[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 28th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
191/02:58:17
248 3
4 3
9 3
9
N/A -1
7 -0
0 219
1
000/00:10:34
496 0
5 0
1 213
8
Coasting Arc #1 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2015/177/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3247613
65 A = 6782251
21 meter
Y = -5235002
29 meter E =
0007311
Z = -2839637
69 I = 51
87576
XDOT = 5665
625170 Wp = 107
59888
YDOT = -751
352589 meter/sec RA = 36
97900 deg
ZDOT = -5107
423362 TA = 104
55036
MA = 104
46925
Ha = 220
070 n
mi
Hp = 211
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10654900
43 X = -3175039
29
Y = -17175204
36 feet Y = -5270913
19 meter
Z = -9316396
63 Z = -2855238
21
XDOT = 18588
009088 XDOT = 5698
415921
YDOT = -2465
067548 feet/sec YDOT = -687
812064 meter/sec
ZDOT = -16756
638326 ZDOT = -5079
821181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17020081
15 X = -5187720
74
Y = 10844216
23 feet Y = 3305317
11 meter
Z = -9382409
39 Z = -2859758
38
XDOT = -1947
637586 XDOT = -593
639936
YDOT = -17415
283811 feet/sec YDOT = -5308
178506 meter/sec
ZDOT = -16637
762094 ZDOT = -5071
189886
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 15177
51909854
00016717 00000-0 10270-3 0 9009
2 25544 51
6441 37
4356 0002832 92
7157 267
4320 15
55368810 29497
Satellite: ISS
Catalog Number: 25544
Epoch time: 15177
51909854 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 37
4356 deg
Eccentricity:
0002832
Arg of perigee: 92
7157 deg
Mean anomaly: 267
4320 deg
Mean motion: 15
55368810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2949
Checksum: 320
Coasting Arc #2 (Orbit 2964)
---------------------------------------
Vector Time (GMT): 2015/178/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1467106
45 A = 6777530
14 meter
Y = 4963853
29 meter E =
0012320
Z = 4366873
06 I = 51
83394
XDOT = -6777
740051 Wp = 104
90873
YDOT = -1039
734163 meter/sec RA = 31
99904 deg
ZDOT = 3447
748281 TA = 310
19218
MA = 310
29996
Ha = 220
077 n
mi
Hp = 211
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4813341
37 X = 1390277
69
Y = 16285607
92 feet Y = 4979829
42 meter
Z = 14327011
34 Z = 4373813
90
XDOT = -22236
679956 XDOT = -6782
357696
YDOT = -3411
201323 feet/sec YDOT = -1115
553462 meter/sec
ZDOT = 11311
510109 ZDOT = 3414
811867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16128823
97 X = 4916065
55
Y = -5236776
68 feet Y = -1596169
53 meter
Z = 14355826
06 Z = 4375655
78
XDOT = -3082
028897 XDOT = -939
402408
YDOT = 21229
117180 feet/sec YDOT = 6470
634917 meter/sec
ZDOT = 11170
068621 ZDOT = 3404
636916
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 15178
54708944
00016717 00000-0 10270-3 0 9011
2 25544 51
6439 32
3005 0002933 92
6425 267
5064 15
55386611 29651
Satellite: ISS
Catalog Number: 25544
Epoch time: 15178
54708944 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 32
3005 deg
Eccentricity:
0002933
Arg of perigee: 92
6425 deg
Mean anomaly: 267
5064 deg
Mean motion: 15
55386611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2965
Checksum: 316
Coasting Arc #3 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2015/179/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 656851
86 A = 6773962
97 meter
Y = -4280133
73 meter E =
0016877
Z = -5223986
02 I = 51
79382
XDOT = 7115
680807 Wp = 83
31575
YDOT = 2561
255849 meter/sec RA = 27
00201 deg
ZDOT = -1205
212467 TA = 175
13906
MA = 175
12266
Ha = 219
937 n
mi
Hp = 211
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2155025
77 X = 730040
78
Y = -14042433
49 feet Y = -4272378
53 meter
Z = -17139061
75 Z = -5220617
89
XDOT = 23345
409473 XDOT = 7092
365870
YDOT = 8403
070370 feet/sec YDOT = 2640
697833 meter/sec
ZDOT = -3954
109145 ZDOT = -1170
702052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14138016
97 X = -4309267
57
Y = -1574082
25 feet Y = -479780
27 meter
Z = -17123675
