[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 19th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
141/14:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 213
2
Coasting Arc #1 (Orbit 34)
---------------------------------------
Vector Time (GMT): 2016/139/10:09:26
369
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 174207
82 A = 6777123
94 meter
Y = 4533732
87 meter E =
0014151
Z = -5047077
36 I = 51
46301
XDOT = -7211
023363 Wp = 80
39451
YDOT = -1788
904038 meter/sec RA = 205
42200 deg
ZDOT = -1857
996955 TA = 171
54856
MA = 171
52470
Ha = 220
726 n
mi
Hp = 213
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 571547
95 X = 148014
46
Y = 14874451
67 feet Y = 4535534
62 meter
Z = -16558652
74 Z = -5046294
61
XDOT = -23658
213132 XDOT = -7181
457952
YDOT = -5869
107735 feet/sec YDOT = -1869
377153 meter/sec
ZDOT = -6095
790534 ZDOT = -1892
955102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7589421
72 X = 2313255
74
Y = 12808756
06 feet Y = 3904108
85 meter
Z = -16556008
16 Z = -5046271
29
XDOT = -22671
694840 XDOT = -6910
332587
YDOT = 5367
315204 feet/sec YDOT = 1635
957674 meter/sec
ZDOT = -6247
456342 ZDOT = -1904
224693
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 16139
44262190
00016717 00000-0 10270-3 0 9005
2 25544 51
6431 206
4229 0001520 118
5683 241
5623 15
54620425 352
Satellite: ISS
Catalog Number: 25544
Epoch time: 16139
44262190 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 206
4229 deg
Eccentricity:
0001520
Arg of perigee: 118
5683 deg
Mean anomaly: 241
5623 deg
Mean motion: 15
54620425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 35
Checksum: 271
Coasting Arc #2 (Orbit 50)
---------------------------------------
Vector Time (GMT): 2016/140/10:09:26
369
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1728168
29 A = 6775748
29 meter
Y = -3853229
29 meter E =
0003765
Z = 5295498
90 I = 51
48838
XDOT = 7117
328266 Wp = 95
42765
YDOT = 2855
773355 meter/sec RA = 200
40638 deg
ZDOT = -244
933691 TA = 356
90929
MA = 356
91162
Ha = 220
570 n
mi
Hp = 213
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5669843
48 X = 1745403
90
Y = -12641828
38 feet Y = -3833807
57 meter
Z = 17373684
05 Z = 5303935
79
XDOT = 23350
814521 XDOT = 7086
055120
YDOT = 9369
335153 feet/sec YDOT = 2935
189206 meter/sec
ZDOT = -803
588226 ZDOT = -210
434717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1272470
59 X = -387849
04
Y = -13749381
43 feet Y = -4190811
46 meter
Z = 17411007
32 Z = 5306875
03
XDOT = 23965
651915 XDOT = 7304
730704
YDOT = -3045
405841 feet/sec YDOT = -928
239700 meter/sec
ZDOT = -654
081095 ZDOT = -199
363918
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 16140
47111500
00016717 00000-0 10270-3 0 9019
2 25544 51
6429 201
2923 0001509 119
0179 241
1125 15
54680916 518
Satellite: ISS
Catalog Number: 25544
Epoch time: 16140
47111500 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 201
2923 deg
Eccentricity:
0001509
Arg of perigee: 119
0179 deg
Mean anomaly: 241
1125 deg
Mean motion: 15
54680916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 51
Checksum: 261
Coasting Arc #3 (Orbit 65)
---------------------------------------
Vector Time (GMT): 2016/141/10:09:26
369
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3566930
01 A = 6777493
15 meter
Y = 3056121
43 meter E =
0013748
Z = -4898732
57 I = 51
52346
XDOT = -6317
607180 Wp = 108
51617
YDOT = -3653
508693 meter/sec RA = 195
39436 deg
ZDOT = 2321
868925 TA = 184
26265
MA = 184
27437
Ha = 220
668 n
mi
Hp = 213
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11702526
28 X = -3577042
83
Y = 10026645
11 feet Y = 3016177
35 meter
Z = -16071957
25 Z = -4916084
57
XDOT = -20727
057676 XDOT = -6287
562047
YDOT = -11986
577078 feet/sec YDOT = -3723
988507 meter/sec
ZDOT = 7617
680199 ZDOT = 2291
251768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5030242
91 X = -1533218
04
Y = 14482128
