[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 15th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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
057/09:19:33
519 0
0 2
7 2
7
N/A 2
6 -0
1 222
3
000/00:06:07
037 0
6 0
2 211
1
Coasting Arc #1 (Orbit 879)
---------------------------------------
Vector Time (GMT): 2015/044/13:25:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6415779
69 A = 6785510
34 meter
Y = 386626
13 meter E =
0004533
Z = -2182310
54 I = 51
54475
XDOT = 1549
302626 Wp = 66
19864
YDOT = -5134
559927 meter/sec RA = 340
90841 deg
ZDOT = -5471
680714 TA = 138
04121
MA = 138
00647
Ha = 221
176 n
mi
Hp = 213
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21049145
97 X = -6409025
48
Y = 1268458
44 feet Y = 314918
38 meter
Z = -7159811
49 Z = -2213460
38
XDOT = 5083
013866 XDOT = 1633
182390
YDOT = -16845
669053 feet/sec YDOT = -5116
765833 meter/sec
ZDOT = -17951
708379 ZDOT = -5463
950659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20521216
68 X = -6254866
84
Y = -4650613
35 feet Y = -1417506
95 meter
Z = -7293140
24 Z = -2222949
15
XDOT = 9357
394224 XDOT = 2852
133759
YDOT = -13228
148309 feet/sec YDOT = -4031
939605 meter/sec
ZDOT = -17917
635343 ZDOT = -5461
295252
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
58706031
00016717 00000-0 10270-3 0 9001
2 25544 51
6465 341
3118 0006234
2269 359
8886 15
54720055 8801
Satellite: ISS
Catalog Number: 25544
Epoch time: 15044
58706031 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 341
3118 deg
Eccentricity:
0006234
Arg of perigee:
2269 deg
Mean anomaly: 359
8886 deg
Mean motion: 15
54720055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 880
Checksum: 296
Coasting Arc #2 (Orbit 895)
---------------------------------------
Vector Time (GMT): 2015/045/13:25:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5590585
18 A = 6781402
21 meter
Y = 765352
17 meter E =
0012839
Z = 3746726
57 I = 51
50167
XDOT = -3576
715926 Wp = 67
47747
YDOT = 5299
363473 meter/sec RA = 335
91606 deg
ZDOT = 4247
584917 TA = 337
49729
MA = 337
55355
Ha = 221
093 n
mi
Hp = 213
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18341814
88 X = 5563411
41
Y = 2510997
94 feet Y = 827717
92 meter
Z = 12292410
01 Z = 3773818
10
XDOT = -11734
632303 XDOT = -3656
341688
YDOT = 17386
363102 feet/sec YDOT = 5258
921232 meter/sec
ZDOT = 13935
646054 ZDOT = 4230
016620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16961249
62 X = 5169788
88
Y = 7223878
49 feet Y = 2201838
16 meter
Z = 12408151
29 Z = 3782004
51
XDOT = -15450
143908 XDOT = -4709
203863
YDOT = 12432
216784 feet/sec YDOT = 3789
339676 meter/sec
ZDOT = 13859
459288 ZDOT = 4224
363191
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 15045
61548353
00016717 00000-0 10270-3 0 9018
2 25544 51
6463 336
1800 0006232 4
4564 355
6644 15
54763806 8965
Satellite: ISS
Catalog Number: 25544
Epoch time: 15045
61548353 = yrday
fracday
Element set: 901
Inclination: 51
6463 deg
RA of node: 336
1800 deg
Eccentricity:
0006232
Arg of perigee: 4
4564 deg
Mean anomaly: 355
6644 deg
Mean motion: 15
54763806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 896
Checksum: 307
Coasting Arc #3 (Orbit 910)
---------------------------------------
Vector Time (GMT): 2015/046/13:25:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4292628
53 A = 6777204
74 meter
Y = -2031804
69 meter E =
0015552
Z = -4849086
75 I = 51
