[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 29th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 819 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
243/06:58:08
099 1
3 1
9 1
9
N/A 0
3 -0
1 219
4
000/00:08:16
198 -1
3 -0
2 212
8
245/10:53:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
4
000/00:00:00
000 0
0 0
0 212
8
250/04:11:18
366 0
8 0
9 0
9
N/A 0
5 0
0 218
9
000/00:04:32
733 -0
1 0
0 213
2
Coasting Arc #1 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2015/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2703799
49 A = 6777770
27 meter
Y = 4554883
08 meter E =
0010948
Z = 4220740
94 I = 51
99999
XDOT = -3686
997507 Wp = 101
26665
YDOT = -5624
111184 meter/sec RA = 82
19097 deg
ZDOT = 3697
300868 TA = 310
99631
MA = 311
09095
Ha = 219
246 n
mi
Hp = 212
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8870733
24 X = -2775034
75
Y = 14943842
14 feet Y = 4524249
41 meter
Z = 13847575
27 Z = 4207433
31
XDOT = -12096
448513 XDOT = -3641
793088
YDOT = -18451
808348 feet/sec YDOT = -5665
088604 meter/sec
ZDOT = 12130
252191 ZDOT = 3679
500667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14341094
52 X = 4371165
61
Y = -9897008
94 feet Y = -3016608
33 meter
Z = 13789339
68 Z = 4202990
73
XDOT = 2723
849305 XDOT = 830
229268
YDOT = 20788
929790 feet/sec YDOT = 6336
465800 meter/sec
ZDOT = 12054
477198 ZDOT = 3674
204650
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 15240
55491707
00016717 00000-0 10270-3 0 9007
2 25544 51
6421 82
6979 0001088 59
2471 300
8789 15
55521496 39300
Satellite: ISS
Catalog Number: 25544
Epoch time: 15240
55491707 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 82
6979 deg
Eccentricity:
0001088
Arg of perigee: 59
2471 deg
Mean anomaly: 300
8789 deg
Mean motion: 15
55521496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3930
Checksum: 321
Coasting Arc #2 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2015/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3591657
83 A = 6773855
24 meter
Y = -2494480
91 meter E =
0014838
Z = -5186410
38 I = 51
98068
XDOT = 2756
587358 Wp = 78
13108
YDOT = 6996
379422 meter/sec RA = 77
20580 deg
ZDOT = -1456
583692 TA = 177
90372
MA = 177
89749
Ha = 219
096 n
mi
Hp = 212
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11783654
31 X = 3644478
00
Y = -8183992
47 feet Y = -2454021
78 meter
Z = -17015782
09 Z = -5168834
57
XDOT = 9043
921777 XDOT = 2685
222695
YDOT = 22954
000729 feet/sec YDOT = 7026
806236 meter/sec
ZDOT = -4778
817886 ZDOT = -1443
366942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14167876
26 X = -4318368
68
Y = 2773733
30 feet Y = 845433
91 meter
Z = -16939503
17 Z = -5163160
57
XDOT = 1017
610916 XDOT = 310
167807
YDOT = -23635
538342 feet/sec YDOT = -7204
112087 meter/sec
ZDOT = -4723
070503 ZDOT = -1439
591889
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 15241
51856097
00016717 00000-0 10270-3 0 9012
2 25544 51
6407 77
8824 0001048 67
5177 292
6087 15
55568096 39452
Satellite: ISS
Catalog Number: 25544
Epoch time: 15241
51856097 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 77
8824 deg
Eccentricity:
0001048
Arg of perigee: 67
5177 deg
Mean anomaly: 292
6087 deg
Mean motion: 15
55568096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3945
Checksum: 338
Coasting Arc #3 (Orbit 3960)
---------------------------------------
Vector Time (GMT): 2015/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4266651
50 A = 6773493
53 meter
Y = 155192
56 meter E =
0004670
Z = 5255366
03 I = 51
97183
XDOT = -1543
028052 Wp = 60
06566
YDOT = -7446
328007 meter/sec RA = 72
21283 deg
