[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 22nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 568 ET - UTC (sec) : 67 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
There are no maneuvers
Coasting Arc #1 (Orbit 2402)
---------------------------------------
Vector Time (GMT): 2015/142/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6170076
78 A = 6785300
23 meter
Y = 2319565
31 meter E =
0010704
Z = 1591707
02 I = 51
46279
XDOT = -430
160337 Wp = 107
50051
YDOT = 5089
583631 meter/sec RA = 211
69204 deg
ZDOT = -5720
842317 TA = 55
03691
MA = 54
93643
Ha = 219
060 n
mi
Hp = 213
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20243034
05 X = 6135948
31
Y = 7610122
40 feet Y = 2388372
18 meter
Z = 5222135
89 Z = 1621597
53
XDOT = -1411
287195 XDOT = -459
251437
YDOT = 16698
109024 feet/sec YDOT = 5084
611108 meter/sec
ZDOT = -18769
167706 ZDOT = -5723
002207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21574360
04 X = 6575864
94
Y = -943387
73 feet Y = -287544
58 meter
Z = 5349962
84 Z = 1630668
67
XDOT = 5304
358908 XDOT = 1616
768595
YDOT = 14287
640973 feet/sec YDOT = 4354
872969 meter/sec
ZDOT = -18779
306001 ZDOT = -5723
932469
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 15142
43611671
00016717 00000-0 10270-3 0 9009
2 25544 51
6430 212
6115 0003805 324
1845 35
9052 15
55127154 24031
Satellite: ISS
Catalog Number: 25544
Epoch time: 15142
43611671 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 212
6115 deg
Eccentricity:
0003805
Arg of perigee: 324
1845 deg
Mean anomaly: 35
9052 deg
Mean motion: 15
55127154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2403
Checksum: 264
Coasting Arc #2 (Orbit 2418)
---------------------------------------
Vector Time (GMT): 2015/143/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5880897
80 A = 6786294
02 meter
Y = -3342093
82 meter E =
0014107
Z = 430771
31 I = 51
49423
XDOT = 2701
145703 Wp = 33
60526
YDOT = -3971
070174 meter/sec RA = 206
70517 deg
ZDOT = 5984
629241 TA = 331
05320
MA = 331
13137
Ha = 219
178 n
mi
Hp = 213
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19294284
13 X = -5845181
17
Y = -10964874
74 feet Y = -3407658
19 meter
Z = 1413291
70 Z = 402289
45
XDOT = 8862
026586 XDOT = 2716
279197
YDOT = -13028
445454 feet/sec YDOT = -3940
779992 meter/sec
ZDOT = 19634
610370 ZDOT = 5997
787423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22098499
67 X = -6735622
70
Y = -2117353
96 feet Y = -645369
49 meter
Z = 1291664
14 Z = 393699
23
XDOT = 2495
146067 XDOT = 760
520521
YDOT = -13848
471119 feet/sec YDOT = -4221
013997 meter/sec
ZDOT = 19691
740307 ZDOT = 6002
042446
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 15143
46427256
00016717 00000-0 10270-3 0 9018
2 25544 51
6435 207
4778 0003985 330
3509 29
7418 15
55152292 24193
Satellite: ISS
Catalog Number: 25544
Epoch time: 15143
46427256 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 207
4778 deg
Eccentricity:
0003985
Arg of perigee: 330
3509 deg
Mean anomaly: 29
7418 deg
Mean motion: 15
55152292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2419
Checksum: 315
Coasting Arc #3 (Orbit 2433)
---------------------------------------
Vector Time (GMT): 2015/144/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4896209
07 A = 6783835
44 meter
Y = 4023244
57 meter E =
0002288
Z = -2422312
79 I = 51
51447
XDOT = -4817
578889 Wp = 99
04538
YDOT = 2650
710233 meter/sec RA = 201
71873 deg
ZDOT = -5339
825898 TA = 108
09255
MA = 108
06762
Ha = 219
222 n
mi
Hp = 213
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16063678
04 X = 4862623
02
Y = 13199621
28 feet Y = 4077809
52 meter
Z = -7947220
