[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 30th 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) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 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
183/05:36:30
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
6
183/06:10:00
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
6
185/03:48:30
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
5
187/04:12:00
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
5
189/01:36:40
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
4
191/04:10:57
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
3
194/19:00:00
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
1
Coasting Arc #1 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2016/181/12:10:42
455
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5197538
91 A = 6783343
48 meter
Y = 2922922
09 meter E =
0012803
Z = 3222667
25 I = 51
62462
XDOT = -4912
171417 Wp = 89
24251
YDOT = -3448
425810 meter/sec RA = 355
98683 deg
ZDOT = -4778
123354 TA = 53
42277
MA = 53
30502
Ha = 220
185 n
mi
Hp = 213
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17052293
02 X = -5245491
84
Y = 9589639
39 feet Y = 2864531
31 meter
Z = 10573055
27 Z = 3197302
64
XDOT = -16116
047956 XDOT = -4850
035045
YDOT = -11313
732971 feet/sec YDOT = -3503
009101 meter/sec
ZDOT = -15676
257723 ZDOT = -4801
834928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12373344
82 X = 3771395
50
Y = 15230887
01 feet Y = 4642374
36 meter
Z = 10461921
30 Z = 3188793
61
XDOT = -7303
551878 XDOT = -2226
122612
YDOT = 16809
354055 feet/sec YDOT = 5123
491116 meter/sec
ZDOT = -15778
841040 ZDOT = -4809
390749
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 16181
54619483
00016717 00000-0 10270-3 0 9004
2 25544 51
6405 356
3775 0000914 359
2245
8906 15
54703614 6907
Satellite: ISS
Catalog Number: 25544
Epoch time: 16181
54619483 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 356
3775 deg
Eccentricity:
0000914
Arg of perigee: 359
2245 deg
Mean anomaly:
8906 deg
Mean motion: 15
54703614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 305
Coasting Arc #2 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2016/182/12:10:42
455
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6219436
37 A = 6786693
48 meter
Y = -2223289
99 meter E =
0009101
Z = -1544016
82 I = 51
60373
XDOT = 2907
123364 Wp = 35
83589
YDOT = 4154
828378 meter/sec RA = 351
00552 deg
ZDOT = 5751
830593 TA = 307
27947
MA = 307
36241
Ha = 220
274 n
mi
Hp = 213
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20404974
96 X = 6251335
70
Y = -7294258
50 feet Y = -2153561
57 meter
Z = -5065671
98 Z = -1513727
03
XDOT = 9537
806313 XDOT = 2832
506971
YDOT = 13631
326701 feet/sec YDOT = 4186
919904 meter/sec
ZDOT = 18870
835280 ZDOT = 5765
771957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11001001
98 X = -3353105
40
Y = -18704850
24 feet Y = -5701238
35 meter
Z = -4933231
75 Z = -1503649
04
XDOT = 10259
548937 XDOT = 3127
110516
YDOT = -11005
147911 feet/sec YDOT = -3354
369083 meter/sec
ZDOT = 18930
695557 ZDOT = 5770
076006
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 16182
51037155
00016717 00000-0 10270-3 0 9013
2 25544 51
6403 351
5669 0000848 23
2590 336
8601 15
54703978 7055
Satellite: ISS
Catalog Number: 25544
Epoch time: 16182
51037155 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 351
5669 deg
Eccentricity:
0000848
Arg of perigee: 23
2590 deg
Mean anomaly: 336
8601 deg
Mean motion: 15
