[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 12th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 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
136/01:11:20
035 -4
0 5
0 5
0
N/A -1
0 -0
7 218
3
000/00:14:40
070 -2
9 -0
2 216
1
Coasting Arc #1 (Orbit 2233)
---------------------------------------
Vector Time (GMT): 2015/131/12:51:38
736
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3996321
28 A = 6774953
77 meter
Y = 2725326
78 meter E =
0006736
Z = 4745935
76 I = 51
26869
XDOT = -1648
460795 Wp = 5
35968
YDOT = 7011
731417 meter/sec RA = 266
19145 deg
ZDOT = -2631
460756 TA = 110
77306
MA = 110
70088
Ha = 217
380 n
mi
Hp = 214
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13111290
29 X = 3942494
88
Y = 8941360
82 feet Y = 2769715
26 meter
Z = 15570655
38 Z = 4765218
52
XDOT = -5408
335940 XDOT = -1713
962393
YDOT = 23004
368166 feet/sec YDOT = 6992
931028 meter/sec
ZDOT = -8633
401430 ZDOT = -2639
627761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14121821
80 X = 4304331
28
Y = -7061376
72 feet Y = -2152307
63 meter
Z = 15652804
33 Z = 4770974
76
XDOT = 17027
306900 XDOT = 5189
923143
YDOT = 14784
562475 feet/sec YDOT = 4506
334642 meter/sec
ZDOT = -8669
683104 ZDOT = -2642
519410
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 15131
57940082
00016717 00000-0 10270-3 0 9003
2 25544 51
6445 266
8464 0006764 297
6682 62
3785 15
55748935 22340
Satellite: ISS
Catalog Number: 25544
Epoch time: 15131
57940082 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 266
8464 deg
Eccentricity:
0006764
Arg of perigee: 297
6682 deg
Mean anomaly: 62
3785 deg
Mean motion: 15
55748935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2234
Checksum: 337
Coasting Arc #2 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2015/132/12:51:38
736
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3459290
63 A = 6779645
57 meter
Y = -4767896
16 meter E =
0004055
Z = -3351055
85 I = 51
28814
XDOT = 2920
970962 Wp = 342
92673
YDOT = -5372
296513 meter/sec RA = 261
16385 deg
ZDOT = 4630
791904 TA = 337
75051
MA = 337
76810
Ha = 217
502 n
mi
Hp = 214
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11349378
69 X = -3389439
46
Y = -15642703
95 feet Y = -4806189
67 meter
Z = -10994277
73 Z = -3367690
87
XDOT = 9583
238063 XDOT = 2958
333322
YDOT = -17625
644729 feet/sec YDOT = -5339
423375 meter/sec
ZDOT = 15192
886824 ZDOT = 4645
072317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19105535
17 X = -5823367
12
Y = 2631970
50 feet Y = 802224
61 meter
Z = -11064717
97 Z = -3372526
04
XDOT = -10930
693105 XDOT = -3331
675258
YDOT = -15246
994387 feet/sec YDOT = -4647
283889 meter/sec
ZDOT = 15255
063452 ZDOT = 4649
743340
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 15132
54289402
00016717 00000-0 10270-3 0 9014
2 25544 51
6447 262
0314 0007064 301
9705 58
0761 15
55797436 22495
Satellite: ISS
Catalog Number: 25544
Epoch time: 15132
54289402 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 262
0314 deg
Eccentricity:
0007064
Arg of perigee: 301
9705 deg
Mean anomaly: 58
0761 deg
Mean motion: 15
55797436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 303
Coasting Arc #3 (Orbit 2264)
---------------------------------------
Vector Time (GMT): 2015/133/12:51:38
736
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2598374
11 A = 6783568
47 meter
Y = 6122152
41 meter E =
0006922
Z = 1320626
54 I = 51
30754
XDOT = -4048
008327 Wp = 114
94553
YDOT = 2972
765086 meter/sec RA = 256
15379 deg
ZDOT = -5795
490333 TA = 50
60442
MA = 50
54315
Ha = 217
672 n
mi
Hp = 213
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8524849
43 X = 2523306
44
Y = 20085801
88 feet Y = 6150789
42 meter
Z = 4332764
23 Z = 1333066
68
XDOT = -13280
867216 XDOT = -4052
796979
YDOT = 9753
166292 feet/sec YDOT = 2927
470772 meter/sec
ZDOT = -19014
075896 ZDOT = -5815
166671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21755565
