[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 29th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 ET - UTC (sec) : 68 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
124/02:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 213
6
132/13:26:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
5
135/07:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 213
2
Coasting Arc #1 (Orbit 3739)
---------------------------------------
Vector Time (GMT): 2016/120/11:18:49
007
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 469015
10 A = 6784183
68 meter
Y = -5942563
91 meter E =
0006240
Z = -3242781
01 I = 51
32926
XDOT = 5636
199934 Wp = 77
56290
YDOT = -2133
220316 meter/sec RA = 300
32133 deg
ZDOT = 4733
469161 TA = 244
69864
MA = 244
76330
Ha = 221
198 n
mi
Hp = 213
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1538763
44 X = 551183
63
Y = -19496600
75 feet Y = -5936859
67 meter
Z = -10639045
31 Z = -3240303
00
XDOT = 18491
469599 XDOT = 5636
641903
YDOT = -6998
754319 feet/sec YDOT = -2070
190065 meter/sec
ZDOT = 15529
754464 ZDOT = 4760
849720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7325443
05 X = -2232795
04
Y = -18140461
19 feet Y = -5529212
57 meter
Z = -10627138
41 Z = -3239151
79
XDOT = 11962
775047 XDOT = 3646
253834
YDOT = -13980
985634 feet/sec YDOT = -4261
404421 meter/sec
ZDOT = 15649
061757 ZDOT = 4769
834023
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 16120
47810519
00016717 00000-0 10270-3 0 9002
2 25544 51
6400 301
0109 0001680 67
2165 292
9165 15
54367588 37404
Satellite: ISS
Catalog Number: 25544
Epoch time: 16120
47810519 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 301
0109 deg
Eccentricity:
0001680
Arg of perigee: 67
2165 deg
Mean anomaly: 292
9165 deg
Mean motion: 15
54367588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3740
Checksum: 290
Coasting Arc #2 (Orbit 3755)
---------------------------------------
Vector Time (GMT): 2016/121/11:18:49
007
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1571348
66 A = 6787342
80 meter
Y = 6389335
76 meter E =
0014882
Z = 1639609
02 I = 51
32497
XDOT = -5137
916919 Wp = 111
27469
YDOT = 206
405434 meter/sec RA = 295
32220 deg
ZDOT = -5691
859800 TA = 50
68313
MA = 50
55129
Ha = 221
053 n
mi
Hp = 213
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5155343
36 X = -1650643
59
Y = 20962387
65 feet Y = 6371320
56 meter
Z = 5379294
69 Z = 1631783
03
XDOT = -16856
682805 XDOT = -5112
194332
YDOT = 677
183183 feet/sec YDOT = 149
093543 meter/sec
ZDOT = -18674
080709 ZDOT = -5716
756220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5144827
44 X = 1568143
40
Y = 20973972
38 feet Y = 6392866
78 meter
Z = 5344090
73 Z = 1628878
86
XDOT = -12976
475583 XDOT = -3955
229758
YDOT = 7999
421457 feet/sec YDOT = 2438
223660 meter/sec
ZDOT = -18782
229043 ZDOT = -5724
823412
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 16121
50677514
00016717 00000-0 10270-3 0 9014
2 25544 51
6399 295
8814 0001595 60
7774 299
3538 15
54425857 37569
Satellite: ISS
Catalog Number: 25544
Epoch time: 16121
50677514 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 295
8814 deg
Eccentricity:
0001595
Arg of perigee: 60
7774 deg
Mean anomaly: 299
3538 deg
Mean motion: 15
54425857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3756
Checksum: 347
Coasting Arc #3 (Orbit 3771)
---------------------------------------
Vector Time (GMT): 2016/122/11:18:49
007
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2442025
73 A = 6788574
53 meter
Y = -6326441
63 meter E =
0013810
Z = 115166
96 I = 51
31526
