[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 13th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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
105/14:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 218
1
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2015/103/12:58:42
434
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5525827
56 A = 6782774
61 meter
Y = -3159735
69 meter E =
0013255
Z = 2318386
51 I = 51
92411
XDOT = 777
044734 Wp = 131
46509
YDOT = -5358
671785 meter/sec RA = 46
34025 deg
ZDOT = -5439
788909 TA = 22
76629
MA = 22
70756
Ha = 218
617 n
mi
Hp = 213
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18129355
50 X = -5501345
82
Y = -10366586
92 feet Y = -3221392
03 meter
Z = 7606254
97 Z = 2291602
80
XDOT = 2549
359365 XDOT = 863
333427
YDOT = -17580
944178 feet/sec YDOT = -5349
500342 meter/sec
ZDOT = -17847
076472 ZDOT = -5435
804143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20827332
29 X = -6348170
88
Y = 2021707
92 feet Y = 616216
57 meter
Z = 7491975
48 Z = 2283554
13
XDOT = -7822
857372 XDOT = -2384
406927
YDOT = -14378
076458 feet/sec YDOT = -4382
437704 meter/sec
ZDOT = -17828
975744 ZDOT = -5434
271807
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 15103
57745229
00016717 00000-0 10270-3 0 9008
2 25544 51
6453 46
8181 0005674 215
8114 144
2659 15
55622921 17982
Satellite: ISS
Catalog Number: 25544
Epoch time: 15103
57745229 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 46
8181 deg
Eccentricity:
0005674
Arg of perigee: 215
8114 deg
Mean anomaly: 144
2659 deg
Mean motion: 15
55622921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 314
Coasting Arc #2 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2015/104/12:58:42
434
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5176646
89 A = 6784913
01 meter
Y = 4378364
55 meter E =
0006190
Z = -174381
39 I = 51
90888
XDOT = -2940
109522 Wp = 47
81285
YDOT = 3710
788106 meter/sec RA = 41
37947 deg
ZDOT = 6031
665870 TA = 310
31501
MA = 310
36908
Ha = 218
331 n
mi
Hp = 213
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16983749
63 X = 5128149
32
Y = 14364713
08 feet Y = 4435982
01 meter
Z = -572117
43 Z = -149352
41
XDOT = -9646
028617 XDOT = -3010
685573
YDOT = 12174
501659 feet/sec YDOT = 3677
515850 meter/sec
ZDOT = 19788
930021 ZDOT = 6017
211571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22192392
28 X = 6764241
17
Y = 1549513
64 feet Y = 472291
76 meter
Z = -465600
71 Z = -141915
10
XDOT = -574
066653 XDOT = -174
975516
YDOT = 13978
810779 feet/sec YDOT = 4260
741526 meter/sec
ZDOT = 19726
235263 ZDOT = 6012
556508
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 15104
54104493
00016717 00000-0 10270-3 0 9019
2 25544 51
6451 42
0033 0005677 220
1289 139
9446 15
55644394 18130
Satellite: ISS
Catalog Number: 25544
Epoch time: 15104
54104493 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 42
0033 deg
Eccentricity:
0005677
Arg of perigee: 220
1289 deg
Mean anomaly: 139
9446 deg
Mean motion: 15
55644394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1813
Checksum: 293
Coasting Arc #3 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2015/105/12:58:42
434
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4099954
10 A = 6783040
19 meter
Y = -5001432
29 meter E =
0009144
Z = -2027136
56 I = 51
87985
XDOT = 4946
032232 Wp = 177
61371
YDOT = -1795
473585 meter/sec RA = 36
41830 deg
ZDOT = -5583
462131 TA = 24
73173
MA = 24
68792
Ha = 218
130 n
mi
Hp = 213
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13451292
98 X = -4033875
06
Y = -16408898
59 feet Y = -5046911
41 meter
Z = -6650710
49 Z = -2046892
39
XDOT = 16227
139869 XDOT = 4992
864558
YDOT = -5890
661367 feet/sec YDOT = -1739
902573 meter/sec
ZDOT = -18318
445312 ZDOT = -5559
321195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20602582
13 X = -6279667
03