54703978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 302
Coasting Arc #3 (Orbit 716)
---------------------------------------
Vector Time (GMT): 2016/183/05:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 840380
06 A = 6775547
61 meter
Y = 4128235
91 meter E =
0002950
Z = 5304334
62 I = 51
54716
XDOT = -7498
863484 Wp = 60
92347
YDOT = 1619
100559 meter/sec RA = 347
39738 deg
ZDOT = -70
607817 TA = 29
75828
MA = 29
74151
Ha = 220
116 n
mi
Hp = 213
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2757152
42 X = 768388
41
Y = 13544081
06 feet Y = 4137230
39 meter
Z = 17402672
62 Z = 5308242
65
XDOT = -24602
570487 XDOT = -7516
068359
YDOT = 5312
009708 feet/sec YDOT = 1535
147082 meter/sec
ZDOT = -231
652944 ZDOT = -107
077073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3345926
67 X = 1019838
45
Y = 13389786
91 feet Y = 4081207
05 meter
Z = 17418823
63 Z = 5309257
44
XDOT = -23314
505128 XDOT = -7106
261163
YDOT = 6340
598158 feet/sec YDOT = 1932
614318 meter/sec
ZDOT = -390
885236 ZDOT = -119
141820
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 16183
28170753
00016717 00000-0 10270-3 0 9021
2 25544 51
6435 347
7236 0001185 8
7515 351
3659 15
54747244 7179
Satellite: ISS
Catalog Number: 25544
Epoch time: 16183
28170753 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 347
7236 deg
Eccentricity:
0001185
Arg of perigee: 8
7515 deg
Mean anomaly: 351
3659 deg
Mean motion: 15
54747244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 717
Checksum: 314
Coasting Arc #4 (Orbit 716)
---------------------------------------
Vector Time (GMT): 2016/183/06:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5602889
44 A = 6782386
47 meter
Y = -1575411
21 meter E =
0005486
Z = -3488481
55 I = 51
56953
XDOT = 4114
505104 Wp = 72
53723
YDOT = -4611
210372 meter/sec RA = 347
30765 deg
ZDOT = -4530
190060 TA = 148
47939
MA = 148
44652
Ha = 220
168 n
mi
Hp = 213
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18382183
19 X = -5567910
80
Y = -5168671
96 feet Y = -1637870
43 meter
Z = -11445149
45 Z = -3515614
28
XDOT = 13499
032494 XDOT = 4187
768766
YDOT = -15128
642953 feet/sec YDOT = -4564
789012 meter/sec
ZDOT = -14862
828282 ZDOT = -4510
025428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18968095
82 X = -5781475
61
Y = -1455686
72 feet Y = -443693
31 meter
Z = -11563026
93 Z = -3524410
61
XDOT = 10235
841899 XDOT = 3119
884611
YDOT = -16131
834829 feet/sec YDOT = -4916
983256 meter/sec
ZDOT = -14773
997218 ZDOT = -4503
114352
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 16183
28170824
00016717 00000-0 10270-3 0 9031
2 25544 51
6440 347
7240 0001186 6
2135 353
9032 15
54705223 7176
Satellite: ISS
Catalog Number: 25544
Epoch time: 16183
28170824 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 347
7240 deg
Eccentricity:
0001186
Arg of perigee: 6
2135 deg
Mean anomaly: 353
9032 deg
Mean motion: 15
54705223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 717
Checksum: 281
Coasting Arc #5 (Orbit 732)
---------------------------------------
Vector Time (GMT): 2016/184/06:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4194664
54 A = 6778274
90 meter
Y = 2554440
09 meter E =
0007795
Z = 4666297
34 I = 51
52514
XDOT = -5744
402349 Wp = 107
02196
YDOT = 4211
575737 meter/sec RA = 342
30772 deg
ZDOT = 2852
109336 TA = 314
59905
MA = 314
66262
Ha = 220
136 n
mi
Hp = 213
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13762022
78 X = 4143121
57
Y = 8380708
97 feet Y = 2601058
77 meter
Z = 15309374
46 Z = 4686549
11
XDOT = -18846
