[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 25th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10 7639 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
062/01:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 214
4
064/09:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 214
6
065/04:03:17
853 -2
4 3
4 3
4
N/A -2
1 -0
4 220
6
000/00:10:35
706 1
0 0
0 216
5
067/19:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
7
Coasting Arc #1 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2016/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2874508
45 A = 6785325
71 meter
Y = 5425713
71 meter E =
0014994
Z = 2868562
16 I = 51
28154
XDOT = -3578
481052 Wp = 110
53403
YDOT = 4562
053504 meter/sec RA = 264
08098 deg
ZDOT = -5026
760028 TA = 36
61240
MA = 36
51002
Ha = 221
311 n
mi
Hp = 213
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9430802
01 X = 2799689
14
Y = 17800898
00 feet Y = 5457440
42 meter
Z = 9411293
17 Z = 2882343
09
XDOT = -11740
423400 XDOT = -3604
811694
YDOT = 14967
367139 feet/sec YDOT = 4521
888645 meter/sec
ZDOT = -16491
994842 ZDOT = -5044
207661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 253413
83 X = 77240
53
Y = 20115612
66 feet Y = 6131238
74 meter
Z = 9470076
25 Z = 2886479
24
XDOT = -15699
146421 XDOT = -4785
099829
YDOT = 8022
751316 feet/sec YDOT = 2445
334601 meter/sec
ZDOT = -16568
420802 ZDOT = -5050
054661
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 16055
53805988
00016717 00000-0 10270-3 0 9000
2 25544 51
6400 264
7880 0003356 164
5960 195
5295 15
54289957 27304
Satellite: ISS
Catalog Number: 25544
Epoch time: 16055
53805988 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 264
7880 deg
Eccentricity:
0003356
Arg of perigee: 164
5960 deg
Mean anomaly: 195
5295 deg
Mean motion: 15
54289957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 338
Coasting Arc #2 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2016/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2251845
98 A = 6788230
36 meter
Y = -6273922
52 meter E =
0007047
Z = -1276102
22 I = 51
29442
XDOT = 4219
158626 Wp = 59
34204
YDOT = -2689
646643 meter/sec RA = 259
08004 deg
ZDOT = 5805
836576 TA = 286
71567
MA = 286
79300
Ha = 221
362 n
mi
Hp = 214
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7387946
11 X = -2175323
39
Y = -20583735
31 feet Y = -6298676
47 meter
Z = -4186687
07 Z = -1286854
24
XDOT = 13842
383943 XDOT = 4220
719482
YDOT = -8824
300011 feet/sec YDOT = -2642
455679 meter/sec
ZDOT = 19048
020262 ZDOT = 5826
336067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2427723
74 X = 739970
19
Y = -21725442
30 feet Y = -6621914
81 meter
Z = -4232206
26 Z = -1289976
47
XDOT = 14616
309101 XDOT = 4455
051014
YDOT = -2077
333442 feet/sec YDOT = -633
171233 meter/sec
ZDOT = 19137
342195 ZDOT = 5833
061901
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 16056
50251098
00016717 00000-0 10270-3 0 9016
2 25544 51
6392 259
9784 0003500 170
1793 189
9429 15
54261730 27452
Satellite: ISS
Catalog Number: 25544
Epoch time: 16056
50251098 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 259
9784 deg
Eccentricity:
0003500
Arg of perigee: 170
1793 deg
Mean anomaly: 189
9429 deg
Mean motion: 15
54261730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 322
Coasting Arc #3 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2016/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1469335
02 A = 6788802
77 meter
Y = 6601711
37 meter E =
0014046
Z = -495877
26 I = 51
30346
XDOT = -4787
295422 Wp = 146
21643
YDOT = 624
729683 meter/sec RA = 254
08520 deg
ZDOT = -5961
045856 TA = 39
15958
MA = 39
05802
Ha = 221
279 n
mi
Hp = 214
