[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 1st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 905 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
There are no maneuvers
Coasting Arc #1 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2015/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5157656
13 A = 6780312
94 meter
Y = 1292935
56 meter E =
0016407
Z = 4194849
64 I = 51
91980
XDOT = 1394
132134 Wp = 98
98356
YDOT = -6566
183453 meter/sec RA = 127
74597 deg
ZDOT = 3723
066569 TA = 312
90925
MA = 313
04684
Ha = 222
515 n
mi
Hp = 211
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16921444
01 X = -5192108
19
Y = 4241914
58 feet Y = 1235066
69 meter
Z = 13762630
06 Z = 4169710
48
XDOT = 4573
924324 XDOT = 1449
367514
YDOT = -21542
596631 feet/sec YDOT = -6550
284445 meter/sec
ZDOT = 12214
785330 ZDOT = 3729
973420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10876469
23 X = 3315147
82
Y = -13748273
88 feet Y = -4190473
88 meter
Z = 13653808
07 Z = 4161680
70
XDOT = 8594
341995 XDOT = 2619
555440
YDOT = 19009
573317 feet/sec YDOT = 5794
117947 meter/sec
ZDOT = 12245
743894 ZDOT = 3732
502739
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 15303
55507763
00016717 00000-0 10270-3 0 9007
2 25544 51
6383 128
4698 0006236 89
1591 271
0276 15
54697518 9102
Satellite: ISS
Catalog Number: 25544
Epoch time: 15303
55507763 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 128
4698 deg
Eccentricity:
0006236
Arg of perigee: 89
1591 deg
Mean anomaly: 271
0276 deg
Mean motion: 15
54697518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 910
Checksum: 323
Coasting Arc #2 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2015/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4454857
08 A = 6776724
32 meter
Y = 464226
27 meter E =
0019441
Z = -5102845
03 I = 51
92678
XDOT = -2772
149452 Wp = 82
14423
YDOT = 6905
541942 meter/sec RA = 122
76565 deg
ZDOT = -1795
161408 TA = 170
54223
MA = 170
50557
Ha = 222
433 n
mi
Hp = 211
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14615672
84 X = 4474123
06
Y = 1523052
08 feet Y = 514151
08 meter
Z = -16741617
56 Z = -5081157
01
XDOT = -9094
978516 XDOT = -2840
442488
YDOT = 22655
977500 feet/sec YDOT = 6874
160066 meter/sec
ZDOT = -5889
637165 ZDOT = -1808
794192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12450880
93 X = -3795028
51
Y = 8002447
87 feet Y = 2439146
11 meter
Z = -16647994
81 Z = -5074308
82
XDOT = -6484
662262 XDOT = -1976
525057
YDOT = -22444
602750 feet/sec YDOT = -6841
114918 meter/sec
ZDOT = -5949
729264 ZDOT = -1813
477480
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 15304
51924946
00016717 00000-0 10270-3 0 9011
2 25544 51
6383 123
6582 0006457 93
1896 266
9995 15
54721065 9251
Satellite: ISS
Catalog Number: 25544
Epoch time: 15304
51924946 = yrday
fracday
Element set: 901
Inclination: 51
6383 deg
RA of node: 123
6582 deg
Eccentricity:
0006457
Arg of perigee: 93
1896 deg
Mean anomaly: 266
9995 deg
Mean motion: 15
54721065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 925
Checksum: 336
Coasting Arc #3 (Orbit 940)
---------------------------------------
Vector Time (GMT): 2015/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3501710
64 A = 6775714
71 meter
Y = -2291874
23 meter E =
0008896
Z = 5321097
85 I = 51
93984
XDOT = 3816
337260 Wp = 90
76888
YDOT = -6651
570657 meter/sec RA = 117
77908 deg
ZDOT = -353
080073 TA = 2
58223
MA = 2
57764
Ha = 222
596 n
mi
Hp = 211
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11488551
97 X = -3501670
38
Y = -7519272
42 feet Y = -2331032
35 meter
Z = 17457670
11 Z = 5304087
10
XDOT = 12520
791534 XDOT = 3892
148261