464399 XDOT = -5804
924607
YDOT = 13817
505698 feet/sec YDOT = 4146
999198 meter/sec
ZDOT = 9357
314095 ZDOT = 2824
058100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15141018
44 X = 4614982
42
Y = 5261793
70 feet Y = 1603794
72 meter
Z = 15397064
27 Z = 4693025
19
XDOT = -15124
949092 XDOT = -4610
084483
YDOT = 16442
503429 feet/sec YDOT = 5011
675045 meter/sec
ZDOT = 9234
209627 ZDOT = 2814
587094
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 16184
31015255
00016717 00000-0 10270-3 0 9043
2 25544 51
6445 342
5924 0001262 14
5468 345
5721 15
54711285 7334
Satellite: ISS
Catalog Number: 25544
Epoch time: 16184
31015255 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 342
5924 deg
Eccentricity:
0001262
Arg of perigee: 14
5468 deg
Mean anomaly: 345
5721 deg
Mean motion: 15
54711285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 733
Checksum: 291
Coasting Arc #6 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2016/185/03:48:30
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3450987
08 A = 6776602
60 meter
Y = 2924603
37 meter E =
0005160
Z = 5042107
45 I = 51
49115
XDOT = -6201
267895 Wp = 110
94186
YDOT = 4121
653479 meter/sec RA = 337
79406 deg
ZDOT = 1850
308903 TA = 321
08951
MA = 321
12663
Ha = 220
078 n
mi
Hp = 213
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11322136
10 X = 3393534
70
Y = 9595155
40 feet Y = 2962872
62 meter
Z = 16542347
28 Z = 5058732
28
XDOT = -20345
367110 XDOT = -6255
884322
YDOT = 13522
485167 feet/sec YDOT = 4052
001118 meter/sec
ZDOT = 6070
567266 ZDOT = 1820
052809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6775921
49 X = 2065300
87
Y = 13113491
86 feet Y = 3996992
32 meter
Z = 16614157
99 Z = 5063995
36
XDOT = -23019
662300 XDOT = -7016
393069
YDOT = 4357
751898 feet/sec YDOT = 1328
242778 meter/sec
ZDOT = 5937
878023 ZDOT = 1809
865221
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 16185
21003432
00016717 00000-0 10270-3 0 9058
2 25544 51
6432 338
1018 0001252 15
4725 344
6466 15
54756370 7475
Satellite: ISS
Catalog Number: 25544
Epoch time: 16185
21003432 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 338
1018 deg
Eccentricity:
0001252
Arg of perigee: 15
4725 deg
Mean anomaly: 344
6466 deg
Mean motion: 15
54756370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 287
Coasting Arc #7 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2016/186/03:48:30
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1636138
35 A = 6775593
13 meter
Y = -3907453
32 meter E =
0015335
Z = -5301298
82 I = 51
45864
XDOT = 6909
081386 Wp = 87
25822
YDOT = -3290
512493 meter/sec RA = 332
77692 deg
ZDOT = 294
462126 TA = 185
55100
MA = 185
56801
Ha = 220
264 n
mi
Hp = 213
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5367907
97 X = -1566571
47
Y = -12819728
75 feet Y = -3925359
97 meter
Z = -17392712
66 Z = -5309078
29
XDOT = 22667
589849 XDOT = 6943
932873
YDOT = -10795
644663 feet/sec YDOT = -3213
055719 meter/sec
ZDOT = 966
083090 ZDOT = 328
108543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -279068
96 X = -85060
22
Y = -13853900
69 feet Y = -4222668
93 meter
Z = -17425782
36 Z = -5311378
46
XDOT = 24018
833467 XDOT = 7320
940441
YDOT = -1878
247181 feet/sec YDOT = -572
489741 meter/sec
ZDOT = 1113
364337 ZDOT = 339
353450
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 16186
17419080
00016717 00000-0 10270-3 0 9065
2 25544 51
6437 333
2914 0001398 21
6107 338
5105 15
54747387 7622
Satellite: ISS
Catalog Number: 25544
Epoch time: 16186
