[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 5th 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
189/01:36:41
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
5
191/04:12:02
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
194/19:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
2
198/02:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
2
Coasting Arc #1 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2016/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6251014
74 A = 6785532
78 meter
Y = -1492445
03 meter E =
0014478
Z = 2155509
44 I = 51
48004
XDOT = -626
070028 Wp = 68
77575
YDOT = 5330
906863 meter/sec RA = 331
08729 deg
ZDOT = 5482
074160 TA = 315
20520
MA = 315
32200
Ha = 220
155 n
mi
Hp = 213
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20508578
56 X = 6256768
64
Y = -4896473
18 feet Y = -1422510
15 meter
Z = 7071881
35 Z = 2185888
71
XDOT = -2054
035525 XDOT = -712
264275
YDOT = 17489
851913 feet/sec YDOT = 5323
423003 meter/sec
ZDOT = 17985
807611 ZDOT = 5478
824316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9068527
46 X = -2764087
17
Y = -18985389
93 feet Y = -5786746
85 meter
Z = 7204549
19 Z = 2195946
59
XDOT = 16174
025327 XDOT = 4929
842920
YDOT = -876
178908 feet/sec YDOT = -267
059331 meter/sec
ZDOT = 17970
527898 ZDOT = 5477
416903
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
55992461
00016717 00000-0 10270-3 0 9000
2 25544 51
6417 331
3624 0000741 32
9632 327
1567 15
54732077 7688
Satellite: ISS
Catalog Number: 25544
Epoch time: 16186
55992461 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 331
3624 deg
Eccentricity:
0000741
Arg of perigee: 32
9632 deg
Mean anomaly: 327
1567 deg
Mean motion: 15
54732077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 312
Coasting Arc #2 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2016/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5657442
90 A = 6781576
18 meter
Y = 209781
73 meter E =
0006605
Z = -3740805
73 I = 51
43980
XDOT = 2591
716393 Wp = 71
03223
YDOT = -5824
546083 meter/sec RA = 326
09162 deg
ZDOT = -4250
299045 TA = 153
79825
MA = 153
76481
Ha = 220
236 n
mi
Hp = 213
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18561164
36 X = -5641197
32
Y = 688260
28 feet Y = 146607
76 meter
Z = -12272984
68 Z = -3768248
27
XDOT = 8503
006540 XDOT = 2677
301114
YDOT = -19109
403159 feet/sec YDOT = -5795
084693 meter/sec
ZDOT = -13944
550671 ZDOT = -4237
502218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4846250
84 X = 1477137
26
Y = 17848089
50 feet Y = 5440097
68 meter
Z = -12392587
77 Z = -3777260
75
XDOT = -19256
763596 XDOT = -5869
461544
YDOT = -4404
766549 feet/sec YDOT = -1342
572844 meter/sec
ZDOT = -13887
582566 ZDOT = -4232
935166
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
52409528
00016717 00000-0 10270-3 0 9016
2 25544 51
6425 326
5521 0000876 30
1966 329
9238 15
54715262 7837
Satellite: ISS
Catalog Number: 25544
Epoch time: 16187
52409528 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 326
5521 deg
Eccentricity:
0000876
Arg of perigee: 30
1966 deg
Mean anomaly: 329
9238 deg
Mean motion: 15
54715262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 317
Coasting Arc #3 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2016/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4604189
45 A = 6777531
77 meter
Y = 1223642
54 meter E =
0007114
Z = 4816084
98 I = 51
40120
XDOT = -4184
184487 Wp = 112
68044
YDOT = 5930
708619 meter/sec RA = 321
08141 deg
ZDOT = 2487
619291 TA = 312
77966
MA = 312
83947
Ha = 220
061 n
mi
Hp = 213
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15105608
44 X = 4566770
12
Y = 4014575
28 feet Y = 1274919
89 meter
Z = 15800803
73 Z = 4838359
85
XDOT = -13727
