[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 20th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 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
329/19:52:57
949 4
8 5
3 5
3
N/A 0
8 -0
6 220
0
000/00:13:55
898 2
3 -0
1 215
5
Coasting Arc #1 (Orbit 1235)
---------------------------------------
Vector Time (GMT): 2015/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6004566
63 A = 6781845
99 meter
Y = -118848
85 meter E =
0007802
Z = -3160947
78 I = 51
79935
XDOT = 2655
706292 Wp = 122
84120
YDOT = 5302
229399 meter/sec RA = 23
33398 deg
ZDOT = 4850
008796 TA = 200
81206
MA = 200
84384
Ha = 220
658 n
mi
Hp = 211
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19700021
74 X = 6020804
25
Y = -389924
03 feet Y = -51611
08 meter
Z = -10370563
58 Z = -3131738
94
XDOT = 8712
947152 XDOT = 2572
658253
YDOT = 17395
765746 feet/sec YDOT = 5331
462994 meter/sec
ZDOT = 15912
102349 ZDOT = 4862
708062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10041284
71 X = -3060583
58
Y = 17029926
39 feet Y = 5190721
56 meter
Z = -10244300
61 Z = -3122462
83
XDOT = -18086
099347 XDOT = -5512
643081
YDOT = -1068
913684 feet/sec YDOT = -325
804891 meter/sec
ZDOT = 15965
892228 ZDOT = 4866
403951
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 15324
50642674
00016717 00000-0 10270-3 0 9006
2 25544 51
6437 23
9061 0005809 158
3728 201
7672 15
55280297 12366
Satellite: ISS
Catalog Number: 25544
Epoch time: 15324
50642674 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 23
9061 deg
Eccentricity:
0005809
Arg of perigee: 158
3728 deg
Mean anomaly: 201
7672 deg
Mean motion: 15
55280297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 306
Coasting Arc #2 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2015/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6560642
92 A = 6785275
21 meter
Y = -1149079
30 meter E =
0018448
Z = 1239725
95 I = 51
78220
XDOT = -249
624563 Wp = 132
41067
YDOT = -4947
742956 meter/sec RA = 18
36230 deg
ZDOT = -5863
643311 TA = 34
12096
MA = 34
00251
Ha = 220
521 n
mi
Hp = 211
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21524419
03 X = -6553328
25
Y = -3769945
21 feet Y = -1222403
82 meter
Z = 4067342
34 Z = 1207872
88
XDOT = -818
978224 XDOT = -165
795288
YDOT = -16232
752480 feet/sec YDOT = -4950
065826 meter/sec
ZDOT = -19237
674906 ZDOT = -5864
652241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14235357
17 X = 4338936
87
Y = -16612245
21 feet Y = -5063412
34 meter
Z = 3929922
45 Z = 1197840
36
XDOT = 13106
971604 XDOT = 3995
004945
YDOT = 6644
998173 feet/sec YDOT = 2025
395443 meter/sec
ZDOT = -19241
009424 ZDOT = -5864
659672
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 15325
53449533
00016717 00000-0 10270-3 0 9010
2 25544 51
6444 18
7719 0005619 160
7204 199
4163 15
55316431 12527
Satellite: ISS
Catalog Number: 25544
Epoch time: 15325
53449533 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 18
7719 deg
Eccentricity:
0005619
Arg of perigee: 160
7204 deg
Mean anomaly: 199
4163 deg
Mean motion: 15
55316431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 301
Coasting Arc #3 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2015/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6360408
89 A = 6785638
71 meter
Y = 2198808
42 meter E =
0012869
Z = 844212
20 I = 51
75211
XDOT = -2276
674578 Wp = 78
09632
YDOT = 4274
867905 meter/sec RA = 13
39541 deg
ZDOT = 5944
618805 TA = 291