17419080 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 333
2914 deg
Eccentricity:
0001398
Arg of perigee: 21
6107 deg
Mean anomaly: 338
5105 deg
Mean motion: 15
54747387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 311
Coasting Arc #8 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2016/187/03:48:30
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -239993
63 A = 6777472
27 meter
Y = 4723439
34 meter E =
0008135
Z = 4850697
67 I = 51
43690
XDOT = -6967
538870 Wp = 52
79820
YDOT = 2125
714639 meter/sec RA = 327
75987 deg
ZDOT = -2407
059730 TA = 60
89892
MA = 60
81750
Ha = 220
209 n
mi
Hp = 213
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -787380
67 X = -316356
74
Y = 15496848
22 feet Y = 4720327
94 meter
Z = 15914362
42 Z = 4849347
02
XDOT = -22859
379494 XDOT = -6979
099015
YDOT = 6974
129394 feet/sec YDOT = 2047
734668 meter/sec
ZDOT = -7897
177592 ZDOT = -2440
933600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6174302
46 X = -1881927
39
Y = 14243208
05 feet Y = 4341329
81 meter
Z = 15907489
36 Z = 4848602
76
XDOT = -22775
516641 XDOT = -6941
977472
YDOT = -859
810519 feet/sec YDOT = -262
070246 meter/sec
ZDOT = -8045
201446 ZDOT = -2452
177401
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 16187
20261743
00016717 00000-0 10270-3 0 9072
2 25544 51
6437 328
1610 0001394 18
2129 341
9074 15
54770747 7786
Satellite: ISS
Catalog Number: 25544
Epoch time: 16187
20261743 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 328
1610 deg
Eccentricity:
0001394
Arg of perigee: 18
2129 deg
Mean anomaly: 341
9074 deg
Mean motion: 15
54770747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 312
Coasting Arc #9 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2016/187/04:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6151939
56 A = 6785362
09 meter
Y = 1764409
11 meter E =
0005397
Z = -2252553
05 I = 51
46346
XDOT = 437
295030 Wp = 123
93267
YDOT = -5392
146588 meter/sec RA = 327
71686 deg
ZDOT = -5430
237364 TA = 81
18241
MA = 81
12131
Ha = 220
205 n
mi
Hp = 213
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20183528
75 X = -6160270
63
Y = 5788743
79 feet Y = 1695567
74 meter
Z = -7390265
91 Z = -2282457
20
XDOT = 1434
694980 XDOT = 523
936240
YDOT = -17690
769647 feet/sec YDOT = -5386
771286 meter/sec
ZDOT = -17815
739382 ZDOT = -5427
903419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20940702
81 X = -6382726
22
Y = 650505
80 feet Y = 198274
17 meter
Z = -7520919
20 Z = -2292376
17
XDOT = 5906
887179 XDOT = 1800
419212
YDOT = -15238
745817 feet/sec YDOT = -4644
769725 meter/sec
ZDOT = -17804
442391 ZDOT = -5426
794041
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 16187
20261781
00016717 00000-0 10270-3 0 9085
2 25544 51
6445 328
1610 0001206 16
9947 343
1241 15
54725258 7787
Satellite: ISS
Catalog Number: 25544
Epoch time: 16187
20261781 = yrday
fracday
Element set: 908
Inclination: 51
6445 deg
RA of node: 328
1610 deg
Eccentricity:
0001206
Arg of perigee: 16
9947 deg
Mean anomaly: 343
1241 deg
Mean motion: 15
54725258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 306
Coasting Arc #10 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2016/188/04:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5592677
29 A = 6781280
83 meter
Y = -449939
01 meter E =
0011853
Z = 3798410
51 I = 51
42385
XDOT = -2363
348147 Wp = 90
63263
YDOT = 5986
810620 meter/sec RA = 322
71868 deg
ZDOT = 4177
468839 TA = 315
18178
MA = 315
27746
Ha = 220
176 n
mi
Hp = 213
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18348678