YDOT = -21822
738377 feet/sec YDOT = -6608
469979 meter/sec
ZDOT = -1158
399188 ZDOT = -334
356504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13729389
60 X = 4184717
95
Y = -1605371
61 feet Y = -489317
27 meter
Z = 17384567
09 Z = 5298816
05
XDOT = 4147
218363 XDOT = 1264
072157
YDOT = 23798
058893 feet/sec YDOT = 7253
648351 meter/sec
ZDOT = -1076
336773 ZDOT = -328
067448
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 15305
54768457
00016717 00000-0 10270-3 0 9029
2 25544 51
6383 118
5257 0006465 96
7673 263
4215 15
54699300 9415
Satellite: ISS
Catalog Number: 25544
Epoch time: 15305
54768457 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 118
5257 deg
Eccentricity:
0006465
Arg of perigee: 96
7673 deg
Mean anomaly: 263
4215 deg
Mean motion: 15
54699300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 941
Checksum: 328
Coasting Arc #4 (Orbit 955)
---------------------------------------
Vector Time (GMT): 2015/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2447302
79 A = 6777471
65 meter
Y = 4034791
44 meter E =
0018262
Z = -4881721
26 I = 51
96099
XDOT = -4483
364776 Wp = 105
23767
YDOT = 5695
249781 meter/sec RA = 112
79484 deg
ZDOT = 2462
580048 TA = 188
85363
MA = 188
88589
Ha = 222
361 n
mi
Hp = 211
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8029208
64 X = 2425716
76
Y = 13237504
74 feet Y = 4062037
96 meter
Z = -16016145
87 Z = -4869885
13
XDOT = -14709
202021 XDOT = -4558
679679
YDOT = 18685
202695 feet/sec YDOT = 5644
692800 meter/sec
ZDOT = 8079
330865 ZDOT = 2440
617351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14787747
67 X = -4507305
49
Y = -4757663
21 feet Y = -1450135
75 meter
Z = -15965707
35 Z = -4866347
60
XDOT = -1300
574526 XDOT = -396
415116
YDOT = -22715
116594 feet/sec YDOT = -6923
567538 meter/sec
ZDOT = 7983
421840 ZDOT = 2433
346977
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 15306
51182598
00016717 00000-0 10270-3 0 9034
2 25544 51
6389 113
7139 0006493 100
6808 259
5077 15
54763562 9563
Satellite: ISS
Catalog Number: 25544
Epoch time: 15306
51182598 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 113
7139 deg
Eccentricity:
0006493
Arg of perigee: 100
6808 deg
Mean anomaly: 259
5077 deg
Mean motion: 15
54763562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 956
Checksum: 331
Coasting Arc #5 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2015/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1331898
16 A = 6781466
16 meter
Y = -5470784
55 meter E =
0017730
Z = 3763999
21 I = 51
98550
XDOT = 4845
561922 Wp = 91
03149
YDOT = -4137
207543 meter/sec RA = 107
82100 deg
ZDOT = -4281
590062 TA = 44
10689
MA = 43
96562
Ha = 222
351 n
mi
Hp = 211
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4369744
63 X = -1288907
84
Y = -17948768
21 feet Y = -5485438
19 meter
Z = 12349078
76 Z = 3757633
68
XDOT = 15897
512866 XDOT = 4912
263660
YDOT = -13573
515562 feet/sec YDOT = -4082
648500 meter/sec
ZDOT = -14047
211488 ZDOT = -4257
888796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15240185
85 X = 4645208
65
Y = 10471125
25 feet Y = 3191598
98 meter
Z = 12322538
94 Z = 3755909
87
XDOT = -2183
522078 XDOT = -665
537529
YDOT = 19653
386546 feet/sec YDOT = 5990
352219 meter/sec
ZDOT = -13944
049889 ZDOT = -4250
146406
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 15307
54022872
00016717 00000-0 10270-3 0 9047
2 25544 51
6385 108
5815 0006406 104
2816 255
9049 15
54771099 9726
Satellite: ISS
Catalog Number: 25544
Epoch time: 15307
54022872 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 108
5815 deg
Eccentricity:
0006406
Arg of perigee: 104
2816 deg
Mean anomaly: 255
9049 deg