Y = -4959990
48 feet Y = -1511805
10 meter
Z = -6734485
15 Z = -2052671
07
XDOT = 9090
964607 XDOT = 2770
926012
YDOT = -13073
715788 feet/sec YDOT = -3984
868572 meter/sec
ZDOT = -18214
572479 ZDOT = -5551
801691
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 15105
56885786
00016717 00000-0 10270-3 0 9024
2 25544 51
6464 36
8676 0005738 223
8096 136
2603 15
55676928 18292
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
56885786 = yrday
fracday
Element set: 902
Inclination: 51
6464 deg
RA of node: 36
8676 deg
Eccentricity:
0005738
Arg of perigee: 223
8096 deg
Mean anomaly: 136
2603 deg
Mean motion: 15
55676928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1829
Checksum: 350
Coasting Arc #4 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2015/105/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -151458
47 A = 6774944
53 meter
Y = -4779311
62 meter E =
0006883
Z = -4805239
15 I = 51
85201
XDOT = 6792
612748 Wp = 93
44779
YDOT = 2407
941167 meter/sec RA = 36
06302 deg
ZDOT = -2612
671554 TA = 150
88868
MA = 150
85029
Ha = 218
083 n
mi
Hp = 213
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -496910
99 X = -74661
63
Y = -15680156
22 feet Y = -4780576
45 meter
Z = -15765220
30 Z = -4805787
85
XDOT = 22285
474896 XDOT = 6777
873187
YDOT = 7900
069447 feet/sec YDOT = 2483
817904 meter/sec
ZDOT = -8571
757066 ZDOT = -2579
710245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14164815
74 X = -4317435
84
Y = -6739931
06 feet Y = -2054330
99 meter
Z = -15766664
68 Z = -4805679
39
XDOT = 16659
044600 XDOT = 5077
676794
YDOT = -15316
658591 feet/sec YDOT = -4668
517538 meter/sec
ZDOT = -8430
856813 ZDOT = -2569
725157
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 15105
63309454
00016717 00000-0 10270-3 0 9036
2 25544 51
6471 36
5470 0005706 225
0070 135
0622 15
55705247 18307
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
63309454 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 36
5470 deg
Eccentricity:
0005706
Arg of perigee: 225
0070 deg
Mean anomaly: 135
0622 deg
Mean motion: 15
55705247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 277
Coasting Arc #5 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2015/106/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2003151
93 A = 6772678
31 meter
Y = 3679968
23 meter E =
0004516
Z = 5322860
24 I = 51
81878
XDOT = -6633
002951 Wp = 204
92389
YDOT = -3848
132904 meter/sec RA = 31
06186 deg
ZDOT = 160
268214 TA = 243
52972
MA = 243
57605
Ha = 217
929 n
mi
Hp = 213
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6572020
77 X = -2070010
05
Y = 12073386
59 feet Y = 3657194
46 meter
Z = 17463452
23 Z = 5312966
41
XDOT = -21761
820705 XDOT = -6590
257764
YDOT = -12625
107952 feet/sec YDOT = -3922
068459 meter/sec
ZDOT = 525
814351 ZDOT = 128
150328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7941070
36 X = 2420438
24
Y = 11287254
07 feet Y = 3440355
04 meter
Z = 17420320
94 Z = 5309713
82
XDOT = -20043
272580 XDOT = -6109
189482
YDOT = 13481
185496 feet/sec YDOT = 4109
065339 meter/sec
ZDOT = 388
817988 ZDOT = 118
511723
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 15106
66088597
00016717 00000-0 10270-3 0 9043
2 25544 51
6475 31
4113 0005796 228
6974 131
3681 15
55734652 18463
Satellite: ISS
Catalog Number: 25544
Epoch time: 15106
66088597 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 31
4113 deg
Eccentricity:
0005796
Arg of perigee: 228
6974 deg
Mean anomaly: 131
3681 deg
Mean motion: 15
55734652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 330
Coasting Arc #6 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2015/107/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4063068
15 A = 6774482
14 meter
Y = -2314770
25 meter E =
0009742
Z = -4910134
46 I = 51
79731
XDOT = 5537
562159 Wp = 135
58449
YDOT = 4754
787273 meter/sec RA = 26
05729 deg
ZDOT = 2336