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4820652
97 X = 1397812
58
Y = 21659158
03 feet Y = 6617742
48 meter
Z = -1626893
90 Z = -488914
28
XDOT = -15706
349811 XDOT = -4764
969618
YDOT = 2049
638067 feet/sec YDOT = 571
318993 meter/sec
ZDOT = -19557
237062 ZDOT = -5984
246944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4800678
96 X = -1463246
95
Y = 21665756
07 feet Y = 6603722
45 meter
Z = -1597842
64 Z = -487022
44
XDOT = -13400
618306 XDOT = -4084
508460
YDOT = -4396
162998 feet/sec YDOT = -1339
950482 meter/sec
ZDOT = -19657
912889 ZDOT = -5991
731849
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 16057
53125014
00016717 00000-0 10270-3 0 9029
2 25544 51
6393 254
8483 0003421 171
9326 188
1882 15
54275479 27613
Satellite: ISS
Catalog Number: 25544
Epoch time: 16057
53125014 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 254
8483 deg
Eccentricity:
0003421
Arg of perigee: 171
9326 deg
Mean anomaly: 188
1882 deg
Mean motion: 15
54275479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 316
Coasting Arc #4 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2016/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -575426
89 A = 6786822
03 meter
Y = -6396967
10 meter E =
0013382
Z = 2179433
02 I = 51
30539
XDOT = 5208
845693 Wp = 85
92358
YDOT = 1398
336020 meter/sec RA = 249
08847 deg
ZDOT = 5451
521602 TA = 298
38847
MA = 298
52331
Ha = 221
221 n
mi
Hp = 214
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1887883
49 X = -514438
31
Y = -20987424
86 feet Y = -6403060
62 meter
Z = 7150370
79 Z = 2176786
71
XDOT = 17089
388758 XDOT = 5166
341093
YDOT = 4587
716602 feet/sec YDOT = 1456
347830 meter/sec
ZDOT = 17885
569559 ZDOT = 5476
721242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6798048
53 X = 2072045
19
Y = -19949211
95 feet Y = -6080519
80 meter
Z = 7139985
12 Z = 2176267
46
XDOT = 12169
388302 XDOT = 3709
229554
YDOT = 10620
355229 feet/sec YDOT = 3237
084274 meter/sec
ZDOT = 17994
567908 ZDOT = 5484
744298
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 16058
55998160
00016717 00000-0 10270-3 0 9033
2 25544 51
6379 249
7182 0003607 176
5612 183
5567 15
54301321 27773
Satellite: ISS
Catalog Number: 25544
Epoch time: 16058
55998160 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 249
7182 deg
Eccentricity:
0003607
Arg of perigee: 176
5612 deg
Mean anomaly: 183
5567 deg
Mean motion: 15
54301321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 330
Coasting Arc #5 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2016/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -492969
18 A = 6783123
55 meter
Y = 5691830
90 meter E =
0006154
Z = -3659138
34 I = 51
30528
XDOT = -5430
086598 Wp = 114
62915
YDOT = -3246
211081 meter/sec RA = 244
08466 deg
ZDOT = -4326
228492 TA = 109
08239
MA = 109
01573
Ha = 221
132 n
mi
Hp = 214
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1617352
94 X = -538805
60
Y = 18673985
90 feet Y = 5686061
48 meter
Z = -12005047
05 Z = -3661645
05
XDOT = -17815
244744 XDOT = -5372
368269
YDOT = -10650
298823 feet/sec YDOT = -3306
611703 meter/sec
ZDOT = -14193
663030 ZDOT = -4352
465742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8741729
43 X = -2664479
13
Y = 16572015
62 feet Y = 5051150
36 meter
Z = -12016871
46 Z = -3662742
42
XDOT = -10916
237067 XDOT = -3327
269058
YDOT = -16112
996989 feet/sec YDOT = -4911
241482 meter/sec
ZDOT = -14306
855868 ZDOT = -4360
729668
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 16059
52441290
00016717 00000-0 10270-3 0 9049
2 25544 51
6378 244
9090 0003485 178
0794 182
0373 15
54306150 27920
Satellite: ISS
Catalog Number: 25544
Epoch time: 16059
52441290 = yrday
