[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 19th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 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
201/08:38:00
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
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 994)
---------------------------------------
Vector Time (GMT): 2016/201/03:19:58
807
Vector Time (MET): N/A
Weight (LBS) : 894430
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4362517
68 A = 6777552
38 meter
Y = -2095196
07 meter E =
0012349
Z = -4756466
39 I = 51
26421
XDOT = 588
464360 Wp = 102
06910
YDOT = -7172
502232 meter/sec RA = 257
69021 deg
ZDOT = 2622
978520 TA = 193
95401
MA = 193
98816
Ha = 220
383 n
mi
Hp = 212
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14312722
05 X = -4315659
96
Y = -6874002
86 feet Y = -2143718
16 meter
Z = -15605204
69 Z = -4777544
48
XDOT = 1930
657348 XDOT = 655
884261
YDOT = -23531
831471 feet/sec YDOT = -7165
544940 meter/sec
ZDOT = 8605
572572 ZDOT = 2626
000083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12213878
39 X = -3722790
13
Y = -10003209
78 feet Y = -3048978
34 meter
Z = -15696665
57 Z = -4784343
67
XDOT = 6587
125121 XDOT = 2007
755737
YDOT = -21552
451652 feet/sec YDOT = -6569
187263 meter/sec
ZDOT = 8620
057283 ZDOT = 2627
393460
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
15032813
00016717 00000-0 10270-3 0 9000
2 25544 51
6393 258
5643 0001704 53
3338 306
7972 15
54845570 9950
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
15032813 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 258
5643 deg
Eccentricity:
0001704
Arg of perigee: 53
3338 deg
Mean anomaly: 306
7972 deg
Mean motion: 15
54845570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 995
Checksum: 304
Coasting Arc #2 (Orbit 998)
---------------------------------------
Vector Time (GMT): 2016/201/08:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 909574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4201386
91 A = 6775194
64 meter
Y = -625315
03 meter E =
0004038
Z = 5275070
47 I = 51
26172
XDOT = 1524
449438 Wp = 70
50413
YDOT = 7513
228665 meter/sec RA = 256
59923 deg
ZDOT = -322
007018 TA = 22
58884
MA = 22
57107
Ha = 220
174 n
mi
Hp = 212
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13784077
79 X = 4182443
51
Y = -2051558
50 feet Y = -578438
78 meter
Z = 17306661
63 Z = 5295433
33
XDOT = 5001
474534 XDOT = 1441
885467
YDOT = 24649
700344 feet/sec YDOT = 7529
814466 meter/sec
ZDOT = -1056
453472 ZDOT = -314
801513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3636477
74 X = 1108398
42
Y = -13338012
61 feet Y = -4065426
24 meter
Z = 17395507
44 Z = 5302150
67
XDOT = 23603
891736 XDOT = 7194
466201
YDOT = 5090
187166 feet/sec YDOT = 1551
489048 meter/sec
ZDOT = -1026
432689 ZDOT = -312
856684
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
40741780
00016717 00000-0 10270-3 0 9019
2 25544 51
6429 257
2805 0001521 61
6693 298
4613 15
54877878 9998
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
40741780 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 257
2805 deg
Eccentricity:
0001521
Arg of perigee: 61
6693 deg
Mean anomaly: 298
4613 deg
Mean motion: 15
54877878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 999
Checksum: 331
Coasting Arc #3 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2016/202/08:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 909574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4553009
67 A = 6777178
81 meter
Y = -1419112
66 meter E =
0013032
Z = -4827416
06 I = 51
27599
XDOT = -340