98 X = 6631096
51
Y = 1533795
83 feet Y = 467500
97 meter
Z = 4384992
57 Z = 1336545
73
XDOT = 2836
482769 XDOT = 864
559948
YDOT = 14564
330454 feet/sec YDOT = 4439
207922 meter/sec
ZDOT = -19098
945212 ZDOT = -5821
358501
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 15133
57059530
00016717 00000-0 10270-3 0 9026
2 25544 51
6448 256
8950 0006957 305
6960 54
3546 15
55850459 22650
Satellite: ISS
Catalog Number: 25544
Epoch time: 15133
57059530 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 256
8950 deg
Eccentricity:
0006957
Arg of perigee: 305
6960 deg
Mean anomaly: 54
3546 deg
Mean motion: 15
55850459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2265
Checksum: 330
Coasting Arc #4 (Orbit 2280)
---------------------------------------
Vector Time (GMT): 2015/134/12:51:38
736
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1429662
23 A = 6783828
05 meter
Y = -6553202
42 meter E =
0013637
Z = 954280
81 I = 51
31803
XDOT = 4913
378022 Wp = 25
20249
YDOT = -211
018502 meter/sec RA = 251
15231 deg
ZDOT = 5892
946197 TA = 345
19285
MA = 345
23274
Ha = 217
822 n
mi
Hp = 213
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4690492
87 X = -1360912
11
Y = -21500007
93 feet Y = -6568805
42 meter
Z = 3130842
56 Z = 947502
71
XDOT = 16120
006635 XDOT = 4886
746328
YDOT = -692
317921 feet/sec YDOT = -156
222765 meter/sec
ZDOT = 19333
812981 ZDOT = 5916
750126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21390743
81 X = -6519898
71
Y = -5182761
51 feet Y = -1579705
71 meter
Z = 3102950
52 Z = 945779
32
XDOT = 6008
130750 XDOT = 1831
278253
YDOT = -13123
310318 feet/sec YDOT = -3999
984985 meter/sec
ZDOT = 19435
884290 ZDOT = 5924
057532
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 15134
59826905
00016717 00000-0 10270-3 0 9038
2 25544 51
6455 251
7581 0007061 311
3257 48
7288 15
55893701 22817
Satellite: ISS
Catalog Number: 25544
Epoch time: 15134
59826905 = yrday
fracday
Element set: 903
Inclination: 51
6455 deg
RA of node: 251
7581 deg
Eccentricity:
0007061
Arg of perigee: 311
3257 deg
Mean anomaly: 48
7288 deg
Mean motion: 15
55893701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2281
Checksum: 319
Coasting Arc #5 (Orbit 2295)
---------------------------------------
Vector Time (GMT): 2015/135/12:51:38
736
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -17103
78 A = 6780065
71 meter
Y = 6045545
67 meter E =
0003743
Z = -3073082
15 I = 51
31696
XDOT = -5367
449911 Wp = 348
47379
YDOT = -2493
824357 meter/sec RA = 246
14596 deg
ZDOT = -4871
490317 TA = 227
01100
MA = 227
04238
Ha = 217
945 n
mi
Hp = 213
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -56114
76 X = -69777
07
Y = 19834467
41 feet Y = 6045059
91 meter
Z = -10082290
52 Z = -3073293
14
XDOT = -17609
743801 XDOT = -5315
500120
YDOT = -8181
838443 feet/sec YDOT = -2553
556190 meter/sec
ZDOT = -15982
579779 ZDOT = -4897
438680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17979880
15 X = 5480267
47
Y = 8372181
33 feet Y = 2551840
87 meter
Z = -10084260
91 Z = -3073682
72
XDOT = -14203
406214 XDOT = -4329
198214
YDOT = 11100
160964 feet/sec YDOT = 3383
329062 meter/sec
ZDOT = -16093
371027 ZDOT = -4905
259489
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 15135
56168857
00016717 00000-0 10270-3 0 9042
2 25544 51
6455 246
9431 0007104 314
4383 45
6189 15
55936780 22966
Satellite: ISS
Catalog Number: 25544
Epoch time: 15135
56168857 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 246
9431 deg
Eccentricity:
0007104
Arg of perigee: 314
4383 deg
Mean anomaly: 45
6189 deg
Mean motion: 15
55936780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2296
Checksum: 332
Coasting Arc #6 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2015/136/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2026875
07 A = 6777400
06 meter
Y = 4421760
56 meter E =
0006777
Z = -4724946
73 I = 51
