[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 27th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1552 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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
304/00:37:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
1
304/02:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
1
307/03:37:45
968 -0
4 4
5 4
5
N/A 4
2 -0
5 222
6
000/00:01:27
935 1
4 -0
1 215
0
308/04:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 215
1
311/14:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 215
3
314/21:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 215
3
Coasting Arc #1 (Orbit 2540)
---------------------------------------
Vector Time (GMT): 2016/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908899
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -772451
40 A = 6780775
93 meter
Y = -5151137
37 meter E =
0015382
Z = 4328538
94 I = 51
94350
XDOT = 5648
755439 Wp = 87
93559
YDOT = -3819
338167 meter/sec RA = 122
05707 deg
ZDOT = -3525
806437 TA = 37
80246
MA = 37
69452
Ha = 223
066 n
mi
Hp = 212
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2534289
38 X = -735819
15
Y = -16900056
99 feet Y = -5159570
22 meter
Z = 14201243
25 Z = 4324875
97
XDOT = 18532
662200 XDOT = 5708
171527
YDOT = -12530
637032 feet/sec YDOT = -3755
838102 meter/sec
ZDOT = -11567
606422 ZDOT = -3498
221126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11722056
70 X = 3572882
88
Y = 12452292
00 feet Y = 3795458
60 meter
Z = 14186037
84 Z = 4323904
33
XDOT = -7351
864805 XDOT = -2240
848392
YDOT = 20002
928823 feet/sec YDOT = 6096
892705 meter/sec
ZDOT = -11446
210558 ZDOT = -3488
804978
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 16300
54193217
00016717 00000-0 10270-3 0 9009
2 25544 51
6385 122
8870 0006602 111
3156 248
8702 15
54336107 25418
Satellite: ISS
Catalog Number: 25544
Epoch time: 16300
54193217 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 122
8870 deg
Eccentricity:
0006602
Arg of perigee: 111
3156 deg
Mean anomaly: 248
8702 deg
Mean motion: 15
54336107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2541
Checksum: 281
Coasting Arc #2 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2016/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908899
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -386297
84 A = 6784638
90 meter
Y = 6039808
78 meter E =
0010565
Z = -3077406
74 I = 51
97250
XDOT = -5442
381473 Wp = 98
94067
YDOT = 2160
932904 meter/sec RA = 117
09170 deg
ZDOT = 4937
114217 TA = 225
93165
MA = 226
01869
Ha = 223
017 n
mi
Hp = 212
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1267381
38 X = -438858
83
Y = 19815645
59 feet Y = 6035194
76 meter
Z = -10096478
82 Z = -3079411
55
XDOT = -17855
582262 XDOT = -5490
123894
YDOT = 7089
674882 feet/sec YDOT = 2099
806061 meter/sec
ZDOT = 16197
881288 ZDOT = 4910
559850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10504970
17 X = -3201914
91
Y = -16843823
58 feet Y = -5133997
43 meter
Z = -10106243
57 Z = -3080383
04
XDOT = 9297
616112 XDOT = 2833
913391
YDOT = -15422
094456 feet/sec YDOT = -4700
654390 meter/sec
ZDOT = 16081
257618 ZDOT = 4901
567322
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 16301
50632686
00016717 00000-0 10270-3 0 9015
2 25544 51
6380 118
0773 0006765 115
2996 244
8859 15
54357838 25566
Satellite: ISS
Catalog Number: 25544
Epoch time: 16301
50632686 = yrday
fracday
Element set: 901
Inclination: 51
6380 deg
RA of node: 118
0773 deg
Eccentricity:
0006765
Arg of perigee: 115
2996 deg
Mean anomaly: 244
8859 deg
Mean motion: 15
54357838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2556
Checksum: 335
Coasting Arc #3 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2016/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908899
