[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 8th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 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
226/10:19:30
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 212
7
Coasting Arc #1 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2015/219/12:13:53
262
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6717538
18 A = 6786295
68 meter
Y = 48047
69 meter E =
0013496
Z = 921082
11 I = 51
61061
XDOT = 785
454098 Wp = 118
71763
YDOT = 4813
660437 meter/sec RA = 186
64631 deg
ZDOT = -5920
066381 TA = 51
30207
MA = 51
18144
Ha = 219
893 n
mi
Hp = 212
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22039167
26 X = 6712027
40
Y = 157636
77 feet Y = 123136
78 meter
Z = 3021922
94 Z = 953700
96
XDOT = 2576
949140 XDOT = 760
325439
YDOT = 15792
849204 feet/sec YDOT = 4822
303480 meter/sec
ZDOT = -19422
789963 ZDOT = -5916
311797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16344404
79 X = -4981774
58
Y = -14756068
29 feet Y = -4497649
61 meter
Z = 3162379
08 Z = 963893
14
XDOT = 7403
993523 XDOT = 2256
737226
YDOT = -12400
094315 feet/sec YDOT = -3779
548747 meter/sec
ZDOT = -19407
413677 ZDOT = -5915
379689
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 15219
54368283
00016717 00000-0 10270-3 0 9004
2 25544 51
6403 187
6127 0001493 30
4403 329
6837 15
55037485 36037
Satellite: ISS
Catalog Number: 25544
Epoch time: 15219
54368283 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 187
6127 deg
Eccentricity:
0001493
Arg of perigee: 30
4403 deg
Mean anomaly: 329
6837 deg
Mean motion: 15
55037485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 305
Coasting Arc #2 (Orbit 3618)
---------------------------------------
Vector Time (GMT): 2015/220/12:13:53
262
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6611065
61 A = 6786150
59 meter
Y = -1044051
32 meter E =
0014890
Z = 1075053
78 I = 51
64180
XDOT = 1694
665224 Wp = 54
95784
YDOT = -4614
436355 meter/sec RA = 181
67122 deg
ZDOT = 5890
674149 TA = 316
71052
MA = 316
82742
Ha = 219
869 n
mi
Hp = 212
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21689847
81 X = -6604121
59
Y = -3425365
21 feet Y = -1117941
79 meter
Z = 3527079
33 Z = 1042955
66
XDOT = 5559
925277 XDOT = 1717
524604
YDOT = -15139
226885 feet/sec YDOT = -4595
357830 meter/sec
ZDOT = 19326
358757 ZDOT = 5898
961830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14232958
15 X = 4338205
64
Y = 16749937
87 feet Y = 5105381
06 meter
Z = 3389011
27 Z = 1032970
63
XDOT = -12768
541156 XDOT = -3891
851344
YDOT = 6898
077759 feet/sec YDOT = 2102
534101 meter/sec
ZDOT = 19362
811575 ZDOT = 5901
784968
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 15220
57191057
00016717 00000-0 10270-3 0 9013
2 25544 51
6401 182
4798 0001367 37
4350 322
6898 15
55068241 36191
Satellite: ISS
Catalog Number: 25544
Epoch time: 15220
57191057 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 182
4798 deg
Eccentricity:
0001367
Arg of perigee: 37
4350 deg
Mean anomaly: 322
6898 deg
Mean motion: 15
55068241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3619
Checksum: 308
Coasting Arc #3 (Orbit 3633)
---------------------------------------
Vector Time (GMT): 2015/221/12:13:53
262
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5765333
17 A = 6782970
74 meter
Y = 2009896
56 meter E =
0005071
Z = -2958102
54 I = 51