Mean motion: 15
54771099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 972
Checksum: 317
Coasting Arc #6 (Orbit 986)
---------------------------------------
Vector Time (GMT): 2015/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 288400
16 A = 6785305
07 meter
Y = 6417444
10 meter E =
0010692
Z = -2188855
43 I = 52
00875
XDOT = -4894
247138 Wp = 76
13268
YDOT = 2091
788513 meter/sec RA = 102
86082 deg
ZDOT = 5512
998256 TA = 259
71003
MA = 259
83060
Ha = 222
263 n
mi
Hp = 211
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 946194
74 X = 227250
07
Y = 21054606
64 feet Y = 6420327
16 meter
Z = -7181284
22 Z = -2187603
29
XDOT = -16057
241266 XDOT = -4944
054687
YDOT = 6862
823207 feet/sec YDOT = 2036
779614 meter/sec
ZDOT = 18087
264620 ZDOT = 5489
101572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14974093
68 X = -4564103
75
Y = -14833391
17 feet Y = -4521217
63 meter
Z = -7177019
81 Z = -2187555
64
XDOT = 6184
145276 XDOT = 1884
927480
YDOT = -14904
325465 feet/sec YDOT = -4542
838402 meter/sec
ZDOT = 17983
612235 ZDOT = 5481
405009
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 15308
50434151
00016717 00000-0 10270-3 0 9052
2 25544 51
6396 103
7700 0006507 107
6671 252
5193 15
54812364 9876
Satellite: ISS
Catalog Number: 25544
Epoch time: 15308
50434151 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 103
7700 deg
Eccentricity:
0006507
Arg of perigee: 107
6671 deg
Mean anomaly: 252
5193 deg
Mean motion: 15
54812364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 987
Checksum: 302
Coasting Arc #7 (Orbit 1002)
---------------------------------------
Vector Time (GMT): 2015/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 729966
32 A = 6787172
66 meter
Y = -6734993
71 meter E =
0018633
Z = 261166
26 I = 52
02092
XDOT = 4723
549060 Wp = 124
64310
YDOT = 266
337694 meter/sec RA = 97
91051 deg
ZDOT = -6039
796683 TA = 52
55559
MA = 52
38622
Ha = 222
128 n
mi
Hp = 211
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2394902
61 X = 803955
74
Y = -22096436
06 feet Y = -6726417
03 meter
Z = 856844
68 Z = 264892
47
XDOT = 15497
208203 XDOT = 4749
559223
YDOT = 873
811332 feet/sec YDOT = 319
304601 meter/sec
ZDOT = -19815
605914 ZDOT = -6016
787117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13494887
96 X = 4113241
85
Y = 17659163
72 feet Y = 5382513
10 meter
Z = 874164
36 Z = 266445
30
XDOT = -10635
169415 XDOT = -3241
599638
YDOT = 9150
088769 feet/sec YDOT = 2788
947057 meter/sec
ZDOT = -19716
205782 ZDOT = -6009
499522
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 15309
53271131
00016717 00000-0 10270-3 0 9064
2 25544 51
6389 98
6370 0006348 109
9322 250
2516 15
54861375 10034
Satellite: ISS
Catalog Number: 25544
Epoch time: 15309
53271131 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 98
6370 deg
Eccentricity:
0006348
Arg of perigee: 109
9322 deg
Mean anomaly: 250
2516 deg
Mean motion: 15
54861375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1003
Checksum: 302
Coasting Arc #8 (Orbit 1018)
---------------------------------------
Vector Time (GMT): 2015/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1620249
16 A = 6785993
85 meter
Y = 6373118
08 meter E =
0018681
Z = 1650818
71 I = 52
02193
XDOT = -4358
120300 Wp = 79
35461
YDOT = -2610
200809 meter/sec RA = 92
96216 deg
ZDOT = 5747
865379 TA = 298
63818
MA = 298
82593
Ha = 222
106 n
mi
Hp = 211
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5315778
09 X = -1699413
70
Y = 20909180
05 feet Y = 6354556
86 meter
Z = 5416071
89 Z = 1642755
03
XDOT = -14298
294949 XDOT = -4356
529931
YDOT = -8563
650947 feet/sec YDOT = -2658
926922 meter/sec
ZDOT = 18857
826047 ZDOT = 5726