664906 Wp = 103
21053
YDOT = -7247
363958 meter/sec RA = 251
56938 deg
ZDOT = 2454
490983 TA = 191
02751
MA = 191
05611
Ha = 220
369 n
mi
Hp = 212
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14937695
77 X = -4513353
36
Y = -4655881
42 feet Y = -1469805
29 meter
Z = -15837979
20 Z = -4849436
82
XDOT = -1117
667015 XDOT = -271
520361
YDOT = -23777
440806 feet/sec YDOT = -7250
787105 meter/sec
ZDOT = 8052
791938 ZDOT = 2453
003455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10040641
34 X = -3060387
48
Y = 11872520
28 feet Y = 3618744
18 meter
Z = -15933686
18 Z = -4856587
55
XDOT = -21507
482149 XDOT = -6555
480559
YDOT = -7400
307713 feet/sec YDOT = -2255
613791 meter/sec
ZDOT = 8047
619748 ZDOT = 2452
914499
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
37150387
00016717 00000-0 10270-3 0 9024
2 25544 51
6422 252
4712 0001604 67
9368 292
1955 15
54873168 10142
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
37150387 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 252
4712 deg
Eccentricity:
0001604
Arg of perigee: 67
9368 deg
Mean anomaly: 292
1955 deg
Mean motion: 15
54873168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 300
Coasting Arc #4 (Orbit 1015)
---------------------------------------
Vector Time (GMT): 2016/202/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4527102
34 A = 6779398
01 meter
Y = 2729270
23 meter E =
0011438
Z = 4237578
43 I = 51
28399
XDOT = -713
688983 Wp = 71
20093
YDOT = 6751
712072 meter/sec RA = 251
07054 deg
ZDOT = -3574
523739 TA = 55
51348
MA = 55
40549
Ha = 220
203 n
mi
Hp = 212
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14852697
98 X = 4475662
57
Y = 8954298
66 feet Y = 2779607
33 meter
Z = 13902816
37 Z = 4259444
82
XDOT = -2341
499287 XDOT = -771
772136
YDOT = 22151
286324 feet/sec YDOT = 6743
406670 meter/sec
ZDOT = -11727
440089 ZDOT = -3578
131087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5460951
63 X = 1664498
06
Y = -16380329
02 feet Y = -4992724
29 meter
Z = 13997615
27 Z = 4266473
13
XDOT = 20906
997639 XDOT = 6372
452880
YDOT = -3098
131183 feet/sec YDOT = -944
310384 meter/sec
ZDOT = -11744
379468 ZDOT = -3579
686862
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
50004680
00016717 00000-0 10270-3 0 9034
2 25544 51
6417 251
8308 0001562 57
3349 302
7955 15
54884451 10162
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
50004680 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 251
8308 deg
Eccentricity:
0001562
Arg of perigee: 57
3349 deg
Mean anomaly: 302
7955 deg
Mean motion: 15
54884451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1016
Checksum: 290
Coasting Arc #5 (Orbit 1030)
---------------------------------------
Vector Time (GMT): 2016/203/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4396206
17 A = 6783729
90 meter
Y = -4326713
63 meter E =
0006271
Z = -2824423
87 I = 51
30856
XDOT = 2048
226940 Wp = 63
22730
YDOT = -5378
376073 meter/sec RA = 246
05786 deg
ZDOT = 5062
528848 TA = 264
53753
MA = 264
60907
Ha = 220
354 n
mi
Hp = 212
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14423248
59 X = -4333777
49
Y = -14195254
71 feet Y = -4375525
70 meter
Z = -9266482
53 Z = -2845627
76
XDOT = 6719
904658 XDOT = 2083
626004
YDOT = -17645
590790 feet/sec YDOT = -5355
273847 meter/sec
ZDOT = 16609
346615 ZDOT = 5072
564028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10363064
26 X = -3158661
99
Y = 17333074
04 feet Y = 5283120
97 meter
Z = -9358124
71 Z = -2852356
41
XDOT = -17447
731472 XDOT = -5318
068553
YDOT = -1460
260584 feet/sec YDOT = -445
087426 meter/sec