fracday
Element set: 904
Inclination: 51
6378 deg
RA of node: 244
9090 deg
Eccentricity:
0003485
Arg of perigee: 178
0794 deg
Mean anomaly: 182
0373 deg
Mean motion: 15
54306150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 313
Coasting Arc #6 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2016/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1637547
16 A = 6779409
24 meter
Y = -4596597
74 meter E =
0009769
Z = 4703663
52 I = 51
30800
XDOT = 5385
599714 Wp = 136
21148
YDOT = 4727
278437 meter/sec RA = 239
07040 deg
ZDOT = 2734
370475 TA = 286
55718
MA = 286
66446
Ha = 221
026 n
mi
Hp = 214
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5372530
04 X = 1665977
51
Y = -15080701
23 feet Y = -4578126
13 meter
Z = 15431966
93 Z = 4711687
81
XDOT = 17669
290401 XDOT = 5319
055534
YDOT = 15509
443691 feet/sec YDOT = 4787
132010 meter/sec
ZDOT = 8971
031743 ZDOT = 2760
370074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10561296
69 X = 3219083
23
Y = -11985491
44 feet Y = -3653177
79 meter
Z = 15467522
08 Z = 4714500
73
XDOT = 9604
095599 XDOT = 2927
328339
YDOT = 20228
323233 feet/sec YDOT = 6165
592922 meter/sec
ZDOT = 9082
958696 ZDOT = 2768
485810
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 16060
55313114
00016717 00000-0 10270-3 0 9058
2 25544 51
6382 239
7788 0003463 183
6261 176
4867 15
54295607 28085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16060
55313114 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 239
7788 deg
Eccentricity:
0003463
Arg of perigee: 183
6261 deg
Mean anomaly: 176
4867 deg
Mean motion: 15
54295607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2808
Checksum: 327
Coasting Arc #7 (Orbit 2822)
---------------------------------------
Vector Time (GMT): 2016/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2859846
65 A = 6777031
22 meter
Y = 3214182
45 meter E =
0014384
Z = -5248398
61 I = 51
31749
XDOT = -4982
788556 Wp = 97
95735
YDOT = -5758
543125 meter/sec RA = 234
04868 deg
ZDOT = -815
362632 TA = 164
22644
MA = 164
18159
Ha = 221
041 n
mi
Hp = 214
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9382698
99 X = -2870081
60
Y = 10545218
01 feet Y = 3182144
01 meter
Z = -17219155
55 Z = -5262316
10
XDOT = -16347
731484 XDOT = -4914
064116
YDOT = -18892
858022 feet/sec YDOT = -5813
879792 meter/sec
ZDOT = -2675
074252 ZDOT = -839
400127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12448769
91 X = -3794385
07
Y = 6493434
41 feet Y = 1979198
81 meter
Z = -17280029
46 Z = -5266952
98
XDOT = -7950
044376 XDOT = -2423
173526
YDOT = -22601
134987 feet/sec YDOT = -6888
825944 meter/sec
ZDOT = -2778
338495 ZDOT = -846
837573
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 16061
51754711
00016717 00000-0 10270-3 0 9068
2 25544 51
6381 234
9699 0003577 182
5729 177
5406 15
54321635 28234
Satellite: ISS
Catalog Number: 25544
Epoch time: 16061
51754711 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 234
9699 deg
Eccentricity:
0003577
Arg of perigee: 182
5729 deg
Mean anomaly: 177
5406 deg
Mean motion: 15
54321635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2823
Checksum: 326
Coasting Arc #8 (Orbit 2831)
---------------------------------------
Vector Time (GMT): 2016/062/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 890989
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2050741
15 A = 6777667
12 meter
Y = -3966197
82 meter E =
0007135
Z = 5097397
63 I = 51
33018
XDOT = 5618
307205 Wp = 149
42850
YDOT = 4970
585633 meter/sec RA = 231
32898 deg
ZDOT = 1600
193973 TA = 285
03396
MA = 285
11291
Ha = 220
839 n
mi
Hp = 214
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6728153
38 X = 2070178
97