66373
XDOT = -4022
121708 Wp = 97
78315
YDOT = 4192
034004 meter/sec RA = 176
69217 deg
ZDOT = -4998
820796 TA = 115
98706
MA = 115
93482
Ha = 219
904 n
mi
Hp = 212
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18915135
08 X = 5756798
71
Y = 6594148
82 feet Y = 2074320
67 meter
Z = -9705060
82 Z = -2930116
69
XDOT = -13195
937361 XDOT = -4044
417019
YDOT = 13753
392400 feet/sec YDOT = 4146
931492 meter/sec
ZDOT = -16400
330695 ZDOT = -5018
413260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10390784
17 X = -3167111
01
Y = -17193477
78 feet Y = -5240572
03 meter
Z = -9584845
62 Z = -2921460
94
XDOT = 17602
537441 XDOT = 5365
253412
YDOT = -1462
717989 feet/sec YDOT = -445
836443 meter/sec
ZDOT = -16485
413510 ZDOT = -5024
754038
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 15221
53586595
00016717 00000-0 10270-3 0 9026
2 25544 51
6408 177
6671 0001514 34
7252 325
3999 15
55069769 36344
Satellite: ISS
Catalog Number: 25544
Epoch time: 15221
53586595 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 177
6671 deg
Eccentricity:
0001514
Arg of perigee: 34
7252 deg
Mean anomaly: 325
3999 deg
Mean motion: 15
55069769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3634
Checksum: 334
Coasting Arc #4 (Orbit 3649)
---------------------------------------
Vector Time (GMT): 2015/222/12:13:53
262
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4286194
57 A = 6778403
32 meter
Y = -2877386
87 meter E =
0010067
Z = 4385454
44 I = 51
68102
XDOT = 5881
760670 Wp = 102
09710
YDOT = -3570
823581 meter/sec RA = 171
70306 deg
ZDOT = 3397
094697 TA = 313
51111
MA = 313
59474
Ha = 219
892 n
mi
Hp = 212
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14062318
13 X = -4275002
93
Y = -9440245
62 feet Y = -2925255
46 meter
Z = 14387973
89 Z = 4364660
37
XDOT = 19297
115058 XDOT = 5904
751788
YDOT = -11715
300464 feet/sec YDOT = -3504
921421 meter/sec
ZDOT = 11145
323809 ZDOT = 3425
722430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5141987
98 X = 1567277
94
Y = 16216756
74 feet Y = 4942867
45 meter
Z = 14298866
45 Z = 4358294
49
XDOT = -21145
557404 XDOT = -6445
165897
YDOT = -3256
840619 feet/sec YDOT = -992
685021 meter/sec
ZDOT = 11269
240509 ZDOT = 3434
864507
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 15222
56407297
00016717 00000-0 10270-3 0 9032
2 25544 51
6413 172
5345 0001333 37
8471 322
2776 15
55109577 36507
Satellite: ISS
Catalog Number: 25544
Epoch time: 15222
56407297 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 172
5345 deg
Eccentricity:
0001333
Arg of perigee: 37
8471 deg
Mean anomaly: 322
2776 deg
Mean motion: 15
55109577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3650
Checksum: 303
Coasting Arc #5 (Orbit 3664)
---------------------------------------
Vector Time (GMT): 2015/223/12:13:53
262
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2351527
48 A = 6775130
96 meter
Y = 3666194
82 meter E =
0015129
Z = -5202951
90 I = 51
70165
XDOT = -7049
824553 Wp = 76
67857
YDOT = 2704
979134 meter/sec RA = 166
70121 deg
ZDOT = -1279
940299 TA = 181
02450
MA = 181
02760
Ha = 219
866 n
mi
Hp = 212
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7714985
18 X = 2335629
95
Y = 12028198
24 feet Y = 3692402
37 meter
Z = -17070052
16 Z = -5191567
39
XDOT = -23129
345645 XDOT = -7073
330974
YDOT = 8874
603458 feet/sec YDOT = 2626
011962 meter/sec
ZDOT = -4199