02300
MA = 291
16061
Ha = 220
473 n
mi
Hp = 211
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20867483
22 X = 6331247
60
Y = 7213938
37 feet Y = 2269771
67 meter
Z = 2769725
05 Z = 875039
58
XDOT = -7469
404783 XDOT = -2353
185296
YDOT = 14025
157169 feet/sec YDOT = 4248
980912 meter/sec
ZDOT = 19503
342535 ZDOT = 5933
373041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16593015
55 X = -5057551
14
Y = 14539998
65 feet Y = 4431791
59 meter
Z = 2902484
14 Z = 884677
17
XDOT = -7364
697710 XDOT = -2244
759862
YDOT = -12334
197365 feet/sec YDOT = -3759
463357 meter/sec
ZDOT = 19453
855229 ZDOT = 5929
535074
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 15326
56254644
00016717 00000-0 10270-3 0 9022
2 25544 51
6439 13
6379 0005506 162
6654 197
4689 15
55284620 12684
Satellite: ISS
Catalog Number: 25544
Epoch time: 15326
56254644 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 13
6379 deg
Eccentricity:
0005506
Arg of perigee: 162
6654 deg
Mean anomaly: 197
4689 deg
Mean motion: 15
55284620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1268
Checksum: 330
Coasting Arc #4 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2015/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5340355
24 A = 6782226
24 meter
Y = -3059881
72 meter E =
0009284
Z = -2843543
61 I = 51
71107
XDOT = 4636
563889 Wp = 143
23470
YDOT = -3376
123712 meter/sec RA = 8
42117 deg
ZDOT = -5090
630105 TA = 69
06465
MA = 68
96531
Ha = 220
244 n
mi
Hp = 211
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17520850
51 X = -5291928
80
Y = -10038982
01 feet Y = -3119330
32 meter
Z = -9329211
32 Z = -2869368
99
XDOT = 15211
823782 XDOT = 4698
700863
YDOT = -11076
521365 feet/sec YDOT = -3323
927154 meter/sec
ZDOT = -16701
542338 ZDOT = -5067
955144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17191658
35 X = 5240017
46
Y = -10494079
33 feet Y = -3198595
38 meter
Z = -9440165
71 Z = -2877362
51
XDOT = 1595
367106 XDOT = 486
267894
YDOT = 17502
781515 feet/sec YDOT = 5334
847806 meter/sec
ZDOT = -16602
854488 ZDOT = -5060
550048
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 15327
52632323
00016717 00000-0 10270-3 0 9034
2 25544 51
6446 8
8244 0005595 166
0689 194
0619 15
55361809 12831
Satellite: ISS
Catalog Number: 25544
Epoch time: 15327
52632323 = yrday
fracday
Element set: 903
Inclination: 51
6446 deg
RA of node: 8
8244 deg
Eccentricity:
0005595
Arg of perigee: 166
0689 deg
Mean anomaly: 194
0619 deg
Mean motion: 15
55361809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 319
Coasting Arc #5 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2015/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3663734
89 A = 6777529
59 meter
Y = 3672359
91 meter E =
0013216
Z = 4358229
55 I = 51
66265
XDOT = -6448
372883 Wp = 130
09758
YDOT = 2336
299520 meter/sec RA = 3
43068 deg
ZDOT = 3436
961792 TA = 284
99702
MA = 285
14327
Ha = 220
144 n
mi
Hp = 212
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12020127
61 X = 3601226
22
Y = 12048424
92 feet Y = 3712980
60 meter
Z = 14298653
37 Z = 4375875
94
XDOT = -21156
079013 XDOT = -6490
714562
YDOT = 7665
024671 feet/sec YDOT = 2263
952729 meter/sec
ZDOT = 11276
121366 ZDOT = 3405
533316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16214926
33 X = -4942309
55
Y = 4955811
01 feet Y = 1510531
19 meter
Z = 14374129
55 Z = 4381234
69
XDOT = 3447
371166 XDOT = 1050
758731
YDOT = -21175
228892 feet/sec YDOT = -6454