Y = -13012460
04 feet Y = -3943155
93 meter
Z = 16723745
52 Z = 5107407
11
XDOT = 18432
766420 XDOT = 5554
534328
YDOT = 16307
695647 feet/sec YDOT = 5033
056844 meter/sec
ZDOT = 5249
980225 ZDOT = 1627
330742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7585720
72 X = -2312127
67
Y = 12472913
27 feet Y = 3801743
96 meter
Z = 16767799
62 Z = 5110825
33
XDOT = -16202
906077 XDOT = -4938
645772
YDOT = -17099
929439 feet/sec YDOT = -5212
058493 meter/sec
ZDOT = 5366
821739 ZDOT = 1635
807266
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 16062
09619336
00016717 00000-0 10270-3 0 9076
2 25544 51
6382 232
0879 0003271 188
2145 171
8954 15
54324594 28322
Satellite: ISS
Catalog Number: 25544
Epoch time: 16062
09619336 = yrday
fracday
Element set: 907
Inclination: 51
6382 deg
RA of node: 232
0879 deg
Eccentricity:
0003271
Arg of perigee: 188
2145 deg
Mean anomaly: 171
8954 deg
Mean motion: 15
54324594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2832
Checksum: 322
Coasting Arc #9 (Orbit 2846)
---------------------------------------
Vector Time (GMT): 2016/063/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 890989
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3376214
58 A = 6776835
67 meter
Y = 2588038
19 meter E =
0014679
Z = -5287786
21 I = 51
34851
XDOT = -5044
387479 Wp = 105
93606
YDOT = -5748
045406 meter/sec RA = 226
30603 deg
ZDOT = 404
486061 TA = 167
95941
MA = 167
92428
Ha = 220
815 n
mi
Hp = 214
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11076819
50 X = -3379218
21
Y = 8490938
95 feet Y = 2550265
88 meter
Z = -17348379
95 Z = -5304194
36
XDOT = -16549
827688 XDOT = -4981
701302
YDOT = -18858
416686 feet/sec YDOT = -5804
104562 meter/sec
ZDOT = 1327
054007 ZDOT = 380
134675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11442777
11 X = 3487758
46
Y = -7833664
99 feet Y = -2387701
09 meter
Z = -17419954
26 Z = -5309602
06
XDOT = 14855
718017 XDOT = 4528
022852
YDOT = 18959
832697 feet/sec YDOT = 5778
957006 meter/sec
ZDOT = 1222
399323 ZDOT = 372
587314
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 16063
06059879
00016717 00000-0 10270-3 0 9085
2 25544 51
6385 227
2786 0003267 191
4934 168
6145 15
54323845 28475
Satellite: ISS
Catalog Number: 25544
Epoch time: 16063
06059879 = yrday
fracday
Element set: 908
Inclination: 51
6385 deg
RA of node: 227
2786 deg
Eccentricity:
0003267
Arg of perigee: 191
4934 deg
Mean anomaly: 168
6145 deg
Mean motion: 15
54323845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2847
Checksum: 344
Coasting Arc #10 (Orbit 2862)
---------------------------------------
Vector Time (GMT): 2016/064/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 890989
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4573808
72 A = 6778508
49 meter
Y = -1154855
11 meter E =
0004884
Z = 4863673
04 I = 51
37785
XDOT = 4050
279977 Wp = 84
75704
YDOT = 6070
969853 meter/sec RA = 221
28662 deg
ZDOT = -2364
880959 TA = 28
49493
MA = 28
46824
Ha = 220
528 n
mi
Hp = 214
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15005934
13 X = 4562757
34
Y = -3788894
70 feet Y = -1103769
13 meter
Z = 15956932
54 Z = 4885864
42
XDOT = 13288
320135 XDOT = 3993
579289
YDOT = 19917
880096 feet/sec YDOT = 6115
945546 meter/sec
ZDOT = -7758
795796 ZDOT = -2345
344185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15046785
34 X = -4586260
17
Y = 3168814
73 feet Y = 965854
73 meter
Z = 16053359
23 Z = 4893063
89
XDOT = -12272
995529 XDOT = -3740
809037
YDOT = -19353
739839 feet/sec YDOT = -5899
019903 meter/sec
ZDOT = -7675
053328 ZDOT = -2339
356255
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 16064
08928881
00016717 00000-0 10270-3 0 9097