279195 ZDOT = -1314
243363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1170060
08 X = 356634
31
Y = -14299692
10 feet Y = -4358546
15 meter
Z = -17021603
78 Z = -5188184
83
XDOT = 22660
130830 XDOT = 6906
807877
YDOT = 7030
269415 feet/sec YDOT = 2142
826118 meter/sec
ZDOT = -4347
523314 ZDOT = -1325
125106
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 15223
52800977
00016717 00000-0 10270-3 0 9042
2 25544 51
6416 167
7213 0001483 39
4437 320
6824 15
55093569 36651
Satellite: ISS
Catalog Number: 25544
Epoch time: 15223
52800977 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 167
7213 deg
Eccentricity:
0001483
Arg of perigee: 39
4437 deg
Mean anomaly: 320
6824 deg
Mean motion: 15
55093569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3665
Checksum: 317
Coasting Arc #6 (Orbit 3680)
---------------------------------------
Vector Time (GMT): 2015/224/12:13:53
262
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -202626
66 A = 6774774
74 meter
Y = -4286326
86 meter E =
0004997
Z = 5239489
03 I = 51
73228
XDOT = 7432
585521 Wp = 53
46409
YDOT = -1607
618062 meter/sec RA = 161
69685 deg
ZDOT = -1024
137162 TA = 46
34441
MA = 46
30299
Ha = 219
840 n
mi
Hp = 212
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -664785
62 X = -180131
79
Y = -14062752
15 feet Y = -4288467
03 meter
Z = 17189924
64 Z = 5238559
33
XDOT = 24385
123101 XDOT = 7454
984661
YDOT = -5274
337474 feet/sec YDOT = -1524
376760 meter/sec
ZDOT = -3360
030058 ZDOT = -987
977475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7790066
33 X = -2374412
22
Y = 11731637
08 feet Y = 3575802
98 meter
Z = 17186622
85 Z = 5238482
65
XDOT = -21858
187042 XDOT = -6662
375410
YDOT = -9803
367399 feet/sec YDOT = -2988
066383 meter/sec
ZDOT = -3203
946525 ZDOT = -976
562901
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 15224
55619727
00016717 00000-0 10270-3 0 9058
2 25544 51
6423 162
5888 0001483 40
9220 319
2044 15
55120285 36819
Satellite: ISS
Catalog Number: 25544
Epoch time: 15224
55619727 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 162
5888 deg
Eccentricity:
0001483
Arg of perigee: 40
9220 deg
Mean anomaly: 319
2044 deg
Mean motion: 15
55120285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3681
Checksum: 301
Coasting Arc #7 (Orbit 3695)
---------------------------------------
Vector Time (GMT): 2015/225/12:13:53
262
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1877192
82 A = 6777696
05 meter
Y = 4691356
33 meter E =
0010509
Z = -4527254
60 I = 51
77251
XDOT = -6965
806051 Wp = 103
25729
YDOT = 275
185534 meter/sec RA = 156
69796 deg
ZDOT = 3177
330727 TA = 198
59011
MA = 198
62853
Ha = 219
841 n
mi
Hp = 212
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6158769
11 X = -1907521
96
Y = 15391589
00 feet Y = 4670194
70 meter
Z = -14853197
51 Z = -4536447
14
XDOT = -22853
694393 XDOT = -6983
799473
YDOT = 902
839677 feet/sec YDOT = 197
188735 meter/sec
ZDOT = 10424
313410 ZDOT = 3143
449235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13913319
84 X = 4240779
89
Y = -8947043
13 feet Y = -2727058
75 meter
Z = -14893585
04 Z = -4539564
72
XDOT = 18476
259645 XDOT = 5631
563940
YDOT = 11643
373607 feet/sec YDOT = 3548
900276 meter/sec
ZDOT = 10278
248344 ZDOT = 3132
810095
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 15225
52011385
00016717 00000-0 10270-3 0 9063
2 25544 51
6427 157
7758 0001502 44