639394 XDOT = -4262
275760
YDOT = 19457
705443 feet/sec YDOT = 5883
481365 meter/sec
ZDOT = 8161
480612 ZDOT = 2467
104914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 254238
13 X = 77491
78
Y = -15529438
51 feet Y = -4733372
86 meter
Z = 15897594
85 Z = 4845586
91
XDOT = 21088
923768 XDOT = 6427
903965
YDOT = 8626
270785 feet/sec YDOT = 2629
287335 meter/sec
ZDOT = 8070
878987 ZDOT = 2460
003915
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
55253612
00016717 00000-0 10270-3 0 9022
2 25544 51
6433 321
4211 0000885 30
3865 329
7339 15
54753789 7999
Satellite: ISS
Catalog Number: 25544
Epoch time: 16188
55253612 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 321
4211 deg
Eccentricity:
0000885
Arg of perigee: 30
3865 deg
Mean anomaly: 329
7339 deg
Mean motion: 15
54753789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 325
Coasting Arc #4 (Orbit 807)
---------------------------------------
Vector Time (GMT): 2016/189/01:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5143879
11 A = 6787602
96 meter
Y = -4414759
75 meter E =
0013862
Z = 167876
82 I = 51
41970
XDOT = 2998
377026 Wp = 44
59800
YDOT = 3732
566385 meter/sec RA = 318
22997 deg
ZDOT = 5993
513018 TA = 317
21690
MA = 317
32471
Ha = 220
350 n
mi
Hp = 213
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16876243
80 X = 5192048
30
Y = -14484119
93 feet Y = -4356968
15 meter
Z = 550776
97 Z = 192980
61
XDOT = 9837
194967 XDOT = 2927
302295
YDOT = 12245
952707 feet/sec YDOT = 3765
698231 meter/sec
ZDOT = 19663
756620 ZDOT = 6007
905876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21858641
20 X = 6662513
84
Y = 4082095
45 feet Y = 1244222
69 meter
Z = 661053
43 Z = 201489
09
XDOT = -3169
143153 XDOT = -965
954833
YDOT = 13646
624453 feet/sec YDOT = 4159
491133 meter/sec
ZDOT = 19725
692741 ZDOT = 6012
391147
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
13103414
00016717 00000-0 10270-3 0 9032
2 25544 51
6427 318
5397 0001489 23
9541 336
1681 15
54717681 8088
Satellite: ISS
Catalog Number: 25544
Epoch time: 16189
13103414 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 318
5397 deg
Eccentricity:
0001489
Arg of perigee: 23
9541 deg
Mean anomaly: 336
1681 deg
Mean motion: 15
54717681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 808
Checksum: 314
Coasting Arc #5 (Orbit 822)
---------------------------------------
Vector Time (GMT): 2016/190/01:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5479566
60 A = 6785717
88 meter
Y = 3434288
13 meter E =
0006047
Z = -2052623
89 I = 51
39124
XDOT = -1183
338370 Wp = 125
94529
YDOT = -5180
842743 meter/sec RA = 313
24028 deg
ZDOT = -5524
121779 TA = 76
83237
MA = 76
76491
Ha = 220
303 n
mi
Hp = 213
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17977580
72 X = -5507591
83
Y = 11267349
50 feet Y = 3372855
43 meter
Z = -6734330
34 Z = -2079309
60
XDOT = -3882
343734 XDOT = -1098
483586
YDOT = -16997
515562 feet/sec YDOT = -5193
600726 meter/sec
ZDOT = -18123
759116 ZDOT = -5529
664362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20131346
44 X = -6136034
40
Y = -6579250
22 feet Y = -2005355
47 meter
Z = -6851287
14 Z = -2088272
32
XDOT = 10179
140681 XDOT = 3102
602080
YDOT = -12299
290315 feet/sec YDOT = -3748
823688 meter/sec
ZDOT = -18146
849897 ZDOT = -5531
159849
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
09519104
00016717 00000-0 10270-3 0 9047
2 25544 51
6436 313
7298 0001441 25
6085 334
5139 15
54733207 8234
Satellite: ISS
Catalog Number: 25544
Epoch time: 16190
09519104 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 313
7298 deg
Eccentricity:
0001441
Arg of perigee: 25
6085 deg
Mean anomaly: 334
5139 deg
Mean motion: 15
54733207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 823