77 X = 5578842
23
Y = -1476177
85 feet Y = -387475
77 meter
Z = 12461976
74 Z = 3825544
23
XDOT = -7753
766888 XDOT = -2450
410522
YDOT = 19641
767127 feet/sec YDOT = 5959
894794 meter/sec
ZDOT = 13705
606427 ZDOT = 4165
777729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18118537
38 X = 5522530
19
Y = 2758451
15 feet Y = 840775
91 meter
Z = 12580283
32 Z = 3834470
36
XDOT = -11941
211873 XDOT = -3639
681379
YDOT = 15996
699496 feet/sec YDOT = 4875
794006 meter/sec
ZDOT = 13653
429275 ZDOT = 4161
565243
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 16188
23103739
00016717 00000-0 10270-3 0 9098
2 25544 51
6450 323
0294 0001474 23
5789 336
5432 15
54748990 7944
Satellite: ISS
Catalog Number: 25544
Epoch time: 16188
23103739 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 323
0294 deg
Eccentricity:
0001474
Arg of perigee: 23
5789 deg
Mean anomaly: 336
5432 deg
Mean motion: 15
54748990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 794
Checksum: 326
Coasting Arc #11 (Orbit 807)
---------------------------------------
Vector Time (GMT): 2016/189/01:36:40
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5175076
10 A = 6787472
57 meter
Y = -4374939
87 meter E =
0014028
Z = 231186
88 I = 51
41955
XDOT = 2928
583537 Wp = 45
33007
YDOT = 3792
098581 meter/sec RA = 318
22976 deg
ZDOT = 5990
857938 TA = 317
16972
MA = 317
27892
Ha = 220
313 n
mi
Hp = 213
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16978596
14 X = 5222490
18
Y = -14353477
26 feet Y = -4316803
63 meter
Z = 758487
12 Z = 256440
38
XDOT = 9608
213705 XDOT = 2856
861187
YDOT = 12441
268310 feet/sec YDOT = 3824
446328 meter/sec
ZDOT = 19655
045727 ZDOT = 6004
910195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21819731
46 X = 6650654
15
Y = 4244265
39 feet Y = 1293652
09 meter
Z = 869407
63 Z = 264995
45
XDOT = -3454
061132 XDOT = -1052
797833
YDOT = 13593
049614 feet/sec YDOT = 4143
161522 meter/sec
ZDOT = 19715
485728 ZDOT = 6009
280050
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 16189
13089861
00016717 00000-0 10270-3 0 9109
2 25544 51
6425 318
5393 0001534 26
2155 333
9076 15
54758302 8088
Satellite: ISS
Catalog Number: 25544
Epoch time: 16189
13089861 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 318
5393 deg
Eccentricity:
0001534
Arg of perigee: 26
2155 deg
Mean anomaly: 333
9076 deg
Mean motion: 15
54758302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 808
Checksum: 311
Coasting Arc #12 (Orbit 822)
---------------------------------------
Vector Time (GMT): 2016/190/01:36:40
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5494173
28 A = 6785461
72 meter
Y = 3366966
66 meter E =
0005913
Z = -2123749
47 I = 51
39070
XDOT = -1092
871342 Wp = 123
92366
YDOT = -5236
966794 meter/sec RA = 313
23965 deg
ZDOT = -5489
591700 TA = 79
69059
MA = 79
62394
Ha = 220
262 n
mi
Hp = 213
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18025502
90 X = -5521099
13
Y = 11046478
55 feet Y = 3305376
77 meter
Z = -6967681
98 Z = -2150503
47
XDOT = -3585
535899 XDOT = -1007
563417
YDOT = -17181
649588 feet/sec YDOT = -5248
710584 meter/sec
ZDOT = -18010
471458 ZDOT = -5494
693729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19990741
90 X = -6093178
13
Y = -6757673
12 feet Y = -2059738
77 meter
Z = -7084922
57 Z = -2159484
40
XDOT = 10498
031390 XDOT = 3199
799968
YDOT = -12198
921569 feet/sec YDOT = -3718
231294 meter/sec
ZDOT = -18031
631516 ZDOT = -5496
041286
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 16190
09502938