4107 315
7167 15
55126553 36967
Satellite: ISS
Catalog Number: 25544
Epoch time: 15225
52011385 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 157
7758 deg
Eccentricity:
0001502
Arg of perigee: 44
4107 deg
Mean anomaly: 315
7167 deg
Mean motion: 15
55126553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3696
Checksum: 304
Coasting Arc #8 (Orbit 3710)
---------------------------------------
Vector Time (GMT): 2015/226/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4760467
90 A = 6777553
03 meter
Y = -1546700
81 meter E =
0009415
Z = 4563086
52 I = 51
79830
XDOT = 4679
758776 Wp = 105
91256
YDOT = -5231
754481 meter/sec RA = 152
15707 deg
ZDOT = 3101
009545 TA = 313
10205
MA = 313
18079
Ha = 219
866 n
mi
Hp = 212
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15618333
00 X = -4764983
79
Y = -5074477
73 feet Y = -1599960
63 meter
Z = 14970756
29 Z = 4539950
66
XDOT = 15353
539292 XDOT = 4722
850496
YDOT = -17164
548821 feet/sec YDOT = -5179
181326 meter/sec
ZDOT = 10173
915830 ZDOT = 3123
847201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2487923
05 X = 758318
94
Y = 16323637
28 feet Y = 4975444
64 meter
Z = 14871291
10 Z = 4532769
53
XDOT = -20997
738906 XDOT = -6400
110819
YDOT = -6182
412791 feet/sec YDOT = -1884
399419 meter/sec
ZDOT = 10273
208102 ZDOT = 3131
273829
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 15226
48401941
00016717 00000-0 10270-3 0 9071
2 25544 51
6421 152
9633 0001324 47
9843 312
1423 15
55174574 37117
Satellite: ISS
Catalog Number: 25544
Epoch time: 15226
48401941 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 152
9633 deg
Eccentricity:
0001324
Arg of perigee: 47
9843 deg
Mean anomaly: 312
1423 deg
Mean motion: 15
55174574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3711
Checksum: 292
Coasting Arc #9 (Orbit 3725)
---------------------------------------
Vector Time (GMT): 2015/227/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3109828
37 A = 6774681
59 meter
Y = 2927887
46 meter E =
0015655
Z = -5272242
41 I = 51
81643
XDOT = -5973
052673 Wp = 80
11423
YDOT = 4706
240729 meter/sec RA = 147
16125 deg
ZDOT = -909
314179 TA = 181
19598
MA = 181
19973
Ha = 219
824 n
mi
Hp = 212
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10202848
99 X = 3102466
96
Y = 9605929
98 feet Y = 2962622
22 meter
Z = -17297383
23 Z = -5257153
78
XDOT = -19596
629506 XDOT = -6020
818048
YDOT = 15440
422340 feet/sec YDOT = 4639
179019 meter/sec
ZDOT = -2983
314235 ZDOT = -938
445725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3746684
52 X = 1141989
44
Y = -13585419
82 feet Y = -4140835
96 meter
Z = -17232823
57 Z = -5252564
62
XDOT = 21752
546539 XDOT = 6630
176185
YDOT = 9944
960484 feet/sec YDOT = 3031
223956 meter/sec
ZDOT = -3109
660319 ZDOT = -947
824465
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 15227
44791838
00016717 00000-0 10270-3 0 9086
2 25544 51
6423 148
1502 0001462 49
0498 311
0782 15
55150387 37261
Satellite: ISS
Catalog Number: 25544
Epoch time: 15227
44791838 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 148
1502 deg
Eccentricity:
0001462
Arg of perigee: 49
0498 deg
Mean anomaly: 311
0782 deg
Mean motion: 15
55150387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3726
Checksum: 311
Coasting Arc #10 (Orbit 3741)
---------------------------------------
Vector Time (GMT): 2015/228/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1233228