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1431128
60 A = 6787633
10 meter
Y = -6470343
59 meter E =
0020370
Z = 1423987
50 I = 51
99723
XDOT = 4991
571256 Wp = 118
64660
YDOT = -189
824280 meter/sec RA = 112
13800 deg
ZDOT = -5825
781841 TA = 45
89030
MA = 45
72287
Ha = 222
834 n
mi
Hp = 212
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4695303
81 X = 1496458
01
Y = -21228161
40 feet Y = -6453974
35 meter
Z = 4671874
99 Z = 1431098
97
XDOT = 16376
546115 XDOT = 5021
622677
YDOT = -622
783070 feet/sec YDOT = -133
837674 meter/sec
ZDOT = -19113
457484 ZDOT = -5801
460513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8844729
28 X = 2695873
48
Y = 19853198
29 feet Y = 6051254
84 meter
Z = 4704084
58 Z = 1433804
98
XDOT = -11461
119360 XDOT = -3493
349181
YDOT = 9650
757957 feet/sec YDOT = 2941
551025 meter/sec
ZDOT = -19006
928332 ZDOT = -5793
311756
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 16302
53499982
00016717 00000-0 10270-3 0 9020
2 25544 51
6384 112
9468 0006512 117
4163 242
7652 15
54414191 25726
Satellite: ISS
Catalog Number: 25544
Epoch time: 16302
53499982 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 112
9468 deg
Eccentricity:
0006512
Arg of perigee: 117
4163 deg
Mean anomaly: 242
7652 deg
Mean motion: 15
54414191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2572
Checksum: 310
Coasting Arc #4 (Orbit 2587)
---------------------------------------
Vector Time (GMT): 2016/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908899
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2256306
55 A = 6788500
89 meter
Y = 6389335
00 meter E =
0016064
Z = 341994
06 I = 52
01079
XDOT = -4350
341798 Wp = 73
07590
YDOT = -1871
241064 meter/sec RA = 107
19096 deg
ZDOT = 6029
648829 TA = 290
59112
MA = 290
76337
Ha = 222
944 n
mi
Hp = 212
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7402580
53 X = -2329247
33
Y = 20962385
17 feet Y = 6363695
65 meter
Z = 1122027
77 Z = 330855
55
XDOT = -14272
774927 XDOT = -4358
383921
YDOT = -6139
242335 feet/sec YDOT = -1919
933992 meter/sec
ZDOT = 19782
312431 ZDOT = 6008
496063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6843164
70 X = -2085796
60
Y = -21154201
96 feet Y = -6447800
76 meter
Z = 1072181
39 Z = 326800
89
XDOT = 13625
693817 XDOT = 4153
111475
YDOT = -3370
021880 feet/sec YDOT = -1027
182669 meter/sec
ZDOT = 19689
999245 ZDOT = 6001
511770
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 16303
56366438
00016717 00000-0 10270-3 0 9034
2 25544 51
6379 107
8166 0006886 122
4521 237
7298 15
54397908 25889
Satellite: ISS
Catalog Number: 25544
Epoch time: 16303
56366438 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 107
8166 deg
Eccentricity:
0006886
Arg of perigee: 122
4521 deg
Mean anomaly: 237
7298 deg
Mean motion: 15
54397908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2588
Checksum: 347
Coasting Arc #5 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2016/304/00:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 893668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4379616
99 A = 6778038
35 meter
Y = 1332528
40 meter E =
0012794
Z = 4991445
23 I = 51
98116
XDOT = 198
103831 Wp = 122
43720
YDOT = -7370
137776 meter/sec RA = 104
59802 deg
ZDOT = 2130
720796 TA = 306
86906
MA = 306
98628
Ha = 222
945 n
mi
Hp = 212
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14368822
16 X = -4418439
07
Y = 4371812
33 feet Y = 1283335
88 meter
Z = 16376132
65 Z = 4970075
22
XDOT = 649
946951 XDOT = 270
153483
YDOT = -24180
242048 feet/sec YDOT = -7367
519437 meter/sec
ZDOT = 6990
553792 ZDOT = 2131
858700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6605308
00 X = -2013297
88
Y = 13601809
93 feet Y = 4145831
