
582602
YDOT = 20388
806479 feet/sec YDOT = 6214
508215 meter/sec
ZDOT = 9497
001267 ZDOT = 2894
685986
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
61569130
00016717 00000-0 10270-3 0 9000
2 25544 51
6449 147
4440 0001165 104
2981 255
8299 15
49727101 16029
Satellite: ISS
Catalog Number: 25544
Epoch time: 13305
61569130 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 147
4440 deg
Eccentricity:
0001165
Arg of perigee: 104
2981 deg
Mean anomaly: 255
8299 deg
Mean motion: 15
49727101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1602
Checksum: 293
Coasting Arc #2 (Orbit 1616)
---------------------------------------
Vector Time (GMT): 2013/306/13:29:29
839
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4651718
59 A = 6792344
16 meter
Y = 1157257
44 meter E =
0012401
Z = -4823949
78 I = 51
84898
XDOT = -4154
075503 Wp = 75
69547
YDOT = 5876
390544 meter/sec RA = 141
73563 deg
ZDOT = -2598
642097 TA = 168
73042
MA = 168
70263
Ha = 228
352 n
mi
Hp = 221
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15261543
94 X = 4661866
30
Y = 3796776
38 feet Y = 1209332
39 meter
Z = -15826606
88 Z = -4801326
89
XDOT = -13628
856636 XDOT = -4206
853975
YDOT = 19279
496534 feet/sec YDOT = 5829
641783 meter/sec
ZDOT = -8525
728664 ZDOT = -2618
951348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10241782
89 X = -3121695
42
Y = 12059499
67 feet Y = 3675735
50 meter
Z = -15731690
01 Z = -4795019
12
XDOT = -10330
974414 XDOT = -3148
881001
YDOT = -19996
744241 feet/sec YDOT = -6095
007645 meter/sec
ZDOT = -8611
854930 ZDOT = -2624
893383
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
58294844
00016717 00000-0 10270-3 0 9015
2 25544 51
6447 142
6538 0001378 108
1801 251
9500 15
49774090 16179
Satellite: ISS
Catalog Number: 25544
Epoch time: 13306
58294844 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 142
6538 deg
Eccentricity:
0001378
Arg of perigee: 108
1801 deg
Mean anomaly: 251
9500 deg
Mean motion: 15
49774090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1617
Checksum: 308
Coasting Arc #3 (Orbit 1632)
---------------------------------------
Vector Time (GMT): 2013/307/13:29:29
839
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4564061
64 A = 6791883
17 meter
Y = -1013741
15 meter E =
0008015
Z = 4922056
55 I = 51
87051
XDOT = 3896
345836 Wp = 120
00511
YDOT = -6173
516247 meter/sec RA = 136
79615 deg
ZDOT = 2334
716006 TA = 307
17512
MA = 307
24827
Ha = 228
404 n
mi
Hp = 221
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14973955
50 X = -4576297
30
Y = -3325922
41 feet Y = -1064847
66 meter
Z = 16148479
50 Z = 4899854
37
XDOT = 12783
286863 XDOT = 3953
748097
YDOT = -20254
318396 feet/sec YDOT = -6129
623805 meter/sec
ZDOT = 7659
829416 ZDOT = 2353
784305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9484894
86 X = 2890995
95
Y = -12178605
37 feet Y = -3712038
92 meter
Z = 16055305
48 Z = 4893657
11
XDOT = 11918
918973 XDOT = 3632
886503
YDOT = 19516
855430 feet/sec YDOT = 5948
737535 meter/sec
ZDOT = 7740
799967 ZDOT = 2359
395830
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 13307
61467314
00016717 00000-0 10270-3 0 9025
2 25544 51
6441 137
5431 0001228 112
5420 247
5860 15
49780357 16339
Satellite: ISS
Catalog Number: 25544
Epoch time: 13307
61467314 = yrday
fracday
Element set: 902
Inclination: 51
6441 deg
RA of node: 137
5431 deg
Eccentricity:
0001228
Arg of perigee: 112
5420 deg
Mean anomaly: 247
5860 deg
Mean motion: 15
49780357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1633
Checksum: 288
Coasting Arc #4 (Orbit 1647)
---------------------------------------
Vector Time (GMT): 2013/308/13:29:29
839
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4477242
19 A = 6791319
28 meter
Y = 921150
98 meter E =
0013762
Z = -5035214