30415
XDOT = -4980
961164 Wp = 30
12777
YDOT = -5165
525438 meter/sec RA = 243
53876 deg
ZDOT = -2693
297770 TA = 213
09260
MA = 213
13502
Ha = 218
263 n
mi
Hp = 216
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6649852
58 X = -2053217
12
Y = 14507088
46 feet Y = 4398947
51 meter
Z = -15501793
73 Z = -4734857
01
XDOT = -16341
736102 XDOT = -4909
745530
YDOT = -16947
261937 feet/sec YDOT = -5220
827570 meter/sec
ZDOT = -8836
278772 ZDOT = -2717
321910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11822597
13 X = -3603527
61
Y = -10656417
56 feet Y = -3248076
07 meter
Z = -15545054
71 Z = -4738132
67
XDOT = 20324
434376 XDOT = 6194
887598
YDOT = -9490
361216 feet/sec YDOT = -2892
662099 meter/sec
ZDOT = -8938
355579 ZDOT = -2724
410781
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 15136
07551576
00016717 00000-0 10270-3 0 9054
2 25544 51
6443 244
3763 0007414 288
0983 71
9362 15
54957498 23042
Satellite: ISS
Catalog Number: 25544
Epoch time: 15136
07551576 = yrday
fracday
Element set: 905
Inclination: 51
6443 deg
RA of node: 244
3763 deg
Eccentricity:
0007414
Arg of perigee: 288
0983 deg
Mean anomaly: 71
9362 deg
Mean motion: 15
54957498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 330
Coasting Arc #7 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2015/137/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3281544
92 A = 6774914
05 meter
Y = -2721284
41 meter E =
0004711
Z = 5269205
18 I = 51
31113
XDOT = 4355
336693 Wp = 290
52720
YDOT = 6287
125917 meter/sec RA = 238
50902 deg
ZDOT = 536
595344 TA = 154
34028
MA = 154
31690
Ha = 218
350 n
mi
Hp = 216
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10766223
48 X = 3286134
71
Y = -8928098
44 feet Y = -2684562
55 meter
Z = 17287418
57 Z = 5285157
68
XDOT = 14289
162380 XDOT = 4282
102217
YDOT = 20627
053533 feet/sec YDOT = 6335
420642 meter/sec
ZDOT = 1760
483413 ZDOT = 557
575523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5479121
56 X = 1670036
25
Y = 12775599
24 feet Y = 3894002
65 meter
Z = 17356285
37 Z = 5290195
78
XDOT = -22933
732973 XDOT = -6990
201810
YDOT = 7332
217803 feet/sec YDOT = 2234
859986 meter/sec
ZDOT = 1849
324236 ZDOT = 563
674027
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 15137
10379957
00016717 00000-0 10270-3 0 9061
2 25544 51
6442 239
2436 0007551 291
5680 68
4668 15
55001127 23204
Satellite: ISS
Catalog Number: 25544
Epoch time: 15137
10379957 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 239
2436 deg
Eccentricity:
0007551
Arg of perigee: 291
5680 deg
Mean anomaly: 68
4668 deg
Mean motion: 15
55001127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 309
Coasting Arc #8 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2015/138/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4411500
83 A = 6775688
04 meter
Y = 866602
15 meter E =
0006309
Z = -5074653
49 I = 51
33180
XDOT = -3277
202748 Wp = 86
67242
YDOT = -6716
712005 meter/sec RA = 233
47776 deg
ZDOT = 1704
118365 TA = 199
85819
MA = 199
88276
Ha = 218
538 n
mi
Hp = 215
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14473427
92 X = -4396212
25
Y = 2843182
92 feet Y = 817355
64 meter
Z = -16649125
61 Z = -5096046
95
XDOT = -10751
977519 XDOT = -3210
129437
YDOT = -22036
456708 feet/sec YDOT = -6752
984897 meter/sec
ZDOT = 5590
939518 ZDOT = 1688
360559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1165821
31 X = 355342
34
Y = -14599209
91 feet Y = -4449839
18 meter
Z = -16741001
15 Z = -5102657
15
XDOT = 23072
392707 XDOT = 7032
465297
YDOT = -4484
373128 feet/sec YDOT = -1366
836929 meter/sec
ZDOT = 5524
553222 ZDOT = 1683
883822
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 15138
06779431
00016717 00000-0 10270-3 0 9079
2 25544 51
6447 234
4318 0007571 296
2321 63
8054 15
55021226 23357
Satellite: ISS
Catalog Number: 25544
Epoch time: 15138
06779431 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 234