Checksum: 295
Coasting Arc #6 (Orbit 838)
---------------------------------------
Vector Time (GMT): 2016/191/01:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5330411
13 A = 6781823
12 meter
Y = -2064880
37 meter E =
0012490
Z = 3637941
72 I = 51
35679
XDOT = -536
694012 Wp = 88
27371
YDOT = 6298
950381 meter/sec RA = 308
23930 deg
ZDOT = 4349
058598 TA = 315
15171
MA = 315
25258
Ha = 220
238 n
mi
Hp = 213
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17488225
49 X = 5335433
69
Y = -6774541
88 feet Y = -2005244
31 meter
Z = 11935504
32 Z = 3663847
20
XDOT = -1760
807127 XDOT = -628
216109
YDOT = 20665
847708 feet/sec YDOT = 6292
436696 meter/sec
ZDOT = 14268
564953 ZDOT = 4346
229630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16496178
45 X = 5028035
19
Y = 8768797
69 feet Y = 2672729
53 meter
Z = 12048775
69 Z = 3672466
83
XDOT = -16227
065406 XDOT = -4946
009536
YDOT = 10883
716103 feet/sec YDOT = 3317
356668 meter/sec
ZDOT = 14254
970143 ZDOT = 4344
914900
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
12361943
00016717 00000-0 10270-3 0 9059
2 25544 51
6435 308
5989 0001484 29
0336 331
0899 15
54740499 8399
Satellite: ISS
Catalog Number: 25544
Epoch time: 16191
12361943 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 308
5989 deg
Eccentricity:
0001484
Arg of perigee: 29
0336 deg
Mean anomaly: 331
0899 deg
Mean motion: 15
54740499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 839
Checksum: 332
Coasting Arc #7 (Orbit 839)
---------------------------------------
Vector Time (GMT): 2016/191/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1936837
73 A = 6776650
84 meter
Y = -4100343
80 meter E =
0013380
Z = -5047752
81 I = 51
33838
XDOT = 5610
126319 Wp = 97
36267
YDOT = -4886
826055 meter/sec RA = 307
65889 deg
ZDOT = 1819
473914 TA = 190
33485
MA = 190
36239
Ha = 220
254 n
mi
Hp = 213
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6354454
51 X = -1866323
26
Y = -13452571
51 feet Y = -4121608
21 meter
Z = -16560868
80 Z = -5056990
34
XDOT = 18405
926243 XDOT = 5655
516993
YDOT = -16032
893880 feet/sec YDOT = -4823
836203 meter/sec
ZDOT = 5969
402605 ZDOT = 1846
836039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3739235
78 X = -1139719
06
Y = -14354852
99 feet Y = -4375359
19 meter
Z = -16600284
91 Z = -5059766
84
XDOT = 19892
505877 XDOT = 6063
235791
YDOT = -12214
488982 feet/sec YDOT = -3722
976242 meter/sec
ZDOT = 6089
587462 ZDOT = 1856
106258
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
18789437
00016717 00000-0 10270-3 0 9068
2 25544 51
6445 308
2789 0001464 22
0692 338
0524 15
54761761 8400
Satellite: ISS
Catalog Number: 25544
Epoch time: 16191
18789437 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 308
2789 deg
Eccentricity:
0001464
Arg of perigee: 22
0692 deg
Mean anomaly: 338
0524 deg
Mean motion: 15
54761761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 840
Checksum: 322
Coasting Arc #8 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2016/192/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 499506
80 A = 6780131
73 meter
Y = 5348602
99 meter E =
0011463
Z = 4130296
27 I = 51
33084
XDOT = -5752
320835 Wp = 69
31333
YDOT = 3433
869177 meter/sec RA = 302
63869 deg
ZDOT = -3738
675589 TA = 59
36333
MA = 59
25036
Ha = 220
230 n
mi
Hp = 213
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1638801
85 X = 419597
30
Y = 17547910
08 feet Y = 5353741
77 meter
Z = 13550840
79 Z = 4132528
94
XDOT = -18872
443684 XDOT = -5772
131046
YDOT = 11265
974991 feet/sec YDOT = 3369
432337 meter/sec
ZDOT = -12265
996027 ZDOT = -3766
666509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1311824
54 X = -399844
12
Y = 17568699
40 feet Y = 5354939
58 meter
Z = 13559499
38 Z = 4132935
41
XDOT = -19088