05 I = 51
89172
XDOT = -3612
809547 Wp = 78
87124
YDOT = 6428
454528 meter/sec RA = 131
85895 deg
ZDOT = -2038
569421 TA = 171
34677
MA = 171
32302
Ha = 228
268 n
mi
Hp = 221
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14689114
79 X = 4491069
35
Y = 3022148
90 feet Y = 971295
64 meter
Z = -16519731
14 Z = -5013429
78
XDOT = -11853
049695 XDOT = -3674
522314
YDOT = 21090
730080 feet/sec YDOT = 6387
708726 meter/sec
ZDOT = -6688
219886 ZDOT = -2056
270587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8880415
47 X = -2706750
63
Y = 12208782
89 feet Y = 3721237
03 meter
Z = -16428293
75 Z = -5007343
93
XDOT = -13406
761762 XDOT = -4086
380985
YDOT = -18843
342308 feet/sec YDOT = -5743
450735 meter/sec
ZDOT = -6763
500563 ZDOT = -2061
514972
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 13308
58189953
00016717 00000-0 10270-3 0 9033
2 25544 51
6450 132
7531 0001426 114
5132 245
6167 15
49825954 16487
Satellite: ISS
Catalog Number: 25544
Epoch time: 13308
58189953 = yrday
fracday
Element set: 903
Inclination: 51
6450 deg
RA of node: 132
7531 deg
Eccentricity:
0001426
Arg of perigee: 114
5132 deg
Mean anomaly: 245
6167 deg
Mean motion: 15
49825954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1648
Checksum: 314
Coasting Arc #5 (Orbit 1663)
---------------------------------------
Vector Time (GMT): 2013/309/13:29:29
839
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4385329
89 A = 6790909
24 meter
Y = -835945
73 meter E =
0006587
Z = 5113513
53 I = 51
91000
XDOT = 3314
588544 Wp = 123
85153
YDOT = -6687
037436 meter/sec RA = 126
92140 deg
ZDOT = 1744
213882 TA = 309
31253
MA = 309
37091
Ha = 228
316 n
mi
Hp = 221
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14387565
26 X = -4400496
96
Y = -2742604
12 feet Y = -885070
15 meter
Z = 16776619
18 Z = 5092172
57
XDOT = 10874
634330 XDOT = 3380
644976
YDOT = -21939
099201 feet/sec YDOT = -6649
602278 meter/sec
ZDOT = 5722
486488 ZDOT = 1760
476653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8293102
19 X = 2527737
55
Y = -12196167
89 feet Y = -3717391
97 meter
Z = 16687025
12 Z = 5086205
26
XDOT = 14906
682429 XDOT = 4543
556804
YDOT = 18083
997025 feet/sec YDOT = 5512
002293 meter/sec
ZDOT = 5791
778438 ZDOT = 1765
334068
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 13309
61359114
00016717 00000-0 10270-3 0 9047
2 25544 51
6446 127
6420 0001263 119
2052 240
9225 15
49835129 16640
Satellite: ISS
Catalog Number: 25544
Epoch time: 13309
61359114 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 127
6420 deg
Eccentricity:
0001263
Arg of perigee: 119
2052 deg
Mean anomaly: 240
9225 deg
Mean motion: 15
49835129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1664
Checksum: 291
Coasting Arc #6 (Orbit 1678)
---------------------------------------
Vector Time (GMT): 2013/310/13:29:29
839
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4306116
47 A = 6790449
22 meter
Y = 798302
55 meter E =
0014851
Z = -5202543
79 I = 51
92808
XDOT = -2993
658424 Wp = 82
82257
YDOT = 6895
261876 meter/sec RA = 121
98677 deg
ZDOT = -1421
467935 TA = 173
53515
MA = 173
51596
Ha = 228
156 n
mi
Hp = 221
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14127678
71 X = 4322142
74
Y = 2619102
86 feet Y = 846546
00 meter
Z = -17068713
22 Z = -5181585
65
XDOT = -9821
713990 XDOT = -3063
635007
YDOT = 22622
250249 feet/sec YDOT = 6861
393652 meter/sec
ZDOT = -4663
608709 ZDOT = -1436
181005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7869147
13 X = -2398516
04
Y = 12145939
28 feet Y = 3702082
29 meter
Z = -16980714
32 Z = -5175721
73
XDOT = -16261
330518 XDOT = -4956
453542
YDOT = -17135
543492 feet/sec YDOT = -5222
913656 meter/sec
ZDOT = -4726
435360 ZDOT = -1440
617498
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 13310
