[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 29th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
118/13:07:34
000 0
0 0
0 0
0
N/A 0
0 0
0 215
7
000/00:00:00
000 0
0 0
0 213
4
126/05:20:56
664 -0
7 4
9 4
9
N/A -4
1 -0
0 216
6
000/00:11:53
328 -2
7 0
2 215
2
Coasting Arc #1 (Orbit 2014)
---------------------------------------
Vector Time (GMT): 2015/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -863628
71 A = 6771585
49 meter
Y = -4186362
04 meter E =
0009009
Z = -5259803
54 I = 51
48642
XDOT = 7221
844501 Wp = 96
17101
YDOT = -2452
602088 meter/sec RA = 336
65490 deg
ZDOT = 766
462950 TA = 181
16982
MA = 181
17193
Ha = 215
790 n
mi
Hp = 213
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2833427
51 X = -791201
31
Y = -13734783
60 feet Y = -4195615
02 meter
Z = -17256573
29 Z = -5263822
76
XDOT = 23693
715553 XDOT = 7245
010123
YDOT = -8046
594776 feet/sec YDOT = -2371
713134 meter/sec
ZDOT = 2514
642225 ZDOT = 801
601876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9994460
83 X = -3046311
66
Y = -9809022
19 feet Y = -2989789
96 meter
Z = -17272977
44 Z = -5264803
53
XDOT = 14302
928707 XDOT = 4359
532670
YDOT = -19266
450557 feet/sec YDOT = -5872
414130 meter/sec
ZDOT = 2665
740515 ZDOT = 812
517709
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 15117
51467619
00016717 00000-0 10270-3 0 9001
2 25544 51
6459 337
1587 0005548 275
7924 84
2597 15
56185828 20156
Satellite: ISS
Catalog Number: 25544
Epoch time: 15117
51467619 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 337
1587 deg
Eccentricity:
0005548
Arg of perigee: 275
7924 deg
Mean anomaly: 84
2597 deg
Mean motion: 15
56185828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2015
Checksum: 341
Coasting Arc #2 (Orbit 2030)
---------------------------------------
Vector Time (GMT): 2015/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1607645
60 A = 6774909
58 meter
Y = 4872250
17 meter E =
0005223
Z = 4424217
87 I = 51
46959
XDOT = -6885
258533 Wp = 36
18443
YDOT = 731
144173 meter/sec RA = 331
62741 deg
ZDOT = -3300
982206 TA = 87
22040
MA = 87
16062
Ha = 215
809 n
mi
Hp = 213
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5274427
82 X = -1683500
14
Y = 15985072
74 feet Y = 4853848
57 meter
Z = 14515150
49 Z = 4416223
64
XDOT = -22589
430882 XDOT = -6876
887568
YDOT = 2398
766973 feet/sec YDOT = 654
195316 meter/sec
ZDOT = -10829
994114 ZDOT = -3334
409430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4859835
85 X = 1481277
97
Y = 16147609
17 feet Y = 4921791
28 meter
Z = 14479932
55 Z = 4413483
44
XDOT = -15814
878830 XDOT = -4820
375067
YDOT = 14617
874174 feet/sec YDOT = 4455
528048 meter/sec
ZDOT = -10973
408249 ZDOT = -3344
694834
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 15118
54214514
00016717 00000-0 10270-3 0 9010
2 25544 51
6462 332
0213 0005739 280
0944 79
9562 15
56242261 20319
Satellite: ISS
Catalog Number: 25544
Epoch time: 15118
54214514 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 332
0213 deg
Eccentricity:
0005739
Arg of perigee: 280
0944 deg
Mean anomaly: 79
9562 deg
Mean motion: 15
56242261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2031
Checksum: 283
Coasting Arc #3 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2015/118/13:07:34
000
Vector Time (MET): N/A
Weight (LBS) : 926120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6227689
05 A = 6780792
37 meter
Y = -1256441
37 meter E =
0008926
Z = 2355165
62 I = 51
48575
XDOT = -950
136296 Wp = 58
40438
YDOT = 5390
063786 meter/sec RA = 331
43464 deg
ZDOT = 5377
481007 TA = 327
96994
MA = 328
02416
Ha = 215
668 n
mi
Hp = 213
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20432050