209766 meter/sec
ZDOT = 11139
829859 ZDOT = 3395
420141
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 15328
55433448
00016717 00000-0 10270-3 0 9046
2 25544 51
6435 3
6902 0005572 168
7704 191
3575 15
55383068 12994
Satellite: ISS
Catalog Number: 25544
Epoch time: 15328
55433448 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 3
6902 deg
Eccentricity:
0005572
Arg of perigee: 168
7704 deg
Mean anomaly: 191
3575 deg
Mean motion: 15
55383068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 324
Coasting Arc #6 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2015/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1472349
38 A = 6774109
09 meter
Y = -4087239
47 meter E =
0015061
Z = -5209778
72 I = 51
62024
XDOT = 7474
818261 Wp = 102
17947
YDOT = -1162
066178 meter/sec RA = 358
42248 deg
ZDOT = -1206
855317 TA = 156
26131
MA = 156
19176
Ha = 220
069 n
mi
Hp = 212
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4830542
57 X = -1401227
72
Y = -13409578
33 feet Y = -4103306
35 meter
Z = -17092449
86 Z = -5216758
71
XDOT = 24523
681958 XDOT = 7493
119801
YDOT = -3812
553077 feet/sec YDOT = -1078
375441 meter/sec
ZDOT = -3959
499070 ZDOT = -1170
498889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14101512
26 X = 4298140
94
Y = 1815480
93 feet Y = 553358
59 meter
Z = -17121745
11 Z = -5218707
91
XDOT = -7503
566199 XDOT = -2287
086977
YDOT = 22611
920000 feet/sec YDOT = 6892
113216 meter/sec
ZDOT = -3802
165003 ZDOT = -1158
899893
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 15329
51807779
00016717 00000-0 10270-3 0 9056
2 25544 51
6444 358
8763 0005529 173
1160 187
0071 15
55395805 13145
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
51807779 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 358
8763 deg
Eccentricity:
0005529
Arg of perigee: 173
1160 deg
Mean anomaly: 187
0071 deg
Mean motion: 15
55395805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 325
Coasting Arc #7 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2015/329/19:59:55
898
Vector Time (MET): N/A
Weight (LBS) : 906102
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5467568
14 A = 6784927
20 meter
Y = -2684758
20 meter E =
0001636
Z = -2991331
33 I = 51
63614
XDOT = 4526
184773 Wp = 147
70116
YDOT = 3680
814556 meter/sec RA = 356
72305 deg
ZDOT = 4969
306830 TA = 178
09128
MA = 178
09065
Ha = 219
993 n
mi
Hp = 215
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17938215
68 X = 5511714
47
Y = -8808261
80 feet Y = -2623369
25 meter
Z = -9814079
17 Z = -2964663
29
XDOT = 14849
687577 XDOT = 4460
549061
YDOT = 12076
163243 feet/sec YDOT = 3731
062082 meter/sec
ZDOT = 16303
500098 ZDOT = 4991
135400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17415123
60 X = 5308129
67
Y = -9916549
23 feet Y = -3022564
20 meter
Z = -9698284
86 Z = -2956037
23
XDOT = 14747
697543 XDOT = 4495
098211
YDOT = 9862
986239 feet/sec YDOT = 3006
238206 meter/sec
ZDOT = 16397
037081 ZDOT = 4997
816902
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 15329
83932176
00016717 00000-0 10270-3 0 9062
2 25544 51
6450 357
2708 0004589 226
6650 133
4121 15
54367954 13196
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
83932176 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 357
2708 deg
Eccentricity:
0004589
Arg of perigee: 226
6650 deg
Mean anomaly: 133
4121 deg
Mean motion: 15
54367954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 322
