[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 7th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 304)
---------------------------------------
Vector Time (GMT): 2015/007/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6417335
11 A = 6792351
62 meter
Y = -2147604
97 meter E =
0014193
Z = 465242
03 I = 51
75334
XDOT = 1904
852339 Wp = 158
02425
YDOT = 4381
887991 meter/sec RA = 164
60330 deg
ZDOT = -6001
158956 TA = 16
96549
MA = 16
91808
Ha = 222
479 n
mi
Hp = 217
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21054249
06 X = 6438613
24
Y = -7045948
05 feet Y = -2075723
21 meter
Z = 1526384
60 Z = 496467
38
XDOT = 6249
515548 XDOT = 1884
862482
YDOT = 14376
272937 feet/sec YDOT = 4403
077829 meter/sec
ZDOT = -19688
841718 ZDOT = -5991
953994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19359556
00 X = 5900792
67
Y = 10849330
35 feet Y = 3306875
89 meter
Z = 1660198
72 Z = 506028
57
XDOT = -5570
453922 XDOT = -1697
874355
YDOT = 12968
214735 feet/sec YDOT = 3952
711851 meter/sec
ZDOT = -19650
232875 ZDOT = -5989
390980
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 15007
60607603
00016717 00000-0 10270-3 0 9008
2 25544 51
6434 165
5533 0006684 223
3195 136
7432 15
53053569 3058
Satellite: ISS
Catalog Number: 25544
Epoch time: 15007
60607603 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 165
5533 deg
Eccentricity:
0006684
Arg of perigee: 223
3195 deg
Mean anomaly: 136
7432 deg
Mean motion: 15
53053569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 305
Checksum: 290
Coasting Arc #2 (Orbit 320)
---------------------------------------
Vector Time (GMT): 2015/008/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6519924
60 A = 6792051
62 meter
Y = 1669401
88 meter E =
0006922
Z = 892229
63 I = 51
78419
XDOT = -419
876187 Wp = 61
36313
YDOT = -4829
393624 meter/sec RA = 159
64664 deg
ZDOT = 5936
107583 TA = 308
26588
MA = 308
32814
Ha = 222
253 n
mi
Hp = 217
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21390828
75 X = -6542441
74
Y = 5477040
30 feet Y = 1596365
92 meter
Z = 2927262
55 Z = 860502
86
XDOT = -1377
546544 XDOT = -394
676597
YDOT = -15844
467271 feet/sec YDOT = -4833
948262 meter/sec
ZDOT = 19475
418581 ZDOT = 5934
128969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18649797
47 X = -5684458
27
Y = -11854438
08 feet Y = -3613232
73 meter
Z = 2791369
47 Z = 850809
41
XDOT = 9655
438600 XDOT = 2942
977685
YDOT = -10580
508433 feet/sec YDOT = -3224
938970 meter/sec
ZDOT = 19467
767648 ZDOT = 5933
775579
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 15008
63561121
00016717 00000-0 10270-3 0 9017
2 25544 51
6448 160
4293 0006566 227
2426 132
8174 15
53086767 3213
Satellite: ISS
Catalog Number: 25544
Epoch time: 15008
63561121 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 160
4293 deg
Eccentricity:
0006566
Arg of perigee: 227
2426 deg
Mean anomaly: 132
8174 deg
Mean motion: 15
53086767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 321
Checksum: 294
Coasting Arc #3 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2015/009/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6323728
68 A = 6790271
50 meter
Y = -1061102
64 meter E =
0008725
Z = -2217160
53 I = 51
80775
XDOT = -1036
969496 Wp = 186
59153
YDOT = 5260
744465 meter/sec RA = 154
69000 deg
ZDOT = -5481
651742 TA = 17
97796
MA = 17
94712
Ha = 222
124 n
mi
Hp = 218
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20747141
35 X = 6345894
20
Y = -3481307
88 feet Y = -990262
62 meter
Z = -7274148
73 Z = -2186387
61
XDOT = -3402
130891 XDOT = -1069
091789
YDOT = 17259
660318 feet/sec YDOT = 5248
968909 meter/sec
ZDOT = -17984
421727 ZDOT = -5486
