[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 14th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
322/07:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 216
8
322/20:20:13
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 217
0
324/22:01:46
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 217
2
326/13:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 217
3
328/20:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 217
6
332/03:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 217
6
Coasting Arc #1 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2016/319/13:58:16
517
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5117242
22 A = 6789636
30 meter
Y = 4134464
47 meter E =
0009290
Z = 1669270
05 I = 51
83381
XDOT = -4205
608378 Wp = 85
80478
YDOT = 2884
199457 meter/sec RA = 27
43285 deg
ZDOT = 5722
165335 TA = 292
42425
MA = 292
52263
Ha = 221
986 n
mi
Hp = 216
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16788852
43 X = 5062520
43
Y = 13564515
98 feet Y = 4191382
92 meter
Z = 5476607
76 Z = 1693996
18
XDOT = -13797
927750 XDOT = -4265
344267
YDOT = 9462
596644 feet/sec YDOT = 2836
835428 meter/sec
ZDOT = 18773
508316 ZDOT = 5701
589910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15554485
79 X = -4741007
27
Y = 14924178
87 feet Y = 4548889
72 meter
Z = 5584062
05 Z = 1702022
11
XDOT = -6560
129100 XDOT = -1999
527350
YDOT = -13859
804935 feet/sec YDOT = -4224
468544 meter/sec
ZDOT = 18682
830548 ZDOT = 5694
526751
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 16319
64312651
00016717 00000-0 10270-3 0 9005
2 25544 51
6428 27
7119 0006342 211
5200 148
5573 15
53601135 28385
Satellite: ISS
Catalog Number: 25544
Epoch time: 16319
64312651 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 27
7119 deg
Eccentricity:
0006342
Arg of perigee: 211
5200 deg
Mean anomaly: 148
5573 deg
Mean motion: 15
53601135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 284
Coasting Arc #2 (Orbit 2852)
---------------------------------------
Vector Time (GMT): 2016/320/13:58:16
517
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4200877
54 A = 6786647
51 meter
Y = -4352266
53 meter E =
0006561
Z = -3069802
93 I = 51
79574
XDOT = 5560
216556 Wp = 173
69761
YDOT = -1896
658381 meter/sec RA = 22
47208 deg
ZDOT = -4927
225854 TA = 41
46542
MA = 41
41566
Ha = 221
763 n
mi
Hp = 216
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13782406
62 X = -4136985
00
Y = -14279089
67 feet Y = -4398886
20 meter
Z = -10071531
91 Z = -3090055
24
XDOT = 18242
180302 XDOT = 5604
947171
YDOT = -6222
632485 feet/sec YDOT = -1834
230007 meter/sec
ZDOT = -16165
439152 ZDOT = -4900
106455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15678279
63 X = 4778739
63
Y = -12093891
32 feet Y = -3686218
07 meter
Z = -10159342
00 Z = -3096567
44
XDOT = 3323
787348 XDOT = 1013
090384
YDOT = 17768
309558 feet/sec YDOT = 5415
780753 meter/sec
ZDOT = -16046
300459 ZDOT = -4890
912380
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 16320
60796181
00016717 00000-0 10270-3 0 9018
2 25544 51
6433 22
9064 0006464 214
7942 145
2788 15
53651978 28539
Satellite: ISS
Catalog Number: 25544
Epoch time: 16320
60796181 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 22
9064 deg
Eccentricity:
0006464
Arg of perigee: 214
7942 deg
Mean anomaly: 145
2788 deg
Mean motion: 15
53651978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2853
Checksum: 321
Coasting Arc #3 (Orbit 2868)
---------------------------------------