4318 deg
Eccentricity:
0007571
Arg of perigee: 296
2321 deg
Mean anomaly: 63
8054 deg
Mean motion: 15
55021226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 300
Coasting Arc #9 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2015/139/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5278409
08 A = 6779192
72 meter
Y = 960086
04 meter E =
0007358
Z = 4145707
15 I = 51
36320
XDOT = 1754
982272 Wp = 27
53141
YDOT = 6468
216889 meter/sec RA = 228
45536 deg
ZDOT = -3723
370602 TA = 100
95229
MA = 100
86950
Ha = 218
790 n
mi
Hp = 215
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17317615
08 X = 5247142
22
Y = 3149888
59 feet Y = 1018937
52 meter
Z = 13601401
41 Z = 4171273
21
XDOT = 5757
815852 XDOT = 1700
609747
YDOT = 21221
184020 feet/sec YDOT = 6487
538516 meter/sec
ZDOT = -12215
782815 ZDOT = -3714
976667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7439267
85 X = -2267488
84
Y = 15858414
75 feet Y = 4833644
82 meter
Z = 13710860
15 Z = 4179070
17
XDOT = -20850
111679 XDOT = -6355
114040
YDOT = 775
962573 feet/sec YDOT = 236
513392 meter/sec
ZDOT = -12180
918019 ZDOT = -3712
743812
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 15139
09603037
00016717 00000-0 10270-3 0 9082
2 25544 51
6443 229
2993 0007641 300
9416 59
0986 15
55067118 23519
Satellite: ISS
Catalog Number: 25544
Epoch time: 15139
09603037 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 229
2993 deg
Eccentricity:
0007641
Arg of perigee: 300
9416 deg
Mean anomaly: 59
0986 deg
Mean motion: 15
55067118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 315
Coasting Arc #10 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2015/140/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5715517
71 A = 6783544
87 meter
Y = -2534157
23 meter E =
0007645
Z = -2618899
33 I = 51
39970
XDOT = 108
653290 Wp = 342
55017
YDOT = -5627
862875 meter/sec RA = 223
44721 deg
ZDOT = 5211
830442 TA = 347
82191
MA = 347
84038
Ha = 218
861 n
mi
Hp = 215
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18751698
51 X = -5674033
56
Y = -8314164
13 feet Y = -2597839
70 meter
Z = -8592189
41 Z = -2646564
05
XDOT = 356
474050 XDOT = 146
259854
YDOT = -18464
117044 feet/sec YDOT = -5626
438031 meter/sec
ZDOT = 17099
181239 ZDOT = 5212
449115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12529739
34 X = 3819064
55
Y = -16177515
08 feet Y = -4930906
60 meter
Z = -8710389
14 Z = -2654926
61
XDOT = 16692
238353 XDOT = 5087
794250
YDOT = 3725
383339 feet/sec YDOT = 1135
496842 meter/sec
ZDOT = 17102
812064 ZDOT = 5212
937117
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 15140
05997936
00016717 00000-0 10270-3 0 9095
2 25544 51
6443 224
4867 0007739 304
5536 55
4886 15
55088352 23665
Satellite: ISS
Catalog Number: 25544
Epoch time: 15140
05997936 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 224
4867 deg
Eccentricity:
0007739
Arg of perigee: 304
5536 deg
Mean anomaly: 55
4886 deg
Mean motion: 15
55088352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 344
Coasting Arc #11 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2015/141/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5608184
47 A = 6786327
90 meter
Y = 3754245
06 meter E =
0005642
Z = 686803
32 I = 51
43204
XDOT = -2167
499610 Wp = 127
10153
YDOT = 4330
791672 meter/sec RA = 218
45371 deg
ZDOT = -5943
782466 TA = 45
45836
MA = 45
41230
Ha = 219
102 n
mi
Hp = 215
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18399555
36 X = 5562450
53
Y = 12317076
95 feet Y = 3816703
66 meter
Z = 2253291
73 Z = 713936
32
XDOT = -7111
219192 XDOT = -2186
893509
YDOT = 14208
634096 feet/sec YDOT = 4306
445381 meter/sec
ZDOT = -19500
598642 ZDOT = -5954
358575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16083453
08 X = -4902236
50
Y = 15200053
87 feet Y = 4632976
42 meter
Z = 2369017
75 Z = 722076
61
XDOT = -11197
954433 XDOT = -3413
136511
YDOT = -8787