246518 XDOT = -5818
097539
YDOT = 8167
626776 feet/sec YDOT = 2489
492641 meter/sec
ZDOT = -12388
617312 ZDOT = -3776
050557
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
21631537
00016717 00000-0 10270-3 0 9071
2 25544 51
6439 303
1476 0001618 22
7469 337
3755 15
54797068 8564
Satellite: ISS
Catalog Number: 25544
Epoch time: 16192
21631537 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 303
1476 deg
Eccentricity:
0001618
Arg of perigee: 22
7469 deg
Mean anomaly: 337
3755 deg
Mean motion: 15
54797068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 329
Coasting Arc #9 (Orbit 870)
---------------------------------------
Vector Time (GMT): 2016/193/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 793614
48 A = 6784429
68 meter
Y = -6173062
67 meter E =
0006250
Z = -2698352
27 I = 51
32707
XDOT = 5462
577846 Wp = 48
52994
YDOT = -1544
491039 meter/sec RA = 297
62988 deg
ZDOT = 5151
787790 TA = 280
84001
MA = 280
91034
Ha = 220
308 n
mi
Hp = 213
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2603722
05 X = 875691
55
Y = -20252830
29 feet Y = -6163728
87 meter
Z = -8852861
79 Z = -2694298
13
XDOT = 17921
843327 XDOT = 5454
417814
YDOT = -5067
227818 feet/sec YDOT = -1483
450770 meter/sec
ZDOT = 16902
190913 ZDOT = 5178
303473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5569134
36 X = 1697472
15
Y = -19653885
15 feet Y = -5990504
20 meter
Z = -8833980
18 Z = -2692597
16
XDOT = 16925
404997 XDOT = 5158
863443
YDOT = -2835
739100 feet/sec YDOT = -864
333278 meter/sec
ZDOT = 17018
003034 ZDOT = 5187
087325
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
18045776
00016717 00000-0 10270-3 0 9083
2 25544 51
6427 298
3372 0001510 25
5335 334
5892 15
54754596 8712
Satellite: ISS
Catalog Number: 25544
Epoch time: 16193
18045776 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 298
3372 deg
Eccentricity:
0001510
Arg of perigee: 25
5335 deg
Mean anomaly: 334
5892 deg
Mean motion: 15
54754596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 871
Checksum: 329
Coasting Arc #10 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2016/194/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1926320
12 A = 6787193
82 meter
Y = 6442888
12 meter E =
0013392
Z = 875987
03 I = 51
32291
XDOT = -4853
693360 Wp = 119
12638
YDOT = -640
002410 meter/sec RA = 292
63127 deg
ZDOT = -5904
138753 TA = 51
34955
MA = 51
22978
Ha = 220
344 n
mi
Hp = 213
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6319947
92 X = -2002478
09
Y = 21138084
40 feet Y = 6420920
85 meter
Z = 2873973
21 Z = 866444
94
XDOT = -15924
190814 XDOT = -4817
496396
YDOT = -2099
745440 feet/sec YDOT = -694
076892 meter/sec
ZDOT = -19370
533968 ZDOT = -5927
628740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8990756
53 X = -2740382
59
Y = 20153684
56 feet Y = 6142843
05 meter
Z = 2831143
10 Z = 862932
42
XDOT = -13930
465271 XDOT = -4246
005815
YDOT = -3450
002550 feet/sec YDOT = -1051
560777 meter/sec
ZDOT = -19472
733067 ZDOT = -5935
289039
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
20887050
00016717 00000-0 10270-3 0 9097
2 25544 51
6434 293
2057 0001498 31
6176 328
5067 15
54755149 8879
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
20887050 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 293
2057 deg
Eccentricity:
0001498
Arg of perigee: 31
6176 deg
Mean anomaly: 328
5067 deg
Mean motion: 15
54755149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 330
Coasting Arc #11 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2016/194/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3699427
33 A = 6785340
50 meter
Y = -5254612
41 meter E =
0015184
Z = 2154925
54 I = 51
30708
XDOT = 3076
531789 Wp = 68
15464
YDOT = 4418
370008 meter/sec RA = 289
56688 deg