2 25544 51
6391 222
1491 0003160 196
8714 163
2335 15
54351671 28634
Satellite: ISS
Catalog Number: 25544
Epoch time: 16064
08928881 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 222
1491 deg
Eccentricity:
0003160
Arg of perigee: 196
8714 deg
Mean anomaly: 163
2335 deg
Mean motion: 15
54351671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2863
Checksum: 315
Coasting Arc #11 (Orbit 2867)
---------------------------------------
Vector Time (GMT): 2016/064/09:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 890989
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1062532
55 A = 6781237
12 meter
Y = 5226163
57 meter E =
0006370
Z = -4193739
96 I = 51
39403
XDOT = -6534
334587 Wp = 93
53156
YDOT = -1608
894526 meter/sec RA = 219
61395 deg
ZDOT = -3665
734245 TA = 138
74818
MA = 138
70003
Ha = 220
614 n
mi
Hp = 214
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3485999
18 X = 1024384
42
Y = 17146205
92 feet Y = 5237831
86 meter
Z = -13758989
38 Z = -4188671
61
XDOT = -21438
105601 XDOT = -6498
051574
YDOT = -5278
525347 feet/sec YDOT = -1681
763230 meter/sec
ZDOT = -12026
687157 ZDOT = -3697
387703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12783094
95 X = -3896287
34
Y = 11971559
58 feet Y = 3648931
36 meter
Z = -13737852
86 Z = -4187297
55
XDOT = -5729
842592 XDOT = -1746
456022
YDOT = -20056
967171 feet/sec YDOT = -6113
363594 meter/sec
ZDOT = -12163
706878 ZDOT = -3707
497856
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 16064
41075163
00016717 00000-0 10270-3 0 9102
2 25544 51
6381 220
5449 0003171 199
0015 161
1020 15
54355801 28681
Satellite: ISS
Catalog Number: 25544
Epoch time: 16064
41075163 = yrday
fracday
Element set: 910
Inclination: 51
6381 deg
RA of node: 220
5449 deg
Eccentricity:
0003171
Arg of perigee: 199
0015 deg
Mean anomaly: 161
1020 deg
Mean motion: 15
54355801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2868
Checksum: 277
Coasting Arc #12 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2016/065/04:08:35
706
Vector Time (MET): N/A
Weight (LBS) : 890633
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5266454
52 A = 6782712
71 meter
Y = 407779
80 meter E =
0006544
Z = -4261669
48 I = 51
41595
XDOT = -3344
028478 Wp = 140
45822
YDOT = -5898
532265 meter/sec RA = 215
63987 deg
ZDOT = 3566
135631 TA = 166
09788
MA = 166
07986
Ha = 220
615 n
mi
Hp = 216
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17278394
11 X = -5249921
98
Y = 1337860
22 feet Y = 348978
86 meter
Z = -13981855
24 Z = -4287212
07
XDOT = -10971
222040 XDOT = -3295
143570
YDOT = -19352
139977 feet/sec YDOT = -5935
653756 meter/sec
ZDOT = 11699
920048 ZDOT = 3550
010707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11290080
22 X = 3441216
45
Y = -13028995
37 feet Y = -3971237
79 meter
Z = -14092707
94 Z = -4295457
38
XDOT = 20507
060887 XDOT = 6250
552158
YDOT = 5182
829627 feet/sec YDOT = 1579
726470 meter/sec
ZDOT = 11630
926320 ZDOT = 3545
106342
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 16065
18226397
00016717 00000-0 10270-3 0 9115
2 25544 51
6413 216
6987 0004243 240
3697 119
7033 15
53718119 28808
Satellite: ISS
Catalog Number: 25544
Epoch time: 16065
18226397 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 216
6987 deg
Eccentricity:
0004243
Arg of perigee: 240
3697 deg
Mean anomaly: 119
7033 deg
Mean motion: 15
53718119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 317
Coasting Arc #13 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2016/066/04:08:35
706
Vector Time (MET): N/A
Weight (LBS) : 890633
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5977054
23 A = 6786280
49 meter
Y = 633666
33 meter E =
0009395
