[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 18th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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
198/02:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
1
198/21:41:46
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 213
1
200/04:45:26
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
1
201/00:22:53
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
0
201/08:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 213
0
202/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
0
Coasting Arc #1 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2016/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4246688
14 A = 6776127
63 meter
Y = -1432413
76 meter E =
0005454
Z = 5078431
14 I = 51
25951
XDOT = 546
680758 Wp = 112
37168
YDOT = 7474
051883 meter/sec RA = 275
97576 deg
ZDOT = 1647
509450 TA = 321
63018
MA = 321
66897
Ha = 220
058 n
mi
Hp = 213
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13932703
87 X = 4237721
44
Y = -4699520
20 feet Y = -1384975
09 meter
Z = 16661519
50 Z = 5099038
46
XDOT = 1793
572042 XDOT = 455
060551
YDOT = 24521
167595 feet/sec YDOT = 7479
652791 meter/sec
ZDOT = 5405
214731 ZDOT = 1649
943273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9710715
17 X = -2959825
98
Y = -10904082
89 feet Y = -3323564
47 meter
Z = 16751565
49 Z = 5105877
16
XDOT = 21106
008504 XDOT = 6433
111392
YDOT = -10460
816257 feet/sec YDOT = -3188
456795 meter/sec
ZDOT = 5414
389817 ZDOT = 1650
306016
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 16197
55106782
00016717 00000-0 10270-3 0 9005
2 25544 51
6440 276
5250 0001223 47
9145 312
2112 15
54856583 9390
Satellite: ISS
Catalog Number: 25544
Epoch time: 16197
55106782 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 276
5250 deg
Eccentricity:
0001223
Arg of perigee: 47
9145 deg
Mean anomaly: 312
2112 deg
Mean motion: 15
54856583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 299
Coasting Arc #2 (Orbit 947)
---------------------------------------
Vector Time (GMT): 2016/198/02:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2428940
87 A = 6782299
82 meter
Y = 5353266
73 meter E =
0013539
Z = 3372379
77 I = 51
27856
XDOT = -3942
484350 Wp = 84
19827
YDOT = 4701
294894 meter/sec RA = 272
97890 deg
ZDOT = -4605
883855 TA = 56
17387
MA = 56
04506
Ha = 220
219 n
mi
Hp = 213
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7968966
09 X = 2352517
31
Y = 17563211
06 feet Y = 5380001
11 meter
Z = 11064238
08 Z = 3383993
81
XDOT = -12934
659942 XDOT = -3972
389152
YDOT = 15424
195846 feet/sec YDOT = 4657
040679 meter/sec
ZDOT = -15111
167504 ZDOT = -4625
107475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3274620
43 X = -998104
31
Y = 18977568
29 feet Y = 5784362
82 meter
Z = 11113817
09 Z = 3387491
45
XDOT = -17882
658282 XDOT = -5450
634244
YDOT = 5846
560126 feet/sec YDOT = 1782
031526 meter/sec
ZDOT = -15195
807635 ZDOT = -4631
682167
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 16198
12952446
00016717 00000-0 10270-3 0 9016
2 25544 51
6441 273
6411 0001757 34
9230 325
2038 15
54871398 9483
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
12952446 = yrday
fracday
Element set: 901
Inclination: 51
6441 deg
RA of node: 273
6411 deg
Eccentricity:
0001757
Arg of perigee: 34
9230 deg
Mean anomaly: 325
2038 deg
Mean motion: 15
54871398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 948
Checksum: 313
Coasting Arc #3 (Orbit 960)
---------------------------------------
Vector Time (GMT): 2016/198/21:41:46