XDOT = 4433
371861 Wp = 49
91274
YDOT = 1828
771612 meter/sec RA = 290
32759 deg
ZDOT = 5985
360405 TA = 311
33371
MA = 311
45246
Ha = 221
172 n
mi
Hp = 213
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8011895
43 X = 2512028
64
Y = -20756042
08 feet Y = -6298741
86 meter
Z = 377844
36 Z = 127200
03
XDOT = 14545
183270 XDOT = 4383
518048
YDOT = 5999
906865 feet/sec YDOT = 1878
069963 meter/sec
ZDOT = 19637
009204 ZDOT = 6006
775640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2931887
17 X = -893639
21
Y = -22053674
12 feet Y = -6721959
87 meter
Z = 431292
16 Z = 131457
85
XDOT = 13921
900948 XDOT = 4243
395409
YDOT = -1438
676289 feet/sec YDOT = -438
508533 meter/sec
ZDOT = 19729
655591 ZDOT = 6013
599024
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 16122
53544190
00016717 00000-0 10270-3 0 9022
2 25544 51
6393 290
7510 0001636 76
1971 283
9364 15
54386374 37720
Satellite: ISS
Catalog Number: 25544
Epoch time: 16122
53544190 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 290
7510 deg
Eccentricity:
0001636
Arg of perigee: 76
1971 deg
Mean anomaly: 283
9364 deg
Mean motion: 15
54386374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3772
Checksum: 316
Coasting Arc #4 (Orbit 3786)
---------------------------------------
Vector Time (GMT): 2016/123/11:18:49
007
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3143299
46 A = 6786890
42 meter
Y = 5704947
98 meter E =
0007916
Z = -1900976
73 I = 51
30010
XDOT = -3589
145674 Wp = 128
06674
YDOT = -3831
710699 meter/sec RA = 285
33209 deg
ZDOT = -5585
185512 TA = 72
97092
MA = 72
88420
Ha = 221
168 n
mi
Hp = 213
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10312662
25 X = -3197625
77
Y = 18717020
92 feet Y = 5669493
68 meter
Z = -6236800
30 Z = -1916378
44
XDOT = -11775
412316 XDOT = -3518
901072
YDOT = -12571
229329 feet/sec YDOT = -3871
454385 meter/sec
ZDOT = -18324
099448 ZDOT = -5602
450084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 335031
69 X = 102117
66
Y = 21347446
57 feet Y = 6506701
72 meter
Z = -6304746
75 Z = -1921686
81
XDOT = -14794
826901 XDOT = -4509
463239
YDOT = -5181
723633 feet/sec YDOT = -1579
389363 meter/sec
ZDOT = -18398
350571 ZDOT = -5607
817254
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 16123
49980749
00016717 00000-0 10270-3 0 9033
2 25544 51
6396 285
9415 0001861 74
3744 285
7614 15
54427235 37877
Satellite: ISS
Catalog Number: 25544
Epoch time: 16123
49980749 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 285
9415 deg
Eccentricity:
0001861
Arg of perigee: 74
3744 deg
Mean anomaly: 285
7614 deg
Mean motion: 15
54427235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3787
Checksum: 344
Coasting Arc #5 (Orbit 3796)
---------------------------------------
Vector Time (GMT): 2016/124/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4149651
46 A = 6776500
79 meter
Y = 865029
97 meter E =
0004129
Z = 5283517
45 I = 51
26142
XDOT = -1599
043589 Wp = 81
48932
YDOT = 7504
091398 meter/sec RA = 282
19622 deg
ZDOT = 27
876616 TA = 8
24719
MA = 8
24040
Ha = 221
021 n
mi
Hp = 213
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13614342
05 X = 4114004
70
Y = 2838024
83 feet Y = 911235
06 meter
Z = 17334374
85 Z = 5303589
04
XDOT = -5246
206001 XDOT = -1682
972783
YDOT = 24619
722436 feet/sec YDOT = 7485
740554 meter/sec
ZDOT = 91
458713 ZDOT = 19
904572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6330029
44 X = -1929392
97
Y = 12260172
00 feet Y = 3736900
43 meter
Z = 17421370
65 Z = 5310033
78
XDOT = -21442
115633 XDOT = -6535
556845
YDOT = -11146