766992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16990790
69 X = 5178793
00
Y = 12481004
91 feet Y = 3804210
30 meter
Z = -7142420
21 Z = -2177009
68
XDOT = -13755
913378 XDOT = -4192
802398
YDOT = 8433
596753 feet/sec YDOT = 2570
560290 meter/sec
ZDOT = -18007
167772 ZDOT = -5488
584737
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 15009
60078270
00016717 00000-0 10270-3 0 9024
2 25544 51
6449 155
6258 0006553 231
4656 128
5910 15
53113916 3362
Satellite: ISS
Catalog Number: 25544
Epoch time: 15009
60078270 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 155
6258 deg
Eccentricity:
0006553
Arg of perigee: 231
4656 deg
Mean anomaly: 128
5910 deg
Mean motion: 15
53113916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 300
Coasting Arc #4 (Orbit 351)
---------------------------------------
Vector Time (GMT): 2015/010/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5870873
11 A = 6787373
56 meter
Y = 344334
00 meter E =
0007967
Z = 3386120
61 I = 51
82738
XDOT = 2361
506311 Wp = 116
12307
YDOT = -5614
065375 meter/sec RA = 149
72979 deg
ZDOT = 4653
375897 TA = 283
27523
MA = 283
36407
Ha = 221
778 n
mi
Hp = 218
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19261394
71 X = -5890735
55
Y = 1129704
72 feet Y = 278570
98 meter
Z = 11109319
57 Z = 3357553
06
XDOT = 7747
724118 XDOT = 2401
504442
YDOT = -18418
849655 feet/sec YDOT = -5587
433890 meter/sec
ZDOT = 15266
981288 ZDOT = 4664
944616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14508957
49 X = -4422330
24
Y = -12824497
80 feet Y = -3908906
93 meter
Z = 10987126
50 Z = 3348876
16
XDOT = 17474
109246 XDOT = 5326
108498
YDOT = -6612
582184 feet/sec YDOT = -2015
515050 meter/sec
ZDOT = 15317
381013 ZDOT = 4668
737733
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 15010
63027811
00016717 00000-0 10270-3 0 9035
2 25544 51
6457 150
5015 0006518 235
6034 124
4502 15
53169099 3526
Satellite: ISS
Catalog Number: 25544
Epoch time: 15010
63027811 = yrday
fracday
Element set: 903
Inclination: 51
6457 deg
RA of node: 150
5015 deg
Eccentricity:
0006518
Arg of perigee: 235
6034 deg
Mean anomaly: 124
4502 deg
Mean motion: 15
53169099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 352
Checksum: 275
Coasting Arc #5 (Orbit 366)
---------------------------------------
Vector Time (GMT): 2015/011/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5184710
06 A = 6784272
04 meter
Y = 518820
63 meter E =
0002353
Z = -4346481
29 I = 51
84368
XDOT = -3514
045471 Wp = 97
13411
YDOT = 5844
915092 meter/sec RA = 144
76514 deg
ZDOT = -3495
960058 TA = 137
41578
MA = 137
39754
Ha = 221
673 n
mi
Hp = 218
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17010203
59 X = 5199636
58
Y = 1702167
43 feet Y = 576882
92 meter
Z = -14260109
23 Z = -4321258
88
XDOT = -11529
020573 XDOT = -3562
161557
YDOT = 19176
230616 feet/sec YDOT = 5805
349743 meter/sec
ZDOT = -11469
685230 ZDOT = -3513
147325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11156842
48 X = 3400605
59
Y = 13070229
31 feet Y = 3983805
89 meter
Z = -14152352
71 Z = -4313637
11
XDOT = -20591
161716 XDOT = -6276
186091
YDOT = 5083
654083 feet/sec YDOT = 1549
497764 meter/sec
ZDOT = -11544
155137 ZDOT = -3518
658486
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 15011
59541402
00016717 00000-0 10270-3 0 9049
2 25544 51
6457 145
6981 0006508 240
2052 119
8453 15
53158087 3678
Satellite: ISS
Catalog Number: 25544
Epoch time: 15011
59541402 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 145
6981 deg
Eccentricity:
0006508
Arg of perigee: 240
2052 deg
Mean anomaly: 119
8453 deg
Mean motion: 15
53158087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 367