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1188314
72 A = 6786142
78 meter
Y = -6470825
63 meter E =
0015638
Z = 1632068
21 I = 51
28809
XDOT = 4606
073686 Wp = 61
53824
YDOT = 2290
380245 meter/sec RA = 268
93758 deg
ZDOT = 5692
897406 TA = 316
43452
MA = 316
55791
Ha = 220
374 n
mi
Hp = 213
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3898670
35 X = 1252656
99
Y = -21229742
89 feet Y = -6457177
53 meter
Z = 5354554
50 Z = 1637996
25
XDOT = 15111
790307 XDOT = 4552
466347
YDOT = 7514
370882 feet/sec YDOT = 2341
588060 meter/sec
ZDOT = 18677
484928 ZDOT = 5715
142418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20202012
87 X = 6157573
52
Y = 7582210
27 feet Y = 2311057
69 meter
Z = 5381601
17 Z = 1640312
04
XDOT = -9512
298372 XDOT = -2899
348544
YDOT = 11939
910029 feet/sec YDOT = 3639
284577 meter/sec
ZDOT = 18773
967155 ZDOT = 5722
305189
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 16198
96507258
00016717 00000-0 10270-3 0 9026
2 25544 51
6420 269
4714 0001781 45
5800 314
5499 15
54833839 9612
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
96507258 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 269
4714 deg
Eccentricity:
0001781
Arg of perigee: 45
5800 deg
Mean anomaly: 314
5499 deg
Mean motion: 15
54833839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 961
Checksum: 332
Coasting Arc #4 (Orbit 975)
---------------------------------------
Vector Time (GMT): 2016/199/21:41:46
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2121038
79 A = 6782394
97 meter
Y = 5502876
65 meter E =
0006176
Z = -3356085
71 I = 51
27818
XDOT = -4200
693682 Wp = 80
32392
YDOT = -4436
013338 meter/sec RA = 263
93229 deg
ZDOT = -4625
051370 TA = 139
01726
MA = 138
97083
Ha = 220
363 n
mi
Hp = 212
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6958788
67 X = -2166113
48
Y = 18054057
26 feet Y = 5478906
14 meter
Z = -11010779
89 Z = -3366497
92
XDOT = -13781
803419 XDOT = -4128
310627
YDOT = -14553
849535 feet/sec YDOT = -4482
583053 meter/sec
ZDOT = -15174
053051 ZDOT = -4645
281742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16707627
51 X = -5092484
86
Y = -9705932
04 feet Y = -2958368
09 meter
Z = -11057172
49 Z = -3370226
17
XDOT = 15861
812687 XDOT = 4834
680507
YDOT = -9941
596078 feet/sec YDOT = -3030
198485 meter/sec
ZDOT = -15261
368600 ZDOT = -4651
665149
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 16199
92916002
00016717 00000-0 10270-3 0 9035
2 25544 51
6428 264
6611 0001774 47
3818 312
7484 15
54856904 9762
Satellite: ISS
Catalog Number: 25544
Epoch time: 16199
92916002 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 264
6611 deg
Eccentricity:
0001774
Arg of perigee: 47
3818 deg
Mean anomaly: 312
7484 deg
Mean motion: 15
54856904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 976
Checksum: 331
Coasting Arc #5 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2016/200/04:45:26
000
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3528066
21 A = 6777100
84 meter
Y = -3117383
63 meter E =
0007462
Z = 4869669
81 I = 51
25762
XDOT = 2773
733902 Wp = 110
25481
YDOT = 6768
556303 meter/sec RA = 262
44605 deg
ZDOT = 2317
980667 TA = 316
92931
MA = 316
98768
Ha = 220
248 n
mi
Hp = 213
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11575020
36 X = 3539008
92
Y = -10227636
57 feet Y = -3077869
80 meter
Z = 15976606
99 Z = 4886834
28
XDOT = 9100
176844 XDOT = 2686
580449
YDOT = 22206
549552 feet/sec YDOT = 6799
086480 meter/sec
ZDOT = 7604
923449 ZDOT = 2331
243679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10152772