698160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10853959
51 X = -3308286
86
Y = -18655607
06 feet Y = -5686229
03 meter
Z = 5380058
59 Z = 1639841
86
XDOT = 14921
730813 XDOT = 4548
143552
YDOT = -3220
280543 feet/sec YDOT = -981
541509 meter/sec
ZDOT = 18766
813963 ZDOT = 5720
124896
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 15310
56106541
00016717 00000-0 10270-3 0 9072
2 25544 51
6402 93
5047 0006484 115
2521 244
9304 15
54885425 10191
Satellite: ISS
Catalog Number: 25544
Epoch time: 15310
56106541 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 93
5047 deg
Eccentricity:
0006484
Arg of perigee: 115
2521 deg
Mean anomaly: 244
9304 deg
Mean motion: 15
54885425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1019
Checksum: 287
Coasting Arc #9 (Orbit 1033)
---------------------------------------
Vector Time (GMT): 2015/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2474583
26 A = 6782255
95 meter
Y = -5322597
84 meter E =
0010937
Z = -3403739
91 I = 52
01036
XDOT = 3808
166130 Wp = 106
01799
YDOT = 4741
868227 meter/sec RA = 88
00580 deg
ZDOT = -4661
813669 TA = 113
51348
MA = 113
39852
Ha = 222
069 n
mi
Hp = 211
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8118711
48 X = 2550452
35
Y = -17462591
35 feet Y = -5294501
43 meter
Z = -11167125
70 Z = -3391534
01
XDOT = 12493
983365 XDOT = 3777
504155
YDOT = 15557
310455 feet/sec YDOT = 4784
281913 meter/sec
ZDOT = -15294
664267 ZDOT = -4643
388759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6724816
28 X = 2049724
00
Y = 18078431
67 feet Y = 5510305
97 meter
Z = -11113389
39 Z = -3387361
09
XDOT = -18603
455046 XDOT = -5670
333098
YDOT = -2402
525487 feet/sec YDOT = -732
289769 meter/sec
ZDOT = -15215
901632 ZDOT = -4637
806818
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 15311
52513274
00016717 00000-0 10270-3 0 9085
2 25544 51
6403 88
6927 0006401 117
2928 242
8878 15
54886912 10348
Satellite: ISS
Catalog Number: 25544
Epoch time: 15311
52513274 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 88
6927 deg
Eccentricity:
0006401
Arg of perigee: 117
2928 deg
Mean anomaly: 242
8878 deg
Mean motion: 15
54886912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1034
Checksum: 317
Coasting Arc #10 (Orbit 1049)
---------------------------------------
Vector Time (GMT): 2015/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3202533
98 A = 6777861
07 meter
Y = 3741737
09 meter E =
0014595
Z = 4648624
29 I = 51
99493
XDOT = -3109
682315 Wp = 117
72496
YDOT = -6360
124889 meter/sec RA = 83
03619 deg
ZDOT = 2963
324789 TA = 302
86326
MA = 303
00365
Ha = 221
982 n
mi
Hp = 211
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10507001
24 X = -3266718
76
Y = 12276040
31 feet Y = 3705565
64 meter
Z = 15251392
04 Z = 4632910
53
XDOT = -10202
369799 XDOT = -3052
725771
YDOT = -20866
551472 feet/sec YDOT = -6394
580771 meter/sec
ZDOT = 9722
194189 ZDOT = 2948
356938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1610465
76 X = -490869
96
Y = -16142889
70 feet Y = -4920352
78 meter
Z = 15182776
82 Z = 4627710
37
XDOT = 21025
568327 XDOT = 6408
593226
YDOT = 7029
102381 feet/sec YDOT = 2142
470406 meter/sec
ZDOT = 9658
685242 ZDOT = 2943
967262
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 15312
55345303
00016717 00000-0 10270-3 0 9096
2 25544 51
6411 83
5600 0006313 121
5585 238
6185 15
54941105 10506
Satellite: ISS
Catalog Number: 25544
Epoch time: 15312
55345303 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 83
5600 deg
Eccentricity:
0006313
Arg of perigee: 121
5585 deg
Mean anomaly: 238
6185 deg
Mean motion: 15
54941105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1050