51 A = 6774934
85 meter
Y = -4190528
88 meter E =
0005899
Z = 5175222
82 I = 51
84429
XDOT = 6574
262481 Wp = 54
47357
YDOT = -3693
684861 meter/sec RA = 142
16419 deg
ZDOT = -1419
792004 TA = 49
16166
MA = 49
11053
Ha = 219
851 n
mi
Hp = 212
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4046025
30 X = -1211416
19
Y = -13748454
32 feet Y = -4204197
40 meter
Z = 16979077
49 Z = 5169285
35
XDOT = 21569
102627 XDOT = 6621
974239
YDOT = -12118
388652 feet/sec YDOT = -3619
900443 meter/sec
ZDOT = -4658
110249 ZDOT = -1387
740003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10093468
23 X = -3076489
12
Y = 10215545
41 feet Y = 3113698
24 meter
Z = 16954171
18 Z = 5167631
38
XDOT = -20218
004764 XDOT = -6162
447852
YDOT = -12451
488850 feet/sec YDOT = -3795
213801 meter/sec
ZDOT = -4519
328919 ZDOT = -1377
491454
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 15228
47606542
00016717 00000-0 10270-3 0 9098
2 25544 51
6427 143
0176 0001481 51
4029 308
7257 15
55172923 37422
Satellite: ISS
Catalog Number: 25544
Epoch time: 15228
47606542 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 143
0176 deg
Eccentricity:
0001481
Arg of perigee: 51
4029 deg
Mean anomaly: 308
7257 deg
Mean motion: 15
55172923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3742
Checksum: 304
Coasting Arc #11 (Orbit 3756)
---------------------------------------
Vector Time (GMT): 2015/229/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -609009
57 A = 6778312
11 meter
Y = 5191422
97 meter E =
0009474
Z = -4324833
06 I = 51
88017
XDOT = -6437
171198 Wp = 103
33979
YDOT = 2185
342700 meter/sec RA = 137
17411 deg
ZDOT = 3534
061495 TA = 202
53475
MA = 202
57638
Ha = 219
785 n
mi
Hp = 212
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1998062
91 X = -646007
95
Y = 17032227
59 feet Y = 5184405
48 meter
Z = -14189084
85 Z = -4327881
67
XDOT = -21119
328078 XDOT = -6478
296697
YDOT = 7169
759516 feet/sec YDOT = 2113
128300 meter/sec
ZDOT = 11594
689945 ZDOT = 3502
691408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15760464
33 X = 4803789
53
Y = -6730474
01 feet Y = -2051448
48 meter
Z = -14203085
75 Z = -4329100
54
XDOT = 16190
236907 XDOT = 4934
784209
YDOT = 13760
486677 feet/sec YDOT = 4194
196339 meter/sec
ZDOT = 11459
085281 ZDOT = 3492
729194
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 15229
43994311
00016717 00000-0 10270-3 0 9101
2 25544 51
6426 138
2045 0001459 53
0694 307
0593 15
55185912 37576
Satellite: ISS
Catalog Number: 25544
Epoch time: 15229
43994311 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 138
2045 deg
Eccentricity:
0001459
Arg of perigee: 53
0694 deg
Mean anomaly: 307
0593 deg
Mean motion: 15
55185912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3757
Checksum: 311
Coasting Arc #12 (Orbit 3772)
---------------------------------------
Vector Time (GMT): 2015/230/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2258717
22 A = 6782853
31 meter
Y = -5747288
30 meter E =
0014507
Z = 2791435
49 I = 51
91860
XDOT = 5687
418037 Wp = 96
22662
YDOT = -273
058636 meter/sec RA = 132
19998 deg
ZDOT = -5142
892275 TA = 52
21937
MA = 52
08807
Ha = 219
759 n
mi
Hp = 212
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7410489
57 X = 2309257
32
Y = -18855932
75 feet Y = -5721747
06 meter
Z = 9158252
92 Z = 2802530
92
XDOT = 18659
507995 XDOT = 5715