ZDOT = 16654
039390 ZDOT = 5076
151206
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
46412868
00016717 00000-0 10270-3 0 9042
2 25544 51
6406 247
0201 0001621 64
9371 295
1950 15
54866194 10315
Satellite: ISS
Catalog Number: 25544
Epoch time: 16203
46412868 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 247
0201 deg
Eccentricity:
0001621
Arg of perigee: 64
9371 deg
Mean anomaly: 295
1950 deg
Mean motion: 15
54866194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1031
Checksum: 291
Coasting Arc #6 (Orbit 1046)
---------------------------------------
Vector Time (GMT): 2016/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3915959
97 A = 6786679
40 meter
Y = 5446374
29 meter E =
0014545
Z = 988757
30 I = 51
33311
XDOT = -3421
908439 Wp = 117
81964
YDOT = 3539
154977 meter/sec RA = 241
05750 deg
ZDOT = -5882
560623 TA = 51
41640
MA = 51
28620
Ha = 220
408 n
mi
Hp = 212
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12847637
71 X = 3849963
35
Y = 17868682
05 feet Y = 5489796
11 meter
Z = 3243954
39 Z = 1007619
63
XDOT = -11226
733725 XDOT = -3432
655485
YDOT = 11611
400843 feet/sec YDOT = 3500
829109 meter/sec
ZDOT = -19299
739578 ZDOT = -5899
208987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14006704
78 X = 4269243
62
Y = -16959658
49 feet Y = -5169303
91 meter
Z = 3325212
49 Z = 1013524
77
XDOT = 12820
433876 XDOT = 3907
668245
YDOT = 6752
317462 feet/sec YDOT = 2058
106362 meter/sec
ZDOT = -19372
923447 ZDOT = -5904
867067
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
49247571
00016717 00000-0 10270-3 0 9054
2 25544 51
6412 241
8877 0001851 62
6255 297
5087 15
54891246 10474
Satellite: ISS
Catalog Number: 25544
Epoch time: 16204
49247571 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 241
8877 deg
Eccentricity:
0001851
Arg of perigee: 62
6255 deg
Mean anomaly: 297
5087 deg
Mean motion: 15
54891246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 322
Coasting Arc #7 (Orbit 1062)
---------------------------------------
Vector Time (GMT): 2016/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3097624
96 A = 6786929
04 meter
Y = -5956248
72 meter E =
0015446
Z = 944318
32 I = 51
34880
XDOT = 4679
456850 Wp = 56
50650
YDOT = -1489
413388 meter/sec RA = 236
06376 deg
ZDOT = 5894
127810 TA = 313
76732
MA = 313
89503
Ha = 220
560 n
mi
Hp = 212
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10162811
54 X = -3035377
47
Y = -19541498
43 feet Y = -5990540
41 meter
Z = 3098157
23 Z = 929422
11
XDOT = 15352
548720 XDOT = 4667
133456
YDOT = -4886
526865 feet/sec YDOT = -1437
153669 meter/sec
ZDOT = 19337
689665 ZDOT = 5916
829043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16040421
15 X = -4889120
37
Y = 15107933
48 feet Y = 4604898
12 meter
Z = 3034256
54 Z = 924841
39
XDOT = -7735
742707 XDOT = -2357
854377
YDOT = -12158
175699 feet/sec YDOT = -3705
811953 meter/sec
ZDOT = 19436
899491 ZDOT = 5924
366965
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
52082096
00016717 00000-0 10270-3 0 9069
2 25544 51
6403 236
7561 0001986 65
1529 294
9830 15
54831148 10638
Satellite: ISS
Catalog Number: 25544
Epoch time: 16205
52082096 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 236
7561 deg
Eccentricity:
0001986
Arg of perigee: 65
1529 deg
Mean anomaly: 294
9830 deg
Mean motion: 15
54831148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1063
Checksum: 311
Coasting Arc #8 (Orbit 1077)
---------------------------------------
Vector Time (GMT): 2016/206/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1888985
20 A = 6783842
77 meter
Y = 5888718