Checksum: 301
Coasting Arc #6 (Orbit 382)
---------------------------------------
Vector Time (GMT): 2015/012/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4339586
88 A = 6781470
54 meter
Y = -1473658
53 meter E =
0006156
Z = 5000933
35 I = 51
86043
XDOT = 4425
348162 Wp = 185
47762
YDOT = -5896
253713 meter/sec RA = 139
79471 deg
ZDOT = 2096
870790 TA = 244
13547
MA = 244
19896
Ha = 221
291 n
mi
Hp = 218
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14237489
75 X = -4347078
11
Y = -4834837
69 feet Y = -1522228
53 meter
Z = 16407261
63 Z = 4979834
35
XDOT = 14518
858799 XDOT = 4480
766781
YDOT = -19344
664414 feet/sec YDOT = -5846
456744 meter/sec
ZDOT = 6879
497341 ZDOT = 2118
502751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7226906
92 X = -2202761
23
Y = -13296536
34 feet Y = -4052784
28 meter
Z = 16317289
66 Z = 4973509
89
XDOT = 22798
079291 XDOT = 6948
854568
YDOT = -3810
703562 feet/sec YDOT = -1161
502446 meter/sec
ZDOT = 6972
993861 ZDOT = 2125
368529
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 15012
62487028
00016717 00000-0 10270-3 0 9058
2 25544 51
6459 140
5734 0006398 244
6756 115
3734 15
53228787 3832
Satellite: ISS
Catalog Number: 25544
Epoch time: 15012
62487028 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 140
5734 deg
Eccentricity:
0006398
Arg of perigee: 244
6756 deg
Mean anomaly: 115
3734 deg
Mean motion: 15
53228787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 383
Checksum: 324
Coasting Arc #7 (Orbit 397)
---------------------------------------
Vector Time (GMT): 2015/013/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3381355
00 A = 6780094
99 meter
Y = 2517217
80 meter E =
0008773
Z = -5317752
80 I = 51
87898
XDOT = -5082
807111 Wp = 97
52510
YDOT = 5707
097125 meter/sec RA = 134
82176 deg
ZDOT = -532
313561 TA = 167
41872
MA = 167
39681
Ha = 221
013 n
mi
Hp = 218
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11093684
39 X = 3378787
17
Y = 8258588
58 feet Y = 2555016
02 meter
Z = -17446695
55 Z = -5301333
08
XDOT = -16675
876348 XDOT = -5143
661670
YDOT = 18724
071934 feet/sec YDOT = 5649
917621 meter/sec
ZDOT = -1746
435568 ZDOT = -557
152543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2833386
66 X = 863616
25
Y = 13626311
49 feet Y = 4153299
74 meter
Z = -17376905
93 Z = -5296480
93
XDOT = -23912
599044 XDOT = -7288
560189
YDOT = 2616
284718 feet/sec YDOT = 797
443582 meter/sec
ZDOT = -1853
630089 ZDOT = -564
986451
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 15013
58996896
00016717 00000-0 10270-3 0 9063
2 25544 51
6456 135
7698 0006362 249
6386 110
4083 15
53222704 3981
Satellite: ISS
Catalog Number: 25544
Epoch time: 15013
58996896 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 135
7698 deg
Eccentricity:
0006362
Arg of perigee: 249
6386 deg
Mean anomaly: 110
4083 deg
Mean motion: 15
53222704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 398
Checksum: 338
Coasting Arc #8 (Orbit 413)
---------------------------------------
Vector Time (GMT): 2015/014/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2386764
31 A = 6780138
92 meter
Y = -3566490
45 meter E =
0002968
Z = 5251758
46 I = 51
90162
XDOT = 5480
080809 Wp = 275
08916
YDOT = -5250
436938 meter/sec RA = 129
84774 deg
ZDOT = -1075
328385 TA = 185
17815
MA = 185
18122
Ha = 220
713 n
mi
Hp = 218
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7830591
56 X = -2372216
63
Y = -11701084
17 feet Y = -3593099
58 meter
Z = 17230178
68 Z = 5240199
29
XDOT = 17979
267747 XDOT = 5543
608672
YDOT = -17225
842972 feet/sec YDOT = -5188
799883 meter/sec
ZDOT = -3527
980266 ZDOT = -1048