ZDOT = 5466
780476 TA = 315
88324
MA = 316
00427
Ha = 220
276 n
mi
Hp = 213
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12137228
77 X = 3747443
14
Y = -17239542
03 feet Y = -5212974
62 meter
Z = 7069965
68 Z = 2173012
60
XDOT = 10093
608232 XDOT = 3000
340703
YDOT = 14495
964592 feet/sec YDOT = 4452
347464 meter/sec
ZDOT = 17935
631483 ZDOT = 5481
540648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 74593
68 X = 22736
15
Y = 21056439
07 feet Y = 6418002
63 meter
Z = 7149780
10 Z = 2179252
97
XDOT = -14979
787596 XDOT = -4565
839259
YDOT = -6086
642799 feet/sec YDOT = -1855
208725 meter/sec
ZDOT = 17999
065620 ZDOT = 5486
115201
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
85162352
00016717 00000-0 10270-3 0 9101
2 25544 51
6406 289
9982 0001431 43
9322 316
1945 15
54808964 8976
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
85162352 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 289
9982 deg
Eccentricity:
0001431
Arg of perigee: 43
9322 deg
Mean anomaly: 316
1945 deg
Mean motion: 15
54808964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 331
Coasting Arc #12 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2016/195/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4115505
84 A = 6781409
55 meter
Y = 3875867
61 meter E =
0007459
Z = -3753672
26 I = 51
28297
XDOT = -1907
298703 Wp = 69
96978
YDOT = -6105
364604 meter/sec RA = 284
55852 deg
ZDOT = -4217
303695 TA = 155
17926
MA = 155
14336
Ha = 220
452 n
mi
Hp = 213
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13502315
76 X = -4140307
27
Y = 12716101
09 feet Y = 3829706
89 meter
Z = -12315197
70 Z = -3773724
20
XDOT = -6257
541678 XDOT = -1818
399481
YDOT = -20030
723766 feet/sec YDOT = -6126
195902 meter/sec
ZDOT = -13836
298212 ZDOT = -4226
353375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3311017
63 X = 1009198
17
Y = -18189866
42 feet Y = -5544271
29 meter
Z = -12403296
90 Z = -3780524
90
XDOT = 15489
509411 XDOT = 4721
202469
YDOT = 12270
606966 feet/sec YDOT = 3740
081003 meter/sec
ZDOT = -13874
537360 ZDOT = -4228
958987
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
81575441
00016717 00000-0 10270-3 0 9116
2 25544 51
6399 285
1869 0001673 45
1015 315
0273 15
54769219 9129
Satellite: ISS
Catalog Number: 25544
Epoch time: 16195
81575441 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 285
1869 deg
Eccentricity:
0001673
Arg of perigee: 45
1015 deg
Mean anomaly: 315
0273 deg
Mean motion: 15
54769219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 319
Coasting Arc #13 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2016/196/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4275341
90 A = 6777383
49 meter
Y = -2073703
51 meter E =
0007486
Z = 4827375
44 I = 51
26258
XDOT = 760
711645 Wp = 108
67874
YDOT = 7238
341154 meter/sec RA = 279
53774 deg
ZDOT = 2430
206248 TA = 317
33646
MA = 317
39457
Ha = 220
243 n
mi
Hp = 213
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14026712
27 X = 4274763
63
Y = -6803489
20 feet Y = -2025897
44 meter
Z = 15837845
95 Z = 4848142
30
XDOT = 2495
773115 XDOT = 667
909317
YDOT = 23747
838433 feet/sec YDOT = 7246
328835 meter/sec
ZDOT = 7973
117613 ZDOT = 2433
676817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6973705
64 X = -2125585
48
Y = 13838971
61 feet Y = 4218118
55 meter
Z = 15928709
33 Z = 4855070
61
XDOT = -15302
217825 XDOT = -4664
115993
YDOT = -16924
448829 feet/sec YDOT = -5158
572003 meter/sec
ZDOT = 7986
845579 ZDOT = 2434
390533
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 16196
84415509
00016717 00000-0 10270-3 0 9129
2 25544 51
6399 280
0560 0001551 43
1997 316
9277 15
54790576 9284
Satellite: ISS
Catalog Number: 25544
Epoch time: 16196