71 X = 3094565
12
Y = -11536592
33 feet Y = -3516353
34 meter
Z = 16051973
73 Z = 4892641
59
XDOT = 10825
092321 XDOT = 3299
488139
YDOT = 20211
432079 feet/sec YDOT = 6160
444498 meter/sec
ZDOT = 7661
452709 ZDOT = 2335
210786
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 16200
25052113
00016717 00000-0 10270-3 0 9049
2 25544 51
6392 263
0536 0001548 53
4597 306
6698 15
54833938 9819
Satellite: ISS
Catalog Number: 25544
Epoch time: 16200
25052113 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 263
0536 deg
Eccentricity:
0001548
Arg of perigee: 53
4597 deg
Mean anomaly: 306
6698 deg
Mean motion: 15
54833938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 312
Coasting Arc #6 (Orbit 992)
---------------------------------------
Vector Time (GMT): 2016/201/00:22:53
000
Vector Time (MET): N/A
Weight (LBS) : 908864
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3410328
76 A = 6783671
42 meter
Y = -5111568
09 meter E =
0006221
Z = -2874261
63 I = 51
28816
XDOT = 3101
020998 Wp = 58
80227
YDOT = -4888
024523 meter/sec RA = 258
30787 deg
ZDOT = 5024
700143 TA = 268
31035
MA = 268
38160
Ha = 220
302 n
mi
Hp = 213
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11188742
67 X = -3338954
76
Y = -16770236
50 feet Y = -5149305
28 meter
Z = -9429992
21 Z = -2890655
08
XDOT = 10173
953407 XDOT = 3131
042210
YDOT = -16036
825862 feet/sec YDOT = -4853
179515 meter/sec
ZDOT = 16485
236689 ZDOT = 5039
836284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8292621
36 X = 2527590
99
Y = -18339214
64 feet Y = -5589792
62 meter
Z = -9500483
43 Z = -2895747
35
XDOT = 17596
262292 XDOT = 5363
340747
YDOT = -599
026868 feet/sec YDOT = -182
583389 meter/sec
ZDOT = 16552
090399 ZDOT = 5045
077154
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 16201
02178525
00016717 00000-0 10270-3 0 9052
2 25544 51
6435 259
2097 0001702 43
1703 316
9583 15
54849885 9931
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
02178525 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 259
2097 deg
Eccentricity:
0001702
Arg of perigee: 43
1703 deg
Mean anomaly: 316
9583 deg
Mean motion: 15
54849885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 993
Checksum: 317
Coasting Arc #7 (Orbit 998)
---------------------------------------
Vector Time (GMT): 2016/201/08:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 908864
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4201461
93 A = 6775152
10 meter
Y = -624786
79 meter E =
0003970
Z = 5275058
22 I = 51
26198
XDOT = 1524
037827 Wp = 71
15546
YDOT = 7513
279408 meter/sec RA = 256
59929 deg
ZDOT = -322
514389 TA = 21
94198
MA = 21
92498
Ha = 220
130 n
mi
Hp = 212
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13784323
93 X = 4182512
68
Y = -2049825
42 feet Y = -577909
73 meter
Z = 17306621
46 Z = 5295421
44
XDOT = 5000
124103 XDOT = 1441
475783
YDOT = 24649
866824 feet/sec YDOT = 7529
860617 meter/sec
ZDOT = -1058
118073 ZDOT = -315
310878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3638163
06 X = 1108912
10
Y = -13337539
33 feet Y = -4065281
99 meter
Z = 17395468
70 Z = 5302138
86
XDOT = 23603
538321 XDOT = 7194
358480
YDOT = 5091
357269 feet/sec YDOT = 1551
845696 meter/sec
ZDOT = -1028
105992 ZDOT = -313
366706
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 16201
40741631
00016717 00000-0 10270-3 0 9069
2 25544 51
6432 257
2804 0001447 63
0516 297
0785 15
54892519 9992
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
40741631 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 257
