[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 20th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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
028/18:41:47
058 1
0 -1
6 1
6
N/A 0
7 0
2 220
4
000/00:03:30
115 -1
0 -0
0 216
6
Coasting Arc #1 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2015/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1806865
44 A = 6784504
80 meter
Y = 5181679
07 meter E =
0001595
Z = -3990873
90 I = 51
99214
XDOT = -4547
491013 Wp = 166
00655
YDOT = 4681
148285 meter/sec RA = 105
41113 deg
ZDOT = 4017
874524 TA = 145
70871
MA = 145
69842
Ha = 219
855 n
mi
Hp = 218
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5928036
23 X = 1768174
26
Y = 17000259
43 feet Y = 5201668
51 meter
Z = -13093418
29 Z = -3982190
31
XDOT = -14919
589938 XDOT = -4619
015745
YDOT = 15358
098047 feet/sec YDOT = 4629
895135 meter/sec
ZDOT = 13182
003033 ZDOT = 3995
610599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12249713
77 X = -3733712
76
Y = 13230356
62 feet Y = 4032612
70 meter
Z = -13057190
10 Z = -3979831
54
XDOT = -19611
434938 XDOT = -5977
565369
YDOT = -5239
401178 feet/sec YDOT = -1596
969479 meter/sec
ZDOT = 13085
894859 ZDOT = 3988
580753
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
50865713
00016717 00000-0 10270-3 0 9008
2 25544 51
6463 106
3067 0006155 274
4912 85
5537 15
53480389 4908
Satellite: ISS
Catalog Number: 25544
Epoch time: 15019
50865713 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 106
3067 deg
Eccentricity:
0006155
Arg of perigee: 274
4912 deg
Mean anomaly: 85
5537 deg
Mean motion: 15
53480389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 490
Checksum: 310
Coasting Arc #2 (Orbit 505)
---------------------------------------
Vector Time (GMT): 2015/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1134562
36 A = 6787752
07 meter
Y = -6057740
72 meter E =
0007274
Z = 2836484
21 I = 52
01052
XDOT = 4671
411873 Wp = 99
52237
YDOT = -3277
162571 meter/sec RA = 100
45782 deg
ZDOT = -5120
387054 TA = 48
43968
MA = 48
37733
Ha = 219
996 n
mi
Hp = 217
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3722317
45 X = -1080517
25
Y = -19874477
41 feet Y = -6070126
06 meter
Z = 9306050
55 Z = 2831103
87
XDOT = 15326
154440 XDOT = 4732
583102
YDOT = -10751
845707 feet/sec YDOT = -3224
581579 meter/sec
ZDOT = -16799
170126 ZDOT = -5097
546255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15612626
21 X = 4758728
47
Y = -12864841
31 feet Y = -3921203
63 meter
Z = 9284117
47 Z = 2829799
01
XDOT = 15907
437151 XDOT = 4848
586844
YDOT = 7228
988931 feet/sec YDOT = 2203
395826 meter/sec
ZDOT = -16700
833346 ZDOT = -5090
414004
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
53792087
00016717 00000-0 10270-3 0 9017
2 25544 51
6461 101
1812 0006094 280
0424 80
0041 15
53504405 5064
Satellite: ISS
Catalog Number: 25544
Epoch time: 15020
53792087 = yrday
fracday
Element set: 901
Inclination: 51
6461 deg
RA of node: 101
1812 deg
Eccentricity:
0006094
Arg of perigee: 280
0424 deg
Mean anomaly: 80
0041 deg
Mean motion: 15
53504405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 506
Checksum: 255
Coasting Arc #3 (Orbit 520)
---------------------------------------
Vector Time (GMT): 2015/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 503503
71 A = 6790277
41 meter
Y = 6607687
75 meter E =
0008354