58 feet Y = 4414152
79 meter
Z = -16147914
77 Z = -4921884
42
XDOT = -22929
153191 XDOT = -6988
805893
YDOT = 377
941316 feet/sec YDOT = 115
196513 meter/sec
ZDOT = 7485
167870 ZDOT = 2281
479167
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 16141
43532379
00016717 00000-0 10270-3 0 9028
2 25544 51
6417 196
4833 0001609 119
2724 240
8590 15
54673668 663
Satellite: ISS
Catalog Number: 25544
Epoch time: 16141
43532379 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 196
4833 deg
Eccentricity:
0001609
Arg of perigee: 119
2724 deg
Mean anomaly: 240
8590 deg
Mean motion: 15
54673668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 66
Checksum: 315
Coasting Arc #4 (Orbit 68)
---------------------------------------
Vector Time (GMT): 2016/141/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5747709
31 A = 6782835
62 meter
Y = -1263565
42 meter E =
0014114
Z = 3359615
91 I = 51
54526
XDOT = 3779
991718 Wp = 92
79435
YDOT = 4794
982339 meter/sec RA = 194
56114 deg
ZDOT = -4647
286561 TA = 47
92641
MA = 47
80644
Ha = 220
657 n
mi
Hp = 213
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18857314
01 X = 5745091
75
Y = -4145555
84 feet Y = -1199305
53 meter
Z = 11022361
90 Z = 3387530
95
XDOT = 12401
547630 XDOT = 3748
667038
YDOT = 15731
569354 feet/sec YDOT = 4837
077825 meter/sec
ZDOT = -15247
003153 ZDOT = -4628
999779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4082676
02 X = -1244399
65
Y = -18799481
82 feet Y = -5730082
06 meter
Z = 11143950
23 Z = 3396676
03
XDOT = 14400
324366 XDOT = 4389
218867
YDOT = -12149
927977 feet/sec YDOT = -3703
298047 meter/sec
ZDOT = -15168
292704 ZDOT = -4623
295616
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 16141
62816457
00016717 00000-0 10270-3 0 9032
2 25544 51
6405 195
5226 0001738 107
9306 252
2036 15
54677601 695
Satellite: ISS
Catalog Number: 25544
Epoch time: 16141
62816457 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 195
5226 deg
Eccentricity:
0001738
Arg of perigee: 107
9306 deg
Mean anomaly: 252
2036 deg
Mean motion: 15
54677601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 69
Checksum: 301
Coasting Arc #5 (Orbit 83)
---------------------------------------
Vector Time (GMT): 2016/142/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6554523
52 A = 6786303
14 meter
Y = 283700
46 meter E =
0008100
Z = -1728054
22 I = 51
58975
XDOT = -1702
240822 Wp = 51
10553
YDOT = -4856
212875 meter/sec RA = 189
57611 deg
ZDOT = 5682
264119 TA = 289
92544
MA = 290
01268
Ha = 220
661 n
mi
Hp = 213
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21504342
25 X = -6548814
48
Y = 930775
80 feet Y = 210435
46 meter
Z = -5669469
24 Z = -1759881
17
XDOT = -5584
779599 XDOT = -1675
413427
YDOT = -15932
456938 feet/sec YDOT = -4875
098865 meter/sec
ZDOT = 18642
598815 ZDOT = 5674
059721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1228776
26 X = 374531
00
Y = 21452368
79 feet Y = 6538682
01 meter
Z = -5807920
71 Z = -1770254
23
XDOT = -14285
489170 XDOT = -4354
217099
YDOT = 5836
173379 feet/sec YDOT = 1778
865646 meter/sec
ZDOT = 18607
734674 ZDOT = 5671
637529
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 16142
59236432
00016717 00000-0 10270-3 0 9049
2 25544 51
6418 190
7126 0001782 113
4570 246
6770 15
54710485 846
Satellite: ISS
Catalog Number: 25544
Epoch time: 16142
59236432 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 190
7126 deg
Eccentricity:
0001782
Arg of perigee: 113
4570 deg
Mean anomaly: 246
6770 deg
Mean motion: 15
54710485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 84
Checksum: 299
Coasting Arc #6 (Orbit 99)
---------------------------------------
Vector Time (GMT): 2016/143/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6746008
84 A = 6787738
60 meter
Y = 674720
89 meter E =
0013502
Z = -165941
16 I = 51
62368
XDOT = -612
654980 Wp = 132
96614
YDOT = 4725
605055 meter/sec RA = 184
60096 deg