484913 feet/sec YDOT = -2678
425401 meter/sec
ZDOT = -19546
708766 ZDOT = -5957
836832
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 15141
08816937
00016717 00000-0 10270-3 0 9102
2 25544 51
6438 219
3538 0007615 307
7923 52
2540 15
55084482 23825
Satellite: ISS
Catalog Number: 25544
Epoch time: 15141
08816937 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 219
3538 deg
Eccentricity:
0007615
Arg of perigee: 307
7923 deg
Mean anomaly: 52
2540 deg
Mean motion: 15
55084482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 311
Coasting Arc #12 (Orbit 2397)
---------------------------------------
Vector Time (GMT): 2015/142/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4874997
39 A = 6785588
49 meter
Y = -4509753
57 meter E =
0013711
Z = 1348060
03 I = 51
45511
XDOT = 4180
313769 Wp = 26
65212
YDOT = -2780
483935 meter/sec RA = 213
46422 deg
ZDOT = 5804
649661 TA = 348
08294
MA = 348
11535
Ha = 219
245 n
mi
Hp = 214
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15994085
94 X = -4830754
35
Y = -14795779
44 feet Y = -4564021
72 meter
Z = 4422769
14 Z = 1324485
16
XDOT = 13714
940187 XDOT = 4182
898113
YDOT = -9122
322621 feet/sec YDOT = -2733
722982 meter/sec
ZDOT = 19044
126185 ZDOT = 5824
962991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17761558
95 X = 5413723
17
Y = -12654267
93 feet Y = -3857020
86 meter
Z = 4322416
92 Z = 1317472
68
XDOT = 5222
274848 XDOT = 1591
749374
YDOT = 13877
482860 feet/sec YDOT = 4229
856776 meter/sec
ZDOT = 19131
740481 ZDOT = 5831
354499
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
11633277
00016717 00000-0 10270-3 0 9112
2 25544 51
6433 214
2195 0007882 312
5111 47
5375 15
55164062 23985
Satellite: ISS
Catalog Number: 25544
Epoch time: 15142
11633277 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 214
2195 deg
Eccentricity:
0007882
Arg of perigee: 312
5111 deg
Mean anomaly: 47
5375 deg
Mean motion: 15
55164062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2398
Checksum: 291
Coasting Arc #13 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2015/143/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3541926
53 A = 6782014
26 meter
Y = 4820186
40 meter E =
0004880
Z = -3200795
49 I = 51
46947
XDOT = -5880
108168 Wp = 347
04249
YDOT = 1142
066448 meter/sec RA = 208
47023 deg
ZDOT = -4780
837165 TA = 230
05112
MA = 230
09400
Ha = 219
379 n
mi
Hp = 214
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11620493
87 X = 3503311
15
Y = 15814259
85 feet Y = 4859578
86 meter
Z = -10501297
53 Z = -3183682
86
XDOT = -19291
693463 XDOT = -5869
218384
YDOT = 3746
937164 feet/sec YDOT = 1076
372474 meter/sec
ZDOT = -15685
161303 ZDOT = -4809
375188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17726896
91 X = -5403158
18
Y = 8509006
09 feet Y = 2593545
06 meter
Z = -10428704
78 Z = -3178669
22
XDOT = 546
184997 XDOT = 166
477187
YDOT = -18260
889941 feet/sec YDOT = -5565
919254 meter/sec
ZDOT = -15807
789207 ZDOT = -4818
214150
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
08021637
00016717 00000-0 10270-3 0 9121
2 25544 51
6426 209
4070 0007941 315
4031 44
6482 15
55171137 24130
Satellite: ISS
Catalog Number: 25544
Epoch time: 15143
08021637 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 209
4070 deg
Eccentricity:
0007941
Arg of perigee: 315
4031 deg
Mean anomaly: 44
6482 deg
Mean motion: 15
55171137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2413
Checksum: 275
Coasting Arc #14 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2015/144/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1693499
00 A = 6777380
73 meter
Y = -4702889
04 meter E =
0003989
Z = 4572960
47 I = 51
48235
XDOT = 7033
293026 Wp = 47
44871
YDOT = 418
465083 meter/sec RA = 203
46244 deg
ZDOT = 3035
941494 TA = 12
17402
MA = 12
16438
Ha = 219
581 n
mi
Hp = 214
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5556099
08 X = -1662998
12
Y = -15429425