23 Z = -5219296
21
XDOT = 7134
186974 XDOT = 2174
500190
YDOT = -22722
350880 feet/sec YDOT = -6925
772548 meter/sec
ZDOT = -3806
223224 ZDOT = -1160
136839
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 15179
51081161
00016717 00000-0 10270-3 0 9025
2 25544 51
6426 27
4860 0002781 97
3367 262
8102 15
55448403 29805
Satellite: ISS
Catalog Number: 25544
Epoch time: 15179
51081161 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 27
4860 deg
Eccentricity:
0002781
Arg of perigee: 97
3367 deg
Mean anomaly: 262
8102 deg
Mean motion: 15
55448403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 304
Coasting Arc #4 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2015/180/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2819809
68 A = 6773986
93 meter
Y = 3284316
46 meter E =
0006370
Z = 5205537
16 I = 51
76552
XDOT = -6603
257072 Wp = 72
98877
YDOT = -3713
549846 meter/sec RA = 21
99767 deg
ZDOT = -1230
903207 TA = 28
80986
MA = 28
77470
Ha = 219
974 n
mi
Hp = 211
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9251344
09 X = -2881612
71
Y = 10775316
46 feet Y = 3252437
23 meter
Z = 17078533
99 Z = 5191689
37
XDOT = -21664
229239 XDOT = -6555
261220
YDOT = -12183
562488 feet/sec YDOT = -3787
123261 meter/sec
ZDOT = -4038
396350 ZDOT = -1262
864548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11372133
85 X = 3466226
40
Y = 8626921
28 feet Y = 2629485
61 meter
Z = 17018282
42 Z = 5187172
48
XDOT = -10097
702112 XDOT = -3077
779604
YDOT = 21566
969370 feet/sec YDOT = 6573
612264 meter/sec
ZDOT = -4175
069897 ZDOT = -1272
561304
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 15180
53876569
00016717 00000-0 10270-3 0 9034
2 25544 51
6429 22
3513 0002716 101
9466 258
1992 15
55466294 29967
Satellite: ISS
Catalog Number: 25544
Epoch time: 15180
53876569 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 22
3513 deg
Eccentricity:
0002716
Arg of perigee: 101
9466 deg
Mean anomaly: 258
1992 deg
Mean motion: 15
55466294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2996
Checksum: 335
Coasting Arc #5 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2015/181/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4740214
58 A = 6777413
80 meter
Y = -2142376
44 meter E =
0011297
Z = -4355864
46 I = 51
74598
XDOT = 5189
446101 Wp = 108
80515
YDOT = 4443
467060 meter/sec RA = 16
99579 deg
ZDOT = 3465
686282 TA = 196
35370
MA = 196
39018
Ha = 219
826 n
mi
Hp = 211
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15551885
09 X = 4784977
97
Y = -7028794
08 feet Y = -2089117
33 meter
Z = -14290893
89 Z = -4332729
03
XDOT = 17025
741801 XDOT = 5122
537514
YDOT = 14578
304004 feet/sec YDOT = 4501
124228 meter/sec
ZDOT = 11370
361819 ZDOT = 3490
733713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8308194
87 X = -2532337
80
Y = -15002862
55 feet Y = -4572872
51 meter
Z = -14190938
57 Z = -4325398
08
XDOT = 12023
143247 XDOT = 3664
654062
YDOT = -17502
250928 feet/sec YDOT = -5334
686083 meter/sec
ZDOT = 11477
140731 ZDOT = 3498
232495
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 15181
50245567
00016717 00000-0 10270-3 0 9041
2 25544 51
6415 17
5358 0002719 105
5049 254
6405 15
55500300 30111
Satellite: ISS
Catalog Number: 25544
Epoch time: 15181
50245567 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 17
5358 deg
Eccentricity:
0002719
Arg of perigee: 105
5049 deg
Mean anomaly: 254
6405 deg
Mean motion: 15
55500300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 276
Coasting Arc #6 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2015/182/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6123876
80 A = 6782040
85 meter
Y = 914568
33 meter E =
0015981
Z = 2749133
19 I = 51
73181
XDOT = -3041
446654 Wp = 101
72356
YDOT = -4804
175384 meter/sec RA = 12
00838 deg
ZDOT = -5154
658684 TA = 47
15466
MA = 47
02050
Ha = 219
693 n
mi
Hp = 211
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20091459