84415509 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 280
0560 deg
Eccentricity:
0001551
Arg of perigee: 43
1997 deg
Mean anomaly: 316
9277 deg
Mean motion: 15
54790576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 337
Coasting Arc #14 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2016/197/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4256277
74 A = 6775492
80 meter
Y = 15597
22 meter E =
0016169
Z = -5285782
05 I = 51
25257
XDOT = 354
862617 Wp = 83
76331
YDOT = -7643
279447 meter/sec RA = 274
50575 deg
ZDOT = -307
388879 TA = 183
28112
MA = 183
29174
Ha = 220
469 n
mi
Hp = 213
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13964165
83 X = -4230459
93
Y = 51171
99 feet Y = -31854
42 meter
Z = -17341804
63 Z = -5306395
15
XDOT = 1164
247432 XDOT = 441
798473
YDOT = -25076
376138 feet/sec YDOT = -7638
825018 meter/sec
ZDOT = -1008
493697 ZDOT = -305
454676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10854139
10 X = 3308341
60
Y = -8606131
24 feet Y = -2623148
80 meter
Z = -17431606
44 Z = -5313153
64
XDOT = 13961
898312 XDOT = 4255
586605
YDOT = 19637
585660 feet/sec YDOT = 5985
536109 meter/sec
ZDOT = -998
611430 ZDOT = -304
376764
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
80827696
00016717 00000-0 10270-3 0 9131
2 25544 51
6408 275
2450 0001689 48
0196 312
1100 15
54780038 9438
Satellite: ISS
Catalog Number: 25544
Epoch time: 16197
80827696 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 275
2450 deg
Eccentricity:
0001689
Arg of perigee: 48
0196 deg
Mean anomaly: 312
1100 deg
Mean motion: 15
54780038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 313
Coasting Arc #15 (Orbit 947)
---------------------------------------
Vector Time (GMT): 2016/198/02:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2470421
92 A = 6782277
11 meter
Y = 5303180
08 meter E =
0013457
Z = 3421022
91 I = 51
27815
XDOT = -3909
378114 Wp = 83
60866
YDOT = 4773
450544 meter/sec RA = 272
98132 deg
ZDOT = -4559
642366 TA = 56
07537
MA = 55
94749
Ha = 220
279 n
mi
Hp = 213
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8105058
80 X = 2394319
08
Y = 17398884
79 feet Y = 5330380
11 meter
Z = 11223828
43 Z = 3432839
23
XDOT = -12826
043681 XDOT = -3940
316859
YDOT = 15660
926983 feet/sec YDOT = 4729
560760 meter/sec
ZDOT = -14959
456580 ZDOT = -4578
707668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3070769
28 X = -935970
48
Y = 18916872
67 feet Y = 5765862
79 meter
Z = 11274298
17 Z = 3436406
08
XDOT = -17930
237965 XDOT = -5465
136532
YDOT = 6088
154256 feet/sec YDOT = 1855
669417 meter/sec
ZDOT = -15043
420725 ZDOT = -4585
234637
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
12964817
00016717 00000-0 10270-3 0 9145
2 25544 51
6440 273
6426 0001714 36
1938 323
9331 15
54830430 9483
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
12964817 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 273
6426 deg
Eccentricity:
0001714
Arg of perigee: 36
1938 deg
Mean anomaly: 323
9331 deg
Mean motion: 15
54830430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 948
Checksum: 312
Coasting Arc #16 (Orbit 962)
---------------------------------------
Vector Time (GMT): 2016/199/02:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1641284
17 A = 6786085
96 meter
Y = -6339620
58 meter E =
0009091
Z = -1766991
50 I = 51
28779
XDOT = 4428
475070 Wp = 38
74815
YDOT = -2712
534899 meter/sec RA = 267
97500 deg
ZDOT = 5641
363639 TA = 301
74868
MA = 301
83723
Ha = 220
387 n
mi
Hp = 213
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5384790
58 X = -1561687
75
Y = -20799280
11 feet Y = -6357529
26 meter
Z = -5797216
20 Z = -1774771
76
XDOT = 14529
117683 XDOT = 4431
075130
YDOT = -8899
392712 feet/sec YDOT = -2662
998835 meter/sec
ZDOT = 18508