553060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1653824
13 X = 504085
60
Y = -14042026
64 feet Y = -4280009
72 meter
Z = 17181354
60 Z = 5236876
88
XDOT = 23860
536427 XDOT = 7272
691503
YDOT = -1364
215851 feet/sec YDOT = -415
812991 meter/sec
ZDOT = -3412
564477 ZDOT = -1040
149653
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 15014
61938605
00016717 00000-0 10270-3 0 9073
2 25544 51
6458 130
6445 0006310 254
1509 105
8948 15
53293252 4141
Satellite: ISS
Catalog Number: 25544
Epoch time: 15014
61938605 = yrday
fracday
Element set: 907
Inclination: 51
6458 deg
RA of node: 130
6445 deg
Eccentricity:
0006310
Arg of perigee: 254
1509 deg
Mean anomaly: 105
8948 deg
Mean motion: 15
53293252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 414
Checksum: 298
Coasting Arc #9 (Orbit 428)
---------------------------------------
Vector Time (GMT): 2015/015/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1405985
57 A = 6781934
51 meter
Y = 4574367
51 meter E =
0006845
Z = -4811689
55 I = 51
92681
XDOT = -5629
652713 Wp = 135
30534
YDOT = 4488
209855 meter/sec RA = 124
87833 deg
ZDOT = 2619
369365 TA = 160
44834
MA = 160
42208
Ha = 220
377 n
mi
Hp = 218
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4612813
54 X = 1378102
77
Y = 15007767
41 feet Y = 4589934
43 meter
Z = -15786383
04 Z = -4804927
11
XDOT = -18469
989216 XDOT = -5692
146417
YDOT = 14725
097950 feet/sec YDOT = 4424
905899 meter/sec
ZDOT = 8593
731514 ZDOT = 2591
870021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6008656
82 X = -1831438
60
Y = 14535974
76 feet Y = 4430565
11 meter
Z = -15758251
87 Z = -4803115
17
XDOT = -22596
966564 XDOT = -6887
555409
YDOT = -143
968435 feet/sec YDOT = -43
881579 meter/sec
ZDOT = 8475
331244 ZDOT = 2583
280963
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 15015
58444794
00016717 00000-0 10270-3 0 9082
2 25544 51
6453 125
8407 0006127 258
0730 101
9735 15
53314393 4292
Satellite: ISS
Catalog Number: 25544
Epoch time: 15015
58444794 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 125
8407 deg
Eccentricity:
0006127
Arg of perigee: 258
0730 deg
Mean anomaly: 101
9735 deg
Mean motion: 15
53314393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 429
Checksum: 308
Coasting Arc #10 (Orbit 444)
---------------------------------------
Vector Time (GMT): 2015/016/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -486203
90 A = 6784808
92 meter
Y = -5448658
20 meter E =
0004730
Z = 4010805
40 I = 51
95443
XDOT = 5575
526898 Wp = 72
89257
YDOT = -3435
542260 meter/sec RA = 119
91466 deg
ZDOT = -3986
056362 TA = 58
44542
MA = 58
39924
Ha = 220
149 n
mi
Hp = 218
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1595157
15 X = -444722
51
Y = -17876175
21 feet Y = -5453863
53 meter
Z = 13158810
36 Z = 4008543
99
XDOT = 18292
411084 XDOT = 5632
892255
YDOT = -11271
464107 feet/sec YDOT = -3372
872135 meter/sec
ZDOT = -13077
612735 ZDOT = -3958
832471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9920534
96 X = 3023779
06
Y = -14963774
25 feet Y = -4560958
39 meter
Z = 13150091
35 Z = 4008147
84
XDOT = 20287
345560 XDOT = 6183
582927
YDOT = 2045
156779 feet/sec YDOT = 623
363786 meter/sec
ZDOT = -12960
555248 ZDOT = -3950
377239
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 15016
61382650
00016717 00000-0 10270-3 0 9090
2 25544 51
6458 120
7153 0006170 263
5629 96
4821 15
53342229 4456
Satellite: ISS
Catalog Number: 25544
Epoch time: 15016
61382650 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 120
7153 deg
Eccentricity:
0006170
Arg of perigee: 263
5629 deg
Mean anomaly: 96
4821 deg
Mean motion: 15
53342229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 445