70 X = 6229835
42
Y = -4122182
98 feet Y = -1186787
14 meter
Z = 7726921
32 Z = 2385424
05
XDOT = -3117
245067 XDOT = -1036
460656
YDOT = 17683
936305 feet/sec YDOT = 5378
956399 meter/sec
ZDOT = 17642
654221 ZDOT = 5372
655390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9221651
02 X = 2810759
23
Y = -18638598
70 feet Y = -5681044
88 meter
Z = 7856856
39 Z = 2394769
83
XDOT = 10646
285756 XDOT = 3244
987898
YDOT = 12709
435452 feet/sec YDOT = 3873
835926 meter/sec
ZDOT = 17620
915893 ZDOT = 5370
855164
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 15118
60636138
00016717 00000-0 10270-3 0 9028
2 25544 51
6439 331
6984 0005667 278
1856 81
8655 15
56229474 20320
Satellite: ISS
Catalog Number: 25544
Epoch time: 15118
60636138 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 331
6984 deg
Eccentricity:
0005667
Arg of perigee: 278
1856 deg
Mean anomaly: 81
8655 deg
Mean motion: 15
56229474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 332
Coasting Arc #4 (Orbit 2046)
---------------------------------------
Vector Time (GMT): 2015/119/13:07:34
000
Vector Time (MET): N/A
Weight (LBS) : 926120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5287720
49 A = 6775506
32 meter
Y = -517587
43 meter E =
0004648
Z = -4209353
93 I = 51
44004
XDOT = 3467
853293 Wp = 28
80038
YDOT = -5786
756571 meter/sec RA = 326
42532 deg
ZDOT = -3642
398415 TA = 203
77535
MA = 203
79683
Ha = 215
913 n
mi
Hp = 213
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17348164
34 X = -5261092
02
Y = -1698121
50 feet Y = -576569
56 meter
Z = -13810216
30 Z = -4234976
21
XDOT = 11377
471433 XDOT = 3549
998042
YDOT = -18985
421822 feet/sec YDOT = -5747
517701 meter/sec
ZDOT = -11950
126032 ZDOT = -3625
352185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11693309
76 X = -3564120
82
Y = 12808849
69 feet Y = 3904137
39 meter
Z = -13919927
20 Z = -4242793
81
XDOT = -7419
043214 XDOT = -2261
324372
YDOT = -19687
191103 feet/sec YDOT = -6000
655848 meter/sec
ZDOT = -11875
941093 ZDOT = -3619
786845
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 15119
56959020
00016717 00000-0 10270-3 0 9033
2 25544 51
6430 326
8815 0005543 283
1097 76
9438 15
56255501 20476
Satellite: ISS
Catalog Number: 25544
Epoch time: 15119
56959020 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 326
8815 deg
Eccentricity:
0005543
Arg of perigee: 283
1097 deg
Mean anomaly: 76
9438 deg
Mean motion: 15
56255501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 313
Coasting Arc #5 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2015/120/13:07:34
000
Vector Time (MET): N/A
Weight (LBS) : 926120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3606941
58 A = 6771622
72 meter
Y = 2425925
84 meter E =
0002148
Z = 5194170
41 I = 51
40066
XDOT = -5306
639908 Wp = 255
82255
YDOT = 5416
995636 meter/sec RA = 321
39360 deg
ZDOT = 1154
931843 TA = 183
06897
MA = 183
07029
Ha = 215
986 n
mi
Hp = 213
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11833797
84 X = 3554314
54
Y = 7959074
27 feet Y = 2465967
08 meter
Z = 17041241
49 Z = 5211564
49
XDOT = -17410
235919 XDOT = -5372
429944
YDOT = 17772
295395 feet/sec YDOT = 5357
285537 meter/sec
ZDOT = 3789
146465 ZDOT = 1128
992724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13314103
83 X = 4058138
85
Y = -4856977
42 feet Y = -1480406
72 meter
Z = 17115313
49 Z = 5216747
55
XDOT = 3869
040787 XDOT = 1179
283632
YDOT = 23564
259158 feet/sec YDOT = 7182
386191 meter/sec
ZDOT = 3676
931224 ZDOT = 1120
728637
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 15120
59700940
00016717 00000-0 10270-3 0 9044
2 25544 51
6428 321
7423 0005543 287
1487 72
9060 15
56239921 20632