67 meter
Z = 16282327
43 Z = 4962853
40
XDOT = -16364
074427 XDOT = -4987
769885
YDOT = -16364
429945 feet/sec YDOT = -4987
878247 meter/sec
ZDOT = 6996
782149 ZDOT = 2132
619199
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 16304
07799118
00016717 00000-0 10270-3 0 9047
2 25544 51
6383 105
2557 0006556 122
0291 238
1499 15
54409968 25961
Satellite: ISS
Catalog Number: 25544
Epoch time: 16304
07799118 = yrday
fracday
Element set: 904
Inclination: 51
6383 deg
RA of node: 105
2557 deg
Eccentricity:
0006556
Arg of perigee: 122
0291 deg
Mean anomaly: 238
1499 deg
Mean motion: 15
54409968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 332
Coasting Arc #6 (Orbit 2596)
---------------------------------------
Vector Time (GMT): 2016/304/02:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 893668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3233671
00 A = 6786327
44 meter
Y = -5507239
57 meter E =
0012375
Z = -2289575
68 I = 52
01132
XDOT = 3335
811878 Wp = 128
35149
YDOT = 4218
511999 meter/sec RA = 104
16091 deg
ZDOT = -5463
078985 TA = 77
00164
MA = 76
86349
Ha = 222
849 n
mi
Hp = 212
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10609156
82 X = 3306136
08
Y = -18068371
30 feet Y = -5470673
48 meter
Z = -7511731
23 Z = -2273690
50
XDOT = 10944
264690 XDOT = 3314
929438
YDOT = 13840
262465 feet/sec YDOT = 4255
698135 meter/sec
ZDOT = -17923
487484 ZDOT = -5446
925056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15763741
01 X = -4804788
26
Y = -13841199
79 feet Y = -4218797
69 meter
Z = -7441237
36 Z = -2268089
15
XDOT = 14649
641372 XDOT = 4465
210690
YDOT = -7134
940834 feet/sec YDOT = -2174
729966 meter/sec
ZDOT = -17853
462331 ZDOT = -5441
735318
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 16304
14228248
00016717 00000-0 10270-3 0 9057
2 25544 51
6400 104
9346 0006539 121
1953 238
9842 15
54408820 25976
Satellite: ISS
Catalog Number: 25544
Epoch time: 16304
14228248 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 104
9346 deg
Eccentricity:
0006539
Arg of perigee: 121
1953 deg
Mean anomaly: 238
9842 deg
Mean motion: 15
54408820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2597
Checksum: 307
Coasting Arc #7 (Orbit 2612)
---------------------------------------
Vector Time (GMT): 2016/305/02:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 893668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3663359
51 A = 6782553
63 meter
Y = 4294577
70 meter E =
0017608
Z = 3750077
30 I = 52
00655
XDOT = -2451
272906 Wp = 106
55822
YDOT = -5863
389183 meter/sec RA = 99
20500 deg
ZDOT = 4298
617354 TA = 298
04243
MA = 298
22040
Ha = 222
782 n
mi
Hp = 212
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12018896
02 X = -3729327
06
Y = 14089821
84 feet Y = 4253242
92 meter
Z = 12303403
23 Z = 3732120
67
XDOT = -8042
233943 XDOT = -2406
406203
YDOT = -19236
841151 feet/sec YDOT = -5890
549855 meter/sec
ZDOT = 14103
075310 ZDOT = 4286
818671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11834643
72 X = 3607199
41
Y = 14313105
49 feet Y = 4362634
55 meter
Z = 12224029
27 Z = 3725884
12
XDOT = -19292
699888 XDOT = -5880
414926
YDOT = 3889
864823 feet/sec YDOT = 1185
630798 meter/sec
ZDOT = 14052
413609 ZDOT = 4283
175668
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 16305
17092616
00016717 00000-0 10270-3 0 9060
2 25544 51
6407 99
8053 0006507 126
1212 234
0544 15
54433110 26133
Satellite: ISS
Catalog Number: 25544
Epoch time: 16305
17092616 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 99
8053 deg
Eccentricity:
0006507
Arg of perigee: 126
1212 deg
Mean anomaly: 234
0544 deg
Mean motion: 15
54433110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2613
Checksum: 277
Coasting Arc #8 (Orbit 2627)
---------------------------------------