Z = 3139548
49 I = 51
45412
XDOT = 1946
511627 Wp = 107
83542
YDOT = 5628
667477 meter/sec RA = 210
64478 deg
ZDOT = -4832
699397 TA = 35
86774
MA = 35
80469
Ha = 220
418 n
mi
Hp = 216
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19609757
96 X = 5954273
88
Y = 2078957
78 feet Y = 700378
68 meter
Z = 10300355
95 Z = 3168527
61
XDOT = 6386
193002 XDOT = 1906
900560
YDOT = 18466
756815 feet/sec YDOT = 5650
212671 meter/sec
ZDOT = -15855
312981 ZDOT = -4823
340706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15153322
77 X = -4618732
78
Y = 12515515
27 feet Y = 3814729
05 meter
Z = 10425962
41 Z = 3177833
34
XDOT = -16823
904422 XDOT = -5127
926068
YDOT = -7170
073671 feet/sec YDOT = -2185
438455 meter/sec
ZDOT = -15815
609311 ZDOT = -4820
597718
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 16066
21137203
00016717 00000-0 10270-3 0 9128
2 25544 51
6412 211
5727 0004313 243
7288 116
3421 15
53704619 28965
Satellite: ISS
Catalog Number: 25544
Epoch time: 16066
21137203 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 211
5727 deg
Eccentricity:
0004313
Arg of perigee: 243
7288 deg
Mean anomaly: 116
3421 deg
Mean motion: 15
53704619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 287
Coasting Arc #14 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2016/067/04:08:35
706
Vector Time (MET): N/A
Weight (LBS) : 890633
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6378575
69 A = 6789076
42 meter
Y = -1520519
19 meter E =
0004287
Z = -1748724
73 I = 51
49338
XDOT = -322
578915 Wp = 7
44534
YDOT = -5154
551402 meter/sec RA = 205
65803 deg
ZDOT = 5664
239475 TA = 333
32924
MA = 333
35129
Ha = 220
295 n
mi
Hp = 216
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20927085
59 X = -6352604
40
Y = -4988580
03 feet Y = -1591703
67 meter
Z = -5737285
85 Z = -1779646
42
XDOT = -1058
329775 XDOT = -292
429411
YDOT = -16911
257879 feet/sec YDOT = -5157
989402 meter/sec
ZDOT = 18583
462843 ZDOT = 5662
746374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17975063
57 X = 5478799
38
Y = -11754635
29 feet Y = -3582812
84 meter
Z = -5871194
92 Z = -1789540
21
XDOT = 12240
871403 XDOT = 3731
017604
YDOT = 9448
554130 feet/sec YDOT = 2879
919299 meter/sec
ZDOT = 18577
794231 ZDOT = 5662
511682
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 16067
17615119
00016717 00000-0 10270-3 0 9132
2 25544 51
6427 206
7653 0004354 249
4130 110
6556 15
53747510 29110
Satellite: ISS
Catalog Number: 25544
Epoch time: 16067
17615119 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 206
7653 deg
Eccentricity:
0004354
Arg of perigee: 249
4130 deg
Mean anomaly: 110
6556 deg
Mean motion: 15
53747510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 296
Coasting Arc #15 (Orbit 2921)
---------------------------------------
Vector Time (GMT): 2016/067/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 890633
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6240432
78 A = 6790437
28 meter
Y = -2663047
54 meter E =
0008565
Z = 99069
50 I = 51
51568
XDOT = 1956
851177 Wp = 35
17435
YDOT = -4352
968887 meter/sec RA = 202
44482 deg
ZDOT = 6000
502639 TA = 325
89436
MA = 325
94936
Ha = 220
321 n
mi
Hp = 216
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20473860
84 X = -6210671
35
Y = -8737032
61 feet Y = -2732665
79 meter
Z = 325031
17 Z = 68828
22
XDOT = 6420
115409 XDOT = 1976
234356
YDOT = -14281
393987 feet/sec YDOT = -4330
976864 meter/sec
ZDOT = 19686
688449 ZDOT = 6010
056053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5009612
32 X = -1526929
83
Y = 21690698
84 feet Y = 6611325
01 meter
Z = 194242
35 Z = 59205
07
XDOT = -13580
513345 XDOT = -4139
340468
YDOT = -3325