ZDOT = -6010
121617 TA = 48
82249
MA = 48
70611
Ha = 220
771 n
mi
Hp = 213
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22132574
94 X = 6738768
65
Y = 2213651
22 feet Y = 750118
78 meter
Z = -544426
37 Z = -133187
70
XDOT = -2010
022901 XDOT = -636
257268
YDOT = 15503
953594 feet/sec YDOT = 4718
622486 meter/sec
ZDOT = -19718
246775 ZDOT = -6013
154716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1523934
16 X = 464495
13
Y = -22193771
11 feet Y = -6764661
43 meter
Z = -402086
97 Z = -122556
11
XDOT = 13934
787487 XDOT = 4247
323226
YDOT = 1288
707323 feet/sec YDOT = 392
797992 meter/sec
ZDOT = -19732
232326 ZDOT = -6014
384413
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 16143
62083797
00016717 00000-0 10270-3 0 9059
2 25544 51
6396 185
5815 0001761 111
8635 248
2714 15
54673794 1005
Satellite: ISS
Catalog Number: 25544
Epoch time: 16143
62083797 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 185
5815 deg
Eccentricity:
0001761
Arg of perigee: 111
8635 deg
Mean anomaly: 248
2714 deg
Mean motion: 15
54673794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 100
Checksum: 318
Coasting Arc #7 (Orbit 115)
---------------------------------------
Vector Time (GMT): 2016/144/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6290818
79 A = 6786030
95 meter
Y = -1543022
43 meter E =
0014994
Z = 2001906
71 I = 51
64919
XDOT = 2868
025448 Wp = 72
97033
YDOT = -4426
242690 meter/sec RA = 179
62744 deg
ZDOT = 5570
698406 TA = 309
14852
MA = 309
28167
Ha = 220
652 n
mi
Hp = 213
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20639169
26 X = -6282821
32
Y = -5062409
54 feet Y = -1613326
02 meter
Z = 6567935
40 Z = 1971366
32
XDOT = 9409
532309 XDOT = 2890
247202
YDOT = -14521
793601 feet/sec YDOT = -4394
046808 meter/sec
ZDOT = 18276
569574 ZDOT = 5584
684307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4057067
56 X = -1236594
19
Y = 20901377
25 feet Y = 6370739
79 meter
Z = 6435348
08 Z = 1961494
10
XDOT = -13427
736701 XDOT = -4092
774147
YDOT = -8283
662828 feet/sec YDOT = -2524
860430 meter/sec
ZDOT = 18338
152036 ZDOT = 5589
468741
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 16144
64930422
00016717 00000-0 10270-3 0 9069
2 25544 51
6385 180
4508 0001581 119
2285 240
9026 15
54703221 1160
Satellite: ISS
Catalog Number: 25544
Epoch time: 16144
64930422 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 180
4508 deg
Eccentricity:
0001581
Arg of perigee: 119
2285 deg
Mean anomaly: 240
9026 deg
Mean motion: 15
54703221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 116
Checksum: 283
Coasting Arc #8 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2016/145/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5214938
31 A = 6782258
35 meter
Y = 2389387
15 meter E =
0006761
Z = -3624314
02 I = 51
66842
XDOT = -4867
285048 Wp = 91
20174
YDOT = 3953
576966 meter/sec RA = 174
64608 deg
ZDOT = -4404
204245 TA = 131
71426
MA = 131
65640
Ha = 220
718 n
mi
Hp = 213
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17109377
66 X = 5205437
55
Y = 7839196
69 feet Y = 2447651
30 meter
Z = -11890794
02 Z = -3599003
70
XDOT = -15968
782967 XDOT = -4889
739223
YDOT = 12971
053037 feet/sec YDOT = 3899
022643 meter/sec
ZDOT = -14449
488992 ZDOT = -4427
902704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6696114
46 X = 2040975
69
Y = -17661905
69 feet Y = -5383348
86 meter
Z = -11781083
55 Z = -3590874
26
XDOT = 12693
314432 XDOT = 3868
922239
YDOT = 14503
895469 feet/sec YDOT = 4420
787339 meter/sec
ZDOT = -14553
257505 ZDOT = -4435
832887
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 16145
61348736
00016717 00000-0 10270-3 0 9079
2 25544 51
6385 175
6394 0001659 117
3146 242
8176 15
54680082 1313
Satellite: ISS
Catalog Number: 25544
Epoch time: 16145
61348736 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 175
6394 deg
Eccentricity:
0001659
Arg of perigee: 117
3146 deg