45 Z = -2398609
22
XDOT = -15805
705016 XDOT = -4820
922737
YDOT = 8696
555882 feet/sec YDOT = 2596
818512 meter/sec
ZDOT = -17519
113837 ZDOT = -5363
236829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20192132
84 X = 6154562
09
Y = 5113226
45 feet Y = 1558511
42 meter
Z = -7846193
59 Z = -2391519
81
XDOT = -10148
067473 XDOT = -3093
130966
YDOT = 13060
798030 feet/sec YDOT = 3980
931240 meter/sec
ZDOT = -17620
015873 ZDOT = -5370
580838
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 15144
42815399
00016717 00000-0 10270-3 0 9025
2 25544 51
6430 202
6657 0003945 332
9970 27
0978 15
55183036 24346
Satellite: ISS
Catalog Number: 25544
Epoch time: 15144
42815399 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 202
6657 deg
Eccentricity:
0003945
Arg of perigee: 332
9970 deg
Mean anomaly: 27
0978 deg
Mean motion: 15
55183036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2434
Checksum: 315
Coasting Arc #4 (Orbit 2449)
---------------------------------------
Vector Time (GMT): 2015/145/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3290773
13 A = 6779287
63 meter
Y = -4334822
34 meter E =
0009186
Z = 4033207
27 I = 51
52985
XDOT = 6482
769347 Wp = 80
84307
YDOT = -1287
626725 meter/sec RA = 196
72115 deg
ZDOT = 3899
347408 TA = 328
66275
MA = 328
71746
Ha = 219
312 n
mi
Hp = 213
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10796499
76 X = -3261647
44
Y = -14221858
08 feet Y = -4371459
25 meter
Z = 13232307
30 Z = 4017291
80
XDOT = 21268
928304 XDOT = 6477
744422
YDOT = -4224
497129 feet/sec YDOT = -1215
160428 meter/sec
ZDOT = 12793
134540 ZDOT = 3930
827334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16026590
90 X = -4884904
91
Y = -7984836
83 feet Y = -2433778
27 meter
Z = 13164739
86 Z = 4012612
71
XDOT = 16587
255509 XDOT = 5055
795479
YDOT = -11943
948972 feet/sec YDOT = -3640
515647 meter/sec
ZDOT = 12928
442430 ZDOT = 3940
589253
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 15145
45627854
00016717 00000-0 10270-3 0 9037
2 25544 51
6434 197
5315 0004000 337
2800 22
8176 15
55228651 24500
Satellite: ISS
Catalog Number: 25544
Epoch time: 15145
45627854 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 197
5315 deg
Eccentricity:
0004000
Arg of perigee: 337
2800 deg
Mean anomaly: 22
8176 deg
Mean motion: 15
55228651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2450
Checksum: 291
Coasting Arc #5 (Orbit 2464)
---------------------------------------
Vector Time (GMT): 2015/146/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1234178
78 A = 6775394
60 meter
Y = 4354395
87 meter E =
0013276
Z = -5053764
06 I = 51
54682
XDOT = -7433
750371 Wp = 58
39581
YDOT = -42
055441 meter/sec RA = 191
71208 deg
ZDOT = -1848
406862 TA = 193
63984
MA = 193
67575
Ha = 219
388 n
mi
Hp = 213
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4049142
96 X = 1209944
61
Y = 14286075
67 feet Y = 4368061
95 meter
Z = -16580590
75 Z = -5047827
32
XDOT = -24388
944787 XDOT = -7423
748674
YDOT = -137
977170 feet/sec YDOT = -125
128506 meter/sec
ZDOT = -6064
326975 ZDOT = -1884
494533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10202183
53 X = 3109625
54
Y = 10826957
18 feet Y = 3300056
55 meter
Z = -16555843
56 Z = -5046221
12
XDOT = -20953
652920 XDOT = -6386
673410
YDOT = 10218
342220 feet/sec YDOT = 3114
550709 meter/sec
ZDOT = -6219
200251 ZDOT = -1895
612237
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 15146
42013318
00016717 00000-0 10270-3 0 9040
2 25544 51
6429 192
7195 0004098 340
6033 19
4964 15
55212484 24650
Satellite: ISS
Catalog Number: 25544
Epoch time: 15146
42013318 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 192