Vector Time (GMT): 2016/306/02:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 893668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3977548
18 A = 6778635
26 meter
Y = -2637267
74 meter E =
0015961
Z = -4827503
86 I = 51
99859
XDOT = 1517
822386 Wp = 91
28803
YDOT = 7039
620715 meter/sec RA = 94
23660 deg
ZDOT = -2602
921968 TA = 153
19822
MA = 153
11566
Ha = 222
679 n
mi
Hp = 212
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13049698
74 X = 4030193
73
Y = -8652453
22 feet Y = -2592493
96 meter
Z = -15838267
27 Z = -4808053
42
XDOT = 4979
732238 XDOT = 1451
634961
YDOT = 23095
868486 feet/sec YDOT = 7056
223843 meter/sec
ZDOT = -8539
770235 ZDOT = -2595
709612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6544926
82 X = -1994893
70
Y = -14318833
95 feet Y = -4364380
59 meter
Z = -15752625
85 Z = -4801400
36
XDOT = 22548
860539 XDOT = 6872
892692
YDOT = -973
423862 feet/sec YDOT = -296
699593 meter/sec
ZDOT = -8509
412725 ZDOT = -2593
668999
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 16306
13526810
00016717 00000-0 10270-3 0 9076
2 25544 51
6414 94
9953 0006472 127
4384 232
7359 15
54452273 26287
Satellite: ISS
Catalog Number: 25544
Epoch time: 16306
13526810 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 94
9953 deg
Eccentricity:
0006472
Arg of perigee: 127
4384 deg
Mean anomaly: 232
7359 deg
Mean motion: 15
54452273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2628
Checksum: 317
Coasting Arc #9 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2016/307/02:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 893668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4137631
04 A = 6776405
53 meter
Y = 759803
22 meter E =
0009147
Z = 5306684
24 I = 51
99301
XDOT = -588
376667 Wp = 126
98350
YDOT = -7626
353860 meter/sec RA = 89
26158 deg
ZDOT = 627
069510 TA = 317
02872
MA = 317
10013
Ha = 222
616 n
mi
Hp = 212
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13574904
99 X = -4171598
11
Y = 2492792
72 feet Y = 713343
66 meter
Z = 17410381
38 Z = 5286501
61
XDOT = -1930
369641 XDOT = -506
099214
YDOT = -25020
845997 feet/sec YDOT = -7632
473426 meter/sec
ZDOT = 2057
314665 ZDOT = 624
411283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 615044
85 X = 187465
67
Y = 13899226
31 feet Y = 4236484
18 meter
Z = 17321855
23 Z = 5279701
47
XDOT = -24039
547011 XDOT = -7327
253929
YDOT = -1512
415968 feet/sec YDOT = -460
984387 meter/sec
ZDOT = 2047
023579 ZDOT = 623
932787
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 16307
16388604
00016717 00000-0 10270-3 0 9088
2 25544 51
6414 89
8667 0006307 132
7193 227
4491 15
54494924 26441
Satellite: ISS
Catalog Number: 25544
Epoch time: 16307
16388604 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 89
8667 deg
Eccentricity:
0006307
Arg of perigee: 132
7193 deg
Mean anomaly: 227
4491 deg
Mean motion: 15
54494924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 333
Coasting Arc #10 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2016/307/03:38:29
935
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3914763
56 A = 6780545
24 meter
Y = 2492169
40 meter E =
0014612
Z = -4957173
72 I = 51
99965
XDOT = -1656
610879 Wp = 116
52652
YDOT = 7121
385135 meter/sec RA = 89
05251 deg
ZDOT = 2270
771502 TA = 175
59025
MA = 175
57736
Ha = 222
560 n
mi
Hp = 215
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12843712
46 X = 3910684
98
Y = 8176408
78 feet Y = 2535923
99 meter
Z = -16263693
29 Z = -4938166
23
XDOT = -5435
075062 XDOT = -1747
151627
YDOT = 23364
124458 feet/sec YDOT = 7102
353611 meter/sec
ZDOT = 7450
037737 ZDOT = 2262
503797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6868301
51 X = 2093458
30
Y = -13686766
03 feet Y = -4171726
29 meter
Z = -16180889