Coasting Arc #8 (Orbit 1334)
---------------------------------------
Vector Time (GMT): 2015/330/19:59:55
898
Vector Time (MET): N/A
Weight (LBS) : 906102
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6337410
33 A = 6787926
16 meter
Y = 1997673
14 meter E =
0013025
Z = 1347016
92 I = 51
61435
XDOT = -2590
130460 Wp = 139
50994
YDOT = -4280
170080 meter/sec RA = 351
74524 deg
ZDOT = -5816
466545 TA = 25
80757
MA = 25
74265
Ha = 219
930 n
mi
Hp = 215
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20792028
66 X = -6365821
21
Y = 6554045
73 feet Y = 1926645
08 meter
Z = 4419346
86 Z = 1316161
61
XDOT = -8497
803347 XDOT = -2513
821341
YDOT = -14042
552755 feet/sec YDOT = -4308
707548 meter/sec
ZDOT = -19082
895490 ZDOT = -5828
864067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20231808
57 X = -6166655
25
Y = 8191587
06 feet Y = 2496795
74 meter
Z = 4285606
26 Z = 1306252
79
XDOT = -8869
989954 XDOT = -2703
572938
YDOT = -11857
456602 feet/sec YDOT = -3614
152772 meter/sec
ZDOT = -19135
553337 ZDOT = -5832
516657
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 15330
86799455
00016717 00000-0 10270-3 0 9079
2 25544 51
6449 352
1407 0004579 229
8622 130
2130 15
54363317 13359
Satellite: ISS
Catalog Number: 25544
Epoch time: 15330
86799455 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 352
1407 deg
Eccentricity:
0004579
Arg of perigee: 229
8622 deg
Mean anomaly: 130
2130 deg
Mean motion: 15
54363317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1335
Checksum: 312
Coasting Arc #9 (Orbit 1350)
---------------------------------------
Vector Time (GMT): 2015/331/19:59:55
898
Vector Time (MET): N/A
Weight (LBS) : 906102
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6661346
12 A = 6788426
59 meter
Y = -1207222
93 meter E =
0008458
Z = 440515
23 I = 51
58534
XDOT = 463
755004 Wp = 46
95055
YDOT = 4768
018222 meter/sec RA = 346
77005 deg
ZDOT = 5986
842218 TA = 317
80309
MA = 317
86816
Ha = 219
663 n
mi
Hp = 215
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21854810
09 X = 6672210
60
Y = -3960705
15 feet Y = -1132670
65 meter
Z = 1445259
93 Z = 472901
46
XDOT = 1521
505917 XDOT = 381
321187
YDOT = 15643
104404 feet/sec YDOT = 4772
742856 meter/sec
ZDOT = 19641
870793 ZDOT = 5988
895224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21359339
34 X = 6510326
63
Y = -6055878
73 feet Y = -1845831
84 meter
Z = 1585446
84 Z = 483244
20
XDOT = 2461
572357 XDOT = 750
287254
YDOT = 13878
919372 feet/sec YDOT = 4230
294625 meter/sec
ZDOT = 19649
729042 ZDOT = 5989
237412
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 15331
89664812
00016717 00000-0 10270-3 0 9082
2 25544 51
6452 347
0100 0004503 235
7463 124
3264 15
54405022 13512
Satellite: ISS
Catalog Number: 25544
Epoch time: 15331
89664812 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 347
0100 deg
Eccentricity:
0004503
Arg of perigee: 235
7463 deg
Mean anomaly: 124
3264 deg
Mean motion: 15
54405022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1351
Checksum: 278
Coasting Arc #10 (Orbit 1365)
---------------------------------------
Vector Time (GMT): 2015/332/19:59:55
898
Vector Time (MET): N/A
Weight (LBS) : 906102
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6408599
93 A = 6786366
00 meter
Y = 265687
75 meter E =
0006785
Z = -2204086
61 I = 51
54831
XDOT = 1664
948340 Wp = 178
22441
YDOT = -5115
791187 meter/sec RA = 341
79124 deg
ZDOT = -5464
