[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 24th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
087/01:36:05
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 211
3
092/18:33:35
100 -0
7 1
4 1
4
N/A 1
1 0
0 220
3
000/00:03:10
200 0
5 -0
1 212
4
Coasting Arc #1 (Orbit 1469)
---------------------------------------
Vector Time (GMT): 2015/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4866079
24 A = 6784823
67 meter
Y = 4356721
43 meter E =
0009487
Z = -1842877
00 I = 51
83070
XDOT = -4465
592470 Wp = 84
50893
YDOT = -2606
320927 meter/sec RA = 150
97526 deg
ZDOT = 5655
636403 TA = 255
28463
MA = 255
38980
Ha = 221
552 n
mi
Hp = 211
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15964826
90 X = -4905483
42
Y = 14293705
47 feet Y = 4302085
20 meter
Z = -6046184
39 Z = -1866611
84
XDOT = -14650
893930 XDOT = -4463
589186
YDOT = -8550
921675 feet/sec YDOT = -2656
246188 meter/sec
ZDOT = 18555
237544 ZDOT = 5633
948507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15969932
08 X = -4867635
30
Y = 14244241
70 feet Y = 4341644
87 meter
Z = -6148569
55 Z = -1874084
00
XDOT = -13703
276341 XDOT = -4176
758629
YDOT = -7430
017733 feet/sec YDOT = -2264
669405 meter/sec
ZDOT = 18462
697894 ZDOT = 5627
430318
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 15082
50368902
00016717 00000-0 10270-3 0 9006
2 25544 51
6444 152
0622 0006735 132
7536 227
4185 15
55163667 14708
Satellite: ISS
Catalog Number: 25544
Epoch time: 15082
50368902 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 152
0622 deg
Eccentricity:
0006735
Arg of perigee: 132
7536 deg
Mean anomaly: 227
4185 deg
Mean motion: 15
55163667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1470
Checksum: 298
Coasting Arc #2 (Orbit 1485)
---------------------------------------
Vector Time (GMT): 2015/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5716794
88 A = 6786118
05 meter
Y = -3632740
42 meter E =
0018567
Z = -233771
92 I = 51
86251
XDOT = 2376
205453 Wp = 136
19654
YDOT = 4108
261867 meter/sec RA = 146
01324 deg
ZDOT = -6030
301767 TA = 46
31694
MA = 46
16322
Ha = 221
499 n
mi
Hp = 210
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18755888
73 X = 5758127
74
Y = -11918439
69 feet Y = -3568580
40 meter
Z = -766968
24 Z = -205899
94
XDOT = 7795
949649 XDOT = 2359
382365
YDOT = 13478
549432 feet/sec YDOT = 4134
739442 meter/sec
ZDOT = -19784
454615 ZDOT = -6018
799874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18590045
53 X = 5666245
88
Y = -12182465
80 feet Y = -3713215
58 meter
Z = -646947
36 Z = -197189
55
XDOT = 7222
603313 XDOT = 2201
449490
YDOT = 12007
898558 feet/sec YDOT = 3660
007480 meter/sec
ZDOT = -19735
798909 ZDOT = -6015
471508
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 15083
53180704
00016717 00000-0 10270-3 0 9013
2 25544 51
6442 146
9281 0006846 135
3585 224
8121 15
55229310 14861
Satellite: ISS
Catalog Number: 25544
Epoch time: 15083
53180704 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 146
9281 deg
Eccentricity:
0006846
Arg of perigee: 135
3585 deg
Mean anomaly: 224
8121 deg
Mean motion: 15
55229310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 298
Coasting Arc #3 (Orbit 1501)
---------------------------------------
Vector Time (GMT): 2015/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5889504
48 A = 6784049
75 meter
Y = 2507155
93 meter E =
0017721
Z = 2233421
94 I = 51
88106
XDOT = -194
055703 Wp = 92
09711
YDOT = -5367
779519 meter/sec RA = 141
05157 deg
ZDOT = 5475
896078 TA = 292
65849
MA = 292
84579
Ha = 221
437 n
mi