96 Z = -4931935
26
XDOT = 22791
235584 XDOT = 6946
768606
YDOT = 2669
161902 feet/sec YDOT = 813
560548 meter/sec
ZDOT = 7412
566393 ZDOT = 2259
350236
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 16307
16388716
00016717 00000-0 10270-3 0 9093
2 25544 51
6428 89
8651 0003352 156
0948 204
0360 15
53615038 26449
Satellite: ISS
Catalog Number: 25544
Epoch time: 16307
16388716 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 89
8651 deg
Eccentricity:
0003352
Arg of perigee: 156
0948 deg
Mean anomaly: 204
0360 deg
Mean motion: 15
53615038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 316
Coasting Arc #11 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/03:38:29
935
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3668179
98 A = 6783529
41 meter
Y = -3897330
92 meter E =
0011258
Z = 4157804
66 I = 52
00843
XDOT = 2331
228864 Wp = 93
23869
YDOT = -6248
956059 meter/sec RA = 84
09078 deg
ZDOT = -3792
578485 TA = 35
64353
MA = 35
56841
Ha = 222
596 n
mi
Hp = 214
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12034711
24 X = -3644523
73
Y = -12786518
77 feet Y = -3938218
65 meter
Z = 13641091
42 Z = 4140042
62
XDOT = 7648
388661 XDOT = 2419
356195
YDOT = -20501
824341 feet/sec YDOT = -6222
393986 meter/sec
ZDOT = -12442
842799 ZDOT = -3781
039551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11306592
16 X = -3446249
29
Y = 13512499
43 feet Y = 4118609
83 meter
Z = 13563998
11 Z = 4134306
62
XDOT = -20270
288446 XDOT = -6178
383918
YDOT = -4495
620201 feet/sec YDOT = -1370
265037 meter/sec
ZDOT = -12391
181493 ZDOT = -3776
832119
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 16308
19305515
00016717 00000-0 10270-3 0 9105
2 25544 51
6429 84
7399 0003347 160
4431 199
6850 15
53627894 26607
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19305515 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 84
7399 deg
Eccentricity:
0003347
Arg of perigee: 160
4431 deg
Mean anomaly: 199
6850 deg
Mean motion: 15
53627894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 326
Coasting Arc #12 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4149350
42 A = 6780195
04 meter
Y = 1911029
39 meter E =
0014668
Z = -5023556
95 I = 51
99831
XDOT = -855
997968 Wp = 116
10510
YDOT = 7319
552429 meter/sec RA = 83
95607 deg
ZDOT = 2075
840078 TA = 174
02921
MA = 174
01170
Ha = 222
401 n
mi
Hp = 215
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13613354
38 X = 4152075
29
Y = 6269781
46 feet Y = 1957445
39 meter
Z = -16481486
05 Z = -5003393
34
XDOT = -2808
392282 XDOT = -947
867241
YDOT = 24014
279622 feet/sec YDOT = 7309
466436 meter/sec
ZDOT = 6810
498943 ZDOT = 2071
458526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1981481
91 X = 603955
69
Y = -14953236
29 feet Y = -4557746
42 meter
Z = -16393517
41 Z = -4996744
11
XDOT = 22708
657710 XDOT = 6921
598870
YDOT = -4440
548280 feet/sec YDOT = -1353
479116 meter/sec
ZDOT = 6789
992470 ZDOT = 2069
589705
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 16308
19305408
00016717 00000-0 10270-3 0 9117
2 25544 51
6439 84
7396 0003277 162
7924 197
3340 15
53641757 26602
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19305408 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 84
7396 deg
Eccentricity:
0003277
Arg of perigee: 162
7924 deg
Mean anomaly: 197
3340 deg
Mean motion: 15
53641757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 323
Coasting Arc #13 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2016/309/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4050397
49 A = 6782993
42 meter
Y = -3363565
80 meter E =
0010453
Z = 4267524
56 I = 52
00423
XDOT = 1614
342923 Wp = 91
08654
YDOT = -6562
235241 meter/sec RA = 78
99250 deg
ZDOT = -3632
540334 TA = 35
87545
MA = 35