829936 feet/sec YDOT = -3397
553765 meter/sec
ZDOT = 55
446227 ZDOT = 16
900010
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 16124
14271543
00016717 00000-0 10270-3 0 9042
2 25544 51
6408 282
7390 0001797 69
3939 290
7406 15
54418028 37972
Satellite: ISS
Catalog Number: 25544
Epoch time: 16124
14271543 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 282
7390 deg
Eccentricity:
0001797
Arg of perigee: 69
3939 deg
Mean anomaly: 290
7406 deg
Mean motion: 15
54418028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3797
Checksum: 328
Coasting Arc #6 (Orbit 3811)
---------------------------------------
Vector Time (GMT): 2016/125/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3696714
72 A = 6777843
43 meter
Y = -2728492
98 meter E =
0014369
Z = -4995953
26 I = 51
25992
XDOT = 2475
796748 Wp = 101
11537
YDOT = -6971
499703 meter/sec RA = 277
16730 deg
ZDOT = 1977
610918 TA = 188
20774
MA = 188
23127
Ha = 221
174 n
mi
Hp = 213
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12128329
12 X = -3641660
69
Y = -8951748
63 feet Y = -2769524
51 meter
Z = -16390922
76 Z = -5013777
42
XDOT = 8122
692743 XDOT = 2543
963253
YDOT = -22872
374355 feet/sec YDOT = -6943
432467 meter/sec
ZDOT = 6488
224796 ZDOT = 1989
803794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11669372
72 X = 3556824
81
Y = -9408999
31 feet Y = -2867862
99 meter
Z = -16467816
86 Z = -5019390
58
XDOT = 19446
717066 XDOT = 5927
359362
YDOT = 12679
985695 feet/sec YDOT = 3864
859640 meter/sec
ZDOT = 6542
454927 ZDOT = 1994
140262
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 16125
10707196
00016717 00000-0 10270-3 0 9058
2 25544 51
6407 277
9293 0001778 74
2200 285
9149 15
54413351 38126
Satellite: ISS
Catalog Number: 25544
Epoch time: 16125
10707196 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 277
9293 deg
Eccentricity:
0001778
Arg of perigee: 74
2200 deg
Mean anomaly: 285
9149 deg
Mean motion: 15
54413351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3812
Checksum: 308
Coasting Arc #7 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2016/126/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3126458
93 A = 6781236
22 meter
Y = 4396289
88 meter E =
0012204
Z = 4100674
11 I = 51
26931
XDOT = -3246
519894 Wp = 76
07542
YDOT = 5839
098557 meter/sec RA = 272
14571 deg
ZDOT = -3772
450634 TA = 53
05214
MA = 52
94045
Ha = 221
062 n
mi
Hp = 213
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10257411
18 X = 3057146
44
Y = 14423523
24 feet Y = 4430864
62 meter
Z = 13453655
21 Z = 4115693
47
XDOT = -10651
311988 XDOT = -3293
247553
YDOT = 19157
147498 feet/sec YDOT = 5802
532416 meter/sec
ZDOT = -12376
806541 ZDOT = -3788
335424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16395936
73 X = -4997481
52
Y = 6533638
61 feet Y = 1991453
05 meter
Z = 13518068
30 Z = 4120307
22
XDOT = -15692
710581 XDOT = -4783
138185
YDOT = -13544
352597 feet/sec YDOT = -4128
318671 meter/sec
ZDOT = -12446
852123 ZDOT = -3793
800527
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 16126
13570986
00016717 00000-0 10270-3 0 9068
2 25544 51
6417 272
7994 0001736 74
7116 285
4228 15
54432508 38288
Satellite: ISS
Catalog Number: 25544
Epoch time: 16126
13570986 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 272
7994 deg
Eccentricity:
0001736
Arg of perigee: 74
7116 deg
Mean anomaly: 285
4228 deg
Mean motion: 15
54432508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 330
Coasting Arc #8 (Orbit 3842)
---------------------------------------
Vector Time (GMT): 2016/127/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2494077