Vector Time (GMT): 2016/321/13:58:16
517
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3005168
77 A = 6783221
84 meter
Y = 4409141
11 meter E =
0009698
Z = 4188175
94 I = 51
75274
XDOT = -6632
879218 Wp = 142
06840
YDOT = 979
779755 meter/sec RA = 17
50047 deg
ZDOT = 3715
819347 TA = 269
76225
MA = 269
87339
Ha = 221
633 n
mi
Hp = 216
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9859477
59 X = 2935296
51
Y = 14465686
07 feet Y = 4442356
02 meter
Z = 13740734
70 Z = 4202605
12
XDOT = -21761
414758 XDOT = -6661
392609
YDOT = 3214
500510 feet/sec YDOT = 905
446818 meter/sec
ZDOT = 12191
008355 ZDOT = 3683
528618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15295283
93 X = -4662002
54
Y = 8414504
87 feet Y = 2564741
08 meter
Z = 13803027
18 Z = 4207162
68
XDOT = -603
140395 XDOT = -183
837193
YDOT = -20926
523490 feet/sec YDOT = -6378
404360 meter/sec
ZDOT = 12049
408704 ZDOT = 3672
659773
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 16321
63711299
00016717 00000-0 10270-3 0 9020
2 25544 51
6419 17
7797 0006341 218
2014 141
8690 15
53650588 28698
Satellite: ISS
Catalog Number: 25544
Epoch time: 16321
63711299 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 17
7797 deg
Eccentricity:
0006341
Arg of perigee: 218
2014 deg
Mean anomaly: 141
8690 deg
Mean motion: 15
53650588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2869
Checksum: 322
Coasting Arc #4 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2016/322/07:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4108736
60 A = 6781747
33 meter
Y = 2753385
68 meter E =
0003731
Z = 4636270
56 I = 51
72580
XDOT = -5927
139839 Wp = 115
65275
YDOT = -3866
326266 meter/sec RA = 13
87120 deg
ZDOT = -2956
319849 TA = 3
75571
MA = 3
75291
Ha = 221
787 n
mi
Hp = 216
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13480106
96 X = -4161741
67
Y = 9033417
60 feet Y = 2707142
40 meter
Z = 15210861
43 Z = 4616182
43
XDOT = -19445
996846 XDOT = -5869
104305
YDOT = -12684
797460 feet/sec YDOT = -3932
282858 meter/sec
ZDOT = -9699
212103 ZDOT = -2984
972143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15494654
31 X = 4722770
63
Y = -5090859
11 feet Y = -1551693
86 meter
Z = 15122336
59 Z = 4609288
19
XDOT = 14931
397770 XDOT = 4551
090040
YDOT = 16261
093476 feet/sec YDOT = 4956
381292 meter/sec
ZDOT = -9823
894379 ZDOT = -2994
323007
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 16322
34465042
00016717 00000-0 10270-3 0 9032
2 25544 51
6426 14
2519 0006702 220
1622 139
9035 15
53635761 28808
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
34465042 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 14
2519 deg
Eccentricity:
0006702
Arg of perigee: 220
1622 deg
Mean anomaly: 139
9035 deg
Mean motion: 15
53635761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 284
Coasting Arc #5 (Orbit 2887)
---------------------------------------
Vector Time (GMT): 2016/322/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3384859
59 A = 6780627
53 meter
Y = -3268554
54 meter E =
0010389
Z = -4891063
14 I = 51
70493
XDOT = 6538
224055 Wp = 138
74179
YDOT = 3204
582879 meter/sec RA = 11
16341 deg
ZDOT = 2378
505133 TA = 154
58978
MA = 154
53866
Ha = 221
324 n
mi
Hp = 217
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11105182
39 X = 3444916
84
Y = -10723604
15 feet Y = -3230366
71 meter
Z = -16046795
08 Z = -4874474
42
XDOT = 21450
866322 XDOT = 6490
349740
YDOT = 10513
723355 feet/sec YDOT = 3277
429879 meter/sec
ZDOT = 7803
494531 ZDOT = 2410