80530
Ha = 222
400 n
mi
Hp = 215
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13288705
69 X = -4033214
46
Y = -11035320
87 feet Y = -3408763
98 meter
Z = 14001064
83 Z = 4247890
05
XDOT = 5296
400666 XDOT = 1705
249242
YDOT = -21529
643180 feet/sec YDOT = -6543
674295 meter/sec
ZDOT = -11917
783249 ZDOT = -3624
477267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6361928
89 X = -1939115
93
Y = 16133120
01 feet Y = 4917374
98 meter
Z = 13915678
98 Z = 4241498
95
XDOT = -20961
205845 XDOT = -6388
975542
YDOT = 2003
631130 feet/sec YDOT = 610
706768 meter/sec
ZDOT = -11881
272017 ZDOT = -3621
411711
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 16309
22220812
00016717 00000-0 10270-3 0 9128
2 25544 51
6444 79
6137 0003123 164
8401 195
2845 15
53680933 26760
Satellite: ISS
Catalog Number: 25544
Epoch time: 16309
22220812 = yrday
fracday
Element set: 912
Inclination: 51
6444 deg
RA of node: 79
6137 deg
Eccentricity:
0003123
Arg of perigee: 164
8401 deg
Mean anomaly: 195
2845 deg
Mean motion: 15
53680933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 302
Coasting Arc #14 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2016/310/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3883492
54 A = 6786481
35 meter
Y = 4580938
34 meter E =
0005379
Z = -3167292
62 I = 52
00824
XDOT = -2408
127963 Wp = 111
50355
YDOT = 5403
253701 meter/sec RA = 74
03613 deg
ZDOT = 4866
913682 TA = 212
20288
MA = 212
23574
Ha = 222
222 n
mi
Hp = 215
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12741117
26 X = 3847364
33
Y = 15029325
26 feet Y = 4624164
16 meter
Z = -10391379
97 Z = -3148514
96
XDOT = -7900
682292 XDOT = -2492
011376
YDOT = 17727
210305 feet/sec YDOT = 5375
855371 meter/sec
ZDOT = 15967
564575 ZDOT = 4855
011634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10046374
43 X = 3062134
93
Y = -16999183
26 feet Y = -5181351
06 meter
Z = -10309975
46 Z = -3142480
52
XDOT = 18128
298756 XDOT = 5525
505461
YDOT = 1071
037661 feet/sec YDOT = 326
452279 meter/sec
ZDOT = 15914
436754 ZDOT = 4850
720323
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 16310
18703017
00016717 00000-0 10270-3 0 9139
2 25544 51
6439 74
8078 0003086 168
9128 191
2093 15
53669174 26916
Satellite: ISS
Catalog Number: 25544
Epoch time: 16310
18703017 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 74
8078 deg
Eccentricity:
0003086
Arg of perigee: 168
9128 deg
Mean anomaly: 191
2093 deg
Mean motion: 15
53669174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 319
Coasting Arc #15 (Orbit 2706)
---------------------------------------
Vector Time (GMT): 2016/311/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3570035
99 A = 6789407
07 meter
Y = -5489082
33 meter E =
0015957
Z = 1761266
51 I = 52
00811
XDOT = 3258
632024 Wp = 124
61448
YDOT = -3959
355159 meter/sec RA = 69
08811 deg
ZDOT = -5706
630381 TA = 36
14165
MA = 36
03391
Ha = 222
266 n
mi
Hp = 215
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11712716
50 X = -3516945
95
Y = -18008800
30 feet Y = -5528708
02 meter
Z = 5778433
42 Z = 1744052
84
XDOT = 10691
049949 XDOT = 3330
385166
YDOT = -12990
010365 feet/sec YDOT = -3922
513761 meter/sec
ZDOT = -18722
540619 ZDOT = -5690
626212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12914624
92 X = -3936377
68
Y = 17192182
33 feet Y = 5240177
17 meter
Z = 5704054
61 Z = 1738595
85
XDOT = -14648
811061 XDOT = -4464
957611
YDOT = -4785
155325 feet/sec YDOT = -1458
515343 meter/sec
ZDOT = -18651
701964 ZDOT = -5685
038759
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 16311
21616389
00016717 00000-0 10270-3 0 9140
2 25544 51
6439 69
6820 0003211 171
4061 188
7147 15
53662558 27076
Satellite: ISS
Catalog Number: 25544
Epoch time: 16311