48 meter E =
0006206
Z = -2790890
24 I = 51
35866
XDOT = -5699
880862 Wp = 107
74743
YDOT = -578
980738 meter/sec RA = 231
06594 deg
ZDOT = -5090
761827 TA = 104
03111
MA = 103
96211
Ha = 220
493 n
mi
Hp = 212
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6197458
01 X = 1836552
41
Y = 19319942
51 feet Y = 5909549
26 meter
Z = -9156464
05 Z = -2781841
39
XDOT = -18700
396529 XDOT = -5668
254571
YDOT = -1899
543105 feet/sec YDOT = -642
543677 meter/sec
ZDOT = -16701
974499 ZDOT = -5118
373204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16696815
69 X = 5089189
42
Y = -11558004
34 feet Y = -3522879
72 meter
Z = -9118024
98 Z = -2779174
01
XDOT = 2694
148155 XDOT = 821
176358
YDOT = 17133
774943 feet/sec YDOT = 5222
374603 meter/sec
ZDOT = -16822
238758 ZDOT = -5127
418373
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
48488746
00016717 00000-0 10270-3 0 9078
2 25544 51
6411 231
9446 0001927 72
8193 287
3171 15
54887887 10784
Satellite: ISS
Catalog Number: 25544
Epoch time: 16206
48488746 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 231
9446 deg
Eccentricity:
0001927
Arg of perigee: 72
8193 deg
Mean anomaly: 287
3171 deg
Mean motion: 15
54887887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1078
Checksum: 346
Coasting Arc #9 (Orbit 1093)
---------------------------------------
Vector Time (GMT): 2016/207/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -403021
55 A = 6779547
21 meter
Y = -5281771
15 meter E =
0011875
Z = 4222529
09 I = 51
36515
XDOT = 6328
927515 Wp = 101
01578
YDOT = 2410
628033 meter/sec RA = 226
05769 deg
ZDOT = 3608
544237 TA = 311
92109
MA = 312
02229
Ha = 220
516 n
mi
Hp = 212
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1322249
18 X = -364440
50
Y = -17328645
51 feet Y = -5286062
36 meter
Z = 13853441
89 Z = 4220664
95
XDOT = 20764
197883 XDOT = 6283
972327
YDOT = 7908
884622 feet/sec YDOT = 2481
150903 meter/sec
ZDOT = 11839
055895 ZDOT = 3639
179096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16074079
39 X = -4899379
40
Y = 6622281
22 feet Y = 2018471
32 meter
Z = 13846209
36 Z = 4220324
61
XDOT = 1716
015318 XDOT = 523
041469
YDOT = -20941
463213 feet/sec YDOT = -6382
957987 meter/sec
ZDOT = 11972
200624 ZDOT = 3649
126750
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
51322106
00016717 00000-0 10270-3 0 9081
2 25544 51
6410 226
8125 0002023 74
4879 285
6498 15
54889786 10948
Satellite: ISS
Catalog Number: 25544
Epoch time: 16207
51322106 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 226
8125 deg
Eccentricity:
0002023
Arg of perigee: 74
4879 deg
Mean anomaly: 285
6498 deg
Mean motion: 15
54889786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1094
Checksum: 323
Coasting Arc #10 (Orbit 1108)
---------------------------------------
Vector Time (GMT): 2016/208/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1300574
47 A = 6776065
52 meter
Y = 4276630
35 meter E =
0015388
Z = -5106384
84 I = 51
37759
XDOT = -6407
917224 Wp = 77
80414
YDOT = -3871
331230 meter/sec RA = 221
03838 deg
ZDOT = -1611
131606 TA = 176
57936
MA = 176
56883
Ha = 220
503 n
mi
Hp = 212
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4266976
62 X = -1323495
75
Y = 14030939
48 feet Y = 4261958
43 meter
Z = -16753231
09 Z = -5112758
21
XDOT = -21023
350473 XDOT = -6356
324651
YDOT = -12701
217945 feet/sec YDOT = -3942
700326 meter/sec
ZDOT = -5285
864849 ZDOT = -1642
134210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14621924
92 X = 4456762
72
Y = -563666
39 feet Y = -171805
51 meter
Z = -16781736
98 Z = -5115073
43
XDOT = -5335
168893 XDOT = -1626