150520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10921260
71 X = 3328800
27
Y = -11017899
66 feet Y = -3358255
82 meter
Z = -15973488
84 Z = -4868719
40
XDOT = 20867
111083 XDOT = 6360
295458
YDOT = 9148
144511 feet/sec YDOT = 2788
354447 meter/sec
ZDOT = 7941
416275 ZDOT = 2420
543681
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 16322
85921907
00016717 00000-0 10270-3 0 9046
2 25544 51
6423 11
6924 0006240 226
1048 133
9590 15
53672410 28881
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
85921907 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 11
6924 deg
Eccentricity:
0006240
Arg of perigee: 226
1048 deg
Mean anomaly: 133
9590 deg
Mean motion: 15
53672410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2888
Checksum: 301
Coasting Arc #6 (Orbit 2903)
---------------------------------------
Vector Time (GMT): 2016/323/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4698624
48 A = 6783769
82 meter
Y = 2719425
37 meter E =
0006061
Z = 4061510
50 I = 51
68330
XDOT = -5492
408787 Wp = 107
15770
YDOT = -3682
841168 meter/sec RA = 6
18092 deg
ZDOT = -3885
059866 TA = 23
06798
MA = 23
04078
Ha = 221
256 n
mi
Hp = 217
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15415434
65 X = -4748413
84
Y = 8921999
24 feet Y = 2666603
63 meter
Z = 13325165
69 Z = 4038564
72
XDOT = -18019
713867 XDOT = -5431
945970
YDOT = -12082
812232 feet/sec YDOT = -3743
922737 meter/sec
ZDOT = -12746
259402 ZDOT = -3911
594180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15097209
25 X = -4601629
38
Y = 9591363
77 feet Y = 2923447
68 meter
Z = 13224135
15 Z = 4030716
39
XDOT = -17747
675807 XDOT = -5409
491586
YDOT = -10188
608912 feet/sec YDOT = -3105
487996 meter/sec
ZDOT = -12861
700026 ZDOT = -3920
246168
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 16323
88835412
00016717 00000-0 10270-3 0 9056
2 25544 51
6420 6
5669 0006246 229
9696 130
0909 15
53670158 29041
Satellite: ISS
Catalog Number: 25544
Epoch time: 16323
88835412 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 6
5669 deg
Eccentricity:
0006246
Arg of perigee: 229
9696 deg
Mean anomaly: 130
0909 deg
Mean motion: 15
53670158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 321
Coasting Arc #7 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2016/324/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5750672
48 A = 6787160
49 meter
Y = -2161918
67 meter E =
0001825
Z = -2885924
79 I = 51
66327
XDOT = 4069
939211 Wp = 212
04329
YDOT = 4080
206792 meter/sec RA = 1
20295 deg
ZDOT = 5050
449008 TA = 115
13359
MA = 115
11465
Ha = 220
953 n
mi
Hp = 217
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18867035
71 X = 5788438
90
Y = -7092909
04 feet Y = -2097399
55 meter
Z = -9468257
17 Z = -2857897
56
XDOT = 13352
818933 XDOT = 3999
477707
YDOT = 13386
505222 feet/sec YDOT = 4125
325475 meter/sec
ZDOT = 16569
714593 ZDOT = 5070
048878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18461459
46 X = 5627052
84
Y = -8232012
80 feet Y = -2509117
50 meter
Z = -9345093
30 Z = -2848384
44
XDOT = 13434
689762 XDOT = 4094
893439
YDOT = 11211
311195 feet/sec YDOT = 3417
207652 meter/sec
ZDOT = 16654
707370 ZDOT = 5076
354806
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 16324
85316247
00016717 00000-0 10270-3 0 9065
2 25544 51
6426 1
7602 0006307 233
9488 126
1080 15
53691894 29195
Satellite: ISS
Catalog Number: 25544
Epoch time: 16324
85316247 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 1
7602 deg
Eccentricity:
0006307
Arg of perigee: 233
9488 deg
Mean anomaly: 126
1080 deg