46065
XDOT = 5169
488991 Wp = 50
88868
YDOT = -5097
035082 meter/sec RA = 330
90858 deg
ZDOT = -2436
220348 TA = 195
08782
MA = 195
13426
Ha = 221
168 n
mi
Hp = 212
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14083426
94 X = -4246034
78
Y = -6666025
89 feet Y = -2079547
30 meter
Z = -15909077
27 Z = -4869825
87
XDOT = 16960
265720 XDOT = 5237
935051
YDOT = -16722
556044 feet/sec YDOT = -5038
843869 meter/sec
ZDOT = -7992
848910 ZDOT = -2410
942037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11910548
51 X = -3630335
18
Y = -9904525
08 feet Y = -3018899
25 meter
Z = -15997398
92 Z = -4876007
19
XDOT = 19881
832229 XDOT = 6059
982463
YDOT = -11152
234643 feet/sec YDOT = -3399
201119 meter/sec
ZDOT = -7883
726558 ZDOT = -2402
959855
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 15046
57959940
00016717 00000-0 10270-3 0 9023
2 25544 51
6471 331
3692 0006241 7
4518 352
6727 15
54839530 9117
Satellite: ISS
Catalog Number: 25544
Epoch time: 15046
57959940 = yrday
fracday
Element set: 902
Inclination: 51
6471 deg
RA of node: 331
3692 deg
Eccentricity:
0006241
Arg of perigee: 7
4518 deg
Mean anomaly: 352
6727 deg
Mean motion: 15
54839530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 911
Checksum: 314
Coasting Arc #4 (Orbit 926)
---------------------------------------
Vector Time (GMT): 2015/047/13:25:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2634993
52 A = 6775125
75 meter
Y = 3309634
55 meter E =
0006543
Z = 5288798
89 I = 51
42695
XDOT = -6215
008173 Wp = 31
76993
YDOT = 4490
574865 meter/sec RA = 325
88868 deg
ZDOT = 291
625063 TA = 55
47454
MA = 55
41278
Ha = 221
043 n
mi
Hp = 212
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8644991
86 X = 2572098
15
Y = 10858381
05 feet Y = 3338749
34 meter
Z = 17351702
38 Z = 5301445
96
XDOT = -20390
446762 XDOT = -6266
177503
YDOT = 14732
857169 feet/sec YDOT = 4420
788504 meter/sec
ZDOT = 956
775142 ZDOT = 261
309964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5814971
13 X = 1772403
20
Y = 12528696
22 feet Y = 3818746
61 meter
Z = 17405165
35 Z = 5305094
40
XDOT = -22319
095396 XDOT = -6802
860277
YDOT = 9235
246109 feet/sec YDOT = 2814
903014 meter/sec
ZDOT = 826
232349 ZDOT = 251
835620
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 15047
60795783
00016717 00000-0 10270-3 0 9032
2 25544 51
6470 326
2371 0006131 9
9554 350
1719 15
54896847 9273
Satellite: ISS
Catalog Number: 25544
Epoch time: 15047
60795783 = yrday
fracday
Element set: 903
Inclination: 51
6470 deg
RA of node: 326
2371 deg
Eccentricity:
0006131
Arg of perigee: 9
9554 deg
Mean anomaly: 350
1719 deg
Mean motion: 15
54896847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 927
Checksum: 329
Coasting Arc #5 (Orbit 941)
---------------------------------------
Vector Time (GMT): 2015/048/13:25:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -869753
91 A = 6776275
41 meter
Y = -4468529
45 meter E =
0014215
Z = -5030570
75 I = 51
40567
XDOT = 6591
283481 Wp = 78
33149
YDOT = -3410
741292 meter/sec RA = 320
86574 deg
ZDOT = 1897
459734 TA = 210
10475
MA = 210
18653
Ha = 221
133 n
mi
Hp = 212
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2853523
32 X = -795285
11
Y = -14660529
68 feet Y = -4477839
56 meter
Z = -16504497
21 Z = -5034614
56
XDOT = 21624
945805 XDOT = 6619
716405
YDOT = -11190
096103 feet/sec YDOT = -3336
874159 meter/sec
ZDOT = 6225
261593 ZDOT = 1929