159478
YDOT = 22888
603746 feet/sec YDOT = 6976
446422 meter/sec
ZDOT = -5420
381438 ZDOT = -1652
132262
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
47728024
00016717 00000-0 10270-3 0 9097
2 25544 51
6421 222
0018 0001925 77
0283 283
1085 15
54882941 11095
Satellite: ISS
Catalog Number: 25544
Epoch time: 16208
47728024 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 222
0018 deg
Eccentricity:
0001925
Arg of perigee: 77
0283 deg
Mean anomaly: 283
1085 deg
Mean motion: 15
54882941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1109
Checksum: 296
Coasting Arc #11 (Orbit 1124)
---------------------------------------
Vector Time (GMT): 2016/209/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3019949
69 A = 6775190
76 meter
Y = -3002059
75 meter E =
0004873
Z = 5265886
27 I = 51
39829
XDOT = 5894
891292 Wp = 72
79323
YDOT = 4876
140582 meter/sec RA = 216
01347 deg
ZDOT = -598
938003 TA = 22
94951
MA = 22
92775
Ha = 220
421 n
mi
Hp = 212
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9907971
41 X = 3027715
78
Y = -9849277
38 feet Y = -2968245
45 meter
Z = 17276529
76 Z = 5280575
08
XDOT = 19340
194526 XDOT = 5842
836301
YDOT = 15997
836556 feet/sec YDOT = 4941
770161 meter/sec
ZDOT = -1965
019696 ZDOT = -570
428508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12573994
01 X = -3832553
37
Y = -5902227
43 feet Y = -1798998
92 meter
Z = 17341079
24 Z = 5285560
95
XDOT = 8105
485547 XDOT = 2470
551995
YDOT = -22696
278833 feet/sec YDOT = -6917
825788 meter/sec
ZDOT = -1841
524903 ZDOT = -561
296791
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
50560597
00016717 00000-0 10270-3 0 9103
2 25544 51
6405 216
8700 0002067 80
2332 279
9054 15
54904102 11256
Satellite: ISS
Catalog Number: 25544
Epoch time: 16209
50560597 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 216
8700 deg
Eccentricity:
0002067
Arg of perigee: 80
2332 deg
Mean anomaly: 279
9054 deg
Mean motion: 15
54904102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1125
Checksum: 283
Coasting Arc #12 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2016/210/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4586784
51 A = 6777550
15 meter
Y = 1639343
01 meter E =
0012798
Z = -4724845
25 I = 51
43412
XDOT = -4726
522885 Wp = 104
92559
YDOT = -5375
081568 meter/sec RA = 210
99314 deg
ZDOT = 2726
427301 TA = 192
14053
MA = 192
17141
Ha = 220
481 n
mi
Hp = 212
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15048505
60 X = -4581824
06
Y = 5378421
96 feet Y = 1588078
54 meter
Z = -15501460
78 Z = -4747114
40
XDOT = -15506
964846 XDOT = -4679
309797
YDOT = -17634
782046 feet/sec YDOT = -5427
672879 meter/sec
ZDOT = 8944
971459 ZDOT = 2703
581552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10311522
85 X = 3142952
16
Y = 12084235
71 feet Y = 3683275
04 meter
Z = -15598845
27 Z = -4754528
04
XDOT = -10116
378420 XDOT = -3083
472142
YDOT = 20038
968806 feet/sec YDOT = 6107
877692 meter/sec
ZDOT = 8846
240131 ZDOT = 2696
333992
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
46965626
00016717 00000-0 10270-3 0 9113
2 25544 51
6419 212
0593 0001911 78
8160 281
3208 15
54888156 11403
Satellite: ISS
Catalog Number: 25544
Epoch time: 16210
46965626 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 212
0593 deg
Eccentricity:
0001911
Arg of perigee: 78
8160 deg
Mean anomaly: 281
3208 deg
Mean motion: 15
54888156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 300
Coasting Arc #13 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2016/211/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5793016