Mean anomaly: 242
8176 deg
Mean motion: 15
54680082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 131
Checksum: 316
Coasting Arc #9 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2016/146/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3658609
01 A = 6778175
42 meter
Y = -3149610
13 meter E =
0009242
Z = 4752776
77 I = 51
68612
XDOT = 6369
531641 Wp = 117
93161
YDOT = -3324
659648 meter/sec RA = 169
65536 deg
ZDOT = 2691
719325 TA = 305
46642
MA = 305
55263
Ha = 220
701 n
mi
Hp = 213
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12003310
39 X = -3646204
48
Y = -10333366
58 feet Y = -3190454
25 meter
Z = 15593099
63 Z = 4735033
83
XDOT = 20897
413521 XDOT = 6393
160105
YDOT = -10907
676012 feet/sec YDOT = -3253
299462 meter/sec
ZDOT = 8831
100148 ZDOT = 2722
718223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9296521
16 X = -2833579
65
Y = 12915797
00 feet Y = 3936734
92 meter
Z = 15516428
82 Z = 4729407
51
XDOT = -11649
636766 XDOT = -3550
809286
YDOT = -19189
737406 feet/sec YDOT = -5849
031961 meter/sec
ZDOT = 8966
544931 ZDOT = 2733
002895
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 16146
64194165
00016717 00000-0 10270-3 0 9089
2 25544 51
6378 170
5084 0001483 117
8404 242
2900 15
54695625 1477
Satellite: ISS
Catalog Number: 25544
Epoch time: 16146
64194165 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 170
5084 deg
Eccentricity:
0001483
Arg of perigee: 117
8404 deg
Mean anomaly: 242
2900 deg
Mean motion: 15
54695625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 147
Checksum: 310
Coasting Arc #10 (Orbit 161)
---------------------------------------
Vector Time (GMT): 2016/147/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1775152
12 A = 6775852
85 meter
Y = 3850844
13 meter E =
0015912
Z = -5298847
65 I = 51
70981
XDOT = -7217
707067 Wp = 88
64525
YDOT = 2483
447904 meter/sec RA = 164
65631 deg
ZDOT = -614
409670 TA = 175
49464
MA = 175
48030
Ha = 220
604 n
mi
Hp = 213
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5823989
90 X = 1757698
73
Y = 12634003
05 feet Y = 3870597
96 meter
Z = -17384670
75 Z = -5290266
39
XDOT = -23680
141297 XDOT = -7241
956615
YDOT = 8147
794960 feet/sec YDOT = 2402
599170 meter/sec
ZDOT = -2015
779757 ZDOT = -649
530335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11977227
84 X = 3650659
04
Y = -7166403
13 feet Y = -2184319
67 meter
Z = -17347978
21 Z = -5287663
76
XDOT = 9945
263551 XDOT = 3031
316330
YDOT = 21862
448272 feet/sec YDOT = 6663
674233 meter/sec
ZDOT = -2169
040084 ZDOT = -661
123418
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 16147
60611295
00016717 00000-0 10270-3 0 9095
2 25544 51
6378 165
6979 0001537 121
6179 238
5124 15
54695634 1620
Satellite: ISS
Catalog Number: 25544
Epoch time: 16147
60611295 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node: 165
6979 deg
Eccentricity:
0001537
Arg of perigee: 121
6179 deg
Mean anomaly: 238
5124 deg
Mean motion: 15
54695634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 162
Checksum: 329
Coasting Arc #11 (Orbit 177)
---------------------------------------
Vector Time (GMT): 2016/148/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 215936
41 A = 6776359
96 meter
Y = -4404101
26 meter E =
0005313
Z = 5141624
59 I = 51
74314
XDOT = 7377
493930 Wp = 69
91938
YDOT = -1440
048000 meter/sec RA = 159
65656 deg
ZDOT = -1540
250730 TA = 34
90950
MA = 34
87467
Ha = 220
511 n
mi
Hp = 213
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 708452
79 X = 240192
25
Y = -14449151
10 feet Y = -4401551
30 meter
Z = 16868847
09 Z = 5142732
12
XDOT = 24204
376412 XDOT = 7400
530496
YDOT = -4724
566930 feet/sec YDOT = -1357
419024 meter/sec
ZDOT = -5053
316043 ZDOT = -1504
356748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14418674
47 X = -4394811
98
Y = 1092637
93 feet Y = 333036
04 meter
Z = 16874413
88 Z = 5143321
35
XDOT = -7445
170776 XDOT = -2269
288052