Checksum: 300
Coasting Arc #11 (Orbit 459)
---------------------------------------
Vector Time (GMT): 2015/017/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -335907
78 A = 6787996
64 meter
Y = 6119895
67 meter E =
0002559
Z = -2913490
12 I = 51
97960
XDOT = -5351
429656 Wp = 309
67789
YDOT = 2117
080019 meter/sec RA = 114
95967 deg
ZDOT = 5062
635217 TA = 17
29999
MA = 17
29127
Ha = 219
991 n
mi
Hp = 218
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1102059
65 X = -390164
38
Y = 20078397
86 feet Y = 6115836
15 meter
Z = -9558694
61 Z = -2915253
27
XDOT = -17557
183912 XDOT = -5399
297827
YDOT = 6945
800587 feet/sec YDOT = 2056
968885 meter/sec
ZDOT = 16609
695595 ZDOT = 5036
523056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13160952
68 X = -4011458
38
Y = 15198057
50 feet Y = 4632367
93 meter
Z = -9567319
98 Z = -2916119
13
XDOT = -17094
101029 XDOT = -5210
281994
YDOT = -4414
652732 feet/sec YDOT = -1345
586153 meter/sec
ZDOT = 16497
609052 ZDOT = 5028
471239
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 15017
57885144
00016717 00000-0 10270-3 0 9104
2 25544 51
6453 115
9108 0006148 267
3577 92
6872 15
53347616 4602
Satellite: ISS
Catalog Number: 25544
Epoch time: 15017
57885144 = yrday
fracday
Element set: 910
Inclination: 51
6453 deg
RA of node: 115
9108 deg
Eccentricity:
0006148
Arg of perigee: 267
3577 deg
Mean anomaly: 92
6872 deg
Mean motion: 15
53347616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 460
Checksum: 320
Coasting Arc #12 (Orbit 475)
---------------------------------------
Vector Time (GMT): 2015/018/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1057796
28 A = 6790391
29 meter
Y = -6513140
17 meter E =
0008764
Z = 1580790
14 I = 52
00098
XDOT = 5013
464707 Wp = 133
66859
YDOT = -589
909530 meter/sec RA = 110
01223 deg
ZDOT = -5771
293960 TA = 29
13505
MA = 29
08618
Ha = 219
966 n
mi
Hp = 218
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3470460
23 X = 1122870
32
Y = -21368570
13 feet Y = -6500947
46 meter
Z = 5186319
36 Z = 1586086
28
XDOT = 16448
375024 XDOT = 5047
723061
YDOT = -1935
398720 feet/sec YDOT = -533
653780 meter/sec
ZDOT = -18934
691471 ZDOT = -5746
856631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15588270
11 X = 4751304
73
Y = -15013928
87 feet Y = -4576245
52 meter
Z = 5210140
77 Z = 1588050
91
XDOT = 13312
046097 XDOT = 4057
511650
YDOT = 7270
974712 feet/sec YDOT = 2216
193092 meter/sec
ZDOT = -18830
027770 ZDOT = -5739
392464
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 15018
60819164
00016717 00000-0 10270-3 0 9119
2 25544 51
6458 110
7857 0006030 272
9943 87
0519 15
53396152 4762
Satellite: ISS
Catalog Number: 25544
Epoch time: 15018
60819164 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 110
7857 deg
Eccentricity:
0006030
Arg of perigee: 272
9943 deg
Mean anomaly: 87
0519 deg
Mean motion: 15
53396152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 476
Checksum: 315
Coasting Arc #13 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2015/019/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1666575
37 A = 6791552
45 meter
Y = 6576134
75 meter E =
0009635
Z = -128640
46 I = 52
01418
XDOT = -4603
315764 Wp = 14
12965
YDOT = -1050
452666 meter/sec RA = 105
06937 deg
ZDOT = 6042
000889 TA = 344
49199
MA = 344
52149
Ha = 220
210 n
mi
Hp = 218
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5467766
95 X = -1739362
51
Y = 21575245
23 feet Y = 6557091
05 meter
Z = -422048
74 Z = -136912
64
XDOT = -15102
742009 XDOT = -4620
576518
YDOT = -3446
367015 feet/sec YDOT = -1102
026787 meter/sec
ZDOT = 19822
837562 ZDOT = 6019