Z = -1454984
20 I = 52
02332
XDOT = -4719
917329 Wp = 354
23326
YDOT = 1639
312979 meter/sec RA = 95
51141 deg
ZDOT = 5816
646224 TA = 349
98010
MA = 349
99675
Ha = 220
307 n
mi
Hp = 218
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1651915
04 X = 436645
18
Y = 21678765
59 feet Y = 6612944
45 meter
Z = -4773570
20 Z = -1452700
62
XDOT = -15485
293075 XDOT = -4766
152176
YDOT = 5378
323421 feet/sec YDOT = 1586
273193 meter/sec
ZDOT = 19083
484986 ZDOT = 5793
606020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17996668
68 X = -5485384
61
Y = 12202435
55 feet Y = 3719302
36 meter
Z = -4764992
78 Z = -1452369
80
XDOT = -11515
851651 XDOT = -3510
031583
YDOT = -9577
342300 feet/sec YDOT = -2919
173933 meter/sec
ZDOT = 18984
581894 ZDOT = 5786
500561
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
50283330
00016717 00000-0 10270-3 0 9022
2 25544 51
6457 96
3756 0006211 285
2907 74
7558 15
53494567 5212
Satellite: ISS
Catalog Number: 25544
Epoch time: 15021
50283330 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 96
3756 deg
Eccentricity:
0006211
Arg of perigee: 285
2907 deg
Mean anomaly: 74
7558 deg
Mean motion: 15
53494567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 521
Checksum: 308
Coasting Arc #4 (Orbit 536)
---------------------------------------
Vector Time (GMT): 2015/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 119884
47 A = 6790948
88 meter
Y = -6785174
36 meter E =
0007057
Z = -67179
87 I = 52
02777
XDOT = 4715
374909 Wp = 156
84292
YDOT = 140
956025 meter/sec RA = 90
56953 deg
ZDOT = -6042
934273 TA = 23
87657
MA = 23
84385
Ha = 220
333 n
mi
Hp = 217
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 393321
74 X = 196075
30
Y = -22261070
72 feet Y = -6783407
72 meter
Z = -220406
39 Z = -66412
39
XDOT = 15470
390123 XDOT = 4742
801924
YDOT = 462
454151 feet/sec YDOT = 193
839714 meter/sec
ZDOT = -19825
899845 ZDOT = -6019
961780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19345170
65 X = 5896408
01
Y = -11021629
43 feet Y = -3359392
65 meter
Z = -215888
74 Z = -65802
89
XDOT = 6759
432007 XDOT = 2060
274876
YDOT = 12236
072988 feet/sec YDOT = 3729
555047 meter/sec
ZDOT = -19727
604300 ZDOT = -6012
973791
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 15022
53205096
00016717 00000-0 10270-3 0 9030
2 25544 51
6451 91
2496 0006024 289
3150 70
7351 15
53570308 5370
Satellite: ISS
Catalog Number: 25544
Epoch time: 15022
53205096 = yrday
fracday
Element set: 903
Inclination: 51
6451 deg
RA of node: 91
2496 deg
Eccentricity:
0006024
Arg of perigee: 289
3150 deg
Mean anomaly: 70
7351 deg
Mean motion: 15
53570308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 537
Checksum: 284
Coasting Arc #5 (Orbit 552)
---------------------------------------
Vector Time (GMT): 2015/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -738583
50 A = 6789877
14 meter
Y = 6553804
35 meter E =
0011222
Z = 1583609
11 I = 52
02339
XDOT = -4667
647289 Wp = 37
92286
YDOT = -1924
338561 meter/sec RA = 85
62652 deg
ZDOT = 5773
952150 TA = 339
30610
MA = 339
35151
Ha = 220
632 n
mi
Hp = 217
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2423174
20 X = -819507
22
Y = 21501982
78 feet Y = 6545092
60 meter
Z = 5195567
95 Z = 1579824
56
XDOT = -15313
803442 XDOT = -4673
829137
YDOT = -6313
446721 feet/sec YDOT = -1976
569641 meter/sec
ZDOT = 18943