547383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 432677
22 X = 131880
02
Y = -14911182
95 feet Y = -4544928
56 meter
Z = -16520943
30 Z = -5035583
52
XDOT = 22383
834549 XDOT = 6822
592771
YDOT = -6373
823000 feet/sec YDOT = -1942
741250 meter/sec
ZDOT = 6363
170544 ZDOT = 1939
494382
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 15048
57201570
00016717 00000-0 10270-3 0 9046
2 25544 51
6473 321
4261 0006172 13
2353 346
8961 15
54924633 9424
Satellite: ISS
Catalog Number: 25544
Epoch time: 15048
57201570 = yrday
fracday
Element set: 904
Inclination: 51
6473 deg
RA of node: 321
4261 deg
Eccentricity:
0006172
Arg of perigee: 13
2353 deg
Mean anomaly: 346
8961 deg
Mean motion: 15
54924633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 942
Checksum: 294
Coasting Arc #6 (Orbit 957)
---------------------------------------
Vector Time (GMT): 2015/049/13:29:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2363009
09 A = 6783179
18 meter
Y = 5612034
85 meter E =
0015509
Z = 2981235
13 I = 51
40477
XDOT = -5854
940344 Wp = 74
06751
YDOT = 178
220531 meter/sec RA = 315
83641 deg
ZDOT = -4950
609807 TA = 71
69610
MA = 71
52744
Ha = 221
207 n
mi
Hp = 212
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7752654
50 X = -2440069
92
Y = 18412187
82 feet Y = 5585179
54 meter
Z = 9780955
15 Z = 2969568
69
XDOT = -19209
121864 XDOT = -5832
450502
YDOT = 584
713027 feet/sec YDOT = 112
872057 meter/sec
ZDOT = -16242
158160 ZDOT = -4978
996635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10978644
31 X = -3346290
79
Y = 16720525
87 feet Y = 5096416
28 meter
Z = 9729993
81 Z = 2965702
11
XDOT = -17683
298946 XDOT = -5389
869519
YDOT = -2039
233091 feet/sec YDOT = -621
558246 meter/sec
ZDOT = -16363
616679 ZDOT = -4987
630364
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 15049
60031243
00016717 00000-0 10270-3 0 9050
2 25544 51
6470 316
2941 0006168 17
5857 342
5509 15
54961651 9588
Satellite: ISS
Catalog Number: 25544
Epoch time: 15049
60031243 = yrday
fracday
Element set: 905
Inclination: 51
6470 deg
RA of node: 316
2941 deg
Eccentricity:
0006168
Arg of perigee: 17
5857 deg
Mean anomaly: 342
5509 deg
Mean motion: 15
54961651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 958
Checksum: 312
Coasting Arc #7 (Orbit 972)
---------------------------------------
Vector Time (GMT): 2015/050/13:29:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3612937
49 A = 6786170
83 meter
Y = -5613968
37 meter E =
0015264
Z = -1174565
89 I = 51
39326
XDOT = 4640
036409 Wp = 30
37474
YDOT = 1772
323166 meter/sec RA = 310
83955 deg
ZDOT = 5847
832580 TA = 316
81421
MA = 316
93382
Ha = 221
128 n
mi
Hp = 212
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11853469
44 X = 3681151
15
Y = -18418531
39 feet Y = -5573184
88 meter
Z = -3853562
64 Z = -1156849
02
XDOT = 15223
216565 XDOT = 4591
467086
YDOT = 5814
708551 feet/sec YDOT = 1823
940188 meter/sec
ZDOT = 19185
802427 ZDOT = 5870
254283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14700028
88 X = 4480568
80
Y = -16255534
69 feet Y = -4954686
97 meter
Z = -3776734
63 Z = -1151148
72
XDOT = 12776
523540 XDOT = 3894
284375
YDOT = 7110
118029 feet/sec YDOT = 2167
163975 meter/sec
ZDOT = 19281
377389 ZDOT = 5876
963828
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 15050
56430970
00016717 00000-0 10270-3 0 9068
2 25544 51
6469 311
4822 0006137 19
4072 340
7313 15
55021557 9730