58078641
00016717 00000-0 10270-3 0 9059
2 25544 51
6461 122
8526 0001400 119
9641 240
1648 15
49877488 16796
Satellite: ISS
Catalog Number: 25544
Epoch time: 13310
58078641 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 122
8526 deg
Eccentricity:
0001400
Arg of perigee: 119
9641 deg
Mean anomaly: 240
1648 deg
Mean motion: 15
49877488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1679
Checksum: 319
Coasting Arc #7 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2013/311/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2303798
59 A = 6791315
53 meter
Y = -3999949
40 meter E =
0006848
Z = 4977164
87 I = 51
94469
XDOT = 4835
292194 Wp = 63
91291
YDOT = -5526
055838 meter/sec RA = 117
63554 deg
ZDOT = -2197
668872 TA = 47
47047
MA = 47
41266
Ha = 228
083 n
mi
Hp = 221
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7558394
31 X = -2283077
20
Y = -13123193
55 feet Y = -4025596
18 meter
Z = 16329281
06 Z = 4966023
26
XDOT = 15863
819533 XDOT = 4907
402270
YDOT = -18130
104455 feet/sec YDOT = -5471
581287 meter/sec
ZDOT = -7210
199711 ZDOT = -2174
003996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12330452
77 X = 3758322
00
Y = 8877875
19 feet Y = 2705976
36 meter
Z = 16283004
03 Z = 4963059
63
XDOT = -6522
375448 XDOT = -1988
020037
YDOT = 22131
092525 feet/sec YDOT = 6745
557002 meter/sec
ZDOT = -7109
913232 ZDOT = -2167
101553
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 13311
48348671
00016717 00000-0 10270-3 0 9063
2 25544 51
6460 118
3832 0000891 113
9716 246
1528 15
49874963 16939
Satellite: ISS
Catalog Number: 25544
Epoch time: 13311
48348671 = yrday
fracday
Element set: 906
Inclination: 51
6460 deg
RA of node: 118
3832 deg
Eccentricity:
0000891
Arg of perigee: 113
9716 deg
Mean anomaly: 246
1528 deg
Mean motion: 15
49874963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 326
Coasting Arc #8 (Orbit 1707)
---------------------------------------
Vector Time (GMT): 2013/312/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2423113
13 A = 6791694
57 meter
Y = 4081144
80 meter E =
0012673
Z = -4869930
58 I = 51
95920
XDOT = -4495
375821 Wp = 108
52065
YDOT = 5660
512985 meter/sec RA = 112
70085 deg
ZDOT = 2508
362409 TA = 186
07051
MA = 186
08588
Ha = 227
987 n
mi
Hp = 221
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7949846
23 X = 2400953
92
Y = 13389582
68 feet Y = 4108117
75 meter
Z = -15977462
54 Z = -4858212
92
XDOT = -14748
608336 XDOT = -4570
523936
YDOT = 18571
236828 feet/sec YDOT = 5609
822625 meter/sec
ZDOT = 8229
535464 ZDOT = 2486
341504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12946667
34 X = -3946144
21
Y = -8741750
66 feet Y = -2664485
60 meter
Z = -15928775
50 Z = -4855090
77
XDOT = 4943
619276 XDOT = 1506
815155
YDOT = -22138
214282 feet/sec YDOT = -6747
727713 meter/sec
ZDOT = 8136
124907 ZDOT = 2479
890872
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 13312
45065301
00016717 00000-0 10270-3 0 9078
2 25544 51
6454 113
5914 0001032 115
4765 244
6492 15
49912688 17086
Satellite: ISS
Catalog Number: 25544
Epoch time: 13312
45065301 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 113
5914 deg
Eccentricity:
0001032
Arg of perigee: 115
4765 deg
Mean anomaly: 244
6492 deg
Mean motion: 15
49912688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1708
Checksum: 298
Coasting Arc #9 (Orbit 1723)
---------------------------------------
Vector Time (GMT): 2013/313/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2540255
58 A = 6792247
01 meter
Y = -4166635
53 meter E =
0008509
Z = 4719063
09 I = 51
97227
XDOT = 4177
205659 Wp = 68
84414
YDOT = -5766
907996 meter/sec RA = 107
76846 deg
ZDOT = -2836
141985 TA = 49
21008
MA = 49
13629
Ha = 228
020 n
mi
Hp = 220