732874 TA = 157
26772
MA = 157
22455
Ha = 217
697 n
mi
Hp = 213
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13330276
09 X = 4112502
42
Y = -7594390
58 feet Y = -2269058
49 meter
Z = -16109365
01 Z = -4890276
26
XDOT = 18167
854853 XDOT = 5472
630297
YDOT = 15599
695776 feet/sec YDOT = 4816
349110 meter/sec
ZDOT = 7666
446436 ZDOT = 2363
475424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1227685
11 X = -374198
42
Y = -15382273
39 feet Y = -4688516
93 meter
Z = -16023767
49 Z = -4884044
33
XDOT = 20661
453548 XDOT = 6297
611042
YDOT = -9767
392275 feet/sec YDOT = -2977
101165 meter/sec
ZDOT = 7780
204317 ZDOT = 2371
406276
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 15107
62442321
00016717 00000-0 10270-3 0 9050
2 25544 51
6475 26
5963 0005825 233
3082 126
7537 15
55756306 18612
Satellite: ISS
Catalog Number: 25544
Epoch time: 15107
62442321 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 26
5963 deg
Eccentricity:
0005825
Arg of perigee: 233
3082 deg
Mean anomaly: 126
7537 deg
Mean motion: 15
55756306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 306
Coasting Arc #7 (Orbit 1876)
---------------------------------------
Vector Time (GMT): 2015/108/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5666116
64 A = 6779032
27 meter
Y = 864757
41 meter E =
0007554
Z = 3611346
88 I = 51
78431
XDOT = -3607
253793 Wp = 108
36229
YDOT = -5124
827697 meter/sec RA = 21
06418 deg
ZDOT = -4427
272163 TA = 28
91250
MA = 28
87067
Ha = 217
533 n
mi
Hp = 213
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18589621
52 X = -5692908
32
Y = 2837130
61 feet Y = 801245
72 meter
Z = 11848250
91 Z = 3583756
35
XDOT = -11834
822156 XDOT = -3528
172241
YDOT = -16813
739165 feet/sec YDOT = -5164
724608 meter/sec
ZDOT = -14525
171140 ZDOT = -4444
603248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4979313
25 X = -1517694
68
Y = 18210519
68 feet Y = 5550566
40 meter
Z = 11729782
64 Z = 3575237
75
XDOT = -18805
282980 XDOT = -5731
850252
YDOT = 4272
471526 feet/sec YDOT = 1302
249321 meter/sec
ZDOT = -14598
489019 ZDOT = -4449
619453
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 15108
65217699
00016717 00000-0 10270-3 0 9063
2 25544 51
6477 21
4610 0005771 238
0281 122
0312 15
55802433 18770
Satellite: ISS
Catalog Number: 25544
Epoch time: 15108
65217699 = yrday
fracday
Element set: 906
Inclination: 51
6477 deg
RA of node: 21
4610 deg
Eccentricity:
0005771
Arg of perigee: 238
0281 deg
Mean anomaly: 122
0312 deg
Mean motion: 15
55802433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1877
Checksum: 297
Coasting Arc #8 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2015/109/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6552321
63 A = 6783353
67 meter
Y = 523399
22 meter E =
0003499
Z = -1665991
55 I = 51
76824
XDOT = 1055
126440 Wp = 353
74446
YDOT = 4995
364506 meter/sec RA = 16
08504 deg
ZDOT = 5721
439502 TA = 348
02939
MA = 348
03770
Ha = 217
238 n
mi
Hp = 214
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21497118
20 X = 6554074
79
Y = 1717189
05 feet Y = 596681
25 meter
Z = -5465851
54 Z = -1634156
82
XDOT = 3461
700918 XDOT = 971
395524
YDOT = 16388
991161 feet/sec YDOT = 5006
695861 meter/sec
ZDOT = 18771
126975 ZDOT = 5726
361464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9977627
21 X = 3041180
77
Y = -19157091
23 feet Y = -5839081
41 meter
Z = -5329462
74 Z = -1624420
24
XDOT = 14999
456649 XDOT = 4571
834387
YDOT = 2586
629652 feet/sec YDOT = 788
404718 meter/sec
ZDOT = 18791
254372 ZDOT = 5727
574333
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 15109
61567901
00016717 00000-0 10270-3 0 9075
2 25544 51
6471 16
6455 0005892 241
9909 118
0649 15
55798770 18924
Satellite: ISS
Catalog Number: 25544
Epoch time: 15109
61567901 = yrday
fracday
Element set: 907
Inclination: 51
6471 deg
RA of node: 16
6455 deg
Eccentricity:
0005892