764102 TA = 26
29323
MA = 26
25881
Ha = 219
456 n
mi
Hp = 215
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21025590
31 X = -6400387
89
Y = 871678
97 feet Y = 194068
64 meter
Z = -7231255
27 Z = -2235198
64
XDOT = 5462
428937 XDOT = 1748
576621
YDOT = -16784
091822 feet/sec YDOT = -5096
704632 meter/sec
ZDOT = -17929
016083 ZDOT = -5456
473296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20743238
51 X = -6322539
10
Y = 3254276
09 feet Y = 991903
35 meter
Z = -7365736
07 Z = -2245076
35
XDOT = 3866
605605 XDOT = 1178
541388
YDOT = -15799
053107 feet/sec YDOT = -4815
551387 meter/sec
ZDOT = -17892
110337 ZDOT = -5453
515231
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 15332
86099451
00016717 00000-0 10270-3 0 9092
2 25544 51
6457 342
2005 0004658 238
6991 121
3706 15
54411738 13662
Satellite: ISS
Catalog Number: 25544
Epoch time: 15332
86099451 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 342
2005 deg
Eccentricity:
0004658
Arg of perigee: 238
6991 deg
Mean anomaly: 121
3706 deg
Mean motion: 15
54411738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1366
Checksum: 318
Coasting Arc #11 (Orbit 1381)
---------------------------------------
Vector Time (GMT): 2015/333/19:59:55
898
Vector Time (MET): N/A
Weight (LBS) : 906102
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5629595
46 A = 6782480
24 meter
Y = 785564
54 meter E =
0008290
Z = 3696475
05 I = 51
50580
XDOT = -3565
404500 Wp = 112
12600
YDOT = 5251
317011 meter/sec RA = 336
80089 deg
ZDOT = 4303
177852 TA = 292
02524
MA = 292
11329
Ha = 219
291 n
mi
Hp = 215
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18469801
38 X = 5602436
50
Y = 2577311
47 feet Y = 848366
30 meter
Z = 12127542
83 Z = 3723756
76
XDOT = -11697
521326 XDOT = -3644
764353
YDOT = 17228
730351 feet/sec YDOT = 5211
002303 meter/sec
ZDOT = 14118
037571 ZDOT = 4285
665296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18571089
09 X = 5660467
96
Y = 147912
09 feet Y = 45083
61 meter
Z = 12245250
69 Z = 3732352
41
XDOT = -9419
123255 XDOT = -2870
948768
YDOT = 17271
022629 feet/sec YDOT = 5264
207697 meter/sec
ZDOT = 14041
264038 ZDOT = 4279
777279
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 15333
88961356
00016717 00000-0 10270-3 0 9109
2 25544 51
6458 337
0697 0004416 243
5031 116
5669 15
54452249 13828
Satellite: ISS
Catalog Number: 25544
Epoch time: 15333
88961356 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 337
0697 deg
Eccentricity:
0004416
Arg of perigee: 243
5031 deg
Mean anomaly: 116
5669 deg
Mean motion: 15
54452249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1382
Checksum: 321
Coasting Arc #12 (Orbit 1396)
---------------------------------------
Vector Time (GMT): 2015/334/19:59:55
898
Vector Time (MET): N/A
Weight (LBS) : 906102
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4407736
73 A = 6778465
13 meter
Y = -1949805
23 meter E =
0006883
Z = -4772852
66 I = 51
46393
XDOT = 5088
858851 Wp = 73
52414
YDOT = -5095
926835 meter/sec RA = 331
79696 deg
ZDOT = -2619
009843 TA = 170
57479
MA = 170
56187
Ha = 219
063 n
mi
Hp = 215
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14461078
51 X = -4362421
13
Y = -6396998
80 feet Y = -1998841
85 meter
Z = -15658965
43 Z = -4794154
69
XDOT = 16695
731139 XDOT = 5158
186747
YDOT = -16718
920062 feet/sec YDOT = -5038
632095 meter/sec
ZDOT = -8592
551979 ZDOT = -2594
120924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15149311