Satellite: ISS
Catalog Number: 25544
Epoch time: 15120
59700940 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 321
7423 deg
Eccentricity:
0005543
Arg of perigee: 287
1487 deg
Mean anomaly: 72
9060 deg
Mean motion: 15
56239921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 300
Coasting Arc #6 (Orbit 2077)
---------------------------------------
Vector Time (GMT): 2015/121/13:07:34
000
Vector Time (MET): N/A
Weight (LBS) : 926120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1521490
62 A = 6771828
75 meter
Y = -4187427
92 meter E =
0008092
Z = -5107017
75 I = 51
37741
XDOT = 6222
443526 Wp = 96
93013
YDOT = -4188
801541 meter/sec RA = 316
35220 deg
ZDOT = 1581
949832 TA = 188
37848
MA = 188
39200
Ha = 216
020 n
mi
Hp = 213
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4991767
14 X = -1449744
32
Y = -13738280
57 feet Y = -4204041
34 meter
Z = -16755307
57 Z = -5114234
48
XDOT = 20414
840963 XDOT = 6261
136581
YDOT = -13742
787209 feet/sec YDOT = -4119
001678 meter/sec
ZDOT = 5190
124120 ZDOT = 1612
271983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14070589
63 X = -4288715
72
Y = -3829686
67 feet Y = -1167288
50 meter
Z = -16785423
18 Z = -5116196
99
XDOT = 67
795176 XDOT = 20
663970
YDOT = -23553
117527 feet/sec YDOT = -7178
990222 meter/sec
ZDOT = 5320
874711 ZDOT = 1621
802612
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 15121
56018837
00016717 00000-0 10270-3 0 9050
2 25544 51
6424 316
9241 0005515 289
6096 70
4462 15
56326531 20783
Satellite: ISS
Catalog Number: 25544
Epoch time: 15121
56018837 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 316
9241 deg
Eccentricity:
0005515
Arg of perigee: 289
6096 deg
Mean anomaly: 70
4462 deg
Mean motion: 15
56326531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 307
Coasting Arc #7 (Orbit 2093)
---------------------------------------
Vector Time (GMT): 2015/122/13:07:34
000
Vector Time (MET): N/A
Weight (LBS) : 926120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -631235
69 A = 6776314
80 meter
Y = 5479802
48 meter E =
0007054
Z = 3934235
84 I = 51
37002
XDOT = -6171
008715 Wp = 54
00920
YDOT = 2171
404958 meter/sec RA = 311
31994 deg
ZDOT = -4005
449314 TA = 77
97636
MA = 77
89731
Ha = 216
181 n
mi
Hp = 213
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2070983
22 X = -711576
65
Y = 17978354
59 feet Y = 5472294
54 meter
Z = 12907597
89 Z = 3930973
98
XDOT = -20246
091586 XDOT = -6175
373876
YDOT = 7124
032016 feet/sec YDOT = 2102
372131 meter/sec
ZDOT = -13141
237908 ZDOT = -4035
438165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13740306
80 X = 4188045
51
Y = 11794154
18 feet Y = 3594858
19 meter
Z = 12892563
15 Z = 3929653
25
XDOT = -4441
994558 XDOT = -1353
919941
YDOT = 19713
720182 feet/sec YDOT = 6008
741911 meter/sec
ZDOT = -13270
162819 ZDOT = -4044
745627
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 15122
58755494
00016717 00000-0 10270-3 0 9061
2 25544 51
6421 311
7852 0005668 293
3109 66
7448 15
56349842 20947
Satellite: ISS
Catalog Number: 25544
Epoch time: 15122
58755494 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 311
7852 deg
Eccentricity:
0005668
Arg of perigee: 293
3109 deg
Mean anomaly: 66
7448 deg
Mean motion: 15
56349842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2094
Checksum: 332
Coasting Arc #8 (Orbit 2108)
---------------------------------------
Vector Time (GMT): 2015/123/13:07:34
000
Vector Time (MET): N/A
Weight (LBS) : 926120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2492999
75 A = 6781176
04 meter
Y = -5997954
54 meter E =
0007974
Z = -1929743
79 I = 51
36703
XDOT = 5250
205609 Wp = 356
09226
YDOT = 388
486203 meter/sec RA = 306