21616389 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 69
6820 deg
Eccentricity:
0003211
Arg of perigee: 171
4061 deg
Mean anomaly: 188
7147 deg
Mean motion: 15
53662558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2707
Checksum: 310
Coasting Arc #16 (Orbit 2712)
---------------------------------------
Vector Time (GMT): 2016/311/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4046521
82 A = 6778708
49 meter
Y = -1137595
04 meter E =
0015566
Z = -5331270
13 I = 51
96763
XDOT = 2636
114141 Wp = 106
47432
YDOT = 7173
274311 meter/sec RA = 67
08215 deg
ZDOT = 467
045305 TA = 167
98590
MA = 167
94873
Ha = 222
153 n
mi
Hp = 215
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13275990
22 X = 4084839
37
Y = -3732267
18 feet Y = -1092129
89 meter
Z = -17491043
72 Z = -5311519
75
XDOT = 8648
668440 XDOT = 2553
436090
YDOT = 23534
364537 feet/sec YDOT = 7202
290830 meter/sec
ZDOT = 1532
300870 ZDOT = 479
650239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 532580
74 X = 162330
61
Y = 13889721
58 feet Y = 4233587
14 meter
Z = -17404319
49 Z = -5304836
58
XDOT = -23882
220257 XDOT = -7279
300734
YDOT = 2916
333507 feet/sec YDOT = 888
898453 meter/sec
ZDOT = 1586
174644 ZDOT = 483
466032
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 16311
60208384
00016717 00000-0 10270-3 0 9156
2 25544 51
6436 67
7560 0003499 176
8986 183
2189 15
53691296 27130
Satellite: ISS
Catalog Number: 25544
Epoch time: 16311
60208384 = yrday
fracday
Element set: 915
Inclination: 51
6436 deg
RA of node: 67
7560 deg
Eccentricity:
0003499
Arg of perigee: 176
8986 deg
Mean anomaly: 183
2189 deg
Mean motion: 15
53691296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2713
Checksum: 340
Coasting Arc #17 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2016/312/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4594095
62 A = 6780083
60 meter
Y = -370986
67 meter E =
0005425
Z = 4967914
61 I = 51
96006
XDOT = -1814
151885 Wp = 88
75790
YDOT = -7119
433829 meter/sec RA = 62
11001 deg
ZDOT = -2207
109804 TA = 22
68065
MA = 22
65668
Ha = 222
111 n
mi
Hp = 215
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15072492
20 X = -4613738
04
Y = -1217147
86 feet Y = -422470
69 meter
Z = 16298932
46 Z = 4945549
63
XDOT = -5951
941879 XDOT = -1723
684384
YDOT = -23357
722536 feet/sec YDOT = -7139
215091 meter/sec
ZDOT = -7241
173896 ZDOT = -2215
702782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4446757
58 X = 1355371
71
Y = -14562603
32 feet Y = -4438681
49 meter
Z = 16201037
03 Z = 4938076
09
XDOT = 23019
563468 XDOT = 7016
362945
YDOT = -1075
164984 feet/sec YDOT = -327
710287 meter/sec
ZDOT = -7277
473907 ZDOT = -2218
174047
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 16312
63119734
00016717 00000-0 10270-3 0 9161
2 25544 51
6443 62
6290 0003339 180
5808 179
5341 15
53747035 27298
Satellite: ISS
Catalog Number: 25544
Epoch time: 16312
63119734 = yrday
fracday
Element set: 916
Inclination: 51
6443 deg
RA of node: 62
6290 deg
Eccentricity:
0003339
Arg of perigee: 180
5808 deg
Mean anomaly: 179
5341 deg
Mean motion: 15
53747035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2729
Checksum: 313
Coasting Arc #18 (Orbit 2743)
---------------------------------------
Vector Time (GMT): 2016/313/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5043705
07 A = 6783111
51 meter
Y = 1772232
56 meter E =
0009276
Z = -4185238
28 I = 51
95302
XDOT = 785
058443 Wp = 129
29147
YDOT = 6629
613196 meter/sec RA = 57
14383 deg
ZDOT = 3753
224800 TA = 179
19350
MA = 179
19200
Ha = 221
929 n
mi
Hp = 215
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16547588
80 X = 5043843
02
Y = 5814411
29 feet Y = 1828635
31 meter
Z = -13731096
72 Z = -4160736
59
XDOT = 2575
651061 XDOT = 692
634261
YDOT = 21750