29 A = 6785187
75 meter
Y = -5678314
08 meter E =
0006526
Z = -2753212
54 I = 51
28214
XDOT = 3892
138403 Wp = 63
55150
YDOT = -4181
091046 meter/sec RA = 267
13507 deg
ZDOT = 5109
692901 TA = 265
11425
MA = 265
18876
Ha = 221
147 n
mi
Hp = 213
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8182668
28 X = -2417021
38
Y = -18629639
38 feet Y = -5705773
70 meter
Z = -9032849
53 Z = -2765141
18
XDOT = 12769
482948 XDOT = 3913
781885
YDOT = -13717
490307 feet/sec YDOT = -4137
445485 meter/sec
ZDOT = 16764
084320 ZDOT = 5128
652984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19945550
46 X = 6079403
78
Y = -3908308
52 feet Y = -1191252
44 meter
Z = -9083613
58 Z = -2768685
42
XDOT = 10372
244866 XDOT = 3161
460235
YDOT = 13870
674633 feet/sec YDOT = 4227
781628 meter/sec
ZDOT = 16847
177901 ZDOT = 5135
019824
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 16127
10005055
00016717 00000-0 10270-3 0 9077
2 25544 51
6415 267
9900 0001818 76
2190 283
9166 15
54433607 38431
Satellite: ISS
Catalog Number: 25544
Epoch time: 16127
10005055 = yrday
fracday
Element set: 907
Inclination: 51
6415 deg
RA of node: 267
9900 deg
Eccentricity:
0001818
Arg of perigee: 76
2190 deg
Mean anomaly: 283
9166 deg
Mean motion: 15
54433607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3843
Checksum: 302
Coasting Arc #9 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2016/128/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1737141
86 A = 6787952
77 meter
Y = 6471685
73 meter E =
0014966
Z = 1042398
38 I = 51
29489
XDOT = -4449
245471 Wp = 118
96775
YDOT = 2148
470212 meter/sec RA = 262
13545 deg
ZDOT = -5867
203663 TA = 49
67208
MA = 49
54143
Ha = 221
141 n
mi
Hp = 213
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5699284
31 X = 1659581
10
Y = 21232564
73 feet Y = 6490677
92 meter
Z = 3419942
18 Z = 1050648
87
XDOT = -14597
262043 XDOT = -4444
438531
YDOT = 7048
786785 feet/sec YDOT = 2098
742747 meter/sec
ZDOT = -19249
355850 ZDOT = -5888
805767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21938209
76 X = -6686766
34
Y = 1334303
56 feet Y = 406695
72 meter
Z = 3454596
59 Z = 1052961
04
XDOT = -3925
806639 XDOT = -1196
585864
YDOT = -13986
923267 feet/sec YDOT = -4263
214212 meter/sec
ZDOT = -19343
554382 ZDOT = -5895
915376
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 16128
12867404
00016717 00000-0 10270-3 0 9085
2 25544 51
6424 262
8603 0001789 80
9589 279
1766 15
54441261 38591
Satellite: ISS
Catalog Number: 25544
Epoch time: 16128
12867404 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 262
8603 deg
Eccentricity:
0001789
Arg of perigee: 80
9589 deg
Mean anomaly: 279
1766 deg
Mean motion: 15
54441261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 340
Coasting Arc #10 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2016/129/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -904366
79 A = 6788149
68 meter
Y = -6678306
48 meter E =
0014854
Z = 754785
02 I = 51
30118
XDOT = 4872
331815 Wp = 56
22358
YDOT = 18
352381 meter/sec RA = 257
14029 deg
ZDOT = 5924
275973 TA = 311
97557
MA = 312
10201
Ha = 221
103 n
mi
Hp = 213
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2967082
65 X = -833287
58
Y = -21910454
34 feet Y = -6688022
31 meter
Z = 2476328
82 Z = 750564
14
XDOT = 15985
340602 XDOT = 4842
986316
YDOT = 60
211225 feet/sec YDOT = 72
673732 meter/sec
ZDOT = 19436
600961 ZDOT = 5947
873738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22086880
10 X = 6732081
05
Y = 1061054
70 feet Y = 323409
47 meter
Z = 2459203
81 Z = 749565
32
XDOT = -2874
719469 XDOT = -876