30567 deg
ZDOT = 5581
610096 TA = 342
52644
MA = 342
55387
Ha = 216
256 n
mi
Hp = 212
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8179133
05 X = 2569259
20
Y = -19678328
55 feet Y = -5969649
84 meter
Z = -6331180
42 Z = -1917447
65
XDOT = 17225
084020 XDOT = 5218
357295
YDOT = 1274
561033 feet/sec YDOT = 447
019493 meter/sec
ZDOT = 18312
369081 ZDOT = 5607
037760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12080523
83 X = -3682143
66
Y = -17574830
20 feet Y = -5356808
24 meter
Z = -6277337
40 Z = -1913332
44
XDOT = 9065
605163 XDOT = 2763
196454
YDOT = -12803
525240 feet/sec YDOT = -3902
514493 meter/sec
ZDOT = 18421
251674 ZDOT = 5614
797510
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 15123
55068777
00016717 00000-0 10270-3 0 9071
2 25544 51
6426 306
9666 0005552 297
1387 62
9201 15
56399782 21093
Satellite: ISS
Catalog Number: 25544
Epoch time: 15123
55068777 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 306
9666 deg
Eccentricity:
0005552
Arg of perigee: 297
1387 deg
Mean anomaly: 62
9201 deg
Mean motion: 15
56399782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2109
Checksum: 338
Coasting Arc #9 (Orbit 2124)
---------------------------------------
Vector Time (GMT): 2015/124/13:07:34
000
Vector Time (MET): N/A
Weight (LBS) : 926120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3857248
11 A = 6782376
38 meter
Y = 5550944
28 meter E =
0005637
Z = -514614
72 I = 51
35367
XDOT = -3687
132668 Wp = 154
58203
YDOT = -3112
133515 meter/sec RA = 301
30463 deg
ZDOT = -5962
094532 TA = 30
99573
MA = 30
96247
Ha = 216
394 n
mi
Hp = 212
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12655013
48 X = -3916533
55
Y = 18211759
45 feet Y = 5507478
52 meter
Z = -1688368
50 Z = -533496
92
XDOT = -12096
891956 XDOT = -3623
095750
YDOT = -10210
411794 feet/sec YDOT = -3153
007418 meter/sec
ZDOT = -19560
677599 ZDOT = -5979
850746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8800092
66 X = 2682268
24
Y = 20349260
25 feet Y = 6202454
52 meter
Z = -1770342
62 Z = -539600
43
XDOT = -13507
851591 XDOT = -4117
193165
YDOT = 4141
182764 feet/sec YDOT = 1262
232506 meter/sec
ZDOT = -19636
164614 ZDOT = -5985
102974
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 15124
57800244
00016717 00000-0 10270-3 0 9088
2 25544 51
6424 301
8273 0005748 303
1843 56
8760 15
56479811 21253
Satellite: ISS
Catalog Number: 25544
Epoch time: 15124
57800244 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 301
8273 deg
Eccentricity:
0005748
Arg of perigee: 303
1843 deg
Mean anomaly: 56
8760 deg
Mean motion: 15
56479811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2125
Checksum: 305
Coasting Arc #10 (Orbit 2140)
---------------------------------------
Vector Time (GMT): 2015/125/13:07:34
000
Vector Time (MET): N/A
Weight (LBS) : 926120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4570064
32 A = 6778956
02 meter
Y = -4111091
99 meter E =
0010033
Z = 2843343
08 I = 51
32728
XDOT = 1794
362744 Wp = 58
21250
YDOT = 5493
367798 meter/sec RA = 296
29768 deg
ZDOT = 5050
676027 TA = 334
31635
MA = 334
36615
Ha = 216
308 n
mi
Hp = 212
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14993649
34 X = 4601883
68
Y = -13487834
61 feet Y = -4059808
67 meter
Z = 9328553
42 Z = 2865621
27
XDOT = 5887
016876 XDOT = 1708
266424
YDOT = 18022
860230 feet/sec YDOT = 5512
952073 meter/sec
ZDOT = 16570
459406 ZDOT = 5059
183829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3918395
72 X = -1194327
01
Y = -19737589
03 feet Y = -6016017
14 meter
Z = 9424800
61 Z = 2872679
22
XDOT = 16999
179312 XDOT = 5181
349854
YDOT = 4566
947080 feet/sec YDOT = 1392
005470 meter/sec
ZDOT = 16605
864355 ZDOT = 5061