Hp = 211
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19322521
27 X = -5927951
53
Y = 8225577
18 feet Y = 2441080
88 meter
Z = 7327499
81 Z = 2204718
19
XDOT = -636
665691 XDOT = -160
617409
YDOT = -17610
825192 feet/sec YDOT = -5369
762098 meter/sec
ZDOT = 17965
538315 ZDOT = 5475
035114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19101358
91 X = -5822094
19
Y = 8829022
32 feet Y = 2691086
00 meter
Z = 7204072
09 Z = 2195801
17
XDOT = -658
134793 XDOT = -200
599485
YDOT = -16184
185260 feet/sec YDOT = -4932
939667 meter/sec
ZDOT = 17962
691841 ZDOT = 5475
028473
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 15084
55990190
00016717 00000-0 10270-3 0 9025
2 25544 51
6439 141
7943 0006820 138
1030 222
0646 15
55242917 15022
Satellite: ISS
Catalog Number: 25544
Epoch time: 15084
55990190 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 141
7943 deg
Eccentricity:
0006820
Arg of perigee: 138
1030 deg
Mean anomaly: 222
0646 deg
Mean motion: 15
55242917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1502
Checksum: 291
Coasting Arc #4 (Orbit 1516)
---------------------------------------
Vector Time (GMT): 2015/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5434873
40 A = 6779458
22 meter
Y = -932392
44 meter E =
0011129
Z = -3950110
46 I = 51
89057
XDOT = -1873
275538 Wp = 108
74008
YDOT = 6224
449188 meter/sec RA = 136
07969 deg
ZDOT = -4059
448589 TA = 119
00089
MA = 118
88931
Ha = 221
345 n
mi
Hp = 211
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17830949
47 X = 5464083
85
Y = -3059030
33 feet Y = -871453
17 meter
Z = -12959680
00 Z = -3923637
89
XDOT = -6145
917118 XDOT = -1923
020305
YDOT = 20421
421221 feet/sec YDOT = 6203
222496 meter/sec
ZDOT = -13318
400882 ZDOT = -4068
669973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17743216
63 X = 5408132
43
Y = -3925685
09 feet Y = -1196548
81 meter
Z = -12846049
64 Z = -3915475
93
XDOT = -5349
657000 XDOT = -1630
575454
YDOT = 19396
429704 feet/sec YDOT = 5912
031774 meter/sec
ZDOT = -13358
918240 ZDOT = -4071
798280
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 15085
52371965
00016717 00000-0 10270-3 0 9037
2 25544 51
6443 136
9808 0006833 141
4655 218
6987 15
55286585 15171
Satellite: ISS
Catalog Number: 25544
Epoch time: 15085
52371965 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 136
9808 deg
Eccentricity:
0006833
Arg of perigee: 141
4655 deg
Mean anomaly: 218
6987 deg
Mean motion: 15
55286585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1517
Checksum: 342
Coasting Arc #5 (Orbit 1532)
---------------------------------------
Vector Time (GMT): 2015/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4465273
71 A = 6775235
93 meter
Y = -865054
22 meter E =
0012601
Z = 5016667
97 I = 51
89884
XDOT = 3551
537813 Wp = 134
81422
YDOT = -6493
285819 meter/sec RA = 131
09492 deg
ZDOT = 2029
726040 TA = 295
48147
MA = 295
61177
Ha = 221
269 n
mi
Hp = 211
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14649848
14 X = -4479637
62
Y = -2838104
40 feet Y = -915067
68 meter
Z = 16458884
42 Z = 4994941
80
XDOT = 11652
026947 XDOT = 3614
023698
YDOT = -21303
431166 feet/sec YDOT = -6453
220637 meter/sec
ZDOT = 6659
206169 ZDOT = 2047
131039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14908434
51 X = -4544090
84
Y = -1861290
26 feet Y = -567321
27 meter
Z = 16365877
39 Z = 4988319
43
XDOT = 10049
284146 XDOT = 3063
021808
YDOT = -20932
353218 feet/sec YDOT = -6380
181261 meter/sec
ZDOT = 6734
863516 ZDOT = 2052
786400
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 15086