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8334171
85 X = -2516398
75
Y = -13670064
08 feet Y = -4194908
88 meter
Z = 15482490
46 Z = 4706780
57
XDOT = 13704
742976 XDOT = 4255
159411
YDOT = -18920
301823 feet/sec YDOT = -5719
759968 meter/sec
ZDOT = -9304
927771 ZDOT = -2815
659887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13560670
25 X = 4133292
29
Y = 8603222
00 feet Y = 2622262
06 meter
Z = 15431441
18 Z = 4703503
27
XDOT = -3470
466519 XDOT = -1057
798195
YDOT = 22046
256246 feet/sec YDOT = 6719
698904 meter/sec
ZDOT = -9217
958528 ZDOT = -2809
633759
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 13313
48228008
00016717 00000-0 10270-3 0 9088
2 25544 51
6455 108
4816 0000941 119
2765 240
8480 15
49919301 17243
Satellite: ISS
Catalog Number: 25544
Epoch time: 13313
48228008 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 108
4816 deg
Eccentricity:
0000941
Arg of perigee: 119
2765 deg
Mean anomaly: 240
8480 deg
Mean motion: 15
49919301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1724
Checksum: 305
Coasting Arc #10 (Orbit 1738)
---------------------------------------
Vector Time (GMT): 2013/314/10:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2697214
88 A = 6792734
36 meter
Y = 4250249
85 meter E =
0010901
Z = -4571733
30 I = 51
98287
XDOT = -3846
713012 Wp = 111
35937
YDOT = 5820
217900 meter/sec RA = 102
83567 deg
ZDOT = 3143
640802 TA = 190
06000
MA = 190
08184
Ha = 227
923 n
mi
Hp = 220
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8849130
18 X = 2671695
69
Y = 13944389
28 feet Y = 4280269
05 meter
Z = -14999125
01 Z = -4558692
39
XDOT = -12620
449514 XDOT = -3926
781211
YDOT = 19095
203083 feet/sec YDOT = 5776
753882 meter/sec
ZDOT = 10313
782158 ZDOT = 3124
758997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14287340
83 X = -4354781
49
Y = -8381449
40 feet Y = -2554665
78 meter
Z = -14944900
34 Z = -4555205
62
XDOT = 2049
446058 XDOT = 624
671159
YDOT = -21728
145744 feet/sec YDOT = -6622
738823 meter/sec
ZDOT = 10233
523120 ZDOT = 3119
177847
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 13314
44941480
00016717 00000-0 10270-3 0 9092
2 25544 51
6456 103
6900 0001103 120
0933 240
0327 15
49961904 17397
Satellite: ISS
Catalog Number: 25544
Epoch time: 13314
44941480 = yrday
fracday
Element set: 909
Inclination: 51
6456 deg
RA of node: 103
6900 deg
Eccentricity:
0001103
Arg of perigee: 120
0933 deg
Mean anomaly: 240
0327 deg
Mean motion: 15
49961904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1739
Checksum: 283
Coasting Arc #11 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2013/314/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4207016
48 A = 6791979
90 meter
Y = 2420714
94 meter E =
0008722
Z = 4745996
07 I = 51
98429
XDOT = -929
994422 Wp = 116
25482
YDOT = -7081
938594 meter/sec RA = 100
23261 deg
ZDOT = 2780
089609 TA = 306
29274
MA = 306
37326
Ha = 227
947 n
mi
Hp = 220
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13802547
50 X = -4256827
82
Y = 7941978
13 feet Y = 2373391
02 meter
Z = 15570853
26 Z = 4725437
45
XDOT = -3051
162802 XDOT = -864
238593
YDOT = -23234
706674 feet/sec YDOT = -7091
970645 meter/sec
ZDOT = 9121
028900 ZDOT = 2775
731640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5289458
05 X = -1612226
81
Y = 15109702
51 feet Y = 4605437
33 meter
Z = 15484034
65 Z = 4719533
76
XDOT = -16475
434682 XDOT = -5021
712491
YDOT = -15122
881608 feet/sec YDOT = -4609
454314 meter/sec
ZDOT = 9103
739080 ZDOT = 2774
819671
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 13315
02968757
00016717 00000-0 10270-3 0 9105
2 25544 51
6458 100
8190 0000874 109
6248 250
4996 15
49989065 17480
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
02968757 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 100