412565 ZDOT = 5751
263096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19589413
62 X = -5970853
27
Y = 9200128
41 feet Y = 2804199
14 meter
Z = 5178172
91 Z = 1578307
10
XDOT = -2061
128415 XDOT = -628
231941
YDOT = -15020
371967 feet/sec YDOT = -4578
209376 meter/sec
ZDOT = 18846
653731 ZDOT = 5744
460057
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 15023
56124487
00016717 00000-0 10270-3 0 9049
2 25544 51
6448 86
1226 0006005 294
7114 65
3413 15
53578074 5534
Satellite: ISS
Catalog Number: 25544
Epoch time: 15023
56124487 = yrday
fracday
Element set: 904
Inclination: 51
6448 deg
RA of node: 86
1226 deg
Eccentricity:
0006005
Arg of perigee: 294
7114 deg
Mean anomaly: 65
3413 deg
Mean motion: 15
53578074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 553
Checksum: 297
Coasting Arc #6 (Orbit 567)
---------------------------------------
Vector Time (GMT): 2015/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1391095
74 A = 6786995
95 meter
Y = -5933166
45 meter E =
0001538
Z = -2988211
32 I = 52
01099
XDOT = 4553
702052 Wp = 319
12759
YDOT = 3591
672197 meter/sec RA = 80
67873 deg
ZDOT = -5008
894088 TA = 254
83305
MA = 254
85005
Ha = 220
658 n
mi
Hp = 217
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4563962
39 X = 1471853
79
Y = -19465769
19 feet Y = -5917158
87 meter
Z = -9803842
91 Z = -2981257
40
XDOT = 14939
967361 XDOT = 4537
531643
YDOT = 11783
701434 feet/sec YDOT = 3642
504072 meter/sec
ZDOT = -16433
379554 ZDOT = -4986
812831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18885286
13 X = 5756235
21
Y = -6610289
04 feet Y = -2014816
10 meter
Z = -9772988
57 Z = -2978806
92
XDOT = -2283
383574 XDOT = -695
975314
YDOT = 17646
245580 feet/sec YDOT = 5378
575653 meter/sec
ZDOT = -16339
530445 ZDOT = -4980
288880
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 15024
52609166
00016717 00000-0 10270-3 0 9059
2 25544 51
6447 81
3162 0005944 298
6097 61
4457 15
53638140 5685
Satellite: ISS
Catalog Number: 25544
Epoch time: 15024
52609166 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 81
3162 deg
Eccentricity:
0005944
Arg of perigee: 298
6097 deg
Mean anomaly: 61
4457 deg
Mean motion: 15
53638140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 568
Checksum: 318
Coasting Arc #7 (Orbit 583)
---------------------------------------
Vector Time (GMT): 2015/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2076942
94 A = 6783427
88 meter
Y = 4952905
60 meter E =
0005233
Z = 4138674
93 I = 51
99325
XDOT = -4358
470089 Wp = 81
72623
YDOT = -5022
481588 meter/sec RA = 75
72247 deg
ZDOT = 3819
965451 TA = 329
04860
MA = 329
07943
Ha = 220
891 n
mi
Hp = 217
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6814117
25 X = -2152277
02
Y = 16249690
28 feet Y = 4929258
78 meter
Z = 13578329
82 Z = 4128402
53
XDOT = -14299
442549 XDOT = -4320
539325
YDOT = -16477
957967 feet/sec YDOT = -5071
008632 meter/sec
ZDOT = 12532
695049 ZDOT = 3798
885397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17351589
02 X = -5288764
33
Y = 3259432
94 feet Y = 993475
16 meter
Z = 13533444
66 Z = 4124993
93
XDOT = 5988
318094 XDOT = 1825
239355
YDOT = -19833
458604 feet/sec YDOT = -6045
238182 meter/sec
ZDOT = 12443
402156 ZDOT = 3792
748977
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 15025
55523850
00016717 00000-0 10270-3 0 9069
2 25544 51
6446 76