32 X = -6147002
77
Y = 3000552
26 feet Y = 845957
42 meter
Z = 9019465
83 Z = 2719328
70
XDOT = -9978
499522 XDOT = -2962
459907
YDOT = -15761
730261 feet/sec YDOT = -4837
744427 meter/sec
ZDOT = -16911
609857 ZDOT = -5169
242225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5009016
06 X = 1526748
10
Y = 19745356
52 feet Y = 6018384
67 meter
Z = 8891089
32 Z = 2710004
03
XDOT = -13252
884203 XDOT = -4039
479105
YDOT = 11038
044895 feet/sec YDOT = 3364
396084 meter/sec
ZDOT = -16973
306859 ZDOT = -5173
463931
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 15182
53037219
00016717 00000-0 10270-3 0 9059
2 25544 51
6419 12
4005 0002471 106
2982 253
8443 15
55564278 30271
Satellite: ISS
Catalog Number: 25544
Epoch time: 15182
53037219 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 12
4005 deg
Eccentricity:
0002471
Arg of perigee: 106
2982 deg
Mean anomaly: 253
8443 deg
Mean motion: 15
55564278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 294
Coasting Arc #7 (Orbit 3041)
---------------------------------------
Vector Time (GMT): 2015/183/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6738210
88 A = 6785024
70 meter
Y = 263031
56 meter E =
0011699
Z = -714175
55 I = 51
70919
XDOT = 437
127444 Wp = 52
34623
YDOT = 4799
492126 meter/sec RA = 7
03177 deg
ZDOT = 5965
708663 TA = 299
94222
MA = 300
05834
Ha = 219
721 n
mi
Hp = 211
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22106991
09 X = 6738237
97
Y = 862964
43 feet Y = 338382
90 meter
Z = -2343095
64 Z = -681442
84
XDOT = 1434
145157 XDOT = 354
446995
YDOT = 15746
365244 feet/sec YDOT = 4803
917235 meter/sec
ZDOT = 19572
534983 ZDOT = 5967
631980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1742351
42 X = -531068
71
Y = -22069608
23 feet Y = -6726816
59 meter
Z = -2202376
85 Z = -671284
46
XDOT = 13875
934442 XDOT = 4229
384818
YDOT = -3023
691359 feet/sec YDOT = -921
621126 meter/sec
ZDOT = 19579
784352 ZDOT = 5967
918270
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 15183
49402990
00016717 00000-0 10270-3 0 9068
2 25544 51
6407 7
5850 0002644 112
7411 247
4022 15
55543173 30422
Satellite: ISS
Catalog Number: 25544
Epoch time: 15183
49402990 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 7
5850 deg
Eccentricity:
0002644
Arg of perigee: 112
7411 deg
Mean anomaly: 247
4022 deg
Mean motion: 15
55543173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3042
Checksum: 284
Coasting Arc #8 (Orbit 3057)
---------------------------------------
Vector Time (GMT): 2015/184/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6462219
59 A = 6784052
18 meter
Y = -1411736
31 meter E =
0010560
Z = -1491188
76 I = 51
67523
XDOT = 2305
650700 Wp = 134
77293
YDOT = -4486
371498 meter/sec RA = 2
05838 deg
ZDOT = -5776
791049 TA = 61
50680
MA = 61
40048
Ha = 219
561 n
mi
Hp = 211
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21201507
85 X = -6438709
40
Y = -4631680
79 feet Y = -1483869
43 meter
Z = -4892351
58 Z = -1522523
63
XDOT = 7564
470800 XDOT = 2383
708129
YDOT = -14719
066593 feet/sec YDOT = -4460
151019 meter/sec
ZDOT = -18952
726539 ZDOT = -5765
401775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1741433
89 X = -530789
05
Y = 21600695
90 feet Y = 6583892
11 meter
Z = -5026813
17 Z = -1532172
65
XDOT = -14045
903772 XDOT = -4281
191470
YDOT = -5507
303084 feet/sec YDOT = -1678
625980 meter/sec
ZDOT = -18902
791004 ZDOT = -5761
570698
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 15184
52191144
00016717 00000-0 10270-3 0 9070
2 25544 51
6409 2
4492 0002635 112
6680 247
4752 15
55600722 30588
Satellite: ISS
Catalog Number: 25544
Epoch time: 15184
52191144 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 2
4492 deg
Eccentricity:
0002635
Arg of perigee: 112
6680 deg
Mean anomaly: 247
4752 deg
Mean motion: 15
55600722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3058
Checksum: 292