Checksum: 276
Coasting Arc #11 (Orbit 1064)
---------------------------------------
Vector Time (GMT): 2015/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3861046
66 A = 6775194
71 meter
Y = -1761563
27 meter E =
0019826
Z = -5298099
84 I = 51
98187
XDOT = 2199
740942 Wp = 95
33998
YDOT = 7286
148070 meter/sec RA = 78
05547 deg
ZDOT = -823
922078 TA = 166
83405
MA = 166
78222
Ha = 221
871 n
mi
Hp = 211
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12667475
93 X = 3906194
76
Y = -5779407
07 feet Y = -1718134
32 meter
Z = -17382217
34 Z = -5279233
41
XDOT = 7216
997841 XDOT = 2122
104369
YDOT = 23904
685270 feet/sec YDOT = 7310
312893 meter/sec
ZDOT = -2703
156423 ZDOT = -813
424827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4370571
59 X = -1332150
22
Y = 13326826
21 feet Y = 4062016
63 meter
Z = -17300340
44 Z = -5273143
77
XDOT = -21539
831189 XDOT = -6565
340547
YDOT = -10497
072156 feet/sec YDOT = -3199
507593 meter/sec
ZDOT = -2659
160036 ZDOT = -810
511979
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 15313
51748977
00016717 00000-0 10270-3 0 9109
2 25544 51
6417 78
7490 0006314 123
3039 236
8720 15
54946833 10654
Satellite: ISS
Catalog Number: 25544
Epoch time: 15313
51748977 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 78
7490 deg
Eccentricity:
0006314
Arg of perigee: 123
3039 deg
Mean anomaly: 236
8720 deg
Mean motion: 15
54946833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1065
Checksum: 317
Coasting Arc #12 (Orbit 1080)
---------------------------------------
Vector Time (GMT): 2015/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4341169
02 A = 6775614
40 meter
Y = -343941
87 meter E =
0008874
Z = 5183049
56 I = 51
97660
XDOT = -1108
602930 Wp = 97
01242
YDOT = -7461
870822 meter/sec RA = 73
06933 deg
ZDOT = -1422
673400 TA = 6
59992
MA = 6
58824
Ha = 221
978 n
mi
Hp = 211
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14242680
50 X = -4362178
31
Y = -1128418
21 feet Y = -392604
98 meter
Z = 17004755
79 Z = 5161909
42
XDOT = -3637
148722 XDOT = -1018
169075
YDOT = -24481
203484 feet/sec YDOT = -7473
762354 meter/sec
ZDOT = -4667
563649 ZDOT = -1427
839010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10355694
60 X = 3156415
71
Y = -9999190
32 feet Y = -3047753
21 meter
Z = 16913449
60 Z = 5155219
44
XDOT = 19993
496079 XDOT = 6094
017605
YDOT = 12770
177741 feet/sec YDOT = 3892
350175 meter/sec
ZDOT = -4688
463943 ZDOT = -1429
043810
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 15314
54577899
00016717 00000-0 10270-3 0 9117
2 25544 51
6425 73
6158 0006302 126
2046 233
9691 15
54953520 10819
Satellite: ISS
Catalog Number: 25544
Epoch time: 15314
54577899 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 73
6158 deg
Eccentricity:
0006302
Arg of perigee: 126
2046 deg
Mean anomaly: 233
9691 deg
Mean motion: 15
54953520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1081
Checksum: 310
Coasting Arc #13 (Orbit 1095)
---------------------------------------
Vector Time (GMT): 2015/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4630514
63 A = 6778858
70 meter
Y = 2351074
96 meter E =
0014643
Z = -4372351
48 I = 51
97808
XDOT = -184
611532 Wp = 118
44392
YDOT = 6820
946860 meter/sec RA = 68
08993 deg
ZDOT = 3474
245576 TA = 186
71377
MA = 186
73341
Ha = 221
687 n
mi
Hp = 211
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15191977
12 X = 4625120
00
Y = 7713500
53 feet Y = 2402826
20 meter
Z = -14344985
16 Z = -4349869
86
XDOT = -605
680880 XDOT = -277
748350
YDOT = 22378
434579 feet/sec YDOT = 6818
361708 meter/sec
ZDOT = 11398
443490 ZDOT = 3473
122409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15793396
