[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 2nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18029 55 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 660)
---------------------------------------
Vector Time (GMT): 2015/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5346411
11 A = 6783777
10 meter
Y = 2089635
42 meter E =
0003259
Z = -3612443
83 I = 51
93264
XDOT = 570
588465 Wp = 7
66098
YDOT = 6220
055379 meter/sec RA = 50
87723 deg
ZDOT = 4446
096580 TA = 309
76591
MA = 309
79462
Ha = 220
422 n
mi
Hp = 216
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17540718
87 X = 5340194
59
Y = 6855759
24 feet Y = 2149387
76 meter
Z = -11851849
83 Z = -3586487
47
XDOT = 1872
009400 XDOT = 479
394801
YDOT = 20407
005838 feet/sec YDOT = 6225
926111 meter/sec
ZDOT = 14586
931036 ZDOT = 4448
646941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5624124
54 X = 1714233
16
Y = 18046026
94 feet Y = 5500429
01 meter
Z = -11741155
51 Z = -3578704
20
XDOT = -13530
138898 XDOT = -4123
986336
YDOT = 13705
865053 feet/sec YDOT = 4177
547668 meter/sec
ZDOT = 14596
640872 ZDOT = 4449
056138
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 15030
50755452
00016717 00000-0 10270-3 0 9009
2 25544 51
6463 51
5213 0006168 308
7781 51
2820 15
54169192 6613
Satellite: ISS
Catalog Number: 25544
Epoch time: 15030
50755452 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 51
5213 deg
Eccentricity:
0006168
Arg of perigee: 308
7781 deg
Mean anomaly: 51
2820 deg
Mean motion: 15
54169192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 661
Checksum: 286
Coasting Arc #2 (Orbit 676)
---------------------------------------
Vector Time (GMT): 2015/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5530510
07 A = 6787209
53 meter
Y = -3289996
96 meter E =
0008576
Z = 2149272
51 I = 51
92233
XDOT = 958
001481 Wp = 93
51648
YDOT = -5230
312818 meter/sec RA = 45
91696 deg
ZDOT = -5522
722969 TA = 62
75281
MA = 62
66548
Ha = 220
428 n
mi
Hp = 216
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18144718
08 X = -5503749
68
Y = -10793953
29 feet Y = -3351693
12 meter
Z = 7051418
99 Z = 2122471
83
XDOT = 3143
049479 XDOT = 1043
243679
YDOT = -17159
818958 feet/sec YDOT = -5219
123139 meter/sec
ZDOT = -18119
169847 ZDOT = -5517
862295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3262398
16 X = -994378
96
Y = -20897194
13 feet Y = -6369464
77 meter
Z = 6937345
85 Z = 2114503
01
XDOT = 13782
017259 XDOT = 4200
758861
YDOT = -8179
885171 feet/sec YDOT = -2493
229000 meter/sec
ZDOT = -18097
345033 ZDOT = -5516
070766
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 15031
53635540
00016717 00000-0 10270-3 0 9019
2 25544 51
6448 46
3919 0006172 313
2491 46
8146 15
54205838 6771
Satellite: ISS
Catalog Number: 25544
Epoch time: 15031
53635540 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 46
3919 deg
Eccentricity:
0006172
Arg of perigee: 313
2491 deg
Mean anomaly: 46
8146 deg
Mean motion: 15
54205838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 677
Checksum: 304
Coasting Arc #3 (Orbit 691)
---------------------------------------
Vector Time (GMT): 2015/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5340409
66 A = 6788854
75 meter
Y = 4151731
02 meter E =
0013059
Z = -466825
60 I = 51
90616
XDOT = -2586
851631 Wp = 13
96278
YDOT = 3998
501168 meter/sec RA = 40
96339 deg
ZDOT = 6014
929301 TA = 341
01845
MA = 341
06708
Ha = 220
454 n
mi
Hp = 215
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17521029
08 X = 5295854
74
Y = 13621164
76 feet Y = 4211201
84 meter
Z = -1531580
04 Z = -440991
70
XDOT = -8487
046032 XDOT = -2660
589185
YDOT = 13118