Coasting Arc #9 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2015/185/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5328215
60 A = 6779959
38 meter
Y = 2428243
94 meter E =
0014695
Z = 3406620
98 I = 51
62958
XDOT = -4736
354271 Wp = 95
44369
YDOT = 3897
853225 meter/sec RA = 357
07258 deg
ZDOT = 4611
149525 TA = 304
45323
MA = 304
59200
Ha = 219
453 n
mi
Hp = 211
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17481022
31 X = 5284118
56
Y = 7966679
60 feet Y = 2487580
60 meter
Z = 11176578
02 Z = 3432397
18
XDOT = -15539
220048 XDOT = -4801
987877
YDOT = 12788
232365 feet/sec YDOT = 3844
520726 meter/sec
ZDOT = 15128
443325 ZDOT = 4587
982596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5236675
81 X = 1596138
79
Y = -18416100
52 feet Y = -5613227
44 meter
Z = 11286916
72 Z = 3440252
22
XDOT = 13668
973883 XDOT = 4166
303239
YDOT = 13134
001234 feet/sec YDOT = 4003
243576 meter/sec
ZDOT = 15027
986020 ZDOT = 4580
530139
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 15185
54977432
00016717 00000-0 10270-3 0 9086
2 25544 51
6405 357
3126 0002649 121
7903 238
3508 15
55623218 30745
Satellite: ISS
Catalog Number: 25544
Epoch time: 15185
54977432 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 357
3126 deg
Eccentricity:
0002649
Arg of perigee: 121
7903 deg
Mean anomaly: 238
3508 deg
Mean motion: 15
55623218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 315
Coasting Arc #10 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2015/186/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3465216
20 A = 6775153
94 meter
Y = -3343560
16 meter E =
0013403
Z = -4778469
95 I = 51
58279
XDOT = 6531
871505 Wp = 80
30487
YDOT = -3016
190985 meter/sec RA = 352
06909 deg
ZDOT = -2630
355973 TA = 163
72446
MA = 163
68137
Ha = 219
529 n
mi
Hp = 211
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11368819
57 X = -3404358
51
Y = -10969685
56 feet Y = -3381969
77 meter
Z = -15677394
87 Z = -4795155
53
XDOT = 21430
024622 XDOT = 6577
890903
YDOT = -9895
639715 feet/sec YDOT = -2942
889775 meter/sec
ZDOT = -8629
776813 ZDOT = -2598
514381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8914670
83 X = -2717191
67
Y = 12956847
36 feet Y = 3949247
07 meter
Z = -15748445
00 Z = -4800126
04
XDOT = -12431
510096 XDOT = -3789
124277
YDOT = -18858
870003 feet/sec YDOT = -5748
183577 meter/sec
ZDOT = -8492
208023 ZDOT = -2588
425005
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 15186
51338004
00016717 00000-0 10270-3 0 9091
2 25544 51
6413 352
4982 0002792 120
9261 239
2167 15
55646915 30893
Satellite: ISS
Catalog Number: 25544
Epoch time: 15186
51338004 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 352
4982 deg
Eccentricity:
0002792
Arg of perigee: 120
9261 deg
Mean anomaly: 239
2167 deg
Mean motion: 15
55646915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3089
Checksum: 318
Coasting Arc #11 (Orbit 3104)
---------------------------------------
Vector Time (GMT): 2015/187/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1172399
25 A = 6773016
22 meter
Y = 4047990
21 meter E =
0005064
Z = 5298139
79 I = 51
54346
XDOT = -7438
348199 Wp = 111
14772
YDOT = 1879
876460 meter/sec RA = 347
04899 deg
ZDOT = 207
743980 TA = 336
86003
MA = 336
88283
Ha = 219
514 n
mi
Hp = 211
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3846454
24 X = 1101310
48
Y = 13280807
76 feet Y = 4060702
88 meter
Z = 17382348
40 Z = 5303662
63
XDOT = -24404
029523 XDOT = -7459
825725
YDOT = 6167
573688 feet/sec YDOT = 1796
575874 meter/sec
ZDOT = 681
574738 ZDOT = 171
558369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12358979
37 X = 3767016
91
Y = -6134661
58 feet Y = -1869844
85 meter
Z = 17405247
98 Z = 5305119
59
XDOT = 10140
751315 XDOT = 3090
901001
YDOT = 21938
999312 feet/sec YDOT = 6687
006990 meter/sec
ZDOT = 525
574072 ZDOT = 160
194977
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 15187