60 X = -4813827
28
Y = 6605170
62 feet Y = 2013256
00 meter
Z = -14248270
19 Z = -4342872
75
XDOT = -16087
774098 XDOT = -4903
553545
YDOT = -13906
743528 feet/sec YDOT = -4238
775427 meter/sec
ZDOT = 11392
267731 ZDOT = 3472
363204
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 15315
50978340
00016717 00000-0 10270-3 0 9121
2 25544 51
6430 68
8046 0006188 130
0722 230
0974 15
54984896 10961
Satellite: ISS
Catalog Number: 25544
Epoch time: 15315
50978340 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 68
8046 deg
Eccentricity:
0006188
Arg of perigee: 130
0722 deg
Mean anomaly: 230
0974 deg
Mean motion: 15
54984896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1096
Checksum: 316
Coasting Arc #14 (Orbit 1111)
---------------------------------------
Vector Time (GMT): 2015/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4595072
92 A = 6783301
67 meter
Y = -4038473
37 meter E =
0018850
Z = 2907172
03 I = 51
98061
XDOT = 1639
808039 Wp = 109
44963
YDOT = -5528
718576 meter/sec RA = 63
12206 deg
ZDOT = -5067
782683 TA = 37
53719
MA = 37
40574
Ha = 221
758 n
mi
Hp = 211
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15075698
57 X = -4563694
54
Y = -13249584
53 feet Y = -4089683
06 meter
Z = 9537965
99 Z = 2884925
68
XDOT = 5379
947633 XDOT = 1726
127690
YDOT = -18138
840473 feet/sec YDOT = -5509
898509 meter/sec
ZDOT = -16626
583607 ZDOT = -5059
606945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19853355
87 X = 6051302
87
Y = -3237663
34 feet Y = -986839
78 meter
Z = 9442603
98 Z = 2878105
69
XDOT = 10260
148569 XDOT = 3127
293284
YDOT = 14332
006858 feet/sec YDOT = 4368
395690 meter/sec
ZDOT = -16590
161541 ZDOT = -5056
681238
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 15316
53803983
00016717 00000-0 10270-3 0 9136
2 25544 51
6434 63
6719 0006292 133
2250 226
9429 15
54992572 11120
Satellite: ISS
Catalog Number: 25544
Epoch time: 15316
53803983 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 63
6719 deg
Eccentricity:
0006292
Arg of perigee: 133
2250 deg
Mean anomaly: 226
9429 deg
Mean motion: 15
54992572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1112
Checksum: 310
Coasting Arc #15 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2015/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4214567
92 A = 6786278
25 meter
Y = 5210250
01 meter E =
0010787
Z = -1064513
68 I = 51
97642
XDOT = -3130
851965 Wp = 72
16231
YDOT = 3731
041237 meter/sec RA = 58
16584 deg
ZDOT = 5918
404841 TA = 276
35046
MA = 276
47330
Ha = 221
539 n
mi
Hp = 211
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13827322
57 X = 4161163
53
Y = 17093996
10 feet Y = 5257081
51 meter
Z = -3492498
95 Z = -1044169
25
XDOT = -10271
824032 XDOT = -3201
090791
YDOT = 12240
948941 feet/sec YDOT = 3695
637156 meter/sec
ZDOT = 19417
338718 ZDOT = 5903
024848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21999275
45 X = -6705379
16
Y = 175727
32 feet Y = 53561
69 meter
Z = -3405598
42 Z = -1038026
40
XDOT = -3081
292795 XDOT = -939
178044
YDOT = -14155
976108 feet/sec YDOT = -4314
741518 meter/sec
ZDOT = 19350
121437 ZDOT = 5897
917014
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 15317
50201358
00016717 00000-0 10270-3 0 9143
2 25544 51
6442 58
8602 0006059 135
0643 225
1002 15
55018627 11278
Satellite: ISS
Catalog Number: 25544
Epoch time: 15317
50201358 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 58
8602 deg
Eccentricity:
0006059
Arg of perigee: 135
0643 deg
Mean anomaly: 225
1002 deg
Mean motion: 15
55018627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1127
Checksum: 275
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