7195 deg
Eccentricity:
0004098
Arg of perigee: 340
6033 deg
Mean anomaly: 19
4964 deg
Mean motion: 15
55212484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2465
Checksum: 304
Coasting Arc #6 (Orbit 2480)
---------------------------------------
Vector Time (GMT): 2015/147/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1041606
57 A = 6774045
53 meter
Y = -4101892
07 meter E =
0005101
Z = 5288447
06 I = 51
57485
XDOT = 7548
557779 Wp = 16
46239
YDOT = 1277
946196 meter/sec RA = 186
69477 deg
ZDOT = -490
631682 TA = 78
24871
MA = 78
19148
Ha = 219
324 n
mi
Hp = 213
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3417344
38 X = 1061707
96
Y = -13457651
14 feet Y = -4090131
94 meter
Z = 17350548
11 Z = 5293555
71
XDOT = 24765
609510 XDOT = 7536
089779
YDOT = 4192
736863 feet/sec YDOT = 1362
289412 meter/sec
ZDOT = -1609
683995 ZDOT = -453
992148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3413168
05 X = -1040333
62
Y = -13429504
40 feet Y = -4093312
94 meter
Z = 17373164
13 Z = 5295340
43
XDOT = 22854
968694 XDOT = 6966
194458
YDOT = -7708
699977 feet/sec YDOT = -2349
611753 meter/sec
ZDOT = -1452
633734 ZDOT = -442
762762
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 15147
44822764
00016717 00000-0 10270-3 0 9057
2 25544 51
6433 187
5853 0004171 344
5029 15
5996 15
55285108 24811
Satellite: ISS
Catalog Number: 25544
Epoch time: 15147
44822764 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 187
5853 deg
Eccentricity:
0004171
Arg of perigee: 344
5029 deg
Mean anomaly: 15
5996 deg
Mean motion: 15
55285108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2481
Checksum: 322
Coasting Arc #7 (Orbit 2495)
---------------------------------------
Vector Time (GMT): 2015/148/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3214834
44 A = 6776398
39 meter
Y = 3650964
99 meter E =
0009857
Z = -4725782
01 I = 51
61343
XDOT = -6743
311431 Wp = 86
93276
YDOT = -2380
545556 meter/sec RA = 181
68293 deg
ZDOT = 2753
666577 TA = 210
32531
MA = 210
38238
Ha = 219
513 n
mi
Hp = 212
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10547357
08 X = -3232465
11
Y = 11978231
58 feet Y = 3614916
21 meter
Z = -15504534
14 Z = -4741441
92
XDOT = -22123
725167 XDOT = -6729
566863
YDOT = -7810
188831 feet/sec YDOT = -2455
876934 meter/sec
ZDOT = 9034
339162 ZDOT = 2720
941773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3317655
18 X = -1011221
30
Y = 15543802
95 feet Y = 4737751
14 meter
Z = -15572369
96 Z = -4746458
36
XDOT = -22048
607543 XDOT = -6720
415579
YDOT = 4186
648199 feet/sec YDOT = 1276
090371 meter/sec
ZDOT = 8894
262930 ZDOT = 2710
971341
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 15148
41205479
00016717 00000-0 10270-3 0 9064
2 25544 51
6423 182
7730 0004239 351
2877 8
8202 15
55290738 24968
Satellite: ISS
Catalog Number: 25544
Epoch time: 15148
41205479 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 182
7730 deg
Eccentricity:
0004239
Arg of perigee: 351
2877 deg
Mean anomaly: 8
8202 deg
Mean motion: 15
55290738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2496
Checksum: 316
Coasting Arc #8 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2015/149/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5043039
30 A = 6780832
07 meter
Y = -2987958
99 meter E =
0012700
Z = 3402951
14 I = 51
66070
XDOT = 5119
813297 Wp = 69
88470
YDOT = 3361
421678 meter/sec RA = 176
68431 deg
ZDOT = -4617
605563 TA = 70
31593
MA = 70
17894
Ha = 219
523 n
mi
Hp = 212
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16545404
51 X = 5059546
05
Y = -9803015
05 feet Y = -2931472
29 meter
Z = 11164537
88 Z = 3427489
56
XDOT = 16797
287720 XDOT = 5104