54120816
00016717 00000-0 10270-3 0 9107
2 25544 51
6409 347
3615 0002759 124
1026 236
0389 15
55618620 31054
Satellite: ISS
Catalog Number: 25544
Epoch time: 15187
54120816 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 347
3615 deg
Eccentricity:
0002759
Arg of perigee: 124
1026 deg
Mean anomaly: 236
0389 deg
Mean motion: 15
55618620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 295
Coasting Arc #12 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2015/188/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1229004
02 A = 6774591
37 meter
Y = -4508786
55 meter E =
0014694
Z = -4918372
67 I = 51
51954
XDOT = 7301
770270 Wp = 110
40522
YDOT = -477
691843 meter/sec RA = 342
02650 deg
ZDOT = 2262
958307 TA = 181
76614
MA = 181
77134
Ha = 219
411 n
mi
Hp = 211
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4032165
41 X = 1303222
38
Y = -14792606
79 feet Y = -4494627
74 meter
Z = -16136393
29 Z = -4912222
48
XDOT = 23955
939206 XDOT = 7295
576757
YDOT = -1567
230455 feet/sec YDOT = -396
073432 meter/sec
ZDOT = 7424
403893 ZDOT = 2298
413472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15324777
86 X = -4670992
29
Y = -1055419
62 feet Y = -321691
90 meter
Z = -16109004
78 Z = -4910024
66
XDOT = -6449
350863 XDOT = -1965
762143
YDOT = -21978
978774 feet/sec YDOT = -6699
192730 meter/sec
ZDOT = 7576
959862 ZDOT = 2309
457366
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 15188
50477717
00016717 00000-0 10270-3 0 9110
2 25544 51
6420 342
5470 0002750 129
1661 230
9737 15
55686416 31209
Satellite: ISS
Catalog Number: 25544
Epoch time: 15188
50477717 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 342
5470 deg
Eccentricity:
0002750
Arg of perigee: 129
1661 deg
Mean anomaly: 230
9737 deg
Mean motion: 15
55686416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 303
Coasting Arc #13 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2015/189/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3393741
78 A = 6779190
29 meter
Y = 4588884
10 meter E =
0013915
Z = 3645299
22 I = 51
50426
XDOT = -6217
980517 Wp = 93
74378
YDOT = -1126
565590 meter/sec RA = 337
01293 deg
ZDOT = -4357
238970 TA = 42
80411
MA = 42
69585
Ha = 219
396 n
mi
Hp = 211
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11134323
41 X = -3462510
94
Y = 15055394
03 feet Y = 4550548
32 meter
Z = 11959643
09 Z = 3628646
43
XDOT = -20400
198548 XDOT = -6183
755154
YDOT = -3696
081332 feet/sec YDOT = -1195
907486 meter/sec
ZDOT = -14295
403444 ZDOT = -4387
361470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17147500
35 X = 5226558
11
Y = 7637511
01 feet Y = 2327913
35 meter
Z = 11887084
07 Z = 3623183
22
XDOT = 1400
781990 XDOT = 426
958350
YDOT = 19374
908998 feet/sec YDOT = 5905
472262 meter/sec
ZDOT = -14424
686907 ZDOT = -4396
644569
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 15189
53256726
00016717 00000-0 10270-3 0 9120
2 25544 51
6412 337
4104 0002688 132
9990 227
1390 15
55697039 31367
Satellite: ISS
Catalog Number: 25544
Epoch time: 15189
53256726 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 337
4104 deg
Eccentricity:
0002688
Arg of perigee: 132
9990 deg
Mean anomaly: 227
1390 deg
Mean motion: 15
55697039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 321
Coasting Arc #14 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2015/190/11:49:32
056
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4999867
95 A = 6783373
97 meter
Y = -4234687
85 meter E =
0007750
Z = -1751195
27 I = 51
49122
XDOT = 4344
329088 Wp = 57
63179
YDOT = 2795
924227 meter/sec RA = 332
01512 deg
ZDOT = 5664
957234 TA = 283
10128
MA = 283
18776
Ha = 219
259 n
mi
Hp = 211
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16403766
23 X = 5055356
26
Y = -13893332
83 feet Y = -4178465
67 meter
Z = -5745391
30 Z = -1726772
49
XDOT = 14253
048189 XDOT = 4285
223366
YDOT = 9172
979747 feet/sec YDOT = 2844