214494
YDOT = 13972
264711 feet/sec YDOT = 4258
746284 meter/sec
ZDOT = 19539
080051 ZDOT = 5955
511600
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 16129
15728903
00016717 00000-0 10270-3 0 9090
2 25544 51
6427 257
7305 0001738 80
6646 279
4703 15
54453629 38754
Satellite: ISS
Catalog Number: 25544
Epoch time: 16129
15728903 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 257
7305 deg
Eccentricity:
0001738
Arg of perigee: 80
6646 deg
Mean anomaly: 279
4703 deg
Mean motion: 15
54453629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 338
Coasting Arc #11 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2016/130/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -80088
82 A = 6785652
60 meter
Y = 6304378
04 meter E =
0006610
Z = -2508410
75 I = 51
30222
XDOT = -5130
232313 Wp = 119
51441
YDOT = -2156
583891 meter/sec RA = 252
14265 deg
ZDOT = -5270
035892 TA = 88
75767
MA = 88
68194
Ha = 221
082 n
mi
Hp = 213
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -262758
58 X = -138395
02
Y = 20683654
99 feet Y = 6303156
56 meter
Z = -8229694
07 Z = -2508941
09
XDOT = -16831
470844 XDOT = -5080
135594
YDOT = -7075
406466 feet/sec YDOT = -2213
673169 meter/sec
ZDOT = -17290
144003 ZDOT = -5294
836109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20363502
08 X = -6206795
43
Y = -3626824
94 feet Y = -1105456
24 meter
Z = -8233129
07 Z = -2509457
74
XDOT = 9479
764451 XDOT = 2889
432205
YDOT = -13834
558053 feet/sec YDOT = -4216
773295 meter/sec
ZDOT = -17397
471177 ZDOT = -5302
749215
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 16130
12160514
00016717 00000-0 10270-3 0 9109
2 25544 51
6438 252
9215 0001737 83
8053 276
3298 15
54473355 38909
Satellite: ISS
Catalog Number: 25544
Epoch time: 16130
12160514 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 252
9215 deg
Eccentricity:
0001737
Arg of perigee: 83
8053 deg
Mean anomaly: 276
3298 deg
Mean motion: 15
54473355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 302
Coasting Arc #12 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2016/131/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1138668
93 A = 6781709
72 meter
Y = -5401827
57 meter E =
0012846
Z = 3929299
70 I = 51
29895
XDOT = 5172
415156 Wp = 98
07233
YDOT = 4011
696535 meter/sec RA = 247
13569 deg
ZDOT = 4003
166423 TA = 309
91790
MA = 310
03073
Ha = 221
065 n
mi
Hp = 213
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3735790
45 X = 1179901
82
Y = -17722531
40 feet Y = -5388863
90 meter
Z = 12891403
22 Z = 3934930
97
XDOT = 16969
865999 XDOT = 5107
725058
YDOT = 13161
734039 feet/sec YDOT = 4069
175981 meter/sec
ZDOT = 13133
748106 ZDOT = 4028
136122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16983290
33 X = 5176506
89
Y = 6241472
47 feet Y = 1902400
81 meter
Z = 12916826
13 Z = 3937048
61
XDOT = -15067
236762 XDOT = -4592
493765
YDOT = 13506
785662 feet/sec YDOT = 4116
868270 meter/sec
ZDOT = 13241
494859 ZDOT = 4036
007633
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 16131
15020148
00016717 00000-0 10270-3 0 9112
2 25544 51
6429 247
7918 0001825 85
8193 274
3168 15
54485550 39068
Satellite: ISS
Catalog Number: 25544
Epoch time: 16131
15020148 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 247
7918 deg
Eccentricity:
0001825
Arg of perigee: 85
8193 deg
Mean anomaly: 274
3168 deg
Mean motion: 15
54485550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3906
Checksum: 314
Coasting Arc #13 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2016/132/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2293985