467455
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 15125
60529243
00016717 00000-0 10270-3 0 9091
2 25544 51
6430 296
6875 0005617 304
8235 55
2390 15
56492595 21411
Satellite: ISS
Catalog Number: 25544
Epoch time: 15125
60529243 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 296
6875 deg
Eccentricity:
0005617
Arg of perigee: 304
8235 deg
Mean anomaly: 55
2390 deg
Mean motion: 15
56492595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2141
Checksum: 316
Coasting Arc #11 (Orbit 2150)
---------------------------------------
Vector Time (GMT): 2015/126/05:26:53
328
Vector Time (MET): N/A
Weight (LBS) : 925597
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4641432
08 A = 6775186
93 meter
Y = 1050259
95 meter E =
0006108
Z = -4827824
46 I = 51
29960
XDOT = 915
428672 Wp = 40
47181
YDOT = -7207
656908 meter/sec RA = 292
88070 deg
ZDOT = -2445
241316 TA = 205
38900
MA = 205
41902
Ha = 216
628 n
mi
Hp = 215
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15227795
54 X = -4629379
15
Y = 3445734
75 feet Y = 998423
93 meter
Z = -15839319
11 Z = -4850342
78
XDOT = 3003
374909 XDOT = 1007
836671
YDOT = -23647
168333 feet/sec YDOT = -7196
903244 meter/sec
ZDOT = -8022
445264 ZDOT = -2440
569973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11432946
46 X = -3484762
08
Y = -10486857
31 feet Y = -3196394
11 meter
Z = -15936010
60 Z = -4857296
03
XDOT = 20426
625535 XDOT = 6226
035463
YDOT = -10096
929227 feet/sec YDOT = -3077
544028 meter/sec
ZDOT = -8001
054029 ZDOT = -2438
721268
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 15126
24734467
00016717 00000-0 10270-3 0 9100
2 25544 51
6463 293
4808 0007354 278
5605 81
4715 15
55549506 21513
Satellite: ISS
Catalog Number: 25544
Epoch time: 15126
24734467 = yrday
fracday
Element set: 910
Inclination: 51
6463 deg
RA of node: 293
4808 deg
Eccentricity:
0007354
Arg of perigee: 278
5605 deg
Mean anomaly: 81
4715 deg
Mean motion: 15
55549506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2151
Checksum: 317
Coasting Arc #12 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2015/127/05:26:53
328
Vector Time (MET): N/A
Weight (LBS) : 925597
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4048440
67 A = 6773078
92 meter
Y = 1255930
95 meter E =
0005194
Z = 5287047
24 I = 51
28142
XDOT = -2318
344596 Wp = 286
93716
YDOT = 7308
626971 meter/sec RA = 287
84251 deg
ZDOT = 40
587314 TA = 162
68298
MA = 162
66526
Ha = 216
890 n
mi
Hp = 215
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13282285
67 X = 4008412
74
Y = 4120508
36 feet Y = 1300979
26 meter
Z = 17345955
50 Z = 5306616
92
XDOT = -7606
117441 XDOT = -2400
096259
YDOT = 23978
434943 feet/sec YDOT = 7282
244625 meter/sec
ZDOT = 133
160480 ZDOT = 29
126743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4322806
52 X = 1317591
43
Y = 13107367
80 feet Y = 3995125
71 meter
Z = 17429576
22 Z = 5312534
83
XDOT = -22965
121514 XDOT = -6999
769038
YDOT = 7470
568730 feet/sec YDOT = 2277
029349 meter/sec
ZDOT = 82
663953 ZDOT = 25
195973
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 15127
27523717
00016717 00000-0 10270-3 0 9119
2 25544 51
6463 288
3456 0007535 282
2541 77
7769 15
55596171 21671
Satellite: ISS
Catalog Number: 25544
Epoch time: 15127
27523717 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 288
3456 deg
Eccentricity:
0007535
Arg of perigee: 282
2541 deg
Mean anomaly: 77
7769 deg
Mean motion: 15
55596171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 334
Coasting Arc #13 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2015/128/05:26:53
328
Vector Time (MET): N/A
Weight (LBS) : 925597
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3195287