72 A = 6781649
15 meter
Y = -279222
28 meter E =
0014191
Z = 3503238
35 I = 51
47461
XDOT = 2994
275322 Wp = 86
98993
YDOT = 5445
818098 meter/sec RA = 205
98515 deg
ZDOT = -4500
832654 TA = 51
64262
MA = 51
51519
Ha = 220
378 n
mi
Hp = 212
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19005960
37 X = 5778691
45
Y = -916083
58 feet Y = -214521
24 meter
Z = 11493564
14 Z = 3531344
29
XDOT = 9823
737934 XDOT = 2955
019160
YDOT = 17866
857276 feet/sec YDOT = 5479
082911 meter/sec
ZDOT = -14766
511331 ZDOT = -4486
382313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7842621
22 X = -2390430
95
Y = -17254713
48 feet Y = -5259236
67 meter
Z = 11616191
75 Z = 3540615
25
XDOT = 11680
418139 XDOT = 3560
191449
YDOT = -15244
316121 feet/sec YDOT = -4646
467554 meter/sec
ZDOT = -14704
390318 ZDOT = -4481
898169
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
49797148
00016717 00000-0 10270-3 0 9120
2 25544 51
6400 206
9272 0002072 80
4650 279
6738 15
54939454 11564
Satellite: ISS
Catalog Number: 25544
Epoch time: 16211
49797148 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 206
9272 deg
Eccentricity:
0002072
Arg of perigee: 80
4650 deg
Mean anomaly: 279
6738 deg
Mean motion: 15
54939454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 318
Coasting Arc #14 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2016/212/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6466536
18 A = 6785450
82 meter
Y = -923952
77 meter E =
0008629
Z = -1829084
99 I = 51
51622
XDOT = -855
023410 Wp = 50
02155
YDOT = -5126
906909 meter/sec RA = 200
99334 deg
ZDOT = 5635
749004 TA = 289
82953
MA = 289
92253
Ha = 220
426 n
mi
Hp = 212
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21215669
90 X = -6446838
92
Y = -3031341
11 feet Y = -996155
62 meter
Z = -6000934
99 Z = -1860449
60
XDOT = -2805
194916 XDOT = -825
005158
YDOT = -16820
560725 feet/sec YDOT = -5136
300934 meter/sec
ZDOT = 18489
990171 ZDOT = 5631
668095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5361066
78 X = 1634053
15
Y = 20709750
63 feet Y = 6312331
99 meter
Z = -6137596
50 Z = -1870739
41
XDOT = -12883
447414 XDOT = -3926
874772
YDOT = 8787
878579 feet/sec YDOT = 2678
545391 meter/sec
ZDOT = 18473
034917 ZDOT = 5630
581043
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
46201421
00016717 00000-0 10270-3 0 9133
2 25544 51
6395 202
1166 0002077 88
8872 271
2519 15
54950335 11713
Satellite: ISS
Catalog Number: 25544
Epoch time: 16212
46201421 = yrday
fracday
Element set: 913
Inclination: 51
6395 deg
RA of node: 202
1166 deg
Eccentricity:
0002077
Arg of perigee: 88
8872 deg
Mean anomaly: 271
2519 deg
Mean motion: 15
54950335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 290
Coasting Arc #15 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2016/213/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6484930
83 A = 6786997
54 meter
Y = 1978263
41 meter E =
0013368
Z = -142123
11 I = 51
55077
XDOT = -1504
515995 Wp = 129
17180
YDOT = 4528
361089 meter/sec RA = 196
01095 deg
ZDOT = -6004
708143 TA = 52
36164
MA = 52
24041
Ha = 220
505 n
mi
Hp = 212
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21276019
80 X = 6463017
78
Y = 6490365
51 feet Y = 2050659
72 meter
Z = -466283
16 Z = -110674
58
XDOT = -4936
076100 XDOT = -1525
873693
YDOT = 14856
827720 feet/sec YDOT = 4511
417591 meter/sec
ZDOT = -19700
486034 ZDOT = -6012
068131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2589433
45 X = -789259
32
Y = -22095194
24 feet Y = -6734615
20 meter
Z = -329406
65 Z = -100403
15
XDOT = 13925
254884 XDOT = 4244