ZDOT = -1029
887175 TA = 39
76107
MA = 39
72685
Ha = 219
228 n
mi
Hp = 212
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13998200
45 X = -4293598
05
Y = 509161
95 feet Y = 107329
97 meter
Z = 17242014
53 Z = 5234574
28
XDOT = -5062
427992 XDOT = -1454
643989
YDOT = -24430
209996 feet/sec YDOT = -7463
089091 meter/sec
ZDOT = -3378
894932 ZDOT = -1037
167311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13231386
99 X = 4032926
76
Y = 4921924
93 feet Y = 1500202
72 meter
Z = 17152287
89 Z = 5228017
35
XDOT = -4323
690590 XDOT = -1317
860892
YDOT = 23536
838093 feet/sec YDOT = 7174
028251 meter/sec
ZDOT = -3408
940791 ZDOT = -1039
045153
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 15242
54643108
00016717 00000-0 10270-3 0 9024
2 25544 51
6410 72
7464 0001004 70
9888 289
1374 15
55575192 39612
Satellite: ISS
Catalog Number: 25544
Epoch time: 15242
54643108 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 72
7464 deg
Eccentricity:
0001004
Arg of perigee: 70
9888 deg
Mean anomaly: 289
1374 deg
Mean motion: 15
55575192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3961
Checksum: 310
Coasting Arc #4 (Orbit 3972)
---------------------------------------
Vector Time (GMT): 2015/243/07:02:16
198
Vector Time (MET): N/A
Weight (LBS) : 927021
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 978447
94 A = 6779972
98 meter
Y = -5543493
97 meter E =
0006224
Z = -3784685
99 I = 51
98561
XDOT = 5103
156054 Wp = 85
60169
YDOT = 3808
570596 meter/sec RA = 68
30413 deg
ZDOT = -4264
725351 TA = 139
48612
MA = 139
43977
Ha = 219
390 n
mi
Hp = 212
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3210131
02 X = 1058748
32
Y = -18187316
17 feet Y = -5532103
77 meter
Z = -12416948
78 Z = -3779737
24
XDOT = 16742
637973 XDOT = 5080
904659
YDOT = 12495
310355 feet/sec YDOT = 3865
512537 meter/sec
ZDOT = -13991
881073 ZDOT = -4239
989940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17733319
64 X = -5405115
83
Y = -5212271
68 feet Y = -1588700
41 meter
Z = -12394580
51 Z = -3777868
14
XDOT = 13839
488844 XDOT = 4218
276200
YDOT = -14108
415476 feet/sec YDOT = -4300
245037 meter/sec
ZDOT = -13885
871887 ZDOT = -4232
413751
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 15243
31732692
00016717 00000-0 10270-3 0 9038
2 25544 51
6443 68
8967 0000972 157
1697 202
9500 15
55264527 39735
Satellite: ISS
Catalog Number: 25544
Epoch time: 15243
31732692 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 68
8967 deg
Eccentricity:
0000972
Arg of perigee: 157
1697 deg
Mean anomaly: 202
9500 deg
Mean motion: 15
55264527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3973
Checksum: 327
Coasting Arc #5 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2015/244/07:02:16
198
Vector Time (MET): N/A
Weight (LBS) : 927021
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2291117
04 A = 6775678
77 meter
Y = 4036717
44 meter E =
0007359
Z = 4932569
55 I = 51
95885
XDOT = -4792
023286 Wp = 126
18325
YDOT = -5534
739591 meter/sec RA = 63
32531 deg
ZDOT = 2297
073540 TA = 301
43933
MA = 301
51126
Ha = 219
410 n
mi
Hp = 212
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7516788
18 X = -2360046
76
Y = 13243823
62 feet Y = 4010711
81 meter
Z = 16182970
98 Z = 4921271
93
XDOT = -15721
861176 XDOT = -4740
934601
YDOT = -18158
594458 feet/sec YDOT = -5588
041237 meter/sec
ZDOT = 7536
330512 ZDOT = 2273
919657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12508903
02 X = 3812713
64
Y = 8776531
05 feet Y = 2675086
66 meter
Z = 16133485
87 Z = 4917486
49
XDOT = -18858
416127 XDOT = -5748
045235
YDOT = 13166
320266 feet/sec YDOT = 4013