574521 feet/sec YDOT = -1013
635114 meter/sec
ZDOT = 19728
815345 ZDOT = 6013
342917
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 16067
88365127
00016717 00000-0 10270-3 0 9142
2 25544 51
6418 203
2397 0004178 250
1695 109
9007 15
53746994 29225
Satellite: ISS
Catalog Number: 25544
Epoch time: 16067
88365127 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 203
2397 deg
Eccentricity:
0004178
Arg of perigee: 250
1695 deg
Mean anomaly: 109
9007 deg
Mean motion: 15
53746994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2922
Checksum: 331
Coasting Arc #16 (Orbit 2936)
---------------------------------------
Vector Time (GMT): 2016/068/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 890633
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5742176
19 A = 6789334
32 meter
Y = 3201993
23 meter E =
0007518
Z = -1675256
97 I = 51
54043
XDOT = -3662
785919 Wp = 174
23295
YDOT = 3592
221068 meter/sec RA = 197
46849 deg
ZDOT = -5698
279237 TA = 24
14774
MA = 24
11252
Ha = 220
328 n
mi
Hp = 216
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18839160
72 X = 5714081
50
Y = 10505227
13 feet Y = 3266048
71 meter
Z = -5496249
89 Z = -1647432
04
XDOT = -12017
014170 XDOT = -3675
003397
YDOT = 11785
502190 feet/sec YDOT = 3551
192163 meter/sec
ZDOT = -18695
141854 ZDOT = -5716
102116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6678499
56 X = 2035606
67
Y = -20542119
04 feet Y = -6261237
88 meter
Z = -5376013
89 Z = -1638609
03
XDOT = 12353
982657 XDOT = 3765
493914
YDOT = 8921
087913 feet/sec YDOT = 2719
147596 meter/sec
ZDOT = -18773
029939 ZDOT = -5722
019525
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 16068
84842032
00016717 00000-0 10270-3 0 9155
2 25544 51
6405 198
4335 0004206 252
5368 107
5325 15
53734852 29376
Satellite: ISS
Catalog Number: 25544
Epoch time: 16068
84842032 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 198
4335 deg
Eccentricity:
0004206
Arg of perigee: 252
5368 deg
Mean anomaly: 107
5325 deg
Mean motion: 15
53734852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2937
Checksum: 315
Coasting Arc #17 (Orbit 2952)
---------------------------------------
Vector Time (GMT): 2016/069/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 890633
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4859519
93 A = 6786410
58 meter
Y = -3585930
39 meter E =
0008825
Z = 3087197
25 I = 51
56185
XDOT = 5193
194680 Wp = 86
92270
YDOT = -2821
419888 meter/sec RA = 192
48864 deg
ZDOT = 4885
715491 TA = 308
60486
MA = 308
68386
Ha = 220
141 n
mi
Hp = 216
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15943306
86 X = -4834056
14
Y = -11764863
49 feet Y = -3640129
89 meter
Z = 10128599
91 Z = 3063653
58
XDOT = 17038
040288 XDOT = 5200
626045
YDOT = -9256
626930 feet/sec YDOT = -2763
303786 meter/sec
ZDOT = 16029
250300 ZDOT = 4910
961001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8155052
95 X = -2485660
14
Y = 18114750
97 feet Y = 5521376
10 meter
Z = 10026988
15 Z = 3056225
99
XDOT = -11271
962671 XDOT = -3435
694222
YDOT = -14029
297539 feet/sec YDOT = -4276
129890 meter/sec
ZDOT = 16139
232160 ZDOT = 4919
237962
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 16069
87749731
00016717 00000-0 10270-3 0 9162
2 25544 51
6406 193
3065 0004258 259
0482 101
0192 15
53771263 29533
Satellite: ISS
Catalog Number: 25544
Epoch time: 16069
87749731 = yrday
fracday
Element set: 916
Inclination: 51
6406 deg
RA of node: 193
3065 deg
Eccentricity:
0004258
Arg of perigee: 259
0482 deg
Mean anomaly: 101
0192 deg
Mean motion: 15
53771263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2953
Checksum: 319
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