597260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17090543
06 X = -5209197
53
Y = 14257237
01 feet Y = 4345605
84 meter
Z = -458626
02 Z = -139789
21
XDOT = -9265
460687 XDOT = -2824
112418
YDOT = -10482
291194 feet/sec YDOT = -3195
002356 meter/sec
ZDOT = 19727
158876 ZDOT = 6012
838025
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 15019
57318016
00016717 00000-0 10270-3 0 9127
2 25544 51
6455 105
9806 0006003 278
5666 81
4806 15
53360949 4912
Satellite: ISS
Catalog Number: 25544
Epoch time: 15019
57318016 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 105
9806 deg
Eccentricity:
0006003
Arg of perigee: 278
5666 deg
Mean anomaly: 81
4806 deg
Mean motion: 15
53360949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 491
Checksum: 313
Coasting Arc #14 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2015/020/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2195072
47 A = 6790554
14 meter
Y = -6277607
64 meter E =
0005739
Z = -1353853
78 I = 52
01940
XDOT = 4151
949709 Wp = 184
04896
YDOT = 2711
660009 meter/sec RA = 100
12761 deg
ZDOT = -5845
831919 TA = 10
61112
MA = 10
59901
Ha = 220
204 n
mi
Hp = 217
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7201681
34 X = 2271683
39
Y = -20595825
58 feet Y = -6252632
50 meter
Z = -4441777
51 Z = -1343004
93
XDOT = 13621
882247 XDOT = 4149
714986
YDOT = 8896
522338 feet/sec YDOT = 2758
077533 meter/sec
ZDOT = -19179
238579 ZDOT = -5825
668293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17727896
61 X = 5403462
89
Y = -12735547
12 feet Y = -3881794
76 meter
Z = -4394218
30 Z = -1339357
74
XDOT = 5236
389112 XDOT = 1596
051401
YDOT = 13872
333316 feet/sec YDOT = 4228
287195 meter/sec
ZDOT = -19093
437644 ZDOT = -5819
679794
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 15020
60248238
00016717 00000-0 10270-3 0 9132
2 25544 51
6460 100
8552 0005881 281
9980 78
0513 15
53445310 5071
Satellite: ISS
Catalog Number: 25544
Epoch time: 15020
60248238 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 100
8552 deg
Eccentricity:
0005881
Arg of perigee: 281
9980 deg
Mean anomaly: 78
0513 deg
Mean motion: 15
53445310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 287
Coasting Arc #15 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2015/021/13:44:59
274
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2649338
73 A = 6788197
75 meter
Y = 5616050
26 meter E =
0008865
Z = 2729422
51 I = 52
01535
XDOT = -3686
784405 Wp = 60
52423
YDOT = -4268
526582 meter/sec RA = 95
18189 deg
ZDOT = 5195
899010 TA = 330
17539
MA = 330
22588
Ha = 220
531 n
mi
Hp = 217
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8692056
19 X = -2725200
03
Y = 18425361
74 feet Y = 5585999
43 meter
Z = 8954798
25 Z = 2716368
64
XDOT = -12095
749359 XDOT = -3664
017896
YDOT = -14004
352304 feet/sec YDOT = -4309
627376 meter/sec
ZDOT = 17046
912764 ZDOT = 5178
044969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17552922
83 X = -5350130
88
Y = 10390198
83 feet Y = 3166932
60 meter
Z = 8897914
15 Z = 2712084
23
XDOT = -1535
827469 XDOT = -468
120213
YDOT = -17152
112660 feet/sec YDOT = -5227
963939 meter/sec
ZDOT = 16971
274148 ZDOT = 5172
844360
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 15021
63176516
00016717 00000-0 10270-3 0 9146
2 25544 51
6452 95
7293 0005771 287
2136 72
8385 15
53446230 5235
Satellite: ISS
Catalog Number: 25544
Epoch time: 15021
63176516 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 95
7293 deg
Eccentricity:
0005771
Arg of perigee: 287
2136 deg
Mean anomaly: 72
8385 deg
Mean motion: 15
53446230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 305
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