094417 meter/sec
ZDOT = 7437
473637 ZDOT = 2266
941965
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 15244
34540254
00016717 00000-0 10270-3 0 9044
2 25544 51
6443 63
7622 0000959 159
3089 200
8103 15
55287350 39893
Satellite: ISS
Catalog Number: 25544
Epoch time: 15244
34540254 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 63
7622 deg
Eccentricity:
0000959
Arg of perigee: 159
3089 deg
Mean anomaly: 200
8103 deg
Mean motion: 15
55287350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 311
Coasting Arc #6 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2015/245/07:02:16
198
Vector Time (MET): N/A
Weight (LBS) : 927021
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3587559
65 A = 6773856
74 meter
Y = -2150299
31 meter E =
0015093
Z = -5341273
74 I = 51
93857
XDOT = 3989
570832 Wp = 93
28883
YDOT = 6538
193156 meter/sec RA = 58
33468 deg
ZDOT = 46
778986 TA = 177
15990
MA = 177
15132
Ha = 219
194 n
mi
Hp = 212
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11770208
83 X = 3637284
04
Y = -7054787
75 feet Y = -2109903
36 meter
Z = -17523863
97 Z = -5323725
11
XDOT = 13089
143148 XDOT = 3915
935425
YDOT = 21450
764946 feet/sec YDOT = 6582
395447 meter/sec
ZDOT = 153
474364 ZDOT = 65
979996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6176425
31 X = -1882574
43
Y = -12362081
28 feet Y = -3767962
38 meter
Z = -17447761
21 Z = -5318077
62
XDOT = 21441
683875 XDOT = 6535
425245
YDOT = -11048
013259 feet/sec YDOT = -3367
434441 meter/sec
ZDOT = 235
078207 ZDOT = 71
651838
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 15245
30920570
00016717 00000-0 10270-3 0 9055
2 25544 51
6449 58
9487 0000804 167
3338 192
7835 15
55331661 40044
Satellite: ISS
Catalog Number: 25544
Epoch time: 15245
30920570 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 58
9487 deg
Eccentricity:
0000804
Arg of perigee: 167
3338 deg
Mean anomaly: 192
7835 deg
Mean motion: 15
55331661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 313
Coasting Arc #7 (Orbit 4006)
---------------------------------------
Vector Time (GMT): 2015/245/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3405278
41 A = 6773998
87 meter
Y = 2422779
86 meter E =
0002832
Z = 5329002
10 I = 51
93245
XDOT = -4243
322861 Wp = 115
85316
YDOT = -6389
797245 meter/sec RA = 57
53756 deg
ZDOT = 192
257572 TA = 332
31544
MA = 332
33051
Ha = 219
383 n
mi
Hp = 212
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11172173
25 X = -3458003
69
Y = 7948752
83 feet Y = 2384405
52 meter
Z = 17483602
69 Z = 5312331
65
XDOT = -13921
662930 XDOT = -4172
489142
YDOT = -20963
901724 feet/sec YDOT = -6436
852801 meter/sec
ZDOT = 630
766312 ZDOT = 171
817044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13800318
26 X = 4206337
01
Y = 276661
05 feet Y = 84326
29 meter
Z = 17411236
72 Z = 5306944
95
XDOT = -1175
205642 XDOT = -358
202680
YDOT = 24132
700268 feet/sec YDOT = 7355
647042 meter/sec
ZDOT = 543
790108 ZDOT = 165
747225
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 15245
50196456
00016717 00000-0 10270-3 0 9066
2 25544 51
6414 57
9836 0000919 172
5930 187
5237 15
55281402 40074
Satellite: ISS
Catalog Number: 25544
Epoch time: 15245
50196456 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 57
9836 deg
Eccentricity:
0000919
Arg of perigee: 172
5930 deg
Mean anomaly: 187
5237 deg
Mean motion: 15
55281402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4007
Checksum: 314
Coasting Arc #8 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2015/246/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4581326
23 A = 6775386
77 meter
Y = -441424
86 meter E =