00016717 00000-0 10270-3 0 9112
2 25544 51
6435 313
7293 0001489 27
8260 332
2972 15
54777203 8233
Satellite: ISS
Catalog Number: 25544
Epoch time: 16190
09502938 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 313
7293 deg
Eccentricity:
0001489
Arg of perigee: 27
8260 deg
Mean anomaly: 332
2972 deg
Mean motion: 15
54777203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 823
Checksum: 309
Coasting Arc #13 (Orbit 838)
---------------------------------------
Vector Time (GMT): 2016/191/01:36:40
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5321189
14 A = 6781480
31 meter
Y = -1967617
76 meter E =
0012363
Z = 3704225
20 I = 51
35598
XDOT = -641
626151 Wp = 89
29775
YDOT = 6338
811220 meter/sec RA = 308
23784 deg
ZDOT = 4276
538612 TA = 315
12694
MA = 315
22682
Ha = 220
191 n
mi
Hp = 213
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17457969
62 X = 5324802
80
Y = -6455438
85 feet Y = -1908092
71 meter
Z = 12152969
80 Z = 3730082
47
XDOT = -2105
072675 XDOT = -733
233918
YDOT = 20796
624736 feet/sec YDOT = 6331
123639 meter/sec
ZDOT = 14030
638491 ZDOT = 4273
199713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16233098
85 X = 4947848
53
Y = 8954302
44 feet Y = 2729271
38 meter
Z = 12266011
52 Z = 3738680
31
XDOT = -16537
173308 XDOT = -5040
530424
YDOT = 10727
355865 feet/sec YDOT = 3269
698068 meter/sec
ZDOT = 14014
814174 ZDOT = 4271
715360
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 16191
12342810
00016717 00000-0 10270-3 0 9129
2 25544 51
6433 308
5981 0001533 31
1482 328
9762 15
54786483 8397
Satellite: ISS
Catalog Number: 25544
Epoch time: 16191
12342810 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 308
5981 deg
Eccentricity:
0001533
Arg of perigee: 31
1482 deg
Mean anomaly: 328
9762 deg
Mean motion: 15
54786483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 839
Checksum: 310
Coasting Arc #14 (Orbit 839)
---------------------------------------
Vector Time (GMT): 2016/191/04:10:57
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2204987
56 A = 6776160
77 meter
Y = -3858115
36 meter E =
0014061
Z = -5128048
50 I = 51
33711
XDOT = 5482
706778 Wp = 95
38301
YDOT = -5131
658627 meter/sec RA = 307
66342 deg
ZDOT = 1505
623859 TA = 189
18566
MA = 189
21141
Ha = 220
209 n
mi
Hp = 213
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7234211
14 X = -2136771
78
Y = -12657858
80 feet Y = -3882391
26 meter
Z = -16824306
12 Z = -5138594
19
XDOT = 17987
883131 XDOT = 5532
369228
YDOT = -16836
150352 feet/sec YDOT = -5070
069760 meter/sec
ZDOT = 4939
710823 ZDOT = 1532
377381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4680165
80 X = -1426514
54
Y = -13752436
54 feet Y = -4191742
66 meter
Z = -16869469
87 Z = -5141814
42
XDOT = 19738
481396 XDOT = 6016
289130
YDOT = -12911
711404 feet/sec YDOT = -3935
489636 meter/sec
ZDOT = 5057
293710 ZDOT = 1541
463123
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 16191
18770112
00016717 00000-0 10270-3 0 9136
2 25544 51
6443 308
2781 0001508 24
5036 335
6189 15
54808814 8409
Satellite: ISS
Catalog Number: 25544
Epoch time: 16191
18770112 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 308
2781 deg
Eccentricity:
0001508
Arg of perigee: 24
5036 deg
Mean anomaly: 335
6189 deg
Mean motion: 15
54808814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 840
Checksum: 299
Coasting Arc #15 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2016/192/04:10:57
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 761444
54 A = 6779383
34 meter
Y = 5184603
75 meter E =
0010963