YDOT = -22466
799677 feet/sec YDOT = -6847
880541 meter/sec
ZDOT = -4896
845182 ZDOT = -1492
558411
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 16148
63455587
00016717 00000-0 10270-3 0 9101
2 25544 51
6383 160
5665 0001414 126
1751 233
9532 15
54720736 1783
Satellite: ISS
Catalog Number: 25544
Epoch time: 16148
63455587 = yrday
fracday
Element set: 910
Inclination: 51
6383 deg
RA of node: 160
5665 deg
Eccentricity:
0001414
Arg of perigee: 126
1751 deg
Mean anomaly: 233
9532 deg
Mean motion: 15
54720736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 178
Checksum: 308
Coasting Arc #12 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2016/149/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2096867
26 A = 6779606
10 meter
Y = 4775303
19 meter E =
0010111
Z = -4342047
44 I = 51
78432
XDOT = -6814
433999 Wp = 112
70791
YDOT = 182
353319 meter/sec RA = 154
66542 deg
ZDOT = 3494
062360 TA = 192
76875
MA = 192
79438
Ha = 220
523 n
mi
Hp = 213
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6879485
76 X = -2129018
18
Y = 15667005
21 feet Y = 4751675
15 meter
Z = -14245562
46 Z = -4352311
30
XDOT = -22357
066925 XDOT = -6832
939363
YDOT = 598
272043 feet/sec YDOT = 106
046076 meter/sec
ZDOT = 11463
459185 ZDOT = 3460
914491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16433560
23 X = 5008949
16
Y = 4628430
59 feet Y = 1410745
64 meter
Z = -14291051
56 Z = -4355912
52
XDOT = 3935
398220 XDOT = 1199
509377
YDOT = 20949
775261 feet/sec YDOT = 6385
491500 meter/sec
ZDOT = 11319
135813 ZDOT = 3450
072596
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 16149
59871520
00016717 00000-0 10270-3 0 9117
2 25544 51
6389 155
7563 0001397 123
5090 236
6196 15
54708964 1931
Satellite: ISS
Catalog Number: 25544
Epoch time: 16149
59871520 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 155
7563 deg
Eccentricity:
0001397
Arg of perigee: 123
5090 deg
Mean anomaly: 236
6196 deg
Mean motion: 15
54708964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 332
Coasting Arc #13 (Orbit 208)
---------------------------------------
Vector Time (GMT): 2016/150/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3699891
63 A = 6783788
83 meter
Y = -4850679
71 meter E =
0014326
Z = 2951260
19 I = 51
82684
XDOT = 5666
306601 Wp = 100
31089
YDOT = 1257
536855 meter/sec RA = 149
68799 deg
ZDOT = -5018
612482 TA = 46
05125
MA = 45
93315
Ha = 220
396 n
mi
Hp = 213
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12138752
08 X = 3739522
14
Y = -15914303
51 feet Y = -4809083
64 meter
Z = 9682612
17 Z = 2969329
42
XDOT = 18590
244755 XDOT = 5676
201761
YDOT = 4125
777084 feet/sec YDOT = 1320
956876 meter/sec
ZDOT = -16465
264049 ZDOT = -4991
062731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17553933
17 X = -5350438
83
Y = -9535624
58 feet Y = -2906458
37 meter
Z = 9762101
77 Z = 2975488
62
XDOT = 559
497726 XDOT = 170
534907
YDOT = -17824
208344 feet/sec YDOT = -5432
818703 meter/sec
ZDOT = -16345
541134 ZDOT = -4982
120938
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 16150
62714644
00016717 00000-0 10270-3 0 9127
2 25544 51
6385 150
6249 0001304 127
3974 232
7298 15
54742292 2093
Satellite: ISS
Catalog Number: 25544
Epoch time: 16150
62714644 = yrday
fracday
Element set: 912
Inclination: 51
6385 deg
RA of node: 150
6249 deg
Eccentricity:
0001304
Arg of perigee: 127
3974 deg
Mean anomaly: 232
7298 deg
Mean motion: 15
54742292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 209
Checksum: 304
Coasting Arc #14 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2016/151/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4848073
31 A = 6786855
32 meter
Y = 4589296
03 meter E =
0009049
Z = -1205996
01 I = 51
86473
XDOT = -4073
925661 Wp = 47
09817
YDOT = -2768
517434 meter/sec RA = 144
72445 deg
ZDOT = 5875
601762 TA = 299
83905
MA = 299
92897
Ha = 220
396 n
mi
Hp = 213
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15905752