2804 deg
Eccentricity:
0001447
Arg of perigee: 63
0516 deg
Mean anomaly: 297
0785 deg
Mean motion: 15
54892519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 999
Checksum: 315
Coasting Arc #8 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2016/202/08:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 908864
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4553253
10 A = 6777146
50 meter
Y = -1425602
28 meter E =
0012980
Z = -4825191
86 I = 51
27628
XDOT = -335
522289 Wp = 103
55828
YDOT = -7245
789937 meter/sec RA = 251
56932 deg
ZDOT = 2459
988851 TA = 190
73775
MA = 190
76549
Ha = 220
325 n
mi
Hp = 212
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14938494
41 X = -4513535
00
Y = -4677172
83 feet Y = -1476297
29 meter
Z = -15830681
96 Z = -4847213
65
XDOT = -1100
794910 XDOT = -266
422433
YDOT = -23772
276697 feet/sec YDOT = -7249
155827 meter/sec
ZDOT = 8070
829563 ZDOT = 2458
526196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10060597
26 X = -3066470
05
Y = 11865052
22 feet Y = 3616467
92 meter
Z = -15926392
27 Z = -4854364
36
XDOT = -21496
773506 XDOT = -6552
216565
YDOT = -7412
298294 feet/sec YDOT = -2259
268520 meter/sec
ZDOT = 8065
765480 ZDOT = 2458
445318
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 16202
37149344
00016717 00000-0 10270-3 0 9070
2 25544 51
6425 252
4711 0001532 69
3790 290
7528 15
54887358 10145
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
37149344 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 252
4711 deg
Eccentricity:
0001532
Arg of perigee: 69
3790 deg
Mean anomaly: 290
7528 deg
Mean motion: 15
54887358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 309
Coasting Arc #9 (Orbit 1015)
---------------------------------------
Vector Time (GMT): 2016/202/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4526381
00 A = 6779369
07 meter
Y = 2735641
82 meter E =
0011380
Z = 4234190
51 I = 51
28429
XDOT = -719
195701 Wp = 71
47749
YDOT = 6748
393000 meter/sec RA = 251
07049 deg
ZDOT = -3579
722703 TA = 55
29828
MA = 55
19112
Ha = 220
158 n
mi
Hp = 212
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14850331
36 X = 4474886
49
Y = 8975202
82 feet Y = 2785970
54 meter
Z = 13891701
15 Z = 4256053
27
XDOT = -2359
565949 XDOT = -777
216077
YDOT = 22140
396980 feet/sec YDOT = 6740
026370 meter/sec
ZDOT = -11744
497056 ZDOT = -3583
356648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5481843
49 X = 1670865
89
Y = -16382724
19 feet Y = -4993454
33 meter
Z = 13986483
05 Z = 4263080
03
XDOT = 20900
182620 XDOT = 6370
375663
YDOT = -3079
731269 feet/sec YDOT = -938
702091 meter/sec
ZDOT = -11761
551744 ZDOT = -3584
920972
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 16202
50003520
00016717 00000-0 10270-3 0 9081
2 25544 51
6419 251
8306 0001483 58
2448 301
8850 15
54898606 10165
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
50003520 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 251
8306 deg
Eccentricity:
0001483
Arg of perigee: 58
2448 deg
Mean anomaly: 301
8850 deg
Mean motion: 15
54898606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1016
Checksum: 290
Coasting Arc #10 (Orbit 1030)
---------------------------------------
Vector Time (GMT): 2016/203/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4392591
10 A = 6783712
13 meter
Y = -4336087
74 meter E =
0006203
Z = -2815574
45 I = 51
30889
XDOT = 2057
968721 Wp = 63
16221
YDOT = -5368
751635 meter/sec RA = 246
05780 deg
ZDOT = 5068
834833 TA = 264
71573
MA = 264
78651
Ha = 220
309 n
mi
Hp = 212