Z = 4295288
55 I = 51
32873
XDOT = -5715
512882 Wp = 65
82297
YDOT = 3741
784680 meter/sec RA = 302
64123 deg
ZDOT = -3491
815384 TA = 59
88947
MA = 59
78084
Ha = 220
162 n
mi
Hp = 213
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2498177
63 X = 682548
00
Y = 17009854
82 feet Y = 5192677
35 meter
Z = 14092154
02 Z = 4298796
08
XDOT = -18751
682684 XDOT = -5739
968143
YDOT = 12276
196457 feet/sec YDOT = 3677
733465 meter/sec
ZDOT = -11456
087217 ZDOT = -3519
638767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -461526
73 X = -140673
35
Y = 17174439
08 feet Y = 5234769
03 meter
Z = 14106399
00 Z = 4299630
41
XDOT = -19209
485409 XDOT = -5855
051153
YDOT = 9024
405484 feet/sec YDOT = 2750
638792 meter/sec
ZDOT = -11578
040130 ZDOT = -3528
986632
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 16192
21609034
00016717 00000-0 10270-3 0 9146
2 25544 51
6437 303
1466 0001642 24
3996 335
7234 15
54848576 8566
Satellite: ISS
Catalog Number: 25544
Epoch time: 16192
21609034 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 303
1466 deg
Eccentricity:
0001642
Arg of perigee: 24
3996 deg
Mean anomaly: 335
7234 deg
Mean motion: 15
54848576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 316
Coasting Arc #16 (Orbit 870)
---------------------------------------
Vector Time (GMT): 2016/193/04:10:57
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 558422
07 A = 6783751
77 meter
Y = -6099513
66 meter E =
0005893
Z = -2915927
40 I = 51
32526
XDOT = 5499
612737 Wp = 55
83077
YDOT = -1880
648979 meter/sec RA = 297
63019 deg
ZDOT = 4997
651622 TA = 270
76221
MA = 270
82973
Ha = 220
248 n
mi
Hp = 213
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1832093
41 X = 640751
05
Y = -20011527
74 feet Y = -6092808
51 meter
Z = -9566690
94 Z = -2913015
13
XDOT = 18043
348874 XDOT = 5495
957675
YDOT = -6170
108198 feet/sec YDOT = -1819
169363 meter/sec
ZDOT = 16396
494824 ZDOT = 5024
358132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4867757
57 X = 1483692
51
Y = -19503547
61 feet Y = -5944681
31 meter
Z = -9552798
10 Z = -2911692
86
XDOT = 17236
115955 XDOT = 5253
568143
YDOT = -3769
379378 feet/sec YDOT = -1148
906834 meter/sec
ZDOT = 16513
204719 ZDOT = 5033
224798
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 16193
18020154
00016717 00000-0 10270-3 0 9154
2 25544 51
6426 298
3359 0001543 28
0173 332
1063 15
54808774 8712
Satellite: ISS
Catalog Number: 25544
Epoch time: 16193
18020154 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 298
3359 deg
Eccentricity:
0001543
Arg of perigee: 28
0173 deg
Mean anomaly: 332
1063 deg
Mean motion: 15
54808774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 871
Checksum: 300
Coasting Arc #17 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2016/194/04:10:57
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1730566
73 A = 6786821
74 meter
Y = 6461738
98 meter E =
0013738
Z = 1110562
76 I = 51
32218
XDOT = -4947
167811 Wp = 116
28077
YDOT = -310
284420 meter/sec RA = 292
63010 deg
ZDOT = -5853
311260 TA = 51
60935
MA = 51
48604
Ha = 220
280 n
mi
Hp = 213
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5677712
36 X = -1808089
50
Y = 21199931
03 feet Y = 6441953
10 meter
Z = 3643578
62 Z = 1101968
27
XDOT = -16230
865523 XDOT = -4914
897786
YDOT = -1017
993504 feet/sec YDOT = -365
426155 meter/sec
ZDOT = -19203
777100 ZDOT = -5877
264837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8462770
85 X = -2579452
55
Y = 20256741
13 feet Y = 6174254
70 meter
Z = 3604872
66 Z = 1098765
19