699463 feet/sec YDOT = 6637
875577 meter/sec
ZDOT = 12313
729658 ZDOT = 3756
813796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8990806
21 X = -2740397
73
Y = 15156587
63 feet Y = 4619727
91 meter
Z = -13624108
99 Z = -4152628
42
XDOT = -20710
260206 XDOT = -6312
487311
YDOT = -1203
038943 feet/sec YDOT = -366
686270 meter/sec
ZDOT = 12328
193857 ZDOT = 3757
633488
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 16313
59598118
00016717 00000-0 10270-3 0 9175
2 25544 51
6430 57
8237 0003366 181
1649 178
9496 15
53758021 27449
Satellite: ISS
Catalog Number: 25544
Epoch time: 16313
59598118 = yrday
fracday
Element set: 917
Inclination: 51
6430 deg
RA of node: 57
8237 deg
Eccentricity:
0003366
Arg of perigee: 181
1649 deg
Mean anomaly: 178
9496 deg
Mean motion: 15
53758021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2744
Checksum: 338
Coasting Arc #19 (Orbit 2759)
---------------------------------------
Vector Time (GMT): 2016/314/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5293679
85 A = 6786616
77 meter
Y = -2981811
03 meter E =
0013621
Z = 3006855
02 I = 51
94685
XDOT = 432
477455 Wp = 110
68949
YDOT = -5812
518515 meter/sec RA = 52
18418 deg
ZDOT = -4989
205296 TA = 35
02733
MA = 34
93782
Ha = 221
885 n
mi
Hp = 215
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17367716
04 X = -5274549
27
Y = -9782844
59 feet Y = -3040901
43 meter
Z = 9865009
90 Z = 2981185
84
XDOT = 1418
889288 XDOT = 521
678167
YDOT = -19069
942635 feet/sec YDOT = -5807
183713 meter/sec
ZDOT = -16368
783778 ZDOT = -4986
887500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12775902
20 X = 3894094
99
Y = -15372460
03 feet Y = -4685525
82 meter
Z = 9753144
35 Z = 2972758
40
XDOT = 17359
286941 XDOT = 5291
110660
YDOT = 4020
571267 feet/sec YDOT = 1225
470122 meter/sec
ZDOT = -16357
522304 ZDOT = -4985
772798
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 16314
62507022
00016717 00000-0 10270-3 0 9185
2 25544 51
6433 52
6970 0003209 186
4268 173
6844 15
53772717 27605
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
62507022 = yrday
fracday
Element set: 918
Inclination: 51
6433 deg
RA of node: 52
6970 deg
Eccentricity:
0003209
Arg of perigee: 186
4268 deg
Mean anomaly: 173
6844 deg
Mean motion: 15
53772717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2760
Checksum: 314
Coasting Arc #20 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5299017
91 A = 6788026
68 meter
Y = -3474903
40 meter E =
0014605
Z = 2411130
61 I = 51
94365
XDOT = 1054
760333 Wp = 117
38316
YDOT = -5359
408974 meter/sec RA = 50
58581 deg
ZDOT = -5387
465015 TA = 35
76776
MA = 35
67002
Ha = 221
849 n
mi
Hp = 215
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17385229
36 X = -5271479
24
Y = -11400601
69 feet Y = -3534006
49 meter
Z = 7910533
51 Z = 2385455
94
XDOT = 3460
499779 XDOT = 1140
782634
YDOT = -17583
362775 feet/sec YDOT = -5347
133192 meter/sec
ZDOT = -17675
410153 ZDOT = -5382
131994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19917740
25 X = -6070927
23
Y = -6104074
40 feet Y = -1860521
88 meter
Z = 7798740
82 Z = 2377056
20
XDOT = -1898
980451 XDOT = -578
809241
YDOT = -16433
250946 feet/sec YDOT = -5008
854888 meter/sec
ZDOT = -17651
026025 ZDOT = -5380
032733
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 16314
94665943
00016717 00000-0 10270-3 0 9198
2 25544 51
6419 51
0955 0002901 185
8519 174
2600 15
53753479 27651
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
94665943 = yrday
fracday
Element set: 919
Inclination: 51
6419 deg
RA of node: 51
0955 deg
Eccentricity:
0002901
Arg of perigee: 185
8519 deg
Mean anomaly: 174
2600 deg
Mean motion: 15
53753479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 333
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