1891 0005931 303
0885 56
9698 15
53676155 5849
Satellite: ISS
Catalog Number: 25544
Epoch time: 15025
55523850 = yrday
fracday
Element set: 906
Inclination: 51
6446 deg
RA of node: 76
1891 deg
Eccentricity:
0005931
Arg of perigee: 303
0885 deg
Mean anomaly: 56
9698 deg
Mean motion: 15
53676155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 584
Checksum: 332
Coasting Arc #8 (Orbit 598)
---------------------------------------
Vector Time (GMT): 2015/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2803161
77 A = 6780319
76 meter
Y = -3705860
95 meter E =
0009922
Z = -4946268
13 I = 51
97517
XDOT = 4025
014599 Wp = 44
62137
YDOT = 6103
085533 meter/sec RA = 70
75712 deg
ZDOT = -2287
417192 TA = 203
08059
MA = 203
12519
Ha = 220
957 n
mi
Hp = 217
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9196724
97 X = 2868420
12
Y = -12158336
43 feet Y = -3674149
39 meter
Z = -16227913
82 Z = -4932492
46
XDOT = 13205
428474 XDOT = 3967
580622
YDOT = 20023
246500 feet/sec YDOT = 6147
774683 meter/sec
ZDOT = -7504
649580 ZDOT = -2268
004280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15290105
64 X = 4660424
20
Y = 741722
36 feet Y = 226076
97 meter
Z = -16168259
01 Z = -4928085
35
XDOT = -8890
125602 XDOT = -2709
710283
YDOT = 21168
161310 feet/sec YDOT = 6452
055567 meter/sec
ZDOT = -7422
703579 ZDOT = -2262
440051
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 15026
52004356
00016717 00000-0 10270-3 0 9073
2 25544 51
6454 71
3824 0005924 307
2463 52
8148 15
53693183 5992
Satellite: ISS
Catalog Number: 25544
Epoch time: 15026
52004356 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 71
3824 deg
Eccentricity:
0005924
Arg of perigee: 307
2463 deg
Mean anomaly: 52
8148 deg
Mean motion: 15
53693183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 599
Checksum: 309
Coasting Arc #9 (Orbit 614)
---------------------------------------
Vector Time (GMT): 2015/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3545134
89 A = 6778545
29 meter
Y = 2261902
90 meter E =
0003416
Z = 5317733
64 I = 51
95797
XDOT = -3520
263450 Wp = 328
75126
YDOT = -6789
501005 meter/sec RA = 65
78502 deg
ZDOT = 544
091068 TA = 116
09663
MA = 116
06147
Ha = 221
179 n
mi
Hp = 216
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11631019
97 X = -3595995
86
Y = 7420941
27 feet Y = 2221974
56 meter
Z = 17446632
67 Z = 5300388
66
XDOT = -11549
420769 XDOT = -3446
722988
YDOT = -22275
265764 feet/sec YDOT = -6828
455687 meter/sec
ZDOT = 1785
075684 ZDOT = 527
169149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12871524
97 X = -3923240
81
Y = -5222509
18 feet Y = -1591820
80 meter
Z = 17371966
76 Z = 5294975
47
XDOT = 10995
375919 XDOT = 3351
390580
YDOT = -21431
181761 feet/sec YDOT = -6532
224201 meter/sec
ZDOT = 1713
932384 ZDOT = 522
406591
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 15027
54914475
00016717 00000-0 10270-3 0 9089
2 25544 51
6449 66
2555 0005882 312
5508 47
5147 15
53747729 6157
Satellite: ISS
Catalog Number: 25544
Epoch time: 15027
54914475 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 66
2555 deg
Eccentricity:
0005882
Arg of perigee: 312
5508 deg
Mean anomaly: 47
5147 deg
Mean motion: 15
53747729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 615
Checksum: 330
Coasting Arc #10 (Orbit 629)
---------------------------------------