Satellite: ISS
Catalog Number: 25544
Epoch time: 15050
56430970 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 311
4822 deg
Eccentricity:
0006137
Arg of perigee: 19
4072 deg
Mean anomaly: 340
7313 deg
Mean motion: 15
55021557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 973
Checksum: 292
Coasting Arc #8 (Orbit 988)
---------------------------------------
Vector Time (GMT): 2015/051/13:29:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4476660
54 A = 6786388
30 meter
Y = 5027174
74 meter E =
0008961
Z = -856764
94 I = 51
37350
XDOT = -3106
328434 Wp = 104
84308
YDOT = -3764
148251 meter/sec RA = 305
84772 deg
ZDOT = -5909
947999 TA = 84
45756
MA = 84
35536
Ha = 221
112 n
mi
Hp = 212
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14687206
49 X = -4528381
11
Y = 16493355
43 feet Y = 4976824
50 meter
Z = -2810908
58 Z = -878637
54
XDOT = -10191
366252 XDOT = -3035
298190
YDOT = -12349
567754 feet/sec YDOT = -3798
488848 meter/sec
ZDOT = -19389
593171 ZDOT = -5924
864649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16901591
85 X = -5151605
20
Y = 14196510
90 feet Y = 4327096
52 meter
Z = -2905389
13 Z = -885562
61
XDOT = -7139
546517 XDOT = -2176
133779
YDOT = -12445
881906 feet/sec YDOT = -3793
504805 meter/sec
ZDOT = -19452
699233 ZDOT = -5929
182726
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 15051
59254368
00016717 00000-0 10270-3 0 9078
2 25544 51
6463 306
3496 0005926 22
9065 337
2352 15
55023978 9890
Satellite: ISS
Catalog Number: 25544
Epoch time: 15051
59254368 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 306
3496 deg
Eccentricity:
0005926
Arg of perigee: 22
9065 deg
Mean anomaly: 337
2352 deg
Mean motion: 15
55023978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 989
Checksum: 332
Coasting Arc #9 (Orbit 1004)
---------------------------------------
Vector Time (GMT): 2015/052/13:29:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4851058
70 A = 6783258
23 meter
Y = -3854208
91 meter E =
0017745
Z = 2736062
65 I = 51
34515
XDOT = 1481
853589 Wp = 62
88527
YDOT = 5517
985667 meter/sec RA = 300
84827 deg
ZDOT = 5127
971836 TA = 328
26551
MA = 328
37235
Ha = 221
020 n
mi
Hp = 211
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15915546
90 X = 4880506
25
Y = -12645042
36 feet Y = -3799796
20 meter
Z = 8976583
49 Z = 2759699
83
XDOT = 4861
724374 XDOT = 1395
130621
YDOT = 18103
627516 feet/sec YDOT = 5534
072486 meter/sec
ZDOT = 16824
054581 ZDOT = 5134
958939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17342973
00 X = 5286138
17
Y = -10515940
36 feet Y = -3205258
62 meter
Z = 9078384
58 Z = 2767091
62
XDOT = 1637
570338 XDOT = 499
131439
YDOT = 17299
385650 feet/sec YDOT = 5272
852746 meter/sec
ZDOT = 16852
928448 ZDOT = 5136
772591
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 15052
62074432
00016717 00000-0 10270-3 0 9086
2 25544 51
6454 301
2157 0006137 25
3475 334
7978 15
55099335 10051
Satellite: ISS
Catalog Number: 25544
Epoch time: 15052
62074432 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 301
2157 deg
Eccentricity:
0006137
Arg of perigee: 25
3475 deg
Mean anomaly: 334
7978 deg
Mean motion: 15
55099335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1005
Checksum: 301
Coasting Arc #10 (Orbit 1019)
---------------------------------------
Vector Time (GMT): 2015/053/13:29:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4829161
03 A = 6778592