442153 feet/sec YDOT = 3969
161000 meter/sec
ZDOT = 19734
020017 ZDOT = 6002
184069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1044435
55 X = 318343
96
Y = 22175570
37 feet Y = 6759113
85 meter
Z = -1421815
71 Z = -433369
43
XDOT = -13951
077574 XDOT = -4252
288445
YDOT = 1908
086861 feet/sec YDOT = 581
584875 meter/sec
ZDOT = 19678
684383 ZDOT = 5998
063000
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 15032
50083726
00016717 00000-0 10270-3 0 9021
2 25544 51
6451 41
5837 0006082 315
5266 44
5398 15
54264888 6927
Satellite: ISS
Catalog Number: 25544
Epoch time: 15032
50083726 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 41
5837 deg
Eccentricity:
0006082
Arg of perigee: 315
5266 deg
Mean anomaly: 44
5398 deg
Mean motion: 15
54264888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 692
Checksum: 312
Coasting Arc #4 (Orbit 707)
---------------------------------------
Vector Time (GMT): 2015/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4730235
09 A = 6788237
55 meter
Y = -4692192
88 meter E =
0002650
Z = -1293079
45 I = 51
87842
XDOT = 4199
207003 Wp = 145
92099
YDOT = -2623
219030 meter/sec RA = 36
00880 deg
ZDOT = -5850
255737 TA = 48
09413
MA = 48
07153
Ha = 220
648 n
mi
Hp = 215
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15519143
99 X = -4671133
18
Y = -15394333
59 feet Y = -4744759
00 meter
Z = -4242386
64 Z = -1315913
86
XDOT = 13776
925863 XDOT = 4256
646031
YDOT = -8606
361646 feet/sec YDOT = -2575
939667 meter/sec
ZDOT = -19193
752417 ZDOT = -5829
717756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1253558
39 X = 382084
60
Y = -21804290
49 feet Y = -6645947
74 meter
Z = -4339203
71 Z = -1322589
29
XDOT = 14068
719026 XDOT = 4288
145559
YDOT = 4605
857600 feet/sec YDOT = 1403
865396 meter/sec
ZDOT = -19105
330529 ZDOT = -5823
304745
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 15033
52959780
00016717 00000-0 10270-3 0 9037
2 25544 51
6439 36
4535 0006177 320
7075 39
3629 15
54247463 7089
Satellite: ISS
Catalog Number: 25544
Epoch time: 15033
52959780 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 36
4535 deg
Eccentricity:
0006177
Arg of perigee: 320
7075 deg
Mean anomaly: 39
3629 deg
Mean motion: 15
54247463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 708
Checksum: 320
Coasting Arc #5 (Orbit 723)
---------------------------------------
Vector Time (GMT): 2015/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3691893
24 A = 6785177
16 meter
Y = 4886057
21 meter E =
0011615
Z = 2904261
31 I = 51
84250
XDOT = -5633
993702 Wp = 53
31749
YDOT = 1246
596877 meter/sec RA = 31
04800 deg
ZDOT = 5057
475285 TA = 339
70329
MA = 339
74942
Ha = 220
639 n
mi
Hp = 215
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12112510
62 X = 3622874
35
Y = 16030371
43 feet Y = 4926956
54 meter
Z = 9528416
38 Z = 2922027
59
XDOT = -18484
231305 XDOT = -5672
081419
YDOT = 4089
884768 feet/sec YDOT = 1183
381073 meter/sec
ZDOT = 16592
766684 ZDOT = 5030
014580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3672203
91 X = -1119287
75
Y = 19717102
89 feet Y = 6009772
96 meter
Z = 9603500
01 Z = 2927146
80
XDOT = -14140
033512 XDOT = -4309
882214
YDOT = -10669
311072 feet/sec YDOT = -3252
006015 meter/sec
ZDOT = 16474
986343 ZDOT = 5021
575837
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 15034
55833549
00016717 00000-0 10270-3 0 9046
2 25544 51
6437 31
3240 0006264 323
4166 36
6558 15
54306250 7241
Satellite: ISS
Catalog Number: 25544
Epoch time: 15034
55833549 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 31
3240 deg
Eccentricity:
0006264
Arg of perigee: 323
4166 deg
Mean anomaly: 36
6558 deg
Mean motion: 15