27 A = 6774945
22 meter
Y = -3491795
08 meter E =
0004328
Z = -4851489
48 I = 51
27945
XDOT = 3419
736286 Wp = 108
08339
YDOT = -6436
065684 meter/sec RA = 282
80318 deg
ZDOT = 2380
400014 TA = 185
36341
MA = 185
36804
Ha = 217
092 n
mi
Hp = 215
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10483225
94 X = -3132436
68
Y = -11456020
59 feet Y = -3527175
26 meter
Z = -15916960
23 Z = -4866859
24
XDOT = 11219
607238 XDOT = 3479
888499
YDOT = -21115
701063 feet/sec YDOT = -6397
487722 meter/sec
ZDOT = 7809
711333 ZDOT = 2397
158499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3004191
12 X = 915677
45
Y = -15166846
46 feet Y = -4622854
80 meter
Z = -15982166
97 Z = -4871364
49
XDOT = 22504
210694 XDOT = 6859
283420
YDOT = -3847
449071 feet/sec YDOT = -1172
702477 meter/sec
ZDOT = 7882
739277 ZDOT = 2402
658932
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 15128
23886484
00016717 00000-0 10270-3 0 9120
2 25544 51
6467 283
5314 0007570 286
8131 73
2192 15
55610955 21824
Satellite: ISS
Catalog Number: 25544
Epoch time: 15128
23886484 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 283
5314 deg
Eccentricity:
0007570
Arg of perigee: 286
8131 deg
Mean anomaly: 73
2192 deg
Mean motion: 15
55610955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 318
Coasting Arc #14 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2015/129/05:26:53
328
Vector Time (MET): N/A
Weight (LBS) : 925597
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2160717
17 A = 6779454
09 meter
Y = 5340499
62 meter E =
0006033
Z = 3572643
51 I = 51
28853
XDOT = -4203
428861 Wp = 55
33807
YDOT = 4656
818943 meter/sec RA = 277
77578 deg
ZDOT = -4410
250736 TA = 82
17608
MA = 82
10760
Ha = 217
428 n
mi
Hp = 215
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7088967
09 X = 2083483
11
Y = 17521324
21 feet Y = 5364230
20 meter
Z = 11721271
37 Z = 3582952
56
XDOT = -13790
777103 XDOT = -4233
766561
YDOT = 15278
277371 feet/sec YDOT = 4609
643987 meter/sec
ZDOT = -14469
326563 ZDOT = -4430
743891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9602701
49 X = -2926903
41
Y = 16248821
81 feet Y = 4952640
89 meter
Z = 11764453
79 Z = 3585805
51
XDOT = -19277
048927 XDOT = -5875
644513
YDOT = -831
457579 feet/sec YDOT = -253
428270 meter/sec
ZDOT = -14558
020341 ZDOT = -4437
284600
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 15129
26670909
00016717 00000-0 10270-3 0 9138
2 25544 51
6465 278
3965 0007573 291
5182 68
5164 15
55648693 21981
Satellite: ISS
Catalog Number: 25544
Epoch time: 15129
26670909 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 278
3965 deg
Eccentricity:
0007573
Arg of perigee: 291
5182 deg
Mean anomaly: 68
5164 deg
Mean motion: 15
55648693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 353
Coasting Arc #15 (Orbit 2212)
---------------------------------------
Vector Time (GMT): 2015/130/05:26:53
328
Vector Time (MET): N/A
Weight (LBS) : 925597
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1026898
54 A = 6783601
09 meter
Y = -6487132
72 meter E =
0009670
Z = -1670694
63 I = 51
29958
XDOT = 4663
476978 Wp = 346
59180
YDOT = -2200
795190 meter/sec RA = 272
76374 deg
ZDOT = 5681
658263 TA = 354
99418
MA = 355
00385
Ha = 217
536 n
mi
Hp = 214
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3369089
71 X = -946165
89
Y = -21283243
84 feet Y = -6498164
73 meter
Z = -5481281
58 Z = -1675487
21
XDOT = 15300
121319 XDOT = 4660
140632
YDOT = -7220
456660 feet/sec YDOT = -2148
663946 meter/sec
ZDOT = 18640
611100 ZDOT = 5704
304528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14557210
79 X = 4437037
85
Y = -15880883
28 feet Y = -4840493
22 meter
Z = -5500621