Arg of perigee: 241
9909 deg
Mean anomaly: 118
0649 deg
Mean motion: 15
55798770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 343
Coasting Arc #9 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2015/110/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6516406
20 A = 6784319
47 meter
Y = -1762582
47 meter E =
0010871
Z = -600116
32 I = 51
74041
XDOT = 1757
146802 Wp = 171
44522
YDOT = -4466
262293 meter/sec RA = 11
11533 deg
ZDOT = -5986
791254 TA = 15
02986
MA = 14
99758
Ha = 217
138 n
mi
Hp = 214
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21379285
43 X = -6493297
07
Y = -5782750
88 feet Y = -1835324
00 meter
Z = -1968885
57 Z = -631716
12
XDOT = 5764
917331 XDOT = 1836
041140
YDOT = -14653
091511 feet/sec YDOT = -4446
171894 meter/sec
ZDOT = -19641
703589 ZDOT = -5978
063373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13355890
37 X = -4070875
38
Y = 17651738
41 feet Y = 5380249
87 meter
Z = -2104016
93 Z = -641304
36
XDOT = -10100
485911 XDOT = -3078
628106
YDOT = -9970
080314 feet/sec YDOT = -3038
880480 meter/sec
ZDOT = -19603
406278 ZDOT = -5975
118234
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 15110
64339655
00016717 00000-0 10270-3 0 9084
2 25544 51
6467 11
5100 0006027 244
2055 115
8478 15
55793797 19086
Satellite: ISS
Catalog Number: 25544
Epoch time: 15110
64339655 = yrday
fracday
Element set: 908
Inclination: 51
6467 deg
RA of node: 11
5100 deg
Eccentricity:
0006027
Arg of perigee: 244
2055 deg
Mean anomaly: 115
8478 deg
Mean motion: 15
55793797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 314
Coasting Arc #10 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2015/111/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5536328
85 A = 6780989
02 meter
Y = 2779996
58 meter E =
0007537
Z = 2750229
21 I = 51
69787
XDOT = -4382
038916 Wp = 87
18804
YDOT = 3619
988672 meter/sec RA = 6
13730 deg
ZDOT = 5150
246992 TA = 303
94599
MA = 304
01762
Ha = 216
776 n
mi
Hp = 214
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18163808
57 X = 5491471
00
Y = 9120723
69 feet Y = 2841656
69 meter
Z = 9023061
71 Z = 2777015
02
XDOT = -14376
768098 XDOT = -4447
211179
YDOT = 11876
603253 feet/sec YDOT = 3570
621598 meter/sec
ZDOT = 16897
135802 ZDOT = 5128
801152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15000113
71 X = 4572034
66
Y = -13639378
94 feet Y = -4157282
70 meter
Z = 9137347
31 Z = 2785063
46
XDOT = 4909
616894 XDOT = 1496
451229
YDOT = 16682
791353 feet/sec YDOT = 5084
914804 meter/sec
ZDOT = 16804
478188 ZDOT = 5122
004952
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 15111
67109295
00016717 00000-0 10270-3 0 9094
2 25544 51
6458 6
3725 0006064 250
0096 110
0405 15
55866119 19246
Satellite: ISS
Catalog Number: 25544
Epoch time: 15111
67109295 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 6
3725 deg
Eccentricity:
0006064
Arg of perigee: 250
0096 deg
Mean anomaly: 110
0405 deg
Mean motion: 15
55866119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 294
Coasting Arc #11 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2015/112/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3713772
53 A = 6775893
02 meter
Y = -3563984
19 meter E =
0003191
Z = -4409965
67 I = 51
64808
XDOT = 6412
799949 Wp = 61
71615
YDOT = -2528
887233 meter/sec RA = 1
14177 deg
ZDOT = -3357
032956 TA = 174
34687
MA = 174
34327
Ha = 216
541 n
mi
Hp = 214
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12184293
07 X = -3652220
95
Y = -11692861
53 feet Y = -3605169
94 meter
Z = -14468391
31 Z = -4427857
13
XDOT = 21039
369912 XDOT = 6456
909372
YDOT = -8296
874123 feet/sec YDOT = -2456
928541 meter/sec
ZDOT = -11013
887651 ZDOT = -3325
773234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15124257
70 X = -4609873
75
Y = 7364239
37 feet Y = 2244620
16 meter
Z = -14544385
96 Z = -4433128
84
XDOT = -42
147896 XDOT = -12
846679