030699
YDOT = -895
861668 feet/sec YDOT = -209
304148 meter/sec
ZDOT = -16873
006150 ZDOT = -5115
197139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19977423
44 X = -6089118
66
Y = 3235430
25 feet Y = 986159
14 meter
Z = 9207045
99 Z = 2806307
62
XDOT = -10062
420283 XDOT = -3067
025702
YDOT = -14257
565888 feet/sec YDOT = -4345
706083 meter/sec
ZDOT = -16753
552887 ZDOT = -5106
482920
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 15230
46806898
00016717 00000-0 10270-3 0 9119
2 25544 51
6429 133
0709 0001479 56
0773 304
0521 15
55207215 37739
Satellite: ISS
Catalog Number: 25544
Epoch time: 15230
46806898 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 133
0709 deg
Eccentricity:
0001479
Arg of perigee: 56
0773 deg
Mean anomaly: 304
0521 deg
Mean motion: 15
55207215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3773
Checksum: 302
Coasting Arc #13 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2015/231/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3510373
84 A = 6785855
33 meter
Y = 5736759
35 meter E =
0011464
Z = -864935
07 I = 51
94888
XDOT = -4462
062178 Wp = 41
61098
YDOT = -1839
735026 meter/sec RA = 127
24010 deg
ZDOT = 5960
732781 TA = 309
06713
MA = 309
16907
Ha = 219
758 n
mi
Hp = 212
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11516974
56 X = -3570061
28
Y = 18821388
95 feet Y = 5697170
25 meter
Z = -2837713
49 Z = -882133
00
XDOT = -14639
311606 XDOT = -4470
112948
YDOT = -6035
876069 feet/sec YDOT = -1889
677349 meter/sec
ZDOT = 19556
209912 ZDOT = 5939
037706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22055675
67 X = 6722569
94
Y = -24681
82 feet Y = -7523
02 meter
Z = -2912827
60 Z = -887829
85
XDOT = 2563
657977 XDOT = 781
402952
YDOT = 14133
265330 feet/sec YDOT = 4307
819273 meter/sec
ZDOT = 19462
973619 ZDOT = 5932
314359
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 15231
43192708
00016717 00000-0 10270-3 0 9126
2 25544 51
6425 128
2580 0001465 56
4496 303
6797 15
55208031 37882
Satellite: ISS
Catalog Number: 25544
Epoch time: 15231
43192708 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 128
2580 deg
Eccentricity:
0001465
Arg of perigee: 56
4496 deg
Mean anomaly: 303
6797 deg
Mean motion: 15
55208031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 312
Coasting Arc #14 (Orbit 3803)
---------------------------------------
Vector Time (GMT): 2015/232/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4342738
12 A = 6785524
07 meter
Y = -5060324
37 meter E =
0009511
Z = -1237947
44 I = 51
96720
XDOT = 2940
099897 Wp = 133
94740
YDOT = 3952
393503 meter/sec RA = 122
28630 deg
ZDOT = -5876
571370 TA = 59
45183
MA = 59
35800
Ha = 219
775 n
mi
Hp = 212
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14247828
47 X = 4405014
58
Y = -16602114
07 feet Y = -5011412
88 meter
Z = -4061507
35 Z = -1216699
81
XDOT = 9645
997039 XDOT = 2924
230776
YDOT = 12967
170287 feet/sec YDOT = 3985
182536 meter/sec
ZDOT = -19280
089796 ZDOT = -5862
327814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21669991
74 X = -6605013
48
Y = -3128081
50 feet Y = -953439
24 meter
Z = -3969031
82 Z = -1209760
90
XDOT = 5465
414180 XDOT = 1665
858242
YDOT = -13622
282622 feet/sec YDOT = -4152
071743 meter/sec
ZDOT = -19219
338819 ZDOT = -5858
054472
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 15232
46003217
00016717 00000-0 10270-3 0 9137