Mean motion: 15
53691894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 314
Coasting Arc #8 (Orbit 2920)
---------------------------------------
Vector Time (GMT): 2016/324/22:01:46
000
Vector Time (MET): N/A
Weight (LBS) : 909067
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6780830
90 A = 6790574
88 meter
Y = 239216
93 meter E =
0006247
Z = 171237
46 I = 51
67380
XDOT = -322
149375 Wp = 39
36375
YDOT = 4746
668999 meter/sec RA =
87733 deg
ZDOT = 6010
213192 TA = 322
47921
MA = 322
52279
Ha = 220
913 n
mi
Hp = 217
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22246820
53 X = 6776820
14
Y = 784832
45 feet Y = 315022
30 meter
Z = 561802
69 Z = 204167
56
XDOT = -1056
920522 XDOT = -404
399155
YDOT = 15573
061020 feet/sec YDOT = 4742
606467 meter/sec
ZDOT = 19718
547217 ZDOT = 6008
448605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19844220
56 X = 6048518
43
Y = -10077755
62 feet Y = -3071699
91 meter
Z = 705946
23 Z = 215172
41
XDOT = 5766
001552 XDOT = 1757
477273
YDOT = 12755
702168 feet/sec YDOT = 3887
938021 meter/sec
ZDOT = 19709
854989 ZDOT = 6007
563801
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 16324
98180221
00016717 00000-0 10270-3 0 9071
2 25544 51
6439 1
1199 0006364 235
3896 124
6656 15
53692857 29211
Satellite: ISS
Catalog Number: 25544
Epoch time: 16324
98180221 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 1
1199 deg
Eccentricity:
0006364
Arg of perigee: 235
3896 deg
Mean anomaly: 124
6656 deg
Mean motion: 15
53692857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2921
Checksum: 326
Coasting Arc #9 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2016/325/22:01:46
000
Vector Time (MET): N/A
Weight (LBS) : 909067
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6497493
32 A = 6789348
53 meter
Y = -904519
39 meter E =
0009275
Z = -1725335
46 I = 51
63781
XDOT = 2158
651909 Wp = 184
81902
YDOT = -4668
506006 meter/sec RA = 355
91007 deg
ZDOT = -5688
646720 TA = 14
10941
MA = 14
08352
Ha = 220
745 n
mi
Hp = 217
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21317235
31 X = -6478514
85
Y = -2967583
31 feet Y = -977072
59 meter
Z = -5660549
41 Z = -1756852
81
XDOT = 7082
191301 XDOT = 2238
329108
YDOT = -15316
620755 feet/sec YDOT = -4643
920946 meter/sec
ZDOT = -18663
539107 ZDOT = -5677
966973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19922990
25 X = -6072527
43
Y = 8045266
06 feet Y = 2452197
10 meter
Z = -5798365
72 Z = -1767341
87
XDOT = -813
879084 XDOT = -248
070345
YDOT = -15416
494379 feet/sec YDOT = -4698
947487 meter/sec
ZDOT = -18615
829739 ZDOT = -5674
104905
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 16325
94660415
00016717 00000-0 10270-3 0 9087
2 25544 51
6444 356
3143 0006447 238
4018 121
6506 15
53666398 29361
Satellite: ISS
Catalog Number: 25544
Epoch time: 16325
94660415 = yrday
fracday
Element set: 908
Inclination: 51
6444 deg
RA of node: 356
3143 deg
Eccentricity:
0006447
Arg of perigee: 238
4018 deg
Mean anomaly: 121
6506 deg
Mean motion: 15
53666398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 322
Coasting Arc #10 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2016/326/13:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6467245
22 A = 6790079
64 meter
Y = 1714555
56 meter E =
0012304
Z = 1110268
37 I = 51
61716
XDOT = -2183
306756 Wp = 149
41674
YDOT = -4415
969533 meter/sec RA = 352
70472 deg
ZDOT = -5879
873458 TA = 18
52895
MA = 18
48419
Ha = 220
723 n
mi
Hp = 217
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21217996