0012774
Z = -4983952
61 I = 51
91930
XDOT = 3001
273174 Wp = 109
71614
YDOT = 6707
115579 meter/sec RA = 52
54408 deg
ZDOT = 2165
080969 TA = 181
32497
MA = 181
32835
Ha = 219
144 n
mi
Hp = 212
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15030597
88 X = 4610132
02
Y = -1448244
28 feet Y = -390032
80 meter
Z = -16351550
55 Z = -4961627
43
XDOT = 9846
696765 XDOT = 2915
532375
YDOT = 22004
972373 feet/sec YDOT = 6740
198564 meter/sec
ZDOT = 7103
284020 ZDOT = 2179
451754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13185553
47 X = -4018956
70
Y = -7569694
91 feet Y = -2307243
01 meter
Z = -16255164
98 Z = -4954574
28
XDOT = 4177
890017 XDOT = 1273
420877
YDOT = -22659
209245 feet/sec YDOT = -6906
526978 meter/sec
ZDOT = 7164
003107 ZDOT = 2183
588147
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 15246
46574755
00016717 00000-0 10270-3 0 9075
2 25544 51
6410 53
1689 0000951 175
2725 184
8438 15
55347968 40222
Satellite: ISS
Catalog Number: 25544
Epoch time: 15246
46574755 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 53
1689 deg
Eccentricity:
0000951
Arg of perigee: 175
2725 deg
Mean anomaly: 184
8438 deg
Mean motion: 15
55347968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 331
Coasting Arc #9 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2015/247/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5396261
78 A = 6779605
01 meter
Y = -1455750
31 meter E =
0011272
Z = 3828025
48 I = 51
91379
XDOT = -1290
931335 Wp = 86
90004
YDOT = -6290
559996 meter/sec RA = 47
56093 deg
ZDOT = -4200
786449 TA = 47
21606
MA = 47
12132
Ha = 219
142 n
mi
Hp = 212
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17704270
93 X = -5398177
26
Y = -4776083
71 feet Y = -1516105
31 meter
Z = 12559138
71 Z = 3801806
96
XDOT = -4235
339026 XDOT = -1200
087000
YDOT = -20638
320196 feet/sec YDOT = -6304
488388 meter/sec
ZDOT = -13782
107772 ZDOT = -4206
836450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11989449
07 X = 3654384
08
Y = 13975918
74 feet Y = 4259860
03 meter
Z = 12446323
00 Z = 3793639
25
XDOT = -7201
143396 XDOT = -2194
908507
YDOT = 18506
595372 feet/sec YDOT = 5640
810269 meter/sec
ZDOT = -13807
001460 ZDOT = -4208
374045
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 15247
49376463
00016717 00000-0 10270-3 0 9086
2 25544 51
6413 48
0347 0000886 189
5619 170
5517 15
55370179 40383
Satellite: ISS
Catalog Number: 25544
Epoch time: 15247
49376463 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 48
0347 deg
Eccentricity:
0000886
Arg of perigee: 189
5619 deg
Mean anomaly: 170
5517 deg
Mean motion: 15
55370179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 333
Coasting Arc #10 (Orbit 4052)
---------------------------------------
Vector Time (GMT): 2015/248/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5702224
21 A = 6783850
32 meter
Y = 3025431
99 meter E =
0005913
Z = -2081412
80 I = 51
90614
XDOT = -750
290800 Wp = 45
80618
YDOT = 5228
099990 meter/sec RA = 42
59072 deg
ZDOT = 5557
566070 TA = 291
24294
MA = 291
30609
Ha = 219
046 n
mi
Hp = 212
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18708084
66 X = 5678079
98
Y = 9925957
97 feet Y = 3089062
89 meter
Z = -6828782
14 Z = -2053771
41
XDOT = -2461
583991 XDOT = -835
693410
YDOT = 17152
559022 feet/sec YDOT = 5219
232569 meter/sec
ZDOT = 18233
484481 ZDOT = 5553
713562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10203749
44 X = -3110102
83
Y = -18601261
25 feet Y = -5669664
43 meter
Z = -6710135
34 Z = -2045249
25
XDOT = 10229
775671 XDOT = 3118
035624
YDOT = -12166
084250 feet/sec YDOT = -3708
222480 meter/sec