53 meter
Y = 2150345
47 meter E =
0013444
Z = -4257714
56 I = 51
31351
XDOT = 117
738858 Wp = 52
19662
YDOT = -6780
449133 meter/sec RA = 295
83494 deg
ZDOT = -3557
619188 TA = 181
27821
MA = 181
28165
Ha = 221
045 n
mi
Hp = 211
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15843704
17 X = -4832165
63
Y = 7054939
20 feet Y = 2096325
33 meter
Z = -13968879
80 Z = -4281180
99
XDOT = 386
282341 XDOT = 210
832086
YDOT = -22245
568021 feet/sec YDOT = -6778
612411 meter/sec
ZDOT = -11671
978963 ZDOT = -3556
820319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16438349
30 X = -5010408
87
Y = 5267906
24 feet Y = 1605657
82 meter
Z = -14069632
82 Z = -4288424
09
XDOT = 3302
075673 XDOT = 1006
472665
YDOT = -20860
504835 feet/sec YDOT = -6358
281874 meter/sec
ZDOT = -11667
330424 ZDOT = -3556
202313
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 15053
58465312
00016717 00000-0 10270-3 0 9094
2 25544 51
6443 296
4028 0005990 27
9529 332
1945 15
55144260 10206
Satellite: ISS
Catalog Number: 25544
Epoch time: 15053
58465312 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 296
4028 deg
Eccentricity:
0005990
Arg of perigee: 27
9529 deg
Mean anomaly: 332
1945 deg
Mean motion: 15
55144260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1020
Checksum: 304
Coasting Arc #11 (Orbit 1035)
---------------------------------------
Vector Time (GMT): 2015/054/13:29:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4425241
29 A = 6774989
18 meter
Y = -87139
32 meter E =
0007419
Z = 5122729
24 I = 51
28886
XDOT = -1547
728442 Wp = 70
35488
YDOT = 7374
604325 meter/sec RA = 290
80589 deg
ZDOT = 1463
163218 TA = 5
50982
MA = 5
50166
Ha = 220
950 n
mi
Hp = 211
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14518508
16 X = 4401002
73
Y = -285890
16 feet Y = -37788
38 meter
Z = 16806854
45 Z = 5144167
14
XDOT = -5077
849220 XDOT = -1637
185413
YDOT = 24194
896078 feet/sec YDOT = 7356
796586 meter/sec
ZDOT = 4800
404260 ZDOT = 1455
426672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14375168
84 X = 4381551
46
Y = 1064193
46 feet Y = 324366
17 meter
Z = 16898555
62 Z = 5150679
75
XDOT = -7270
204679 XDOT = -2215
958386
YDOT = 22563
534414 feet/sec YDOT = 6877
365289 meter/sec
ZDOT = 4765
985538 ZDOT = 1452
672392
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 15054
61279322
00016717 00000-0 10270-3 0 9105
2 25544 51
6443 291
2687 0006056 32
5936 327
5590 15
55176024 10362
Satellite: ISS
Catalog Number: 25544
Epoch time: 15054
61279322 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 291
2687 deg
Eccentricity:
0006056
Arg of perigee: 32
5936 deg
Mean anomaly: 327
5590 deg
Mean motion: 15
55176024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1036
Checksum: 301
Coasting Arc #12 (Orbit 1050)
---------------------------------------
Vector Time (GMT): 2015/055/13:29:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3774997
11 A = 6774334
49 meter
Y = -2087840
67 meter E =
0018096
Z = -5238273
16 I = 51
27571
XDOT = 2729
472295 Wp = 79
80192
YDOT = -7101
601438 meter/sec RA = 285
76780 deg
ZDOT = 869
217477 TA = 198
53108
MA = 198
59707
Ha = 220
963 n
mi
Hp = 211
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12385161
11 X = -3725924
47
Y = -6849870
96 feet Y = -2129781
24 meter
Z = -17185935
56 Z = -5256491
82
XDOT = 8954
961597 XDOT = 2804
458923
YDOT = -23299
217317 feet/sec YDOT = -7070
659347 meter/sec