YDOT = -21570
955357 feet/sec YDOT = -6574
827193 meter/sec
ZDOT = -10879
373745 ZDOT = -3316
033118
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 15112
63454257
00016717 00000-0 10270-3 0 9104
2 25544 51
6445 1
5568 0006066 253
3269 106
7219 15
55880387 19398
Satellite: ISS
Catalog Number: 25544
Epoch time: 15112
63454257 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 1
5568 deg
Eccentricity:
0006066
Arg of perigee: 253
3269 deg
Mean anomaly: 106
7219 deg
Mean motion: 15
55880387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 316
Coasting Arc #12 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2015/113/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1341431
24 A = 6772521
90 meter
Y = 4074226
57 meter E =
0004262
Z = 5243941
89 I = 51
60514
XDOT = -7506
767477 Wp = 222
55474
YDOT = 1256
165837 meter/sec RA = 356
12686 deg
ZDOT = 941
685300 TA = 218
41654
MA = 218
44690
Ha = 216
383 n
mi
Hp = 214
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4401021
13 X = 1270299
22
Y = 13366885
06 feet Y = 4088829
68 meter
Z = 17204533
78 Z = 5250285
54
XDOT = -24628
502221 XDOT = -7524
830699
YDOT = 4121
278993 feet/sec YDOT = 1172
119275 meter/sec
ZDOT = 3089
518701 ZDOT = 905
174634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14037297
91 X = 4278568
40
Y = 297105
37 feet Y = 90557
72 meter
Z = 17230919
34 Z = 5251984
22
XDOT = -4110
508427 XDOT = -1252
882969
YDOT = 23622
221596 feet/sec YDOT = 7200
053142 meter/sec
ZDOT = 2932
749793 ZDOT = 893
902137
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 15113
66220489
00016717 00000-0 10270-3 0 9117
2 25544 51
6446 356
4196 0005993 256
9033 103
1452 15
55878943 19557
Satellite: ISS
Catalog Number: 25544
Epoch time: 15113
66220489 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 356
4196 deg
Eccentricity:
0005993
Arg of perigee: 256
9033 deg
Mean anomaly: 103
1452 deg
Mean motion: 15
55878943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1955
Checksum: 328
Coasting Arc #13 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2015/114/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1226758
56 A = 6773029
72 meter
Y = -4289638
66 meter E =
0008147
Z = -5103020
16 I = 51
57456
XDOT = 7481
614104 Wp = 119
19875
YDOT = 162
087841 meter/sec RA = 351
10294 deg
ZDOT = 1660
429862 TA = 166
86326
MA = 166
84203
Ha = 216
188 n
mi
Hp = 214
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4024798
43 X = 1299423
88
Y = -14073617
65 feet Y = -4275514
06 meter
Z = -16742192
11 Z = -5096884
17
XDOT = 24545
978032 XDOT = 7471
179744
YDOT = 531
784254 feet/sec YDOT = 245
693832 meter/sec
ZDOT = 5447
604534 ZDOT = 1696
748999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12106034
74 X = -3689919
39
Y = -8283609
40 feet Y = -2524844
15 meter
Z = -16715036
67 Z = -5094743
18
XDOT = 7486
688367 XDOT = 2281
942614
YDOT = -22260
411339 feet/sec YDOT = -6784
973376 meter/sec
ZDOT = 5603
266166 ZDOT = 1707
875527
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 15114
62561922
00016717 00000-0 10270-3 0 9125
2 25544 51
6434 351
6024 0006054 260
0173 100
0298 15
55946630 19701
Satellite: ISS
Catalog Number: 25544
Epoch time: 15114
62561922 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 351
6024 deg
Eccentricity:
0006054
Arg of perigee: 260
0173 deg
Mean anomaly: 100
0298 deg
Mean motion: 15
55946630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 280
Coasting Arc #14 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2015/115/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3573892
38 A = 6777270
69 meter
Y = 4148586
78 meter E =
0004790
Z = 3990608
71 I = 51
55835
XDOT = -6356
610564 Wp = 72
67738
YDOT = -1662
878020 meter/sec RA = 346
08834 deg
ZDOT = -3958
798040 TA = 58
56182
MA = 58
51500
Ha = 215
986 n
mi
Hp = 214
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11725368
71 X = -3639402