275484
YDOT = 11028
286345 feet/sec YDOT = 3418
588124 meter/sec
ZDOT = -15149
624549 ZDOT = -4592
771718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9354677
58 X = 2851305
73
Y = -16732148
91 feet Y = -5099958
99 meter
Z = 11270386
90 Z = 3435213
93
XDOT = 18924
036013 XDOT = 5768
046177
YDOT = 407
145563 feet/sec YDOT = 124
097967 meter/sec
ZDOT = -15043
576667 ZDOT = -4585
282168
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 15149
44012022
00016717 00000-0 10270-3 0 9079
2 25544 51
6426 177
6385 0004392 353
8326 6
2773 15
55329260 25124
Satellite: ISS
Catalog Number: 25544
Epoch time: 15149
44012022 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 177
6385 deg
Eccentricity:
0004392
Arg of perigee: 353
8326 deg
Mean anomaly: 6
2773 deg
Mean motion: 15
55329260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 297
Coasting Arc #9 (Orbit 2526)
---------------------------------------
Vector Time (GMT): 2015/150/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6229367
67 A = 6784842
64 meter
Y = 2162720
07 meter E =
0011731
Z = -1571844
09 I = 51
70431
XDOT = -2892
756609 Wp = 24
23040
YDOT = -4169
256063 meter/sec RA = 171
70315 deg
ZDOT = 5753
389077 TA = 318
58522
MA = 318
67408
Ha = 219
692 n
mi
Hp = 212
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20437557
98 X = -6245453
19
Y = 7095538
29 feet Y = 2092969
37 meter
Z = -5156968
80 Z = -1602144
59
XDOT = -9490
671288 XDOT = -2873
868262
YDOT = -13678
661624 feet/sec YDOT = -4201
499507 meter/sec
ZDOT = 18875
948415 ZDOT = 5739
382013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13828661
36 X = -4214975
98
Y = 16596564
58 feet Y = 5058632
88 meter
Z = -5287431
90 Z = -1611609
24
XDOT = -14074
548972 XDOT = -4289
922527
YDOT = -5758
730137 feet/sec YDOT = -1755
260946 meter/sec
ZDOT = 18816
513638 ZDOT = 5735
273357
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 15150
40391912
00016717 00000-0 10270-3 0 9086
2 25544 51
6416 172
8254 0004458 358
2065 1
9071 15
55292338 25271
Satellite: ISS
Catalog Number: 25544
Epoch time: 15150
40391912 = yrday
fracday
Element set: 908
Inclination: 51
6416 deg
RA of node: 172
8254 deg
Eccentricity:
0004458
Arg of perigee: 358
2065 deg
Mean anomaly: 1
9071 deg
Mean motion: 15
55292338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2527
Checksum: 301
Coasting Arc #10 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2015/151/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6666734
88 A = 6785644
48 meter
Y = -1126640
96 meter E =
0008510
Z = -549582
12 I = 51
73898
XDOT = 319
780085 Wp = 117
01564
YDOT = 4776
699453 meter/sec RA = 166
73253 deg
ZDOT = -5988
213361 TA = 68
90668
MA = 68
81572
Ha = 219
787 n
mi
Hp = 212
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21872489
76 X = 6681507
47
Y = -3696328
62 feet Y = -1052006
53 meter
Z = -1803090
95 Z = -517160
06
XDOT = 1049
147260 XDOT = 295
431120
YDOT = 15671
586133 feet/sec YDOT = 4780
139786 meter/sec
ZDOT = -19646
369296 ZDOT = -5986
718660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16596848
72 X = 5058719
49
Y = -14734197
77 feet Y = -4490983
48 meter
Z = -1663676
49 Z = -507088
60
XDOT = 8227
106298 XDOT = 2507
622000
YDOT = 11454
685081 feet/sec YDOT = 3491
388013 meter/sec
ZDOT = -19640
764159 ZDOT = -5986
504916
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 15151
43195545
00016717 00000-0 10270-3 0 9095
2 25544 51
6418 167
6906 0004466 4
1247 355
9943 15
55357813 25435
Satellite: ISS
Catalog Number: 25544
Epoch time: 15151
43195545 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 167
6906 deg
Eccentricity:
0004466
Arg of perigee: 4
1247 deg
Mean anomaly: 355