ZDOT = 2851
763375 ZDOT = 882
659372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11717055
56 X = -3571358
53
Y = -7768669
77 feet Y = -2367890
55 meter
Z = -17263479
03 Z = -5261908
41
XDOT = 10122
990481 XDOT = 3085
487498
YDOT = -21694
216200 feet/sec YDOT = -6612
397098 meter/sec
ZDOT = 2910
525240 ZDOT = 887
128093
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 15055
57664357
00016717 00000-0 10270-3 0 9118
2 25544 51
6430 286
4545 0005974 35
2007 324
9540 15
55256329 10514
Satellite: ISS
Catalog Number: 25544
Epoch time: 15055
57664357 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 286
4545 deg
Eccentricity:
0005974
Arg of perigee: 35
2007 deg
Mean anomaly: 324
9540 deg
Mean motion: 15
55256329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1051
Checksum: 306
Coasting Arc #13 (Orbit 1066)
---------------------------------------
Vector Time (GMT): 2015/056/13:29:23
361
Vector Time (MET): N/A
Weight (LBS) : 927334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2903567
57 A = 6777156
58 meter
Y = 4128224
20 meter E =
0014174
Z = 4517083
00 I = 51
27844
XDOT = -3664
970121 Wp = 55
15627
YDOT = 5986
520164 meter/sec RA = 280
73424 deg
ZDOT = -3100
428353 TA = 66
10762
MA = 65
95918
Ha = 220
841 n
mi
Hp = 211
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9526140
33 X = 2835246
93
Y = 13544042
65 feet Y = 4160312
14 meter
Z = 14819826
12 Z = 4531021
55
XDOT = -12024
180188 XDOT = -3716
579852
YDOT = 19640
814185 feet/sec YDOT = 5945
247268 meter/sec
ZDOT = -10172
009033 ZDOT = -3118
357703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8613770
76 X = 2625477
33
Y = 14079870
99 feet Y = 4291544
68 meter
Z = 14878705
37 Z = 4535029
40
XDOT = -12074
213242 XDOT = -3680
220196
YDOT = 18269
500312 feet/sec YDOT = 5568
543695 meter/sec
ZDOT = -10249
756731 ZDOT = -3124
125852
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 15056
60472023
00016717 00000-0 10270-3 0 9121
2 25544 51
6435 281
3205 0005878 37
5063 322
6500 15
55308659 10678
Satellite: ISS
Catalog Number: 25544
Epoch time: 15056
60472023 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 281
3205 deg
Eccentricity:
0005878
Arg of perigee: 37
5063 deg
Mean anomaly: 322
6500 deg
Mean motion: 15
55308659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1067
Checksum: 293
Coasting Arc #14 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2015/057/09:22:37
037
Vector Time (MET): N/A
Weight (LBS) : 927066
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4266484
39 A = 6775356
33 meter
Y = -232280
81 meter E =
0009495
Z = 5250285
07 I = 51
26564
XDOT = -368
084752 Wp = 66
39289
YDOT = 7641
499747 meter/sec RA = 276
60545 deg
ZDOT = 640
006553 TA = 17
48843
MA = 17
45575
Ha = 222
348 n
mi
Hp = 211
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13997652
20 X = 4243261
11
Y = -762076
13 feet Y = -184699
66 meter
Z = 17225344
70 Z = 5270954
17
XDOT = -1207
627138 XDOT = -456
615322
YDOT = 25070
537229 feet/sec YDOT = 7636
888628 meter/sec
ZDOT = 2099
759032 ZDOT = 638
002897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6714536
64 X = 2046590
77
Y = 12180938
30 feet Y = 3712749
99 meter
Z = 17313788
35 Z = 5277242
69
XDOT = -22226
653761 XDOT = -6774
684066
YDOT = 9294
696334 feet/sec YDOT = 2833
023443 meter/sec
ZDOT = 2089
838933 ZDOT = 636
982907
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 15057
44003184
00016717 00000-0 10270-3 0 9133