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14411388
12 X = -4330100
85
Y = -14226009
65 feet Y = -4384859
03 meter
Z = -9237449
00 Z = -2836760
63
XDOT = 6751
865881 XDOT = 2093
228807
YDOT = -17614
014550 feet/sec YDOT = -5345
541247 meter/sec
ZDOT = 16630
035541 ZDOT = 5078
916998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10395712
50 X = -3168613
17
Y = 17329068
43 feet Y = 5281900
06 meter
Z = -9329012
33 Z = -2843482
96
XDOT = -17424
942488 XDOT = -5311
122470
YDOT = -1496
316788 feet/sec YDOT = -456
077357 meter/sec
ZDOT = 16674
931377 ZDOT = 5082
519084
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 16203
46410845
00016717 00000-0 10270-3 0 9090
2 25544 51
6408 247
0200 0001544 65
9817 294
1498 15
54879677 10312
Satellite: ISS
Catalog Number: 25544
Epoch time: 16203
46410845 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 247
0200 deg
Eccentricity:
0001544
Arg of perigee: 65
9817 deg
Mean anomaly: 294
1498 deg
Mean motion: 15
54879677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1031
Checksum: 316
Coasting Arc #11 (Orbit 1046)
---------------------------------------
Vector Time (GMT): 2016/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3907459
57 A = 6786653
75 meter
Y = 5455033
81 meter E =
0014500
Z = 974228
81 I = 51
33341
XDOT = -3434
298761 Wp = 118
27372
YDOT = 3521
902725 meter/sec RA = 241
05746 deg
ZDOT = -5885
742048 TA = 51
12230
MA = 50
99304
Ha = 220
363 n
mi
Hp = 212
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12819749
24 X = 3841437
31
Y = 17897092
55 feet Y = 5498360
43 meter
Z = 3196288
74 Z = 993049
79
XDOT = -11267
384386 XDOT = -3444
836513
YDOT = 11554
798966 feet/sec YDOT = 3483
439471 meter/sec
ZDOT = -19310
177324 ZDOT = -5902
450092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14041205
61 X = 4279759
47
Y = -16940235
45 feet Y = -5163383
76 meter
Z = 3277365
07 Z = 998940
87
XDOT = 12777
469693 XDOT = 3894
572762
YDOT = 6803
478282 feet/sec YDOT = 2073
700180 meter/sec
ZDOT = -19383
618289 ZDOT = -5908
126854
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 16204
49244659
00016717 00000-0 10270-3 0 9104
2 25544 51
6414 241
8875 0001772 63
3148 296
8186 15
54904360 10479
Satellite: ISS
Catalog Number: 25544
Epoch time: 16204
49244659 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 241
8875 deg
Eccentricity:
0001772
Arg of perigee: 63
3148 deg
Mean anomaly: 296
8186 deg
Mean motion: 15
54904360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 317
Coasting Arc #12 (Orbit 1062)
---------------------------------------
Vector Time (GMT): 2016/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3082580
64 A = 6786876
16 meter
Y = -5960993
66 meter E =
0015384
Z = 963254
84 I = 51
34901
XDOT = 4692
115230 Wp = 56
72267
YDOT = -1464
912387 meter/sec RA = 236
06368 deg
ZDOT = 5890
198083 TA = 313
75949
MA = 313
88671
Ha = 220
515 n
mi
Hp = 212
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10113453
55 X = -3020373
20
Y = -19557065
82 feet Y = -5995117
34 meter
Z = 3160284
91 Z = 948431
61
XDOT = 15394
078839 XDOT = 4679
536008
YDOT = -4806
143001 feet/sec YDOT = -1412
512543 meter/sec
ZDOT = 19324
796861 ZDOT = 5912
960186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16068696
03 X = -4897738
55
Y = 15065045
78 feet Y = 4591825
95 meter
Z = 3096703
17 Z = 943875
13
XDOT = -7672
813622 XDOT = -2338
673592
YDOT = -12217
996967 feet/sec YDOT = -3724
045475 meter/sec
ZDOT = 19424
267772 ZDOT = 5920
516817
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 16205
52078322