54306250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 724
Checksum: 291
Coasting Arc #6 (Orbit 738)
---------------------------------------
Vector Time (GMT): 2015/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2278121
84 A = 6781243
46 meter
Y = -4807051
17 meter E =
0009143
Z = -4214749
36 I = 51
80151
XDOT = 6714
314897 Wp = 27
53842
YDOT = 55
225176 meter/sec RA = 26
07423 deg
ZDOT = -3687
441825 TA = 204
66788
MA = 204
71163
Ha = 220
849 n
mi
Hp = 215
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7474153
01 X = -2203725
78
Y = -15771165
27 feet Y = -4832110
84 meter
Z = -13827917
86 Z = -4225634
85
XDOT = 22028
592181 XDOT = 6731
110104
YDOT = 181
184962 feet/sec YDOT = 130
402755 meter/sec
ZDOT = -12097
906251 ZDOT = -3654
785008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6356302
79 X = 1937401
09
Y = -16214979
32 feet Y = -4942325
70 meter
Z = -13873564
44 Z = -4228662
44
XDOT = 13902
994246 XDOT = 4237
632646
YDOT = 15694
591125 feet/sec YDOT = 4783
711375 meter/sec
ZDOT = -11958
146559 ZDOT = -3644
843071
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 15035
52275965
00016717 00000-0 10270-3 0 9057
2 25544 51
6434 26
5141 0006254 328
4106 31
6670 15
54306110 7393
Satellite: ISS
Catalog Number: 25544
Epoch time: 15035
52275965 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 26
5141 deg
Eccentricity:
0006254
Arg of perigee: 328
4106 deg
Mean anomaly: 31
6670 deg
Mean motion: 15
54306110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 739
Checksum: 284
Coasting Arc #7 (Orbit 754)
---------------------------------------
Vector Time (GMT): 2015/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 567918
67 A = 6777857
70 meter
Y = 4483449
43 meter E =
0002913
Z = 5049259
42 I = 51
76176
XDOT = -7329
487504 Wp = 31
50759
YDOT = -1216
408851 meter/sec RA = 21
08839 deg
ZDOT = 1906
418309 TA = 40
05573
MA = 40
03425
Ha = 220
955 n
mi
Hp = 215
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1863250
23 X = 493214
64
Y = 14709479
75 feet Y = 4489382
89 meter
Z = 16565811
74 Z = 5051836
47
XDOT = -24046
875012 XDOT = -7324
601044
YDOT = -3990
842686 feet/sec YDOT = -1298
344513 meter/sec
ZDOT = 6254
653246 ZDOT = 1870
825859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9263021
51 X = -2823368
96
Y = 11562895
03 feet Y = 3524370
40 meter
Z = 16575961
68 Z = 5052353
12
XDOT = -13187
992156 XDOT = -4019
700009
YDOT = -19304
135255 feet/sec YDOT = -5883
900426 meter/sec
ZDOT = 6102
564633 ZDOT = 1860
061700
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 15036
55145634
00016717 00000-0 10270-3 0 9061
2 25544 51
6434 21
3842 0006383 331
7444 28
3361 15
54344994 7559
Satellite: ISS
Catalog Number: 25544
Epoch time: 15036
55145634 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 21
3842 deg
Eccentricity:
0006383
Arg of perigee: 331
7444 deg
Mean anomaly: 28
3361 deg
Mean motion: 15
54344994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 755
Checksum: 304
Coasting Arc #8 (Orbit 769)
---------------------------------------
Vector Time (GMT): 2015/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1265301
12 A = 6776664
75 meter
Y = -4008332
14 meter E =
0013456
Z = -5326079
09 I = 51
72841
XDOT = 7337
910574 Wp = 65
45123
YDOT = 2196
057752 meter/sec RA = 16
09359 deg
ZDOT = 96
169450 TA = 205
43191
MA = 205
49818
Ha = 221
038 n
mi
Hp = 214
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4151250
40 X = 1335900
76
Y = -13150696
00 feet Y = -3993788
37 meter
Z = -17474012
75 Z = -5319760
85
XDOT = 24074
509758 XDOT = 7312
341228
YDOT = 7204
913886 feet/sec YDOT = 2277
972089 meter/sec
ZDOT = 315
516567 ZDOT = 131