ZDOT = 18215
858943 ZDOT = 5552
193806
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 15248
45751425
00016717 00000-0 10270-3 0 9099
2 25544 51
6413 43
2203 0000921 181
9631 178
1519 15
55401523 40532
Satellite: ISS
Catalog Number: 25544
Epoch time: 15248
45751425 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 43
2203 deg
Eccentricity:
0000921
Arg of perigee: 181
9631 deg
Mean anomaly: 178
1519 deg
Mean motion: 15
55401523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4053
Checksum: 285
Coasting Arc #11 (Orbit 4068)
---------------------------------------
Vector Time (GMT): 2015/249/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5350038
90 A = 6785418
41 meter
Y = -4163517
59 meter E =
0012306
Z = -39213
62 I = 51
88800
XDOT = 2930
386807 Wp = 137
17254
YDOT = -3719
166040 meter/sec RA = 37
63086 deg
ZDOT = -6035
713446 TA = 43
24868
MA = 43
15212
Ha = 218
835 n
mi
Hp = 212
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17552621
05 X = -5302893
32
Y = -13659834
62 feet Y = -4223081
64 meter
Z = -128653
62 Z = -65088
16
XDOT = 9614
129945 XDOT = 3001
076696
YDOT = -12201
988321 feet/sec YDOT = -3686
001635 meter/sec
ZDOT = -19802
209469 ZDOT = -6021
306360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7509220
69 X = 2288810
47
Y = 20934574
42 feet Y = 6380858
28 meter
Z = -239453
36 Z = -72985
38
XDOT = -13234
282603 XDOT = -4033
809337
YDOT = 4543
874799 feet/sec YDOT = 1384
973039 meter/sec
ZDOT = -19739
344592 ZDOT = -6016
552232
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 15249
48549271
00016717 00000-0 10270-3 0 9109
2 25544 51
6412 38
0854 0000613 194
1062 166
0074 15
55474248 40690
Satellite: ISS
Catalog Number: 25544
Epoch time: 15249
48549271 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 38
0854 deg
Eccentricity:
0000613
Arg of perigee: 194
1062 deg
Mean anomaly: 166
0074 deg
Mean motion: 15
55474248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4069
Checksum: 303
Coasting Arc #12 (Orbit 4079)
---------------------------------------
Vector Time (GMT): 2015/250/04:13:34
733
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2286859
85 A = 6773945
87 meter
Y = -3513556
71 meter E =
0014073
Z = -5332980
50 I = 51
83332
XDOT = 6375
554912 Wp = 91
56949
YDOT = 4245
722458 meter/sec RA = 34
03636 deg
ZDOT = -63
822366 TA = 177
82638
MA = 177
82026
Ha = 218
867 n
mi
Hp = 213
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7502821
04 X = 2351884
75
Y = -11527417
01 feet Y = -3487620
29 meter
Z = -17496655
19 Z = -5321713
31
XDOT = 20917
174909 XDOT = 6327
914394
YDOT = 13929
535624 feet/sec YDOT = 4316
751731 meter/sec
ZDOT = -209
390965 ZDOT = -32
967384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3585224
36 X = -1092776
38
Y = -13343236
91 feet Y = -4067018
61 meter
Z = -17447372
42 Z = -5317959
11
XDOT = 23322
295022 XDOT = 7108
635523
YDOT = -6167
908114 feet/sec YDOT = -1879
978393 meter/sec
ZDOT = -77
128892 ZDOT = -23
508886
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 15250
19221936
00016717 00000-0 10270-3 0 9115
2 25544 51
6450 34
5597 0000979 237
5480 122
5579 15
55300187 40808
Satellite: ISS
Catalog Number: 25544
Epoch time: 15250
19221936 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 34
5597 deg
Eccentricity:
0000979
Arg of perigee: 237
5480 deg
Mean anomaly: 122
5579 deg
Mean motion: 15
55300187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4080
Checksum: 307
Coasting Arc #13 (Orbit 4095)
---------------------------------------
Vector Time (GMT): 2015/251/04:13:34
733
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4120131
75 A = 6775562