00016717 00000-0 10270-3 0 9112
2 25544 51
6405 236
7559 0001906 65
7580 294
3772 15
54844148 10635
Satellite: ISS
Catalog Number: 25544
Epoch time: 16205
52078322 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 236
7559 deg
Eccentricity:
0001906
Arg of perigee: 65
7580 deg
Mean anomaly: 294
3772 deg
Mean motion: 15
54844148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1063
Checksum: 311
Coasting Arc #13 (Orbit 1077)
---------------------------------------
Vector Time (GMT): 2016/206/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1866752
95 A = 6783760
03 meter
Y = 5886319
36 meter E =
0006142
Z = -2810672
60 I = 51
35877
XDOT = -5709
268433 Wp = 107
65603
YDOT = -608
297247 meter/sec RA = 231
06573 deg
ZDOT = -5076
851682 TA = 104
37476
MA = 104
30658
Ha = 220
447 n
mi
Hp = 212
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6124517
54 X = 1814444
73
Y = 19312071
38 feet Y = 5906902
22 meter
Z = -9221366
81 Z = -2801731
45
XDOT = -18731
195646 XDOT = -5677
381188
YDOT = -1995
725876 feet/sec YDOT = -671
963705 meter/sec
ZDOT = -16656
337539 ZDOT = -5104
508027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16710169
64 X = 5093259
71
Y = -11486290
79 feet Y = -3501021
43 meter
Z = -9183396
79 Z = -2799099
34
XDOT = 2616
238263 XDOT = 797
429422
YDOT = 17190
289953 feet/sec YDOT = 5239
600378 meter/sec
ZDOT = -16776
792814 ZDOT = -5113
566450
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 16206
48484194
00016717 00000-0 10270-3 0 9127
2 25544 51
6414 231
9443 0001849 73
5854 286
5502 15
54900142 10788
Satellite: ISS
Catalog Number: 25544
Epoch time: 16206
48484194 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 231
9443 deg
Eccentricity:
0001849
Arg of perigee: 73
5854 deg
Mean anomaly: 286
5502 deg
Mean motion: 15
54900142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1078
Checksum: 309
Coasting Arc #14 (Orbit 1093)
---------------------------------------
Vector Time (GMT): 2016/207/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -374064
65 A = 6779451
68 meter
Y = -5270665
46 meter E =
0011744
Z = 4239022
06 I = 51
36522
XDOT = 6331
161148 Wp = 101
56104
YDOT = 2441
540732 meter/sec RA = 226
05725 deg
ZDOT = 3583
666876 TA = 311
67321
MA = 311
77367
Ha = 220
469 n
mi
Hp = 212
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1227246
24 X = -335690
06
Y = -17292209
51 feet Y = -5274634
01 meter
Z = 13907552
70 Z = 4237298
08
XDOT = 20771
526076 XDOT = 6285
980963
YDOT = 8010
304238 feet/sec YDOT = 2512
087323 meter/sec
ZDOT = 11757
437256 ZDOT = 3614
312040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16068199
23 X = -4897587
12
Y = 6521027
73 feet Y = 1987609
25 meter
Z = 13900929
33 Z = 4237003
26
XDOT = 1802
832735 XDOT = 549
503418
YDOT = -20980
262582 feet/sec YDOT = -6394
784035 meter/sec
ZDOT = 11890
621675 ZDOT = 3624
261486
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 16207
51316751
00016717 00000-0 10270-3 0 9136
2 25544 51
6413 226
8123 0001942 75
0972 285
0396 15
54901997 10949
Satellite: ISS
Catalog Number: 25544
Epoch time: 16207
51316751 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 226
8123 deg
Eccentricity:
0001942
Arg of perigee: 75
0972 deg
Mean anomaly: 285
0396 deg
Mean motion: 15
54901997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1094
Checksum: 309
Coasting Arc #15 (Orbit 1108)
---------------------------------------
Vector Time (GMT): 2016/208/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1334015
98 A = 6775995
22 meter
Y = 4256243
71 meter E =
0015366
Z = -5114672
24 I = 51
37773