Vector Time (GMT): 2015/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4257499
60 A = 6778960
18 meter
Y = -768373
06 meter E =
0009916
Z = -5226971
52 I = 51
94684
XDOT = 2799
383216 Wp = 78
49516
YDOT = 7020
584684 meter/sec RA = 60
81015 deg
ZDOT = 1252
060697 TA = 203
46082
MA = 203
50609
Ha = 221
276 n
mi
Hp = 216
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13968174
54 X = 4291165
72
Y = -2520909
00 feet Y = -720574
68 meter
Z = -17148856
70 Z = -5206207
85
XDOT = 9184
328138 XDOT = 2714
587351
YDOT = 23033
414318 feet/sec YDOT = 7051
415083 meter/sec
ZDOT = 4107
810685 ZDOT = 1265
453486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10418020
09 X = 3175412
52
Y = 9796679
47 feet Y = 2986027
90 meter
Z = -17059838
71 Z = -5199838
84
XDOT = -12316
807594 XDOT = -3754
162955
YDOT = 20326
201996 feet/sec YDOT = 6195
426368 meter/sec
ZDOT = 4163
792980 ZDOT = 1269
124100
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 15028
51390642
00016717 00000-0 10270-3 0 9092
2 25544 51
6461 61
4488 0005958 316
3103 43
7574 15
53758320 6308
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
51390642 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 61
4488 deg
Eccentricity:
0005958
Arg of perigee: 316
3103 deg
Mean anomaly: 43
7574 deg
Mean motion: 15
53758320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 630
Checksum: 304
Coasting Arc #11 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2015/028/18:43:32
115
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -588736
75 A = 6782254
04 meter
Y = 5349449
89 meter E =
0005329
Z = 4122123
17 I = 51
95564
XDOT = -5596
421116 Wp = 77
11175
YDOT = -3575
183399 meter/sec RA = 59
45513 deg
ZDOT = 3837
357177 TA = 333
43289
MA = 333
46019
Ha = 220
375 n
mi
Hp = 216
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1931551
02 X = -668535
32
Y = 17550688
61 feet Y = 5342420
05 meter
Z = 13524026
16 Z = 4119069
45
XDOT = -18360
961668 XDOT = -5574
666887
YDOT = -11729
604328 feet/sec YDOT = -3637
644609 meter/sec
ZDOT = 12589
754519 ZDOT = 3810
223950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11638577
93 X = 3547438
55
Y = 13292181
64 feet Y = 4051456
96 meter
Z = 13509931
71 Z = 4117827
18
XDOT = -20109
874844 XDOT = -6129
489852
YDOT = 4919
434176 feet/sec YDOT = 1499
443537 meter/sec
ZDOT = 12474
304637 ZDOT = 3802
168053
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 15028
83547669
00016717 00000-0 10270-3 0 9102
2 25544 51
6448 59
8462 0006169 306
2191 53
8391 15
54087008 6359
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
83547669 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 59
8462 deg
Eccentricity:
0006169
Arg of perigee: 306
2191 deg
Mean anomaly: 53
8391 deg
Mean motion: 15
54087008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 325
Coasting Arc #12 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2015/029/18:43:32
115
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1762588
91 A = 6778849
72 meter
Y = -4252213
58 meter E =
0010475
Z = -4985228
80 I = 51
92834
XDOT = 5533
723951 Wp = 44
61643
YDOT = 4835
777828 meter/sec RA = 54
48320 deg
ZDOT = -2163
716464 TA = 204
33411
MA = 204
38361
Ha = 220
455 n
mi
Hp = 216
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5782772
03 X = 1834223
22
Y = -13950831
96 feet Y = -4232102
57 meter
Z = -16355737
54 Z = -4976492
67
XDOT = 18155