97 Z = -1676589
58
XDOT = 13953
217314 XDOT = 4252
940637
YDOT = 6302
926729 feet/sec YDOT = 1921
132067 meter/sec
ZDOT = 18738
074017 ZDOT = 5711
364960
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 15130
23028887
00016717 00000-0 10270-3 0 9140
2 25544 51
6467 273
5815 0007740 295
2562 64
7790 15
55689236 22132
Satellite: ISS
Catalog Number: 25544
Epoch time: 15130
23028887 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 273
5815 deg
Eccentricity:
0007740
Arg of perigee: 295
2562 deg
Mean anomaly: 64
7790 deg
Mean motion: 15
55689236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2213
Checksum: 326
Coasting Arc #16 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2015/131/05:26:53
328
Vector Time (MET): N/A
Weight (LBS) : 925597
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -171984
09 A = 6784691
77 meter
Y = 6757591
44 meter E =
0004603
Z = -543823
97 I = 51
30216
XDOT = -4796
103477 Wp = 175
55440
YDOT = -600
513364 meter/sec RA = 267
76276 deg
ZDOT = -5953
150695 TA = 10
34309
MA = 10
33362
Ha = 217
751 n
mi
Hp = 214
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -564252
25 X = -244894
59
Y = 22170575
58 feet Y = 6755260
54 meter
Z = -1784199
38 Z = -544836
46
XDOT = -15735
247629 XDOT = -4760
113575
YDOT = -1970
188203 feet/sec YDOT = -653
945228 meter/sec
ZDOT = -19531
334301 ZDOT = -5976
361975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17441640
20 X = -5316211
93
Y = 13697520
32 feet Y = 4175004
19 meter
Z = -1789774
73 Z = -545523
34
XDOT = -7426
058681 XDOT = -2263
462686
YDOT = -12017
572888 feet/sec YDOT = -3662
956216 meter/sec
ZDOT = -19630
706385 ZDOT = -5983
439306
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 15131
25808388
00016717 00000-0 10270-3 0 9156
2 25544 51
6463 268
4462 0007747 298
1227 61
9143 15
55680681 22299
Satellite: ISS
Catalog Number: 25544
Epoch time: 15131
25808388 = yrday
fracday
Element set: 915
Inclination: 51
6463 deg
RA of node: 268
4462 deg
Eccentricity:
0007747
Arg of perigee: 298
1227 deg
Mean anomaly: 61
9143 deg
Mean motion: 15
55680681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 329
Coasting Arc #17 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2015/132/05:26:53
328
Vector Time (MET): N/A
Weight (LBS) : 925597
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1382257
76 A = 6781587
09 meter
Y = -6072843
45 meter E =
0009833
Z = 2666747
19 I = 51
29393
XDOT = 4598
224829 Wp = 42
61676
YDOT = 3318
815400 meter/sec RA = 262
75648 deg
ZDOT = 5170
273357 TA = 347
67442
MA = 347
69845
Ha = 217
899 n
mi
Hp = 214
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4534966
39 X = 1437108
85
Y = -19924027
05 feet Y = -6057079
44 meter
Z = 8749170
59 Z = 2673595
23
XDOT = 15086
039464 XDOT = 4535
655845
YDOT = 10888
501970 feet/sec YDOT = 3369
885926 meter/sec
ZDOT = 16962
839098 ZDOT = 5192
458832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18049155
44 X = 5501382
58
Y = -9551283
16 feet Y = -2911231
11 meter
Z = 8779620
60 Z = 2676028
36
XDOT = 768
749896 XDOT = 234
314968
YDOT = 17144
241482 feet/sec YDOT = 5225
564804 meter/sec
ZDOT = 17057
327684 ZDOT = 5199
073478
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 15132
28585193
00016717 00000-0 10270-3 0 9167
2 25544 51
6456 263
3093 0007956 304
0703 55
9695 15
55746495 22452
Satellite: ISS
Catalog Number: 25544
Epoch time: 15132
28585193 = yrday
fracday
Element set: 916
Inclination: 51
6456 deg
RA of node: 263
3093 deg
Eccentricity:
0007956
Arg of perigee: 304
0703 deg
Mean anomaly: 55
9695 deg
Mean motion: 15
55746495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 333
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