XDOT = -6399
229091 Wp = 78
08836
YDOT = -3899
731031 meter/sec RA = 221
03769 deg
ZDOT = -1577
076325 TA = 176
63356
MA = 176
62320
Ha = 220
457 n
mi
Hp = 212
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4376692
84 X = -1356666
54
Y = 13964054
17 feet Y = 4241199
34 meter
Z = -16780420
74 Z = -5121207
41
XDOT = -20994
846100 XDOT = -6347
485015
YDOT = -12794
393147 feet/sec YDOT = -3971
002125 meter/sec
ZDOT = -5174
134924 ZDOT = -1608
036357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14593728
52 X = 4448168
45
Y = -438456
20 feet Y = -133641
45 meter
Z = -16809628
59 Z = -5123574
80
XDOT = -5423
191280 XDOT = -1652
988702
YDOT = 22894
246147 feet/sec YDOT = 6978
166226 meter/sec
ZDOT = -5308
461134 ZDOT = -1618
018954
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 16208
47721946
00016717 00000-0 10270-3 0 9149
2 25544 51
6423 222
0015 0001845 77
6088 282
5271 15
54894366 11098
Satellite: ISS
Catalog Number: 25544
Epoch time: 16208
47721946 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 222
0015 deg
Eccentricity:
0001845
Arg of perigee: 77
6088 deg
Mean anomaly: 282
5271 deg
Mean motion: 15
54894366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1109
Checksum: 311
Coasting Arc #16 (Orbit 1124)
---------------------------------------
Vector Time (GMT): 2016/209/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3054319
74 A = 6775173
26 meter
Y = -2973493
32 meter E =
0004842
Z = 5262303
04 I = 51
39861
XDOT = 5872
149615 Wp = 72
12556
YDOT = 4898
456032 meter/sec RA = 216
01266 deg
ZDOT = -638
440368 TA = 23
99702
MA = 23
97446
Ha = 220
373 n
mi
Hp = 212
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10020734
07 X = 3061781
26
Y = -9755555
50 feet Y = -2939296
37 meter
Z = 17264773
75 Z = 5277158
07
XDOT = 19265
582728 XDOT = 5820
038663
YDOT = 16071
049974 feet/sec YDOT = 4963
830987 meter/sec
ZDOT = -2094
620630 ZDOT = -610
041480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12523805
76 X = -3817256
00
Y = -6040056
15 feet Y = -1841009
12 meter
Z = 17330043
22 Z = 5282197
17
XDOT = 8189
223898 XDOT = 2496
075444
YDOT = -22655
166516 feet/sec YDOT = -6905
294754 meter/sec
ZDOT = -1971
611848 ZDOT = -600
947291
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 16209
50553774
00016717 00000-0 10270-3 0 9157
2 25544 51
6407 216
8697 0001985 80
7558 279
3820 15
54915367 11256
Satellite: ISS
Catalog Number: 25544
Epoch time: 16209
50553774 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 216
8697 deg
Eccentricity:
0001985
Arg of perigee: 80
7558 deg
Mean anomaly: 279
3820 deg
Mean motion: 15
54915367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1125
Checksum: 337
Coasting Arc #17 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2016/210/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4617139
23 A = 6777588
78 meter
Y = 1604547
32 meter E =
0012620
Z = -4707072
09 I = 51
43462
XDOT = -4688
760897 Wp = 105
23715
YDOT = -5388
429658 meter/sec RA = 210
99238 deg
ZDOT = 2765
329004 TA = 192
24720
MA = 192
27790
Ha = 220
436 n
mi
Hp = 212
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15148094
58 X = -4611873
76
Y = 5264262
86 feet Y = 1552945
11 meter
Z = -15443149
91 Z = -4729487
96
XDOT = -15383
073808 XDOT = -4641
590320
YDOT = -17678
574994 feet/sec YDOT = -5440
598930 meter/sec
ZDOT = 9072
601719 ZDOT = 2742
666588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10240049
70 X = 3121167
15
Y = 12218084
09 feet Y = 3724072
03 meter
Z = -15541168
41 Z = -4736948
13
XDOT = -10191
055472 XDOT = -3106
233708