8190 deg
Eccentricity:
0000874
Arg of perigee: 109
6248 deg
Mean anomaly: 250
4996 deg
Mean motion: 15
49989065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 339
Coasting Arc #12 (Orbit 1762)
---------------------------------------
Vector Time (GMT): 2013/315/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4069659
07 A = 6791372
21 meter
Y = -2372208
96 meter E =
0012625
Z = -4903917
31 I = 51
98698
XDOT = 1243
202889 Wp = 75
03271
YDOT = 7148
650578 meter/sec RA = 95
29965 deg
ZDOT = -2428
408941 TA = 171
22332
MA = 171
20123
Ha = 227
867 n
mi
Hp = 220
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13351899
83 X = 4119705
43
Y = -7782837
79 feet Y = -2326419
80 meter
Z = -16088967
56 Z = -4884025
33
XDOT = 4078
749636 XDOT = 1174
969433
YDOT = 23453
578012 feet/sec YDOT = 7162
171259 meter/sec
ZDOT = -7967
220936 ZDOT = -2422
535486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4802328
62 X = 1463749
76
Y = -14781061
16 feet Y = -4505267
44 meter
Z = -16004953
65 Z = -4878309
87
XDOT = 17668
884051 XDOT = 5385
475859
YDOT = 14334
583071 feet/sec YDOT = 4369
180920 meter/sec
ZDOT = -7943
577141 ZDOT = -2421
202312
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 13315
99679775
00016717 00000-0 10270-3 0 9111
2 25544 51
6459 96
0272 0000968 105
4432 254
6826 15
49990071 17635
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
99679775 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 96
0272 deg
Eccentricity:
0000968
Arg of perigee: 105
4432 deg
Mean anomaly: 254
6826 deg
Mean motion: 15
49990071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1763
Checksum: 340
Coasting Arc #13 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2013/316/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3939771
46 A = 6790672
50 meter
Y = 2310572
34 meter E =
0006804
Z = 5021308
17 I = 51
98743
XDOT = -1575
706051 Wp = 121
28491
YDOT = -7208
278361 meter/sec RA = 90
36801 deg
ZDOT = 2075
090721 TA = 308
58686
MA = 308
64779
Ha = 227
830 n
mi
Hp = 220
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12925759
37 X = -3989708
58
Y = 7580617
91 feet Y = 2266236
28 meter
Z = 16474108
18 Z = 5002047
38
XDOT = -5169
639274 XDOT = -1505
064796
YDOT = -23649
207222 feet/sec YDOT = -7225
503853 meter/sec
ZDOT = 6808
040423 ZDOT = 2067
607803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4374823
07 X = -1333446
07
Y = 14424834
51 feet Y = 4396689
56 meter
Z = 16392752
55 Z = 4996510
98
XDOT = -18871
429962 XDOT = -5752
011852
YDOT = -13446
336605 feet/sec YDOT = -4098
443397 meter/sec
ZDOT = 6777
648638 ZDOT = 2065
827305
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 13317
02836266
00016717 00000-0 10270-3 0 9128
2 25544 51
6462 90
9173 0000772 106
1478 253
9758 15
50046477 17790
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
02836266 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 90
9173 deg
Eccentricity:
0000772
Arg of perigee: 106
1478 deg
Mean anomaly: 253
9758 deg
Mean motion: 15
50046477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1779
Checksum: 322
Coasting Arc #14 (Orbit 1793)
---------------------------------------
Vector Time (GMT): 2013/317/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3855964
92 A = 6790201
23 meter
Y = -2217620
24 meter E =
0014150
Z = -5143015
61 I = 51
98551
XDOT = 1900
162595 Wp = 78
70071
YDOT = 7216
391250 meter/sec RA = 85
43422 deg
ZDOT = -1688
236453 TA = 175
04174
MA = 175
02771
Ha = 227
732 n
mi
Hp = 220
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12650803
54 X = 3905460
18
Y = -7275656
97 feet Y = -2174223
81 meter
Z = -16873410
79 Z = -5124162
97
XDOT = 6234
129249 XDOT = 1827
527265
YDOT = 23675
824311 feet/sec YDOT = 7237
233898 meter/sec
ZDOT = -5538
833508 ZDOT = -1679