12 X = -6491330
41
Y = 5625182
27 feet Y = 1642099
80 meter
Z = 3642612
76 Z = 1078793
36
XDOT = -7163
079907 XDOT = -2105
201856
YDOT = -14488
089019 feet/sec YDOT = -4439
948003 meter/sec
ZDOT = -19290
923420 ZDOT = -5890
289812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1896207
51 X = -577964
05
Y = -21891501
79 feet Y = -6672529
74 meter
Z = 3504455
62 Z = 1068158
07
XDOT = 13886
442968 XDOT = 4232
587817
YDOT = -4308
116921 feet/sec YDOT = -1313
114038 meter/sec
ZDOT = -19335
635174 ZDOT = -5893
501601
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 16326
58980138
00016717 00000-0 10270-3 0 9096
2 25544 51
6417 353
1088 0006071 238
8234 121
2324 15
53705084 29462
Satellite: ISS
Catalog Number: 25544
Epoch time: 16326
58980138 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 353
1088 deg
Eccentricity:
0006071
Arg of perigee: 238
8234 deg
Mean anomaly: 121
2324 deg
Mean motion: 15
53705084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 312
Coasting Arc #11 (Orbit 2961)
---------------------------------------
Vector Time (GMT): 2016/327/13:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6683978
04 A = 6790323
15 meter
Y = -1082541
61 meter E =
0006905
Z = 456630
07 I = 51
58584
XDOT = 361
925610 Wp = 39
35566
YDOT = 4777
640052 meter/sec RA = 347
73469 deg
ZDOT = 5984
259489 TA = 325
57061
MA = 325
61533
Ha = 220
505 n
mi
Hp = 217
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21929061
83 X = 6693368
40
Y = -3551645
70 feet Y = -1007744
37 meter
Z = 1498130
14 Z = 489122
31
XDOT = 1187
419979 XDOT = 279
404661
YDOT = 15674
672087 feet/sec YDOT = 4781
225966 meter/sec
ZDOT = 19633
397275 ZDOT = 5985
817199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 118619
15 X = 36155
12
Y = 22204429
35 feet Y = 6767910
07 meter
Z = 1640603
65 Z = 500055
99
XDOT = -14032
615284 XDOT = -4277
141138
YDOT = -1385
947873 feet/sec YDOT = -422
436912 meter/sec
ZDOT = 19639
251192 ZDOT = 5986
043763
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 16327
61891221
00016717 00000-0 10270-3 0 9107
2 25544 51
6409 347
9827 0006292 242
2459 117
8056 15
53750014 29622
Satellite: ISS
Catalog Number: 25544
Epoch time: 16327
61891221 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 347
9827 deg
Eccentricity:
0006292
Arg of perigee: 242
2459 deg
Mean anomaly: 117
8056 deg
Mean motion: 15
53750014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2962
Checksum: 313
Coasting Arc #12 (Orbit 2976)
---------------------------------------
Vector Time (GMT): 2016/328/13:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6473492
08 A = 6788768
35 meter
Y = 347526
63 meter E =
0007512
Z = -1998236
76 I = 51
54866
XDOT = 1443
944984 Wp = 189
49573
YDOT = -5074
538791 meter/sec RA = 342
75970 deg
ZDOT = -5564
616238 TA = 12
59838
MA = 12
57962
Ha = 220
201 n
mi
Hp = 217
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21238491
09 X = -6467190
39
Y = 1140179
25 feet Y = 275170
92 meter
Z = -6555894
87 Z = -2029668
46
XDOT = 4737
352310 XDOT = 1527
613320
YDOT = -16648
749313 feet/sec YDOT = -5057
923839 meter/sec
ZDOT = -18256
614954 ZDOT = -5557
398574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1788852
11 X = 545242
12
Y = -21150636
72 feet Y = -6446714
07 meter
Z = -6693567
40 Z = -2040199
34
XDOT = 14281
210505 XDOT = 4352
912962
YDOT = 6970
893172 feet/sec YDOT = 2124
728239 meter/sec
ZDOT = -18223
993759 ZDOT = -5554
673298
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 16328
58370184
00016717 00000-0 10270-3 0 9115