XDOT = -14351
829820 XDOT = -4374
437729
YDOT = -2530
062748 feet/sec YDOT = -771
163126 meter/sec
ZDOT = -19308
060318 ZDOT = -5885
096785
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 16194
20857899
00016717 00000-0 10270-3 0 9163
2 25544 51
6433 293
2042 0001571 33
2879 326
8372 15
54815827 8872
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
20857899 = yrday
fracday
Element set: 916
Inclination: 51
6433 deg
RA of node: 293
2042 deg
Eccentricity:
0001571
Arg of perigee: 33
2879 deg
Mean anomaly: 326
8372 deg
Mean motion: 15
54815827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 339
Coasting Arc #18 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2016/194/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3780436
60 A = 6784903
00 meter
Y = -5132966
56 meter E =
0015162
Z = 2301273
35 I = 51
30601
XDOT = 2947
457204 Wp = 70
06136
YDOT = 4597
863457 meter/sec RA = 289
56485 deg
ZDOT = 5389
633313 TA = 315
72629
MA = 315
84748
Ha = 220
213 n
mi
Hp = 213
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12403007
20 X = 3826375
22
Y = -16840441
47 feet Y = -5090434
49 meter
Z = 7550109
43 Z = 2319748
90
XDOT = 9670
135184 XDOT = 2869
643316
YDOT = 15084
853862 feet/sec YDOT = 4630
388447 meter/sec
ZDOT = 17682
523993 ZDOT = 5403
762547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -370277
38 X = -112860
55
Y = 20882071
30 feet Y = 6364855
33 meter
Z = 7631592
37 Z = 2326109
35
XDOT = -14987
863804 XDOT = -4568
300888
YDOT = -6778
551448 feet/sec YDOT = -2066
102481 meter/sec
ZDOT = 17743
174681 ZDOT = 5408
119643
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 16194
85130932
00016717 00000-0 10270-3 0 9177
2 25544 51
6404 289
9965 0001492 45
3037 314
8238 15
54862732 8974
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
85130932 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 289
9965 deg
Eccentricity:
0001492
Arg of perigee: 45
3037 deg
Mean anomaly: 314
8238 deg
Mean motion: 15
54862732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 335
Coasting Arc #19 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2016/195/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4170450
19 A = 6780837
19 meter
Y = 3689569
91 meter E =
0008068
Z = -3878577
99 I = 51
28147
XDOT = -1748
267065 Wp = 68
29327
YDOT = -6250
748581 meter/sec RA = 284
55497 deg
ZDOT = -4070
225685 TA = 158
80786
MA = 158
77442
Ha = 220
388 n
mi
Hp = 213
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13682579
36 X = -4192557
56
Y = 12104888
17 feet Y = 3642809
84 meter
Z = -12724993
41 Z = -3898890
31
XDOT = -5735
784335 XDOT = -1658
468380
YDOT = -20507
705319 feet/sec YDOT = -6269
796463 meter/sec
ZDOT = -13353
758808 ZDOT = -4078
500659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3815586
69 X = 1162990
82
Y = -17801813
56 feet Y = -5425992
77 meter
Z = -12814190
75 Z = -3905765
34
XDOT = 15381
387767 XDOT = 4688
246991
YDOT = 12925
070332 feet/sec YDOT = 3939
561437 meter/sec
ZDOT = -13388
595103 ZDOT = -4080
843788
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 16195
81540470
00016717 00000-0 10270-3 0 9187
2 25544 51
6397 285
1849 0001721 46
7144 313
4153 15
54826048 9122
Satellite: ISS
Catalog Number: 25544
Epoch time: 16195
81540470 = yrday
fracday
Element set: 918
Inclination: 51
6397 deg
RA of node: 285
1849 deg
Eccentricity:
0001721
Arg of perigee: 46
7144 deg
Mean anomaly: 313
4153 deg
Mean motion: 15
54826048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 313
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