59 A = 6777888
29 meter
Y = 4081650
45 meter E =
0013820
Z = -4913612
15 I = 51
30044
XDOT = -4903
437885 Wp = 75
28271
YDOT = -5442
123004 meter/sec RA = 242
11780 deg
ZDOT = -2233
277865 TA = 172
78558
MA = 172
76567
Ha = 220
965 n
mi
Hp = 213
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7526199
45 X = -2315588
74
Y = 13391241
63 feet Y = 4055877
05 meter
Z = -16120774
78 Z = -4924808
10
XDOT = -16087
394636 XDOT = -4831
369885
YDOT = -17854
734265 feet/sec YDOT = -5496
553431 meter/sec
ZDOT = -7327
027115 ZDOT = -2256
922974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12299015
46 X = -3748739
91
Y = -9116438
24 feet Y = -2778690
38 meter
Z = -16170132
41 Z = -4928656
36
XDOT = 19142
493628 XDOT = 5834
632058
YDOT = -12659
178943 feet/sec YDOT = -3858
517742 meter/sec
ZDOT = -7428
784928 ZDOT = -2264
293646
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 16132
11450067
00016717 00000-0 10270-3 0 9127
2 25544 51
6434 242
9830 0001644 86
8755 273
2586 15
54528648 39213
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
11450067 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 242
9830 deg
Eccentricity:
0001644
Arg of perigee: 86
8755 deg
Mean anomaly: 273
2586 deg
Mean motion: 15
54528648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 314
Coasting Arc #14 (Orbit 3927)
---------------------------------------
Vector Time (GMT): 2016/132/13:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4693657
24 A = 6785846
96 meter
Y = -4291994
05 meter E =
0006602
Z = -2364249
57 I = 51
33348
XDOT = 1981
951874 Wp = 57
48093
YDOT = -5110
605957 meter/sec RA = 239
74529 deg
ZDOT = 5357
401595 TA = 276
01547
MA = 276
09071
Ha = 220
949 n
mi
Hp = 213
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15399137
92 X = -4633829
66
Y = -14081345
31 feet Y = -4344147
02 meter
Z = -7756724
32 Z = -2386905
23
XDOT = 6502
466778 XDOT = 2012
928527
YDOT = -16767
079913 feet/sec YDOT = -5088
269514 meter/sec
ZDOT = 17576
776888 ZDOT = 5367
104474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18412855
90 X = -5612238
48
Y = 9739595
62 feet Y = 2968628
74 meter
Z = -7854395
03 Z = -2394019
61
XDOT = -12943
010903 XDOT = -3945
029723
YDOT = -10297
374205 feet/sec YDOT = -3138
639658 meter/sec
ZDOT = 17619
827719 ZDOT = 5370
523489
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 16132
56450341
00016717 00000-0 10270-3 0 9132
2 25544 51
6430 240
7356 0001516 100
4191 259
7132 15
54488691 39289
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
56450341 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 240
7356 deg
Eccentricity:
0001516
Arg of perigee: 100
4191 deg
Mean anomaly: 259
7132 deg
Mean motion: 15
54488691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3928
Checksum: 295
Coasting Arc #15 (Orbit 3943)
---------------------------------------
Vector Time (GMT): 2016/133/13:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4267648
80 A = 6788033
31 meter
Y = 5238277
87 meter E =
0014675
Z = 577882
04 I = 51
35721
XDOT = -3400
161543 Wp = 126
03058
YDOT = 3437
805431 meter/sec RA = 234
75112 deg
ZDOT = -5954
637088 TA = 47
70571
MA = 47
58141
Ha = 220
980 n
mi
Hp = 213
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14001472
44 X = 4205948
77
Y = 17185951
01 feet Y = 5285656
55 meter
Z = 1895938
44 Z = 598463
63
XDOT = -11155
385639 XDOT = -3409
426035
YDOT = 11278
889210 feet/sec YDOT = 3399
730971 meter/sec
ZDOT = -19536
210918 ZDOT = -5971
176683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20750687
19 X = 6324809
46
Y = -7775838
35 feet Y = -2370075
53 meter