2 25544 51
6405 343
1759 0006078 247
1462 112
9049 15
53714253 29779
Satellite: ISS
Catalog Number: 25544
Epoch time: 16328
58370184 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 343
1759 deg
Eccentricity:
0006078
Arg of perigee: 247
1462 deg
Mean anomaly: 112
9049 deg
Mean motion: 15
53714253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2977
Checksum: 318
Coasting Arc #13 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2016/328/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4617015
52 A = 6786896
20 meter
Y = -4018291
49 meter E =
0001753
Z = -2931025
54 I = 51
53736
XDOT = 5278
984930 Wp = 264
39097
YDOT = 2412
653144 meter/sec RA = 341
32461 deg
ZDOT = 5005
194172 TA = 62
13303
MA = 62
11527
Ha = 220
114 n
mi
Hp = 217
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15147688
72 X = 4675843
80
Y = -13183371
02 feet Y = -3966332
00 meter
Z = -9616225
52 Z = -2908454
02
XDOT = 17319
504364 XDOT = 5227
300264
YDOT = 7915
528689 feet/sec YDOT = 2471
397338 meter/sec
ZDOT = 16421
240723 ZDOT = 5030
712966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14501646
19 X = 4420101
76
Y = -13959300
03 feet Y = -4254794
65 meter
Z = -9516603
32 Z = -2900660
69
XDOT = 16584
100494 XDOT = 5054
833831
YDOT = 5951
376718 feet/sec YDOT = 1813
979624 meter/sec
ZDOT = 16532
468983 ZDOT = 5039
096546
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 16328
84097784
00016717 00000-0 10270-3 0 9127
2 25544 51
6441 341
8952 0006272 250
1664 109
8812 15
53738733 29810
Satellite: ISS
Catalog Number: 25544
Epoch time: 16328
84097784 = yrday
fracday
Element set: 912
Inclination: 51
6441 deg
RA of node: 341
8952 deg
Eccentricity:
0006272
Arg of perigee: 250
1664 deg
Mean anomaly: 109
8812 deg
Mean motion: 15
53738733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 331
Coasting Arc #14 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2016/329/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5487920
38 A = 6789671
27 meter
Y = 3697366
41 meter E =
0010538
Z = 1490271
84 I = 51
51544
XDOT = -3812
142896 Wp = 143
13736
YDOT = -3330
778080 meter/sec RA = 336
34468 deg
ZDOT = -5761
629562 TA = 20
56198
MA = 20
51960
Ha = 220
055 n
mi
Hp = 217
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18004988
13 X = -5536096
62
Y = 12130467
23 feet Y = 3635727
43 meter
Z = 4889343
30 Z = 1463495
44
XDOT = -12507
030499 XDOT = -3746
625977
YDOT = -10927
749606 feet/sec YDOT = -3373
041692 meter/sec
ZDOT = -18902
984127 ZDOT = -5779
989172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17152180
74 X = -5227984
69
Y = 13351781
66 feet Y = 4069623
05 meter
Z = 4771386
91 Z = 1454318
73
XDOT = -12138
287524 XDOT = -3699
750037
YDOT = -8794
132051 feet/sec YDOT = -2680
451449 meter/sec
ZDOT = -18982
682389 ZDOT = -5785
921592
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 16329
87007771
00016717 00000-0 10270-3 0 9139
2 25544 51
6435 336
7692 0006162 253
0631 106
9846 15
53703141 29978
Satellite: ISS
Catalog Number: 25544
Epoch time: 16329
87007771 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 336
7692 deg
Eccentricity:
0006162
Arg of perigee: 253
0631 deg
Mean anomaly: 106
9846 deg
Mean motion: 15
53703141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 321
Coasting Arc #15 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2016/330/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5983667
73 A = 6790432
41 meter
Y = -3198927
51 meter E =
0007722
Z = 75078
90 I = 51
48889
XDOT = 2190
634039 Wp = 20
76510