99 feet Y = -4721656
59 meter
Z = 15003151
16 Z = 4564807
56
XDOT = 23075
108353 XDOT = 7013
343397
YDOT = 1372
916940 feet/sec YDOT = 497
004239 meter/sec
ZDOT = 9960
437974 ZDOT = 3070
059568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16166862
71 X = 4927659
75
Y = -2931640
13 feet Y = -893563
91 meter
Z = 14968968
05 Z = 4562541
46
XDOT = -5499
924191 XDOT = -1676
376893
YDOT = 21259
141422 feet/sec YDOT = 6479
786305 meter/sec
ZDOT = 10106
756775 ZDOT = 3080
539465
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
10833720
00016717 00000-0 10270-3 0 9130
2 25544 51
6424 204
2722 0007942 321
1267 38
9315 15
55194995 24296
Satellite: ISS
Catalog Number: 25544
Epoch time: 15144
10833720 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 204
2722 deg
Eccentricity:
0007942
Arg of perigee: 321
1267 deg
Mean anomaly: 38
9315 deg
Mean motion: 15
55194995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 300
Coasting Arc #15 (Orbit 2443)
---------------------------------------
Vector Time (GMT): 2015/145/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -441031
90 A = 6774285
49 meter
Y = 4260997
24 meter E =
0012660
Z = -5257284
94 I = 51
50113
XDOT = -7406
833473 Wp = 50
26752
YDOT = -1784
205477 meter/sec RA = 198
44352 deg
ZDOT = -818
119980 TA = 211
85310
MA = 211
92972
Ha = 219
597 n
mi
Hp = 214
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1446955
04 X = -463108
57
Y = 13979649
74 feet Y = 4255942
15 meter
Z = -17248310
16 Z = -5259480
81
XDOT = -24300
634754 XDOT = -7382
357431
YDOT = -5853
692509 feet/sec YDOT = -1866
896640 meter/sec
ZDOT = -2684
120670 ZDOT = -854
041734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13605639
25 X = -4146998
84
Y = -3472877
43 feet Y = -1058533
04 meter
Z = -17258452
77 Z = -5260376
40
XDOT = 9268
613788 XDOT = 2825
073483
YDOT = -22100
526670 feet/sec YDOT = -6736
240529 meter/sec
ZDOT = -2837
965638 ZDOT = -865
011926
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
07217714
00016717 00000-0 10270-3 0 9147
2 25544 51
6413 199
4584 0008015 323
9629 36
0983 15
55269195 24441
Satellite: ISS
Catalog Number: 25544
Epoch time: 15145
07217714 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 199
4584 deg
Eccentricity:
0008015
Arg of perigee: 323
9629 deg
Mean anomaly: 36
0983 deg
Mean motion: 15
55269195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2444
Checksum: 322
Coasting Arc #16 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2015/146/01:18:40
070
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2650943
90 A = 6774718
88 meter
Y = -3553528
65 meter E =
0009456
Z = 5125198
17 I = 51
53378
XDOT = 6920
949089 Wp = 357
58049
YDOT = 2916
493157 meter/sec RA = 193
42278 deg
ZDOT = -1548
487975 TA = 107
41699
MA = 107
31358
Ha = 219
625 n
mi
Hp = 213
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8697322
52 X = 2665586
84
Y = -11658558
55 feet Y = -3523802
39 meter
Z = 16814954
64 Z = 5138111
45
XDOT = 22706
525883 XDOT = 6895
343804
YDOT = 9568
547104 feet/sec YDOT = 2993
744631 meter/sec
ZDOT = -5080
341124 ZDOT = -1514
929220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10371221
13 X = 3161148
20
Y = 10105255
93 feet Y = 3080082
01 meter
Z = 16870971
55 Z = 5142272
13
XDOT = -11854
028972 XDOT = -3613
108031
YDOT = 20458
101002 feet/sec YDOT = 6235
629185 meter/sec
ZDOT = -4936
810174 ZDOT = -1504
739741
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
10025271
00016717 00000-0 10270-3 0 9158
2 25544 51
6418 194
3243 0008004 327
3607 32
7050 15
55292297 24609
Satellite: ISS
Catalog Number: 25544
Epoch time: 15146
10025271 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 194
3243 deg
Eccentricity:
0008004
Arg of perigee: 327
3607 deg
Mean anomaly: 32
7050 deg
Mean motion: 15
55292297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2460
Checksum: 281
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