262306 XDOT = 5489
748256
YDOT = 15865
412820 feet/sec YDOT = 4897
413675 meter/sec
ZDOT = -7098
807295 ZDOT = -2136
941806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6608084
02 X = -2014144
01
Y = -13625268
31 feet Y = -4152981
78 meter
Z = -16317524
46 Z = -4973581
45
XDOT = 22934
377384 XDOT = 6990
398227
YDOT = -2739
789846 feet/sec YDOT = -835
087945 meter/sec
ZDOT = -6985
139500 ZDOT = -2129
070520
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 15029
80002588
00016717 00000-0 10270-3 0 9117
2 25544 51
6453 55
0380 0006169 311
0034 49
0585 15
54131472 6506
Satellite: ISS
Catalog Number: 25544
Epoch time: 15029
80002588 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 55
0380 deg
Eccentricity:
0006169
Arg of perigee: 311
0034 deg
Mean anomaly: 49
0585 deg
Mean motion: 15
54131472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 277
Coasting Arc #13 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2015/030/18:43:32
115
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2993210
73 A = 6777192
64 meter
Y = 2929429
77 meter E =
0004400
Z = 5329870
43 I = 51
90400
XDOT = -5126
984710 Wp = 331
06028
YDOT = -5695
689242 meter/sec RA = 49
50321 deg
ZDOT = 255
060575 TA = 116
53972
MA = 116
49460
Ha = 220
579 n
mi
Hp = 216
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9820245
16 X = -3051635
92
Y = 9610990
06 feet Y = 2895630
99 meter
Z = 17486451
54 Z = 5315188
37
XDOT = -16820
815978 XDOT = -5064
152096
YDOT = -18686
644494 feet/sec YDOT = -5752
671206 meter/sec
ZDOT = 836
812910 ZDOT = 230
307617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 915874
06 X = 279158
41
Y = 13790692
57 feet Y = 4203403
10 meter
Z = 17423039
50 Z = 5310542
44
XDOT = -24128
343294 XDOT = -7354
319036
YDOT = 693
630728 feet/sec YDOT = 211
418646 meter/sec
ZDOT = 731
970241 ZDOT = 223
104530
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
82885313
00016717 00000-0 10270-3 0 9127
2 25544 51
6451 49
9094 0006263 313
6373 46
4260 15
54187029 6664
Satellite: ISS
Catalog Number: 25544
Epoch time: 15030
82885313 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 49
9094 deg
Eccentricity:
0006263
Arg of perigee: 313
6373 deg
Mean anomaly: 46
4260 deg
Mean motion: 15
54187029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 305
Coasting Arc #14 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2015/031/18:43:32
115
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4168257
82 A = 6778132
48 meter
Y = -1540286
16 meter E =
0009067
Z = -5125467
47 I = 51
88640
XDOT = 4319
692457 Wp = 79
11629
YDOT = 6100
570670 meter/sec RA = 44
52011 deg
ZDOT = 1683
834202 TA = 207
07874
MA = 207
12606
Ha = 220
723 n
mi
Hp = 216
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13675386
54 X = 4210068
97
Y = -5053432
30 feet Y = -1493440
16 meter
Z = -16815838
15 Z = -5105117
75
XDOT = 14172
219346 XDOT = 4242
974121
YDOT = 20014
995638 feet/sec YDOT = 6148
447308 meter/sec
ZDOT = 5524
390428 ZDOT = 1704
631738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4812922
94 X = 1466978
91
Y = -13867985
74 feet Y = -4226962
05 meter
Z = -16728434
84 Z = -5098826
94
XDOT = 23432
150918 XDOT = 7142
119600
YDOT = 1379
046475 feet/sec YDOT = 420
333366 meter/sec
ZDOT = 5612
219185 ZDOT = 1710
604407
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
79335856
00016717 00000-0 10270-3 0 9137