YDOT = 4242
707502 meter/sec RA = 331
36609 deg
ZDOT = 5998
847537 TA = 340
04511
MA = 340
07529
Ha = 219
681 n
mi
Hp = 217
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19631455
81 X = 6018629
53
Y = -10495169
00 feet Y = -3131818
64 meter
Z = 246321
85 Z = 104231
49
XDOT = 7187
119549 XDOT = 2113
887821
YDOT = 13919
644034 feet/sec YDOT = 4266
775463 meter/sec
ZDOT = 19681
258322 ZDOT = 6009
302924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18648566
85 X = 5684083
18
Y = -12152940
17 feet Y = -3704216
16 meter
Z = 374571
21 Z = 114169
31
XDOT = 7350
320266 XDOT = 2240
377617
YDOT = 11899
117888 feet/sec YDOT = 3626
851132 meter/sec
ZDOT = 19726
171541 ZDOT = 6012
537086
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 16330
89917050
00016717 00000-0 10270-3 0 9144
2 25544 51
6431 331
6420 0006290 258
6555 101
3891 15
53747302 30131
Satellite: ISS
Catalog Number: 25544
Epoch time: 16330
89917050 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 331
6420 deg
Eccentricity:
0006290
Arg of perigee: 258
6555 deg
Mean anomaly: 101
3891 deg
Mean motion: 15
53747302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 289
Coasting Arc #16 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2016/331/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6097139
73 A = 6789330
87 meter
Y = 2479328
09 meter E =
0007243
Z = -1645119
53 I = 51
45745
XDOT = -535
411002 Wp = 192
33838
YDOT = -5098
599199 meter/sec RA = 326
38612 deg
ZDOT = -5701
943493 TA = 5
72232
MA = 5
71405
Ha = 219
475 n
mi
Hp = 217
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20003739
27 X = -6116419
61
Y = 8134278
52 feet Y = 2411038
02 meter
Z = -5397373
78 Z = -1674785
27
XDOT = -1756
597775 XDOT = -450
659227
YDOT = -16727
687660 feet/sec YDOT = -5104
112506 meter/sec
ZDOT = -18707
163692 ZDOT = -5704
338710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19018405
38 X = -5796809
96
Y = 10158361
47 feet Y = 3096268
58 meter
Z = -5527717
86 Z = -1684848
41
XDOT = -2618
553174 XDOT = -798
135007
YDOT = -15083
192470 feet/sec YDOT = -4597
357065 meter/sec
ZDOT = -18716
625245 ZDOT = -5704
827375
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 16331
86394258
00016717 00000-0 10270-3 0 9152
2 25544 51
6434 326
8361 0006424 261
2742 98
7683 15
53713870 30288
Satellite: ISS
Catalog Number: 25544
Epoch time: 16331
86394258 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 326
8361 deg
Eccentricity:
0006424
Arg of perigee: 261
2742 deg
Mean anomaly: 98
7683 deg
Mean motion: 15
53713870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 324
Coasting Arc #17 (Orbit 3032)
---------------------------------------
Vector Time (GMT): 2016/332/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4900561
24 A = 6781363
26 meter
Y = 1018081
57 meter E =
0004980
Z = 4576616
08 I = 51
42210
XDOT = -4029
016249 Wp = 162
97854
YDOT = 5778
628924 meter/sec RA = 324
90363 deg
ZDOT = 3023
221957 TA = 256
69753
MA = 256
75306
Ha = 219
562 n
mi
Hp = 217
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16077956
84 X = 4866580
89
Y = 3340162
62 feet Y = 1072692
80 meter
Z = 15015144
62 Z = 4600339
76
XDOT = -13218
557246 XDOT = -4108
020717
YDOT = 18958
756312 feet/sec YDOT = 5733
131928 meter/sec
ZDOT = 9918
707207 ZDOT = 3003
457884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3199657
46 X = -975255
59
Y = -16009268
98 feet Y = -4879625
19 meter
Z = 15118778
03 Z = 4608203
54
XDOT = 21484
429764 XDOT = 6548
454192
YDOT = 5007
210484 feet/sec YDOT = 1526
197756 meter/sec