752581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12261468
99 X = 3737295
75
Y = -6387621
01 feet Y = -1946946
88 meter
Z = -17446188
20 Z = -5317598
16
XDOT = 11642
691509 XDOT = 3548
692372
YDOT = 21123
112279 feet/sec YDOT = 6438
324623 meter/sec
ZDOT = 467
363959 ZDOT = 142
452535
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 15037
51583950
00016717 00000-0 10270-3 0 9076
2 25544 51
6437 16
5749 0006331 335
9396 24
1461 15
54367501 7700
Satellite: ISS
Catalog Number: 25544
Epoch time: 15037
51583950 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 16
5749 deg
Eccentricity:
0006331
Arg of perigee: 335
9396 deg
Mean anomaly: 24
1461 deg
Mean motion: 15
54367501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 770
Checksum: 310
Coasting Arc #9 (Orbit 785)
---------------------------------------
Vector Time (GMT): 2015/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3096241
08 A = 6778061
92 meter
Y = 3400127
16 meter E =
0009850
Z = 4979935
49 I = 51
70305
XDOT = -6725
839374 Wp = 17
23601
YDOT = -3017
898832 meter/sec RA = 11
09691 deg
ZDOT = -2110
964481 TA = 93
35489
MA = 93
24221
Ha = 221
159 n
mi
Hp = 214
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10158271
26 X = -3158222
22
Y = 11155272
85 feet Y = 3365156
83 meter
Z = 16338371
03 Z = 4964744
00
XDOT = -22066
402145 XDOT = -6681
338549
YDOT = -9901
242886 feet/sec YDOT = -3092
862903 meter/sec
ZDOT = -6925
736487 ZDOT = -2143
528385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15124023
33 X = -4609802
31
Y = 1017938
05 feet Y = 310267
52 meter
Z = 16272697
25 Z = 4959918
12
XDOT = -9067
373142 XDOT = -2763
735334
YDOT = -21245
530047 feet/sec YDOT = -6475
637558 meter/sec
ZDOT = -7064
492579 ZDOT = -2153
257338
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 15038
54449300
00016717 00000-0 10270-3 0 9081
2 25544 51
6439 11
4449 0006416 339
1014 20
9876 15
54413612 7866
Satellite: ISS
Catalog Number: 25544
Epoch time: 15038
54449300 = yrday
fracday
Element set: 908
Inclination: 51
6439 deg
RA of node: 11
4449 deg
Eccentricity:
0006416
Arg of perigee: 339
1014 deg
Mean anomaly: 20
9876 deg
Mean motion: 15
54413612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 786
Checksum: 301
Coasting Arc #10 (Orbit 800)
---------------------------------------
Vector Time (GMT): 2015/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4683225
43 A = 6781532
29 meter
Y = -2735451
64 meter E =
0006294
Z = -4072424
96 I = 51
68392
XDOT = 5504
545388 Wp = 50
81412
YDOT = 3667
836894 meter/sec RA = 6
10579 deg
ZDOT = 3874
348058 TA = 259
25328
MA = 259
32415
Ha = 221
280 n
mi
Hp = 214
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15364912
82 X = 4733247
85
Y = -8974578
88 feet Y = -2682801
42 meter
Z = -13360974
27 Z = -4049553
37
XDOT = 18059
532114 XDOT = 5444
301808
YDOT = 12033
585610 feet/sec YDOT = 3729
055791 meter/sec
ZDOT = 12711
115675 ZDOT = 3900
941044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17450499
10 X = 5318912
13
Y = 3837119
37 feet Y = 1169553
98 meter
Z = -13262572
96 Z = -4042432
24
XDOT = 5383
563508 XDOT = 1640
910157
YDOT = 19751
720364 feet/sec YDOT = 6020
324367 meter/sec
ZDOT = 12824
185461 ZDOT = 3908
811729
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 15039
50883525
00016717 00000-0 10270-3 0 9090
2 25544 51
6442 6
6357 0006445 343
1728 16
9210 15
54425606 8014
Satellite: ISS
Catalog Number: 25544
Epoch time: 15039
50883525 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 6
6357 deg
Eccentricity:
0006445
Arg of perigee: 343
1728 deg
Mean anomaly: 16
9210 deg
Mean motion: 15
54425606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 801