410888 ZDOT = 5662
881874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6848959
65 X = 2087562
90
Y = -20354791
30 feet Y = -6204140
39 meter
Z = -5829919
48 Z = -1776959
46
XDOT = 15446
278758 XDOT = 4708
025765
YDOT = -109
486584 feet/sec YDOT = -33
371511 meter/sec
ZDOT = 18602
670352 ZDOT = 5670
093923
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
09376614
00016717 00000-0 10270-3 0 9155
2 25544 51
6421 268
8319 0001657 40
2436 319
8840 15
54781958 9630
Satellite: ISS
Catalog Number: 25544
Epoch time: 16199
09376614 = yrday
fracday
Element set: 915
Inclination: 51
6421 deg
RA of node: 268
8319 deg
Eccentricity:
0001657
Arg of perigee: 40
2436 deg
Mean anomaly: 319
8840 deg
Mean motion: 15
54781958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 963
Checksum: 339
Coasting Arc #17 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2016/200/02:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 700725
63 A = 6787432
02 meter
Y = 6744342
35 meter E =
0011943
Z = -161034
80 I = 51
29457
XDOT = -4785
027138 Wp = 128
64529
YDOT = 361
685641 meter/sec RA = 262
97792 deg
ZDOT = -5981
920312 TA = 53
09818
MA = 52
98881
Ha = 220
408 n
mi
Hp = 213
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2298968
60 X = 626038
84
Y = 22127107
44 feet Y = 6751760
75 meter
Z = -528329
41 Z = -157811
54
XDOT = -15698
907933 XDOT = -4759
658747
YDOT = 1186
632681 feet/sec YDOT = 308
318797 meter/sec
ZDOT = -19625
722807 ZDOT = -6005
102826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9783130
97 X = -2981898
32
Y = 19979935
88 feet Y = 6089884
46 meter
Z = -515541
29 Z = -157136
98
XDOT = -12372
909404 XDOT = -3771
262786
YDOT = -6540
635238 feet/sec YDOT = -1993
585621 meter/sec
ZDOT = -19726
797283 ZDOT = -6012
727812
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
12215582
00016717 00000-0 10270-3 0 9169
2 25544 51
6423 263
7011 0001499 47
7258 312
4022 15
54777415 9794
Satellite: ISS
Catalog Number: 25544
Epoch time: 16200
12215582 = yrday
fracday
Element set: 916
Inclination: 51
6423 deg
RA of node: 263
7011 deg
Eccentricity:
0001499
Arg of perigee: 47
7258 deg
Mean anomaly: 312
4022 deg
Mean motion: 15
54777415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 979
Checksum: 297
Coasting Arc #18 (Orbit 994)
---------------------------------------
Vector Time (GMT): 2016/201/02:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 288472
25 A = 6785523
24 meter
Y = -6460144
52 meter E =
0015326
Z = 2031149
72 I = 51
29268
XDOT = 4946
430262 Wp = 66
87495
YDOT = 1966
910746 meter/sec RA = 257
97825 deg
ZDOT = 5525
943701 TA = 315
70754
MA = 315
83008
Ha = 220
294 n
mi
Hp = 213
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 946431
28 X = 350823
49
Y = -21194699
88 feet Y = -6456570
22 meter
Z = 6663877
02 Z = 2032701
78
XDOT = 16228
445743 XDOT = 4897
225927
YDOT = 6453
119244 feet/sec YDOT = 2021
949326 meter/sec
ZDOT = 18129
736551 ZDOT = 5549
852534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11703460
27 X = 3567214
69
Y = -17692767
35 feet Y = -5392755
49 meter
Z = 6671828
33 Z = 2033573
28
XDOT = 9184
750661 XDOT = 2799
512002
YDOT = 12985
136277 feet/sec YDOT = 3957
869537 meter/sec
ZDOT = 18233
554967 ZDOT = 5557
587554
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
15053891
00016717 00000-0 10270-3 0 9177
2 25544 51
6414 258
5685 0001475 47
9164 312
2114 15
54835824 9952
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
15053891 = yrday
fracday
Element set: 917
Inclination: 51
6414 deg
RA of node: 258
5685 deg
Eccentricity:
0001475
Arg of perigee: 47
9164 deg
Mean anomaly: 312
2114 deg
Mean motion: 15
54835824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 995
Checksum: 313
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