174468 meter/sec
ZDOT = 18585
817697 ZDOT = 5685
917716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17380402
34 X = -5297546
63
Y = -12697848
96 feet Y = -3870304
36 meter
Z = -5639504
53 Z = -1718920
98
XDOT = 4654
968297 XDOT = 1418
834337
YDOT = -14632
603643 feet/sec YDOT = -4460
017590 meter/sec
ZDOT = 18675
355952 ZDOT = 5692
248494
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 15190
49610264
00016717 00000-0 10270-3 0 9139
2 25544 51
6425 332
5956 0002662 135
2886 224
8483 15
55744797 31512
Satellite: ISS
Catalog Number: 25544
Epoch time: 15190
49610264 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 332
5956 deg
Eccentricity:
0002662
Arg of perigee: 135
2886 deg
Mean anomaly: 224
8483 deg
Mean motion: 15
55744797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 325
Coasting Arc #15 (Orbit 3160)
---------------------------------------
Vector Time (GMT): 2015/191/03:03:34
496
Vector Time (MET): N/A
Weight (LBS) : 877310
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 818321
03 A = 6777497
74 meter
Y = -4848178
76 meter E =
0009672
Z = -4674276
27 I = 51
44842
XDOT = 6944
744015 Wp = 116
72877
YDOT = -1560
374965 meter/sec RA = 328
83420 deg
ZDOT = 2834
519581 TA = 181
50401
MA = 181
50692
Ha = 219
129 n
mi
Hp = 213
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2684780
29 X = 895179
54
Y = -15906098
29 feet Y = -4838597
63 meter
Z = -15335552
06 Z = -4670114
76
XDOT = 22784
593224 XDOT = 6947
907353
YDOT = -5119
340437 feet/sec YDOT = -1482
696836 meter/sec
ZDOT = 9299
604926 ZDOT = 2868
263276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9749929
46 X = 2971778
50
Y = -12873623
43 feet Y = -3923880
42 meter
Z = -15316653
05 Z = -4668515
85
XDOT = 21610
999285 XDOT = 6587
032582
YDOT = 5130
959499 feet/sec YDOT = 1563
916455 meter/sec
ZDOT = 9445
006967 ZDOT = 2878
838124
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 15191
13845116
00016717 00000-0 10270-3 0 9148
2 25544 51
6441 329
3900 0001616 237
6978 122
4019 15
55021944 31611
Satellite: ISS
Catalog Number: 25544
Epoch time: 15191
13845116 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 329
3900 deg
Eccentricity:
0001616
Arg of perigee: 237
6978 deg
Mean anomaly: 122
4019 deg
Mean motion: 15
55021944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3161
Checksum: 293
Coasting Arc #16 (Orbit 3176)
---------------------------------------
Vector Time (GMT): 2015/192/03:03:34
496
Vector Time (MET): N/A
Weight (LBS) : 877310
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2605101
48 A = 6781858
25 meter
Y = 5255893
59 meter E =
0011137
Z = 3392851
81 I = 51
43607
XDOT = -6136
484991 Wp = 94
17708
YDOT = -61
011421 meter/sec RA = 323
82502 deg
ZDOT = -4604
937542 TA = 46
00756
MA = 45
91580
Ha = 219
122 n
mi
Hp = 213
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8546920
88 X = -2680161
69
Y = 17243745
38 feet Y = 5226341
62 meter
Z = 11131403
57 Z = 3380014
97
XDOT = -20132
824774 XDOT = -6112
977669
YDOT = -200
168703 feet/sec YDOT = -129
501719 meter/sec
ZDOT = -15108
062802 ZDOT = -4634
690231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15352408
31 X = -4679414
05
Y = 11659756
53 feet Y = 3553893
79 meter
Z = 11075124
99 Z = 3375698
10
XDOT = -17033
372358 XDOT = -5191
771895
YDOT = -7917
403812 feet/sec YDOT = -2413
224682 meter/sec
ZDOT = -15235
966065 ZDOT = -4643
922457
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 15192
16668494
00016717 00000-0 10270-3 0 9155
2 25544 51
6438 324
2572 0001584 241
4966 118
6028 15
55034288 31779
Satellite: ISS
Catalog Number: 25544
Epoch time: 15192
16668494 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 324
2572 deg
Eccentricity:
0001584
Arg of perigee: 241
4966 deg
Mean anomaly: 118
6028 deg
Mean motion: 15
55034288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3177
Checksum: 328
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