417689
YDOT = -1364
569225 feet/sec YDOT = -415
920700 meter/sec
ZDOT = -19733
338469 ZDOT = -6014
721565
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 16213
49032126
00016717 00000-0 10270-3 0 9142
2 25544 51
6388 196
9834 0002053 86
9600 273
1788 15
54929453 11872
Satellite: ISS
Catalog Number: 25544
Epoch time: 16213
49032126 = yrday
fracday
Element set: 914
Inclination: 51
6388 deg
RA of node: 196
9834 deg
Eccentricity:
0002053
Arg of perigee: 86
9600 deg
Mean anomaly: 273
1788 deg
Mean motion: 15
54929453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 328
Coasting Arc #16 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2016/214/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5822390
50 A = 6785162
52 meter
Y = -2796242
90 meter E =
0015691
Z = 2055392
14 I = 51
57592
XDOT = 3763
921278 Wp = 71
91694
YDOT = -3743
365649 meter/sec RA = 191
03129 deg
ZDOT = 5539
577280 TA = 310
85482
MA = 310
99071
Ha = 220
404 n
mi
Hp = 212
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19102331
04 X = -5800673
47
Y = -9174025
25 feet Y = -2861231
45 meter
Z = 6743412
55 Z = 2027161
61
XDOT = 12348
823090 XDOT = 3778
592492
YDOT = -12281
383363 feet/sec YDOT = -3701
193259 meter/sec
ZDOT = 18174
466142 ZDOT = 5557
896495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -358863
70 X = -109381
66
Y = 21226707
55 feet Y = 6469900
46 meter
Z = 6620687
78 Z = 2017985
64
XDOT = -14712
260304 XDOT = -4484
296941
YDOT = -5973
798788 feet/sec YDOT = -1820
813871 meter/sec
ZDOT = 18255
009911 ZDOT = 5564
127021
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 16214
51862084
00016717 00000-0 10270-3 0 9151
2 25544 51
6386 191
8517 0001899 93
5107 266
6263 15
54969231 12037
Satellite: ISS
Catalog Number: 25544
Epoch time: 16214
51862084 = yrday
fracday
Element set: 915
Inclination: 51
6386 deg
RA of node: 191
8517 deg
Eccentricity:
0001899
Arg of perigee: 93
5107 deg
Mean anomaly: 266
6263 deg
Mean motion: 15
54969231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 322
Coasting Arc #17 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2016/215/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930540
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4504455
02 A = 6781207
23 meter
Y = 3446177
09 meter E =
0007635
Z = -3724707
43 I = 51
59368
XDOT = -5692
880032 Wp = 82
99701
YDOT = 2814
875822 meter/sec RA = 186
04284 deg
ZDOT = -4286
914247 TA = 141
47136
MA = 141
41684
Ha = 220
488 n
mi
Hp = 212
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14778395
74 X = 4483676
82
Y = 11306355
27 feet Y = 3496432
89 meter
Z = -12220168
75 Z = -3702876
75
XDOT = -18677
427926 XDOT = -5703
110085
YDOT = 9235
156896 feet/sec YDOT = 2751
157212 meter/sec
ZDOT = -14064
679289 ZDOT = -4314
592921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3770141
87 X = 1149139
24
Y = -18284597
03 feet Y = -5573145
17 meter
Z = -12125457
37 Z = -3695839
41
XDOT = 15028
898458 XDOT = 4580
808250
YDOT = 12491
694859 feet/sec YDOT = 3807
468593 meter/sec
ZDOT = -14185
924708 ZDOT = -4323
869851
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 16215
48265110
00016717 00000-0 10270-3 0 9166
2 25544 51
6381 187
0395 0001997 91
9258 268
2123 15
54930294 12187
Satellite: ISS
Catalog Number: 25544
Epoch time: 16215
48265110 = yrday
fracday
Element set: 916
Inclination: 51
6381 deg
RA of node: 187
0395 deg
Eccentricity:
0001997
Arg of perigee: 91
9258 deg
Mean anomaly: 268
2123 deg
Mean motion: 15
54930294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 317
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