9943 deg
Mean motion: 15
55357813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 324
Coasting Arc #11 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2015/152/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6271996
37 A = 6783106
51 meter
Y = -55781
51 meter E =
0016068
Z = 2558237
59 I = 51
75999
XDOT = 2207
767736 Wp = 61
08423
YDOT = -5111
783821 meter/sec RA = 161
76070 deg
ZDOT = 5283
844123 TA = 327
65585
MA = 327
75426
Ha = 220
010 n
mi
Hp = 212
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20577415
92 X = -6283333
62
Y = -183010
20 feet Y = -125982
72 meter
Z = 8393167
94 Z = 2527741
40
XDOT = 7243
332468 XDOT = 2239
097481
YDOT = -16770
944293 feet/sec YDOT = -5086
920473 meter/sec
ZDOT = 17335
446597 ZDOT = 5294
644793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17402165
89 X = -5304180
16
Y = 11081938
00 feet Y = 3377774
70 meter
Z = 8262207
87 Z = 2518320
96
XDOT = -2341
530426 XDOT = -713
698474
YDOT = -16680
091793 feet/sec YDOT = -5084
091978 meter/sec
ZDOT = 17382
707888 ZDOT = 5298
249364
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 15152
45997696
00016717 00000-0 10270-3 0 9107
2 25544 51
6409 162
5559 0004547 9
5274 350
5965 15
55344223 25595
Satellite: ISS
Catalog Number: 25544
Epoch time: 15152
45997696 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 162
5559 deg
Eccentricity:
0004547
Arg of perigee: 9
5274 deg
Mean anomaly: 350
5965 deg
Mean motion: 15
55344223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 336
Coasting Arc #12 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2015/153/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5150091
90 A = 6778318
33 meter
Y = 1385918
48 meter E =
0010788
Z = -4195298
12 I = 51
77516
XDOT = -4387
352665 Wp = 50
32978
YDOT = 5064
292889 meter/sec RA = 156
77761 deg
ZDOT = -3712
496072 TA = 181
57673
MA = 181
58014
Ha = 219
900 n
mi
Hp = 212
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16896626
96 X = 5154590
93
Y = 4546976
63 feet Y = 1443535
81 meter
Z = -13764101
43 Z = -4170268
52
XDOT = -14394
201656 XDOT = -4425
622547
YDOT = 16615
134149 feet/sec YDOT = 5015
017095 meter/sec
ZDOT = -12180
105224 ZDOT = -3733
901654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16623991
97 X = 5066992
75
Y = -5723223
07 feet Y = -1744438
39 meter
Z = -13656833
31 Z = -4162602
79
XDOT = -3002
941887 XDOT = -915
296687
YDOT = 20566
206637 feet/sec YDOT = 6268
579783 meter/sec
ZDOT = -12272
921632 ZDOT = -3740
786513
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 15153
42373123
00016717 00000-0 10270-3 0 9119
2 25544 51
6417 157
7419 0004477 12
6719 347
4546 15
55391476 25745
Satellite: ISS
Catalog Number: 25544
Epoch time: 15153
42373123 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 157
7419 deg
Eccentricity:
0004477
Arg of perigee: 12
6719 deg
Mean anomaly: 347
4546 deg
Mean motion: 15
55391476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 318
Coasting Arc #13 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2015/154/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3451894
32 A = 6774423
36 meter
Y = -2739672
01 meter E =
0005548
Z = 5140090
77 I = 51
79036
XDOT = 5955
009293 Wp = 74
47777
YDOT = -4585
093220 meter/sec RA = 151
78113 deg
ZDOT = 1555
361831 TA =
57634
MA =
57570
Ha = 220
056 n
mi
Hp = 211
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11325112
60 X = -3445971
00
Y = -8988425
24 feet Y = -2778240
88 meter
Z = 16863814
85 Z = 5123335
99
XDOT = 19537
432064 XDOT = 5998
282863
YDOT = -15042
956759 feet/sec YDOT = -4518
258653 meter/sec
ZDOT = 5102
893146 ZDOT = 1584
394960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14518804