98 X = -4617510
29
Y = -4202949
20 feet Y = -1281058
92 meter
Z = -15750592
00 Z = -4800780
44
XDOT = 13785
281663 XDOT = 4201
753851
YDOT = -17909
669265 feet/sec YDOT = -5458
867192 meter/sec
ZDOT = -8483
948384 ZDOT = -2585
907467
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 15334
85392587
00016717 00000-0 10270-3 0 9112
2 25544 51
6458 332
2600 0004543 248
4473 111
6196 15
54505805 13978
Satellite: ISS
Catalog Number: 25544
Epoch time: 15334
85392587 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 332
2600 deg
Eccentricity:
0004543
Arg of perigee: 248
4473 deg
Mean anomaly: 111
6196 deg
Mean motion: 15
54505805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1397
Checksum: 314
Coasting Arc #13 (Orbit 1412)
---------------------------------------
Vector Time (GMT): 2015/335/19:59:55
898
Vector Time (MET): N/A
Weight (LBS) : 906102
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2895396
68 A = 6776313
02 meter
Y = 3127350
26 meter E =
0003088
Z = 5269905
04 I = 51
42934
XDOT = -6106
725992 Wp = 211
14135
YDOT = 4595
336034 meter/sec RA = 326
78174 deg
ZDOT = 625
698663 TA = 232
85394
MA = 232
88215
Ha = 218
914 n
mi
Hp = 215
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9499332
94 X = 2834611
39
Y = 10260335
51 feet Y = 3159388
46 meter
Z = 17289714
70 Z = 5283822
82
XDOT = -20035
190263 XDOT = -6160
697717
YDOT = 15076
561792 feet/sec YDOT = 4526
744798 meter/sec
ZDOT = 2052
817136 ZDOT = 595
902337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10952769
20 X = 3338404
05
Y = 8572538
58 feet Y = 2612909
76 meter
Z = 17349192
34 Z = 5288033
82
XDOT = -16660
887878 XDOT = -5078
238625
YDOT = 17378
802059 feet/sec YDOT = 5297
058868 meter/sec
ZDOT = 1923
125299 ZDOT = 586
168591
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 15335
88250955
00016717 00000-0 10270-3 0 9129
2 25544 51
6460 327
1296 0004491 251
1252 108
9414 15
54522904 14133
Satellite: ISS
Catalog Number: 25544
Epoch time: 15335
88250955 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 327
1296 deg
Eccentricity:
0004491
Arg of perigee: 251
1252 deg
Mean anomaly: 108
9414 deg
Mean motion: 15
54522904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1413
Checksum: 296
Coasting Arc #14 (Orbit 1427)
---------------------------------------
Vector Time (GMT): 2015/336/19:59:55
898
Vector Time (MET): N/A
Weight (LBS) : 906102
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1244534
09 A = 6776836
14 meter
Y = -4245082
81 meter E =
0009808
Z = -5142473
75 I = 51
40441
XDOT = 6556
525545 Wp = 112
65323
YDOT = -3687
412691 meter/sec RA = 321
76098 deg
ZDOT = 1455
708757 TA = 171
42435
MA = 171
40758
Ha = 218
829 n
mi
Hp = 215
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4083117
09 X = -1171991
72
Y = -13927437
05 feet Y = -4258594
29 meter
Z = -16871633
05 Z = -5148343
38
XDOT = 21510
910582 XDOT = 6590
200482
YDOT = -12097
810666 feet/sec YDOT = -3613
905038 meter/sec
ZDOT = 4775
947364 ZDOT = 1487
640935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6442581
25 X = -1963698
76
Y = -12973509
27 feet Y = -3954325
62 meter
Z = -16896110
62 Z = -5149934
52
XDOT = 17974
807722 XDOT = 5478
721394
YDOT = -15333
155230 feet/sec YDOT = -4673
545714 meter/sec
ZDOT = 4914
667975 ZDOT = 1497
990799
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 15336
84678938
00016717 00000-0 10270-3 0 9132
2 25544 51
6452 322
3188 0004563 255
6931 104