24
Y = 13610849
02 feet Y = 4108255
02 meter
Z = 13092548
26 Z = 3973088
09
XDOT = -20855
021535 XDOT = -6318
312964
YDOT = -5455
636549 feet/sec YDOT = -1733
747788 meter/sec
ZDOT = -12988
182547 ZDOT = -3989
584312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9554265
16 X = 2912140
02
Y = 15278674
29 feet Y = 4656939
92 meter
Z = 13016621
35 Z = 3967466
19
XDOT = -10190
080534 XDOT = -3105
936547
YDOT = 17564
552420 feet/sec YDOT = 5353
675577 meter/sec
ZDOT = -13119
823858 ZDOT = -3998
922312
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 15115
65324370
00016717 00000-0 10270-3 0 9134
2 25544 51
6440 346
4658 0006245 264
4796 95
5646 15
55976621 19869
Satellite: ISS
Catalog Number: 25544
Epoch time: 15115
65324370 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 346
4658 deg
Eccentricity:
0006245
Arg of perigee: 264
4796 deg
Mean anomaly: 95
5646 deg
Mean motion: 15
55976621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 337
Coasting Arc #15 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2015/116/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5333182
25 A = 6782062
37 meter
Y = -3607270
81 meter E =
0004918
Z = -2120356
67 I = 51
54318
XDOT = 4315
728314 Wp = 337
50018
YDOT = 3144
106836 meter/sec RA = 341
08824 deg
ZDOT = 5506
331302 TA = 358
95638
MA = 358
95741
Ha = 215
881 n
mi
Hp = 214
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17497317
08 X = 5383423
18
Y = -11834877
98 feet Y = -3547350
86 meter
Z = -6956550
75 Z = -2094326
78
XDOT = 14159
213628 XDOT = 4253
501574
YDOT = 10315
311143 feet/sec YDOT = 3192
020446 meter/sec
ZDOT = 18065
391410 ZDOT = 5527
145096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6523024
70 X = -1988217
93
Y = -20130083
68 feet Y = -6135649
50 meter
Z = -6844261
84 Z = -2086131
01
XDOT = 12330
542997 XDOT = 3758
349505
YDOT = -10167
770883 feet/sec YDOT = -3099
136565 meter/sec
ZDOT = 18153
988773 ZDOT = 5533
335778
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 15116
61662665
00016717 00000-0 10270-3 0 9144
2 25544 51
6431 341
6487 0006110 266
9415 93
1040 15
55993177 20018
Satellite: ISS
Catalog Number: 25544
Epoch time: 15116
61662665 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 341
6487 deg
Eccentricity:
0006110
Arg of perigee: 266
9415 deg
Mean anomaly: 93
1040 deg
Mean motion: 15
55993177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 296
Coasting Arc #16 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2015/117/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6249404
60 A = 6783694
16 meter
Y = 2619122
51 meter E =
0008343
Z = -172622
79 I = 51
51995
XDOT = -1706
292850 Wp = 166
03769
YDOT = -4462
424872 meter/sec RA = 336
10117 deg
ZDOT = -6002
364022 TA = 15
82661
MA = 15
80055
Ha = 215
732 n
mi
Hp = 213
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20503295
94 X = -6277389
24
Y = 8592921
61 feet Y = 2549081
10 meter
Z = -566347
74 Z = -203049
49
XDOT = -5598
073655 XDOT = -1627
108720
YDOT = -14640
501550 feet/sec YDOT = -4481
063337 meter/sec
ZDOT = -19692
795348 ZDOT = -6010
460338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2968142
22 X = 904689
75
Y = 22028348
30 feet Y = 6714240
56 meter
Z = -697279
75 Z = -212530
87
XDOT = -13955
298958 XDOT = -4253
575122
YDOT = 1261
719089 feet/sec YDOT = 384
571978 meter/sec
ZDOT = -19726
620928 ZDOT = -6012
674059
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
64421541
00016717 00000-0 10270-3 0 9155
2 25544 51
6434 336
5119 0006135 273
3028 86
7424 15
56062385 20175
Satellite: ISS
Catalog Number: 25544
Epoch time: 15117
64421541 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 336
5119 deg
Eccentricity:
0006135
Arg of perigee: 273
3028 deg
Mean anomaly: 86
7424 deg
Mean motion: 15
56062385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 294
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