ZDOT = 9831
042870 ZDOT = 2996
501867
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 16332
18553099
00016717 00000-0 10270-3 0 9169
2 25544 51
6421 325
2277 0006385 258
6099 101
4336 15
53773128 30339
Satellite: ISS
Catalog Number: 25544
Epoch time: 16332
18553099 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 325
2277 deg
Eccentricity:
0006385
Arg of perigee: 258
6099 deg
Mean anomaly: 101
4336 deg
Mean motion: 15
53773128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3033
Checksum: 312
Coasting Arc #18 (Orbit 3047)
---------------------------------------
Vector Time (GMT): 2016/333/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3826986
50 A = 6778990
55 meter
Y = -2169467
83 meter E =
0007755
Z = -5164649
23 I = 51
38815
XDOT = 5015
177377 Wp = 77
21364
YDOT = -5633
289212 meter/sec RA = 319
89592 deg
ZDOT = -1349
936459 TA = 179
75584
MA = 179
75546
Ha = 219
419 n
mi
Hp = 217
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12555729
98 X = -3777354
37
Y = -7117676
61 feet Y = -2211986
02 meter
Z = -16944387
24 Z = -5183119
70
XDOT = 16453
994018 XDOT = 5084
355060
YDOT = -18481
919987 feet/sec YDOT = -5576
819273 meter/sec
ZDOT = -4428
925391 ZDOT = -1325
405722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1417114
43 X = -431936
48
Y = 14267727
95 feet Y = 4348803
48 meter
Z = -17024795
46 Z = -5189157
66
XDOT = -22560
947579 XDOT = -6876
576822
YDOT = -7395
996896 feet/sec YDOT = -2254
299854 meter/sec
ZDOT = -4320
432389 ZDOT = -1316
867792
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 16333
15029592
00016717 00000-0 10270-3 0 9174
2 25544 51
6421 320
4220 0006235 262
9546 97
0898 15
53762949 30481
Satellite: ISS
Catalog Number: 25544
Epoch time: 16333
15029592 = yrday
fracday
Element set: 917
Inclination: 51
6421 deg
RA of node: 320
4220 deg
Eccentricity:
0006235
Arg of perigee: 262
9546 deg
Mean anomaly: 97
0898 deg
Mean motion: 15
53762949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3048
Checksum: 319
Coasting Arc #19 (Orbit 3063)
---------------------------------------
Vector Time (GMT): 2016/334/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2638400
59 A = 6778437
07 meter
Y = 3334465
93 meter E =
0003733
Z = 5282195
60 I = 51
36224
XDOT = -5644
776368 Wp = 278
85489
YDOT = 5167
344986 meter/sec RA = 314
88116 deg
ZDOT = -442
163002 TA = 175
38176
MA = 175
37832
Ha = 219
181 n
mi
Hp = 217
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8656169
91 X = 2575258
53
Y = 10939848
85 feet Y = 3363616
92 meter
Z = 17330038
06 Z = 5294859
37
XDOT = -18519
607506 XDOT = -5699
991531
YDOT = 16953
231581 feet/sec YDOT = 5103
912606 meter/sec
ZDOT = -1450
666017 ZDOT = -469
718229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6287447
71 X = 1916414
06
Y = -12376450
70 feet Y = -3772342
17 meter
Z = 17384799
64 Z = 5298886
93
XDOT = 22298
901461 XDOT = 6796
705165
YDOT = 9118
305315 feet/sec YDOT = 2779
259460 meter/sec
ZDOT = -1572
298598 ZDOT = -479
236613
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 16334
17937211
00016717 00000-0 10270-3 0 9184
2 25544 51
6420 315
2944 0006254 266
8861 93
1576 15
53781190 30646
Satellite: ISS
Catalog Number: 25544
Epoch time: 16334
17937211 = yrday
fracday
Element set: 918
Inclination: 51
6420 deg
RA of node: 315
2944 deg
Eccentricity:
0006254
Arg of perigee: 266
8861 deg
Mean anomaly: 93
1576 deg
Mean motion: 15
53781190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3064
Checksum: 314
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