2 25544 51
6456 45
1007 0006200 318
4454 41
6227 15
54191571 6819
Satellite: ISS
Catalog Number: 25544
Epoch time: 15031
79335856 = yrday
fracday
Element set: 913
Inclination: 51
6456 deg
RA of node: 45
1007 deg
Eccentricity:
0006200
Arg of perigee: 318
4454 deg
Mean anomaly: 41
6227 deg
Mean motion: 15
54191571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 681
Checksum: 290
Coasting Arc #15 (Orbit 696)
---------------------------------------
Vector Time (GMT): 2015/032/18:43:32
115
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5191440
45 A = 6781093
36 meter
Y = 151746
10 meter E =
0009615
Z = 4360100
92 I = 51
87307
XDOT = -3101
973145 Wp = 34
25970
YDOT = -6092
359140 meter/sec RA = 39
54123 deg
ZDOT = -3469
927031 TA = 90
91922
MA = 90
80904
Ha = 220
811 n
mi
Hp = 215
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17032284
93 X = -5213930
73
Y = 497854
65 feet Y = 93566
28 meter
Z = 14304793
03 Z = 4334827
85
XDOT = -10177
077249 XDOT = -3016
761184
YDOT = -19988
054922 feet/sec YDOT = -6126
570976 meter/sec
ZDOT = -11384
275037 ZDOT = -3484
788506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10219607
77 X = -3114936
45
Y = 13747371
12 feet Y = 4190198
72 meter
Z = 14196587
51 Z = 4327119
87
XDOT = -20947
500313 XDOT = -6384
798095
YDOT = -3712
216309 feet/sec YDOT = -1131
483531 meter/sec
ZDOT = -11446
693532 ZDOT = -3488
952188
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
82213896
00016717 00000-0 10270-3 0 9142
2 25544 51
6452 39
9716 0006188 322
6786 37
3936 15
54231033 6977
Satellite: ISS
Catalog Number: 25544
Epoch time: 15032
82213896 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 39
9716 deg
Eccentricity:
0006188
Arg of perigee: 322
6786 deg
Mean anomaly: 37
3936 deg
Mean motion: 15
54231033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 697
Checksum: 323
Coasting Arc #16 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2015/033/18:43:32
115
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5914403
30 A = 6784829
80 meter
Y = 1085383
70 meter E =
0006391
Z = -3135776
56 I = 51
86181
XDOT = 1535
538593 Wp = 7
62737
YDOT = 5711
881644 meter/sec RA = 34
56972 deg
ZDOT = 4880
546459 TA = 316
36527
MA = 316
41580
Ha = 220
913 n
mi
Hp = 215
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19404210
29 X = 5917058
77
Y = 3560970
15 feet Y = 1151537
21 meter
Z = -10287980
85 Z = -3107039
81
XDOT = 5037
856275 XDOT = 1447
845577
YDOT = 18739
769174 feet/sec YDOT = 5728
562791 meter/sec
ZDOT = 16012
291532 ZDOT = 4887
792544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14632406
36 X = 4459957
46
Y = -13326963
25 feet Y = -4062058
40 meter
Z = -10165194
05 Z = -3098351
15
XDOT = 16926
292622 XDOT = 5159
133991
YDOT = 6366
583403 feet/sec YDOT = 1940
534621 meter/sec
ZDOT = 16042
186230 ZDOT = 4889
658363
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
78659711
00016717 00000-0 10270-3 0 9159
2 25544 51
6459 35
1622 0006187 325
9640 34
1115 15
54274243 7124
Satellite: ISS
Catalog Number: 25544
Epoch time: 15033
78659711 = yrday
fracday
Element set: 915
Inclination: 51
6459 deg
RA of node: 35
1622 deg
Eccentricity:
0006187
Arg of perigee: 325
9640 deg
Mean anomaly: 34
1115 deg
Mean motion: 15
54274243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 297
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