YDOT = 19944
522058 feet/sec YDOT = 6079
090323 meter/sec
ZDOT = 8974
672091 ZDOT = 2735
480053
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 16210
46958135
00016717 00000-0 10270-3 0 9165
2 25544 51
6421 212
0590 0001832 79
1153 281
0206 15
54899015 11402
Satellite: ISS
Catalog Number: 25544
Epoch time: 16210
46958135 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 212
0590 deg
Eccentricity:
0001832
Arg of perigee: 79
1153 deg
Mean anomaly: 281
0206 deg
Mean motion: 15
54899015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 281
Coasting Arc #18 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2016/211/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5813819
73 A = 6781714
68 meter
Y = -241028
89 meter E =
0014182
Z = 3471576
38 I = 51
47519
XDOT = 2942
128369 Wp = 87
54888
YDOT = 5448
121016 meter/sec RA = 205
98462 deg
ZDOT = -4532
281795 TA = 51
53891
MA = 51
41174
Ha = 220
334 n
mi
Hp = 212
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19074211
71 X = 5799219
62
Y = -790777
21 feet Y = -176096
76 meter
Z = 11389686
27 Z = 3499782
70
XDOT = 9652
652128 XDOT = 2903
003095
YDOT = 17874
412782 feet/sec YDOT = 5480
803421 meter/sec
ZDOT = -14869
690930 ZDOT = -4518
084451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7751640
25 X = -2362699
95
Y = -17365039
62 feet Y = -5292864
08 meter
Z = 11512745
39 Z = 3509084
80
XDOT = 11742
328639 XDOT = 3579
061769
YDOT = -15095
372108 feet/sec YDOT = -4601
069418 meter/sec
ZDOT = -14808
673715 ZDOT = -4513
683748
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 16211
49788975
00016717 00000-0 10270-3 0 9173
2 25544 51
6403 206
9268 0001993 80
6643 279
4735 15
54949448 11566
Satellite: ISS
Catalog Number: 25544
Epoch time: 16211
49788975 = yrday
fracday
Element set: 917
Inclination: 51
6403 deg
RA of node: 206
9268 deg
Eccentricity:
0001993
Arg of perigee: 80
6643 deg
Mean anomaly: 279
4735 deg
Mean motion: 15
54949448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 353
Coasting Arc #19 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2016/212/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929830
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6472751
04 A = 6785486
76 meter
Y = -962802
56 meter E =
0008679
Z = -1786250
07 I = 51
51671
XDOT = -792
364651 Wp = 49
38210
YDOT = -5117
755493 meter/sec RA = 200
99304 deg
ZDOT = 5653
354653 TA = 290
96043
MA = 291
05328
Ha = 220
380 n
mi
Hp = 212
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21236059
85 X = -6452826
96
Y = -3158801
04 feet Y = -1035073
64 meter
Z = -5860400
49 Z = -1817644
33
XDOT = -2599
621558 XDOT = -762
538908
YDOT = -16790
536393 feet/sec YDOT = -5126
449903 meter/sec
ZDOT = 18547
751486 ZDOT = 5649
577653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5251664
40 X = 1600707
31
Y = 20778506
94 feet Y = 6333288
91 meter
Z = -5997184
89 Z = -1827941
96
XDOT = -12929
780456 XDOT = -3940
997083
YDOT = 8594
931849 feet/sec YDOT = 2619
735228 meter/sec
ZDOT = 18532
120389 ZDOT = 5648
590294
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 16212
46192636
00016717 00000-0 10270-3 0 9185
2 25544 51
6397 202
1163 0001996 89
4208 270
7173 15
54961094 11715
Satellite: ISS
Catalog Number: 25544
Epoch time: 16212
46192636 = yrday
fracday
Element set: 918
Inclination: 51
6397 deg
RA of node: 202
1163 deg
Eccentricity:
0001996
Arg of perigee: 89
4208 deg
Mean anomaly: 270
7173 deg
Mean motion: 15
54961094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 314
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