33 X = -4893173
39
Y = 15056745
52 feet Y = 4534829
54 meter
Z = -3956679
82 Z = -1229656
25
XDOT = -13365
897839 XDOT = -4071
205999
YDOT = -9083
062449 feet/sec YDOT = -2814
059870 meter/sec
ZDOT = 19276
908668 ZDOT = 5855
817954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17509287
14 X = 5336830
72
Y = 13125975
50 feet Y = 4000797
33 meter
Z = -4060478
95 Z = -1237633
98
XDOT = -5729
776654 XDOT = -1746
435924
YDOT = 13546
475031 feet/sec YDOT = 4128
965589 meter/sec
ZDOT = 19191
245735 ZDOT = 5849
491700
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 16151
59129530
00016717 00000-0 10270-3 0 9139
2 25544 51
6388 145
8147 0001400 133
2442 226
8828 15
54754551 2243
Satellite: ISS
Catalog Number: 25544
Epoch time: 16151
59129530 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 145
8147 deg
Eccentricity:
0001400
Arg of perigee: 133
2442 deg
Mean anomaly: 226
8828 deg
Mean motion: 15
54754551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 296
Coasting Arc #15 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2016/152/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5501727
46 A = 6787282
49 meter
Y = -3896333
04 meter E =
0011747
Z = -738131
43 I = 51
89294
XDOT = 2223
217187 Wp = 139
58565
YDOT = 4259
914180 meter/sec RA = 139
76769 deg
ZDOT = -5977
444404 TA = 48
36491
MA = 48
26436
Ha = 220
381 n
mi
Hp = 213
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18050286
95 X = 5548473
90
Y = -12783244
89 feet Y = -3834547
65 meter
Z = -2421691
03 Z = -711291
76
XDOT = 7294
019644 XDOT = 2204
452715
YDOT = 13976
096391 feet/sec YDOT = 4284
671069 meter/sec
ZDOT = -19611
038071 ZDOT = -5966
689798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15902785
57 X = -4847169
04
Y = -15390941
80 feet Y = -4691159
06 meter
Z = -2304152
33 Z = -702305
63
XDOT = 11239
355049 XDOT = 3425
755419
YDOT = -8716
009997 feet/sec YDOT = -2656
639847 meter/sec
ZDOT = -19564
943633 ZDOT = -5963
394819
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 16152
61971361
00016717 00000-0 10270-3 0 9141
2 25544 51
6399 140
6826 0001214 134
1417 225
9836 15
54760404 2408
Satellite: ISS
Catalog Number: 25544
Epoch time: 16152
61971361 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 140
6826 deg
Eccentricity:
0001214
Arg of perigee: 134
1417 deg
Mean anomaly: 225
9836 deg
Mean motion: 15
54760404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 293
Coasting Arc #16 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2016/153/14:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5614542
75 A = 6784739
26 meter
Y = 2814016
54 meter E =
0014292
Z = 2551438
46 I = 51
90774
XDOT = -355
987281 Wp = 80
58091
YDOT = -5535
790032 meter/sec RA = 134
80997 deg
ZDOT = 5299
197338 TA = 307
98989
MA = 308
11887
Ha = 220
352 n
mi
Hp = 213
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18420415
85 X = -5657986
48
Y = 9232337
73 feet Y = 2750987
91 meter
Z = 8370861
07 Z = 2524058
66
XDOT = -1167
937273 XDOT = -319
799830
YDOT = -18162
040786 feet/sec YDOT = -5539
568922 meter/sec
ZDOT = 17385
818039 ZDOT = 5297
555557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12770227
94 X = 3892365
48
Y = 16231421
11 feet Y = 4947337
15 meter
Z = 8251141
88 Z = 2514948
05
XDOT = -16345
186926 XDOT = -4982
012975
YDOT = 3986
096818 feet/sec YDOT = 1214
962310 meter/sec
ZDOT = 17379
632070 ZDOT = 5297
311855
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 16153
64812531
00016717 00000-0 10270-3 0 9159
2 25544 51
6391 135
5516 0001282 140
4824 219
6423 15
54785558 2562
Satellite: ISS
Catalog Number: 25544
Epoch time: 16153
64812531 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 135
5516 deg
Eccentricity:
0001282
Arg of perigee: 140
4824 deg
Mean anomaly: 219
6423 deg
Mean motion: 15
54785558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 305
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