81 meter
Y = 2147044
53 meter E =
0005673
Z = 4928921
08 I = 51
81198
XDOT = -5342
411574 Wp = 55
62266
YDOT = -5014
142120 meter/sec RA = 29
03764 deg
ZDOT = -2276
614009 TA = 56
58474
MA = 56
53049
Ha = 218
848 n
mi
Hp = 213
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13517492
61 X = -4167776
91
Y = 7044109
35 feet Y = 2100704
46 meter
Z = 16171000
91 Z = 4908790
61
XDOT = -17527
597026 XDOT = -5274
886339
YDOT = -16450
597505 feet/sec YDOT = -5073
507089 meter/sec
ZDOT = -7469
206067 ZDOT = -2302
401766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3496575
81 X = -1065756
31
Y = 14930845
44 feet Y = 4550921
69 meter
Z = 16083754
72 Z = 4902328
44
XDOT = -22774
388080 XDOT = -6941
633487
YDOT = 2849
038916 feet/sec YDOT = 868
387062 meter/sec
ZDOT = -7579
456343 ZDOT = -2310
218293
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 15251
22027488
00016717 00000-0 10270-3 0 9127
2 25544 51
6448 29
4256 0001040 252
1260 107
9780 15
55349261 40963
Satellite: ISS
Catalog Number: 25544
Epoch time: 15251
22027488 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 29
4256 deg
Eccentricity:
0001040
Arg of perigee: 252
1260 deg
Mean anomaly: 107
9780 deg
Mean motion: 15
55349261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4096
Checksum: 294
Coasting Arc #14 (Orbit 4110)
---------------------------------------
Vector Time (GMT): 2015/252/04:13:34
733
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5589175
83 A = 6779873
58 meter
Y = -753319
30 meter E =
0004876
Z = -3768232
30 I = 51
79858
XDOT = 3580
626334 Wp = 106
15429
YDOT = 5269
424510 meter/sec RA = 24
04708 deg
ZDOT = 4260
732684 TA = 208
85750
MA = 208
88447
Ha = 218
736 n
mi
Hp = 213
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18337191
03 X = 5615488
67
Y = -2471520
00 feet Y = -690670
65 meter
Z = -12362966
87 Z = -3741017
52
XDOT = 11747
461725 XDOT = 3500
739432
YDOT = 17288
138156 feet/sec YDOT = 5309
019119 meter/sec
ZDOT = 13978
781773 ZDOT = 4277
931982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9818637
31 X = 2992720
65
Y = -15774900
48 feet Y = -4808189
66 meter
Z = -12245440
47 Z = -3732410
26
XDOT = 19604
374502 XDOT = 5975
413348
YDOT = 1302
567000 feet/sec YDOT = 397
022422 meter/sec
ZDOT = 14051
934177 ZDOT = 4283
029537
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 15252
18406001
00016717 00000-0 10270-3 0 9136
2 25544 51
6453 24
6119 0001035 258
9882 101
1155 15
55348240 41118
Satellite: ISS
Catalog Number: 25544
Epoch time: 15252
18406001 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 24
6119 deg
Eccentricity:
0001035
Arg of perigee: 258
9882 deg
Mean anomaly: 101
1155 deg
Mean motion: 15
55348240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4111
Checksum: 268
Coasting Arc #15 (Orbit 4126)
---------------------------------------
Vector Time (GMT): 2015/253/04:13:34
733
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6455435
45 A = 6784184
58 meter
Y = -580535
45 meter E =
0013181
Z = 1981884
86 I = 51
78357
XDOT = -1266
051719 Wp = 114
36017
YDOT = -5097
253106 meter/sec RA = 19
07042 deg
ZDOT = -5592
989778 TA = 43
78991
MA = 43
68545
Ha = 218
783 n
mi
Hp = 213
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21179250
18 X = -6458091
13
Y = -1904643
85 feet Y = -652739
02 meter
Z = 6502246
92 Z = 1950519
59
XDOT = -4153
712989 XDOT = -1181
790575
YDOT = -16723
271345 feet/sec YDOT = -5110
940360 meter/sec
ZDOT = -18349
703997 ZDOT = -5598
934766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14716406
61 X = -4485560
73
Y = 15406333
34 feet Y = 4695850
40 meter
Z = 6367086
52 Z = 1940687