2 25544 51
6453 277
1510 0007875 50
2854 309
8992 15
54855171 10801
Satellite: ISS
Catalog Number: 25544
Epoch time: 15057
44003184 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 277
1510 deg
Eccentricity:
0007875
Arg of perigee: 50
2854 deg
Mean anomaly: 309
8992 deg
Mean motion: 15
54855171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 308
Coasting Arc #15 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2015/058/09:22:37
037
Vector Time (MET): N/A
Weight (LBS) : 927066
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4053670
89 A = 6775956
99 meter
Y = -1866267
87 meter E =
0019756
Z = -5115480
11 I = 51
26551
XDOT = 1443
542970 Wp = 84
21694
YDOT = -7357
352884 meter/sec RA = 271
57159 deg
ZDOT = 1547
382410 TA = 200
76038
MA = 200
84073
Ha = 222
472 n
mi
Hp = 210
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13299445
18 X = -4007651
86
Y = -6122926
09 feet Y = -1911341
74 meter
Z = -16783071
23 Z = -5135059
84
XDOT = 4736
033367 XDOT = 1518
190851
YDOT = -24138
296864 feet/sec YDOT = -7340
792750 meter/sec
ZDOT = 5076
713942 ZDOT = 1554
576609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -460485
84 X = -140356
08
Y = -14537756
17 feet Y = -4431108
08 meter
Z = -16866491
76 Z = -5140906
69
XDOT = 22615
565048 XDOT = 6893
224227
YDOT = -6616
478807 feet/sec YDOT = -2016
702740 meter/sec
ZDOT = 5108
772442 ZDOT = 1557
153840
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 15058
40411401
00016717 00000-0 10270-3 0 9146
2 25544 51
6457 272
3398 0007913 52
9954 307
1922 15
54884263 10953
Satellite: ISS
Catalog Number: 25544
Epoch time: 15058
40411401 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 272
3398 deg
Eccentricity:
0007913
Arg of perigee: 52
9954 deg
Mean anomaly: 307
1922 deg
Mean motion: 15
54884263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 313
Coasting Arc #16 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2015/059/09:22:37
037
Vector Time (MET): N/A
Weight (LBS) : 927066
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3638324
59 A = 6779206
50 meter
Y = 3827663
78 meter E =
0017660
Z = 4241560
04 I = 51
27680
XDOT = -2480
548229 Wp = 65
42028
YDOT = 6328
033126 meter/sec RA = 266
54375 deg
ZDOT = -3563
823416 TA = 61
19617
MA = 61
01895
Ha = 222
349 n
mi
Hp = 210
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11936760
47 X = 3574648
80
Y = 12557952
04 feet Y = 3867994
21 meter
Z = 13915879
38 Z = 4259079
02
XDOT = -8138
281590 XDOT = -2533
814021
YDOT = 20761
263537 feet/sec YDOT = 6299
995903 meter/sec
ZDOT = -11692
334042 ZDOT = -3576
003107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5611736
85 X = -1710457
39
Y = 16328628
69 feet Y = 4976966
02 meter
Z = 13990153
80 Z = 4264198
88
XDOT = -20938
676656 XDOT = -6382
108645
YDOT = 2920
300554 feet/sec YDOT = 890
107609 meter/sec
ZDOT = -11745
526573 ZDOT = -3580
036499
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 15059
43243628
00016717 00000-0 10270-3 0 9155
2 25544 51
6453 267
2075 0007935 55
7085 304
4818 15
54952559 11111
Satellite: ISS
Catalog Number: 25544
Epoch time: 15059
43243628 = yrday
fracday
Element set: 915
Inclination: 51
6453 deg
RA of node: 267
2075 deg
Eccentricity:
0007935
Arg of perigee: 55
7085 deg
Mean anomaly: 304
4818 deg
Mean motion: 15
54952559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 320
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