84 X = -4425331
71
Y = -812808
75 feet Y = -247744
11 meter
Z = 16792315
59 Z = 5118297
79
XDOT = 7303
542936 XDOT = 2226
119887
YDOT = -22446
462794 feet/sec YDOT = -6841
681859 meter/sec
ZDOT = 5228
412492 ZDOT = 1593
620128
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 15154
45172057
00016717 00000-0 10270-3 0 9127
2 25544 51
6408 152
6069 0004548 16
9945 343
1360 15
55420575 25905
Satellite: ISS
Catalog Number: 25544
Epoch time: 15154
45172057 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 152
6069 deg
Eccentricity:
0004548
Arg of perigee: 16
9945 deg
Mean anomaly: 343
1360 deg
Mean motion: 15
55420575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 306
Coasting Arc #14 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2015/155/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1463391
62 A = 6773820
70 meter
Y = 4003376
77 meter E =
0016163
Z = -5278037
09 I = 51
81733
XDOT = -6713
016119 Wp = 80
74259
YDOT = 3585
237753 meter/sec RA = 146
77862 deg
ZDOT = 862
922677 TA = 197
47025
MA = 197
52592
Ha = 220
007 n
mi
Hp = 211
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4801153
61 X = 1444155
04
Y = 13134438
22 feet Y = 4019634
50 meter
Z = -17316394
64 Z = -5270974
37
XDOT = -22024
331098 XDOT = -6756
799959
YDOT = 11762
591054 feet/sec YDOT = 3509
923497 meter/sec
ZDOT = 2831
111146 ZDOT = 830
206035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11686064
04 X = 3561912
32
Y = 7747659
46 feet Y = 2361486
60 meter
Z = -17286750
62 Z = -5269001
59
XDOT = -10371
897042 XDOT = -3161
354218
YDOT = 21611
013540 feet/sec YDOT = 6587
036927 meter/sec
ZDOT = 2689
917302 ZDOT = 819
886794
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 15155
41544674
00016717 00000-0 10270-3 0 9133
2 25544 51
6422 147
7930 0004557 19
0178 341
1144 15
55419754 26057
Satellite: ISS
Catalog Number: 25544
Epoch time: 15155
41544674 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 147
7930 deg
Eccentricity:
0004557
Arg of perigee: 19
0178 deg
Mean anomaly: 341
1144 deg
Mean motion: 15
55419754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 304
Coasting Arc #15 (Orbit 2620)
---------------------------------------
Vector Time (GMT): 2015/156/09:37:06
327
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 594733
23 A = 6776639
87 meter
Y = -4998954
06 meter E =
0012546
Z = 4531916
00 I = 51
85253
XDOT = 6670
358338 Wp = 52
66580
YDOT = -2088
126001 meter/sec RA = 141
78179 deg
ZDOT = -3165
254436 TA = 69
03989
MA = 68
90569
Ha = 219
989 n
mi
Hp = 211
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1951224
50 X = 628574
11
Y = -16400767
91 feet Y = -4992114
72 meter
Z = 14868490
80 Z = 4534886
67
XDOT = 21884
377748 XDOT = 6708
588167
YDOT = -6850
807089 feet/sec YDOT = -2013
319540 meter/sec
ZDOT = -10384
693033 ZDOT = -3132
758437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8371246
26 X = -2551555
86
Y = -14223528
31 feet Y = -4335331
43 meter
Z = 14882135
68 Z = 4536074
95
XDOT = 12389
504696 XDOT = 3776
321031
YDOT = -18056
950030 feet/sec YDOT = -5503
758369 meter/sec
ZDOT = -10244
687333 ZDOT = -3122
580699
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 15156
44340462
00016717 00000-0 10270-3 0 9147
2 25544 51
6412 142
6577 0004649 23
6137 336
5229 15
55485375 26217
Satellite: ISS
Catalog Number: 25544
Epoch time: 15156
44340462 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 142
6577 deg
Eccentricity:
0004649
Arg of perigee: 23
6137 deg
Mean anomaly: 336
5229 deg
Mean motion: 15
55485375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2621
Checksum: 308
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