Checksum: 298
Coasting Arc #11 (Orbit 816)
---------------------------------------
Vector Time (GMT): 2015/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5918557
10 A = 6785389
07 meter
Y = 1983753
61 meter E =
0012203
Z = 2655114
24 I = 51
66631
XDOT = -3752
014195 Wp = 74
04905
YDOT = -4192
464812 meter/sec RA = 1
12349 deg
ZDOT = -5208
109848 TA = 76
01766
MA = 75
88199
Ha = 221
256 n
mi
Hp = 214
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19417838
24 X = -5953197
42
Y = 6508377
97 feet Y = 1917374
97 meter
Z = 8711004
74 Z = 2626279
09
XDOT = -12309
757858 XDOT = -3679
555462
YDOT = -13754
805814 feet/sec YDOT = -4234
017561 meter/sec
ZDOT = -17086
974566 ZDOT = -5226
159853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18887198
03 X = -5756817
96
Y = -8051463
25 feet Y = -2454086
00 meter
Z = 8587241
67 Z = 2617391
26
XDOT = -587
165965 XDOT = -178
968186
YDOT = -17010
433326 feet/sec YDOT = -5184
780078 meter/sec
ZDOT = -17163
381329 ZDOT = -5231
398629
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 15040
53744482
00016717 00000-0 10270-3 0 9105
2 25544 51
6447 1
5054 0006473 346
7166 13
3815 15
54485466 8172
Satellite: ISS
Catalog Number: 25544
Epoch time: 15040
53744482 = yrday
fracday
Element set: 910
Inclination: 51
6447 deg
RA of node: 1
5054 deg
Eccentricity:
0006473
Arg of perigee: 346
7166 deg
Mean anomaly: 13
3815 deg
Mean motion: 15
54485466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 817
Checksum: 301
Coasting Arc #12 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2015/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6606128
39 A = 6787858
13 meter
Y = -1193195
21 meter E =
0015031
Z = -943734
94 I = 51
64333
XDOT = 1668
197906 Wp = 19
93107
YDOT = 4584
855535 meter/sec RA = 356
14912 deg
ZDOT = 5922
137330 TA = 329
84291
MA = 329
92935
Ha = 221
314 n
mi
Hp = 214
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21673649
56 X = 6623564
26
Y = -3914682
46 feet Y = -1119223
76 meter
Z = -3096243
24 Z = -911601
53
XDOT = 5473
090244 XDOT = 1588
037747
YDOT = 15042
176952 feet/sec YDOT = 4603
062646 meter/sec
ZDOT = 19429
584416 ZDOT = 5930
045993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19021237
15 X = 5797673
08
Y = 11139935
94 feet Y = 3395452
48 meter
Z = -2958531
80 Z = -901760
49
XDOT = -4912
157111 XDOT = -1497
225488
YDOT = 13518
351238 feet/sec YDOT = 4120
393457 meter/sec
ZDOT = 19462
520934 ZDOT = 5932
176381
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 15041
50174519
00016717 00000-0 10270-3 0 9112
2 25544 51
6446 356
6961 0006406 350
3340 9
7689 15
54516345 8329
Satellite: ISS
Catalog Number: 25544
Epoch time: 15041
50174519 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 356
6961 deg
Eccentricity:
0006406
Arg of perigee: 350
3340 deg
Mean anomaly: 9
7689 deg
Mean motion: 15
54516345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 832
Checksum: 305
Coasting Arc #13 (Orbit 847)
---------------------------------------
Vector Time (GMT): 2015/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6717739
55 A = 6787696
11 meter
Y = 303450
98 meter E =
0005580
Z = -922215
63 I = 51
61273
XDOT = 589
497702 Wp = 102
43545
YDOT = -4834
802414 meter/sec RA = 351
17630 deg
ZDOT = -5916
419197 TA = 87
54660
MA = 87
48272
Ha = 221
326 n
mi
Hp = 213
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22039827
94 X = -6716153
80
Y = 995574
08 feet Y = 228337
65 meter
Z = -3025641
83 Z = -954844
97
XDOT = 1934
047579 XDOT = 672
257274
YDOT = -15862
212643 feet/sec YDOT = -4827
747905 meter/sec
ZDOT = -19410
824136 ZDOT = -5913
354239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17601232