182088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4141273
15 X = 1262260
06
Y = -14089315
32 feet Y = -4294423
31 meter
Z = -16793780
31 Z = -5118744
24
XDOT = 19909
377471 XDOT = 6068
378253
YDOT = 12405
032762 feet/sec YDOT = 3781
053986 meter/sec
ZDOT = -5501
848147 ZDOT = -1676
963315
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 13317
99543981
00016717 00000-0 10270-3 0 9134
2 25544 51
6466 86
1253 0000835 101
3869 258
7375 15
50045576 17945
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
99543981 = yrday
fracday
Element set: 913
Inclination: 51
6466 deg
RA of node: 86
1253 deg
Eccentricity:
0000835
Arg of perigee: 101
3869 deg
Mean anomaly: 258
7375 deg
Mean motion: 15
50045576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1794
Checksum: 333
Coasting Arc #15 (Orbit 1809)
---------------------------------------
Vector Time (GMT): 2013/318/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3785648
09 A = 6789636
79 meter
Y = 2113531
70 meter E =
0004854
Z = 5221931
59 I = 51
98160
XDOT = -2235
271988 Wp = 121
11071
YDOT = -7215
981885 meter/sec RA = 80
50165 deg
ZDOT = 1296
812696 TA = 316
46864
MA = 316
50694
Ha = 227
721 n
mi
Hp = 220
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12420105
28 X = -3834368
07
Y = 6934159
11 feet Y = 2070925
86 meter
Z = 17132321
48 Z = 5203422
41
XDOT = -7333
569516 XDOT = -2160
714873
YDOT = -23674
481250 feet/sec YDOT = -7240
561223 meter/sec
ZDOT = 4254
634828 ZDOT = 1286
134911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3977083
88 X = -1212215
17
Y = 13754887
65 feet Y = 4192489
76 meter
Z = 17054145
73 Z = 5198103
62
XDOT = -20921
454319 XDOT = -6376
859276
YDOT = -11283
680608 feet/sec YDOT = -3439
265849 meter/sec
ZDOT = 4210
837567 ZDOT = 1283
463290
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 13319
02696954
00016717 00000-0 10270-3 0 9140
2 25544 51
6474 81
0154 0000695 101
0416 259
0812 15
50102943 18108
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
02696954 = yrday
fracday
Element set: 914
Inclination: 51
6474 deg
RA of node: 81
0154 deg
Eccentricity:
0000695
Arg of perigee: 101
0416 deg
Mean anomaly: 259
0812 deg
Mean motion: 15
50102943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1810
Checksum: 282
Coasting Arc #16 (Orbit 1824)
---------------------------------------
Vector Time (GMT): 2013/319/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3765748
55 A = 6789355
90 meter
Y = -1993577
79 meter E =
0015185
Z = -5299069
08 I = 51
97508
XDOT = 2552
649529 Wp = 83
83649
YDOT = 7158
351072 meter/sec RA = 75
56674 deg
ZDOT = -879
619757 TA = 177
77439
MA = 177
76763
Ha = 227
612 n
mi
Hp = 220
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12354818
07 X = 3813503
40
Y = -6540609
54 feet Y = -1951199
79 meter
Z = -17385397
25 Z = -5280658
94
XDOT = 8374
834412 XDOT = 2476
686610
YDOT = 23485
403778 feet/sec YDOT = 7186
471689 meter/sec
ZDOT = -2885
891591 ZDOT = -867
403424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3978085
18 X = 1212520
36
Y = -13501600
28 feet Y = -4115287
77 meter
Z = -17307650
57 Z = -5275371
89
XDOT = 21718
949775 XDOT = 6619
935891
YDOT = 10031
764314 feet/sec YDOT = 3057
681763 meter/sec
ZDOT = -2835
631028 ZDOT = -864
300337
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 13319
99401375
00016717 00000-0 10270-3 0 9158
2 25544 51
6479 76
2235 0000746 96
0051 264
1185 15
50100988 18257
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
99401375 = yrday
fracday
Element set: 915
Inclination: 51
6479 deg
RA of node: 76
2235 deg
Eccentricity:
0000746
Arg of perigee: 96
0051 deg
Mean anomaly: 264
1185 deg
Mean motion: 15
50100988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1825
Checksum: 309
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