3715 15
54561376 14280
Satellite: ISS
Catalog Number: 25544
Epoch time: 15336
84678938 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 322
3188 deg
Eccentricity:
0004563
Arg of perigee: 255
6931 deg
Mean anomaly: 104
3715 deg
Mean motion: 15
54561376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1428
Checksum: 326
Coasting Arc #15 (Orbit 1443)
---------------------------------------
Vector Time (GMT): 2015/337/19:59:55
898
Vector Time (MET): N/A
Weight (LBS) : 906102
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -382939
46 A = 6779789
48 meter
Y = 5160540
15 meter E =
0004997
Z = 4377968
68 I = 51
39046
XDOT = -6462
938164 Wp = 61
59783
YDOT = 2384
654190 meter/sec RA = 316
74514 deg
ZDOT = -3370
957714 TA = 62
65534
MA = 62
60448
Ha = 218
613 n
mi
Hp = 215
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1256363
05 X = -461884
09
Y = 16930906
00 feet Y = 5155816
39 meter
Z = 14363414
32 Z = 4375916
77
XDOT = -21203
865366 XDOT = -6472
748656
YDOT = 7823
668603 feet/sec YDOT = 2312
326553 meter/sec
ZDOT = -11059
572551 ZDOT = -3402
377400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2044763
03 X = 623243
77
Y = 16862327
58 feet Y = 5139637
45 meter
Z = 14353485
62 Z = 4374942
42
XDOT = -17926
086191 XDOT = -5463
871071
YDOT = 11718
529978 feet/sec YDOT = 3571
807937 meter/sec
ZDOT = -11195
800733 ZDOT = -3412
480063
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 15337
87533603
00016717 00000-0 10270-3 0 9146
2 25544 51
6454 317
1884 0004628 260
6525 99
4105 15
54615245 14444
Satellite: ISS
Catalog Number: 25544
Epoch time: 15337
87533603 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 317
1884 deg
Eccentricity:
0004628
Arg of perigee: 260
6525 deg
Mean anomaly: 99
4105 deg
Mean motion: 15
54615245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1444
Checksum: 314
Coasting Arc #16 (Orbit 1458)
---------------------------------------
Vector Time (GMT): 2015/338/19:59:55
898
Vector Time (MET): N/A
Weight (LBS) : 906102
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1837587
45 A = 6783963
23 meter
Y = -5757125
15 meter E =
0000818
Z = -3081177
72 I = 51
38033
XDOT = 5871
793618 Wp = 339
01764
YDOT = -733
794184 meter/sec RA = 311
73739 deg
ZDOT = 4873
314542 TA = 345
43600
MA = 345
43836
Ha = 218
611 n
mi
Hp = 215
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6028830
21 X = 1916795
79
Y = -18888205
86 feet Y = -5736133
10 meter
Z = -10108850
80 Z = -3072058
71
XDOT = 19264
414758 XDOT = 5855
889734
YDOT = -2407
461232 feet/sec YDOT = -668
220919 meter/sec
ZDOT = 15988
564769 ZDOT = 4901
800184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1877035
35 X = 572120
37
Y = -19758707
44 feet Y = -6022454
03 meter
Z = -10068276
77 Z = -3068810
76
XDOT = 16751
295294 XDOT = 5105
794806
YDOT = -6618
018838 feet/sec YDOT = -2017
172142 meter/sec
ZDOT = 16111
771846 ZDOT = 4910
868059
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 15338
83958364
00016717 00000-0 10270-3 0 9159
2 25544 51
6440 312
3773 0004638 263
1308 96
9318 15
54599760 14598
Satellite: ISS
Catalog Number: 25544
Epoch time: 15338
83958364 = yrday
fracday
Element set: 915
Inclination: 51
6440 deg
RA of node: 312
3773 deg
Eccentricity:
0004638
Arg of perigee: 263
1308 deg
Mean anomaly: 96
9318 deg
Mean motion: 15
54599760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1459
Checksum: 341
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