54 X = -5364855
68
Y = -13269409
34 feet Y = -4044515
97 meter
Z = -3165293
14 Z = -964781
35
XDOT = 10729
417209 XDOT = 3270
326365
YDOT = -9628
660955 feet/sec YDOT = -2934
815859 meter/sec
ZDOT = -19396
763297 ZDOT = -5912
133453
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 15042
53030992
00016717 00000-0 10270-3 0 9123
2 25544 51
6455 351
5654 0006468 353
6536 6
4534 15
54552437 8485
Satellite: ISS
Catalog Number: 25544
Epoch time: 15042
53030992 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 351
5654 deg
Eccentricity:
0006468
Arg of perigee: 353
6536 deg
Mean anomaly: 6
4534 deg
Mean motion: 15
54552437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 848
Checksum: 312
Coasting Arc #14 (Orbit 863)
---------------------------------------
Vector Time (GMT): 2015/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6199223
43 A = 6784911
11 meter
Y = 646726
14 meter E =
0015826
Z = 2655863
39 I = 51
57271
XDOT = -2749
070657 Wp = 54
28955
YDOT = 4927
062827 meter/sec RA = 346
19715 deg
ZDOT = 5204
285005 TA = 335
73610
MA = 335
81055
Ha = 221
262 n
mi
Hp = 213
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20338659
55 X = 6178629
79
Y = 2121804
93 feet Y = 715934
89 meter
Z = 8713462
57 Z = 2685927
66
XDOT = -9019
260687 XDOT = -2829
242135
YDOT = 16164
904289 feet/sec YDOT = 4895
872930 meter/sec
ZDOT = 17074
425870 ZDOT = 5190
735708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14523714
79 X = 4426828
27
Y = 14316745
83 feet Y = 4363744
13 meter
Z = 8841948
64 Z = 2695025
95
XDOT = -16176
817391 XDOT = -4930
693941
YDOT = 5876
601287 feet/sec YDOT = 1791
188072 meter/sec
ZDOT = 17015
496575 ZDOT = 5186
323356
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 15043
55885118
00016717 00000-0 10270-3 0 9135
2 25544 51
6455 346
4350 0006407 357
3360 2
7758 15
54588414 8649
Satellite: ISS
Catalog Number: 25544
Epoch time: 15043
55885118 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 346
4350 deg
Eccentricity:
0006407
Arg of perigee: 357
3360 deg
Mean anomaly: 2
7758 deg
Mean motion: 15
54588414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 864
Checksum: 318
Coasting Arc #15 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2015/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5146706
24 A = 6780663
07 meter
Y = -1684227
87 meter E =
0011495
Z = -4093366
72 I = 51
52894
XDOT = 4606
318462 Wp = 38
42846
YDOT = -4776
796523 meter/sec RA = 341
20455 deg
ZDOT = -3823
203336 TA = 191
94308
MA = 191
97036
Ha = 221
411 n
mi
Hp = 213
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16885519
15 X = -5107606
49
Y = -5525681
97 feet Y = -1741563
23 meter
Z = -13429680
83 Z = -4118273
08
XDOT = 15112
593379 XDOT = 4677
962842
YDOT = -15671
904603 feet/sec YDOT = -4724
885236 meter/sec
ZDOT = -12543
318033 ZDOT = -3800
652800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9930919
76 X = -3026944
34
Y = -14634432
08 feet Y = -4460574
90 meter
Z = -13535895
83 Z = -4125741
05
XDOT = 20533
523348 XDOT = 6258
617916
YDOT = -2413
273586 feet/sec YDOT = -735
565789 meter/sec
ZDOT = -12445
915649 ZDOT = -3793
515090
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 15044
52308755
00016717 00000-0 10270-3 0 9141
2 25544 51
6459 341
6246 0006482 1
0278 359
0888 15
54631601 8793
Satellite: ISS
Catalog Number: 25544
Epoch time: 15044
52308755 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 341
6246 deg
Eccentricity:
0006482
Arg of perigee: 1
0278 deg
Mean anomaly: 359
0888 deg
Mean motion: 15
54631601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 879
Checksum: 318
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