2 25544 51
6433 123
1238 0001413 62
5732 297
5564 15
55223216 38043
Satellite: ISS
Catalog Number: 25544
Epoch time: 15232
46003217 = yrday
fracday
Element set: 913
Inclination: 51
6433 deg
RA of node: 123
1238 deg
Eccentricity:
0001413
Arg of perigee: 62
5732 deg
Mean anomaly: 297
5564 deg
Mean motion: 15
55223216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3804
Checksum: 274
Coasting Arc #15 (Orbit 3819)
---------------------------------------
Vector Time (GMT): 2015/233/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4690942
94 A = 6782042
46 meter
Y = 3764779
61 meter E =
0014407
Z = 3118795
08 I = 51
97163
XDOT = -1343
955259 Wp = 82
60519
YDOT = -5749
583044 meter/sec RA = 117
32689 deg
ZDOT = 4901
540873 TA = 313
15360
MA = 313
27395
Ha = 219
828 n
mi
Hp = 212
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15390232
74 X = -4747842
85
Y = 12351639
13 feet Y = 3712004
42 meter
Z = 10232267
32 Z = 3095869
09
XDOT = -4409
302032 XDOT = -1303
371891
YDOT = -18863
461431 feet/sec YDOT = -5764
384859 meter/sec
ZDOT = 16081
170842 ZDOT = 4895
111107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18826450
93 X = 5738302
24
Y = 6083868
06 feet Y = 1854362
99 meter
Z = 10132760
85 Z = 3088465
51
XDOT = -12805
298318 XDOT = -3903
054927
YDOT = 12790
386726 feet/sec YDOT = 3898
509874 meter/sec
ZDOT = 16054
425098 ZDOT = 4893
388770
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 15233
48812658
00016717 00000-0 10270-3 0 9148
2 25544 51
6430 117
9898 0001487 63
1830 296
9475 15
55242707 38208
Satellite: ISS
Catalog Number: 25544
Epoch time: 15233
48812658 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 117
9898 deg
Eccentricity:
0001487
Arg of perigee: 63
1830 deg
Mean anomaly: 296
9475 deg
Mean motion: 15
55242707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3820
Checksum: 330
Coasting Arc #16 (Orbit 3834)
---------------------------------------
Vector Time (GMT): 2015/234/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4644284
70 A = 6777283
69 meter
Y = -1921104
19 meter E =
0011195
Z = -4557708
01 I = 51
97081
XDOT = -204
308587 Wp = 69
07384
YDOT = 6979
012246 meter/sec RA = 112
35419 deg
ZDOT = -3152
230624 TA = 169
44515
MA = 169
42164
Ha = 219
684 n
mi
Hp = 212
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15237154
51 X = 4687561
32
Y = -6302835
28 feet Y = -1868926
96 meter
Z = -14953110
26 Z = -4535041
88
XDOT = -670
303763 XDOT = -267
022112
YDOT = 22897
021803 feet/sec YDOT = 6976
376751 meter/sec
ZDOT = -10341
963988 ZDOT = -3153
375722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13870773
53 X = -4227811
77
Y = -9078649
06 feet Y = -2767172
23 meter
Z = -14855029
10 Z = -4527812
87
XDOT = 18561
808111 XDOT = 5657
639112
YDOT = -11440
035012 feet/sec YDOT = -3486
922672 meter/sec
ZDOT = -10348
106451 ZDOT = -3154
102846
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 15234
45195450
00016717 00000-0 10270-3 0 9151
2 25544 51
6439 113
1766 0001464 64
0876 296
0428 15
55284592 38357
Satellite: ISS
Catalog Number: 25544
Epoch time: 15234
45195450 = yrday
fracday
Element set: 915
Inclination: 51
6439 deg
RA of node: 113
1766 deg
Eccentricity:
0001464
Arg of perigee: 64
0876 deg
Mean anomaly: 296
0428 deg
Mean motion: 15
55284592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3835
Checksum: 322
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