Z = 1984450
59 Z = 604860
54
XDOT = 6602
570663 XDOT = 2012
463538
YDOT = 12537
333941 feet/sec YDOT = 3821
379385 meter/sec
ZDOT = -19608
670036 ZDOT = -5976
722627
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 16133
59307640
00016717 00000-0 10270-3 0 9140
2 25544 51
6422 235
6057 0001705 104
2392 255
8950 15
54521796 39443
Satellite: ISS
Catalog Number: 25544
Epoch time: 16133
59307640 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 235
6057 deg
Eccentricity:
0001705
Arg of perigee: 104
2392 deg
Mean anomaly: 255
8950 deg
Mean motion: 15
54521796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3944
Checksum: 307
Coasting Arc #16 (Orbit 3959)
---------------------------------------
Vector Time (GMT): 2016/134/13:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3500049
42 A = 6787543
82 meter
Y = -5673298
11 meter E =
0014965
Z = 1242929
01 I = 51
37458
XDOT = 4720
165124 Wp = 63
29155
YDOT = -1625
674576 meter/sec RA = 229
76028 deg
ZDOT = 5823
781476 TA = 310
27777
MA = 310
40851
Ha = 220
972 n
mi
Hp = 213
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11483101
76 X = -3442386
69
Y = -18613182
78 feet Y = -5712115
61 meter
Z = 4077851
08 Z = 1226066
50
XDOT = 15486
106051 XDOT = 4709
703459
YDOT = -5333
578006 feet/sec YDOT = -1572
949167 meter/sec
ZDOT = 19106
894606 ZDOT = 5846
685518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21223114
73 X = -6468805
37
Y = 5336289
58 feet Y = 1626501
06 meter
Z = 4005556
59 Z = 1220893
65
XDOT = -43
152117 XDOT = -13
152765
YDOT = -14708
334805 feet/sec YDOT = -4483
100449 meter/sec
ZDOT = 19206
697260 ZDOT = 5854
201325
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 16134
62164042
00016717 00000-0 10270-3 0 9153
2 25544 51
6419 230
4755 0001681 104
0276 256
1064 15
54526688 39602
Satellite: ISS
Catalog Number: 25544
Epoch time: 16134
62164042 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 230
4755 deg
Eccentricity:
0001681
Arg of perigee: 104
0276 deg
Mean anomaly: 256
1064 deg
Mean motion: 15
54526688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3960
Checksum: 299
Coasting Arc #17 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2016/135/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3607157
02 A = 6776275
57 meter
Y = 2321022
06 meter E =
0016451
Z = -5260265
09 I = 51
35113
XDOT = -4856
812643 Wp = 97
20040
YDOT = -5873
247428 meter/sec RA = 225
96422 deg
ZDOT = 738
973550 TA = 179
89816
MA = 179
89782
Ha = 220
983 n
mi
Hp = 213
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11834504
67 X = -3607290
94
Y = 7614901
78 feet Y = 2280683
75 meter
Z = -17258087
57 Z = -5277788
15
XDOT = -15934
424681 XDOT = -4794
365187
YDOT = -19269
184476 feet/sec YDOT = -5927
210384 meter/sec
ZDOT = 2424
453903 ZDOT = 715
531844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13322012
29 X = -4060549
35
Y = 4233010
91 feet Y = 1290221
73 meter
Z = -17334630
76 Z = -5283595
46
XDOT = -9962
012256 XDOT = -3036
421336
YDOT = -21836
419789 feet/sec YDOT = -6655
740752 meter/sec
ZDOT = 2323
591921 ZDOT = 708
230818
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 16135
32877328
00016717 00000-0 10270-3 0 9160
2 25544 51
6398 226
9463 0001872 107
9203 252
2154 15
54557783 39717
Satellite: ISS
Catalog Number: 25544
Epoch time: 16135
32877328 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 226
9463 deg
Eccentricity:
0001872
Arg of perigee: 107
9203 deg
Mean anomaly: 252
2154 deg
Mean motion: 15
54557783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 331
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