97
XDOT = -14470
706436 XDOT = -4410
671322
YDOT = -6195
870091 feet/sec YDOT = -1888
501204 meter/sec
ZDOT = -18374
348018 ZDOT = -5600
501276
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 15253
21207832
00016717 00000-0 10270-3 0 9143
2 25544 51
6453 19
4776 0000950 258
6762 101
4285 15
55349832 41270
Satellite: ISS
Catalog Number: 25544
Epoch time: 15253
21207832 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 19
4776 deg
Eccentricity:
0000950
Arg of perigee: 258
6762 deg
Mean anomaly: 101
4285 deg
Mean motion: 15
55349832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4127
Checksum: 307
Coasting Arc #16 (Orbit 4142)
---------------------------------------
Vector Time (GMT): 2015/254/04:13:34
733
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6554711
58 A = 6785565
19 meter
Y = 1728810
17 meter E =
0011652
Z = 101149
20 I = 51
75894
XDOT = -1303
668845 Wp = 42
38210
YDOT = 4567
255500 meter/sec RA = 14
10156 deg
ZDOT = 6023
792130 TA = 318
70634
MA = 318
79440
Ha = 218
575 n
mi
Hp = 213
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21504959
24 X = 6534401
10
Y = 5671949
38 feet Y = 1801995
72 meter
Z = 331854
32 Z = 132940
84
XDOT = -4277
128755 XDOT = -1383
905128
YDOT = 14984
434054 feet/sec YDOT = 4552
229086 meter/sec
ZDOT = 19763
097539 ZDOT = 6017
263815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17607515
79 X = 5366770
81
Y = -13583084
74 feet Y = -4140124
23 meter
Z = 468620
87 Z = 142835
64
XDOT = 8201
839126 XDOT = 2499
920566
YDOT = 11344
393575 feet/sec YDOT = 3457
771162 meter/sec
ZDOT = 19734
051910 ZDOT = 6014
939022
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 15254
24007319
00016717 00000-0 10270-3 0 9156
2 25544 51
6457 14
3426 0001121 274
1239 85
9786 15
55421962 41438
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
24007319 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 14
3426 deg
Eccentricity:
0001121
Arg of perigee: 274
1239 deg
Mean anomaly: 85
9786 deg
Mean motion: 15
55421962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4143
Checksum: 298
Coasting Arc #17 (Orbit 4157)
---------------------------------------
Vector Time (GMT): 2015/255/04:13:34
733
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5818307
99 A = 6783473
81 meter
Y = -2697553
07 meter E =
0005141
Z = -2204960
17 I = 51
72078
XDOT = 3818
701121 Wp = 145
16654
YDOT = -3766
032719 meter/sec RA = 9
13077 deg
ZDOT = -5479
593087 TA = 59
30134
MA = 59
25070
Ha = 218
505 n
mi
Hp = 213
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19088936
99 X = -5777000
09
Y = -8850239
73 feet Y = -2762386
54 meter
Z = -7234121
29 Z = -2233123
46
XDOT = 12528
546984 XDOT = 3887
147589
YDOT = -12355
750390 feet/sec YDOT = -3722
947487 meter/sec
ZDOT = -17977
667608 ZDOT = -5460
876003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18457328
21 X = -5625793
64
Y = 10013848
03 feet Y = 3052220
88 meter
Z = -7355042
67 Z = -2241817
01
XDOT = -1655
620822 XDOT = -504
633227
YDOT = -16171
451905 feet/sec YDOT = -4929
058541 meter/sec
ZDOT = -17896
220031 ZDOT = -5454
767865
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 15255
20380240
00016717 00000-0 10270-3 0 9161
2 25544 51
6457 9
5293 0001239 275
9846 84
1166 15
55408504 41585
Satellite: ISS
Catalog Number: 25544
Epoch time: 15255
20380240 = yrday
fracday
Element set: 916
Inclination: 51
6457 deg
RA of node: 9
5293 deg
Eccentricity:
0001239
Arg of perigee: 275
9846 deg
Mean anomaly: 84
1166 deg
Mean motion: 15
55408504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4158
Checksum: 310
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