55176907
00016717 00000-0 10270-3 0 9041
2 25544 51
6440 131
8471 0006774 144
6222 215
5382 15
55335458 15334
Satellite: ISS
Catalog Number: 25544
Epoch time: 15086
55176907 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 131
8471 deg
Eccentricity:
0006774
Arg of perigee: 144
6222 deg
Mean anomaly: 215
5382 deg
Mean motion: 15
55335458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1533
Checksum: 309
Coasting Arc #6 (Orbit 1541)
---------------------------------------
Vector Time (GMT): 2015/087/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4499056
77 A = 6785701
99 meter
Y = 5049567
97 meter E =
0013759
Z = 518078
95 I = 51
94407
XDOT = -3226
359472 Wp = 78
32998
YDOT = -3504
574806 meter/sec RA = 128
26227 deg
ZDOT = 6008
155599 TA = 287
23655
MA = 287
38709
Ha = 220
976 n
mi
Hp = 211
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14760684
94 X = -4557704
48
Y = 16566824
06 feet Y = 4998928
72 meter
Z = 1699734
08 Z = 496080
56
XDOT = -10585
168871 XDOT = -3216
115940
YDOT = -11497
948837 feet/sec YDOT = -3540
596204 meter/sec
ZDOT = 19711
796585 ZDOT = 5992
507863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5134109
41 X = 1564876
55
Y = -21593812
44 feet Y = -6581794
03 meter
Z = 1604606
04 Z = 489083
92
XDOT = 13309
534527 XDOT = 4056
746124
YDOT = 4658
318926 feet/sec YDOT = 1419
855609 meter/sec
ZDOT = 19645
269698 ZDOT = 5987
878204
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 15087
13003661
00016717 00000-0 10270-3 0 9053
2 25544 51
6425 128
9575 0006455 147
4147 212
7405 15
55341885 15428
Satellite: ISS
Catalog Number: 25544
Epoch time: 15087
13003661 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 128
9575 deg
Eccentricity:
0006455
Arg of perigee: 147
4147 deg
Mean anomaly: 212
7405 deg
Mean motion: 15
55341885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1542
Checksum: 305
Coasting Arc #7 (Orbit 1556)
---------------------------------------
Vector Time (GMT): 2015/088/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4945585
57 A = 6782942
08 meter
Y = -3856986
64 meter E =
0011468
Z = -2575460
63 I = 51
95377
XDOT = 1435
010552 Wp = 141
14339
YDOT = 5360
486951 meter/sec RA = 123
30448 deg
ZDOT = -5293
617516 TA = 67
69603
MA = 67
57449
Ha = 220
928 n
mi
Hp = 211
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16225674
44 X = 5000858
29
Y = -12654155
65 feet Y = -3801373
11 meter
Z = -8449673
99 Z = -2551301
41
XDOT = 4708
039870 XDOT = 1400
675928
YDOT = 17586
899446 feet/sec YDOT = 5376
341625 meter/sec
ZDOT = -17367
511536 ZDOT = -5286
730532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7992774
32 X = -2436197
61
Y = 19006999
20 feet Y = 5793333
36 meter
Z = -8345459
64 Z = -2543696
10
XDOT = -11428
869168 XDOT = -3483
519322
YDOT = -12387
828899 feet/sec YDOT = -3775
810248 meter/sec
ZDOT = -17338
847446 ZDOT = -5284
880702
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 15088
09380115
00016717 00000-0 10270-3 0 9062
2 25544 51
6422 124
1441 0006445 150
3040 209
8480 15
55379664 15571
Satellite: ISS
Catalog Number: 25544
Epoch time: 15088
09380115 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 124
1441 deg
Eccentricity:
0006445
Arg of perigee: 150
3040 deg
Mean anomaly: 209
8480 deg
Mean motion: 15
55379664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1557
Checksum: 297
Coasting Arc #8 (Orbit 1572)
---------------------------------------
Vector Time (GMT): 2015/089/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4877222
02 A = 6778260
62 meter
Y = 2145285
06 meter E =
0015309
Z = 4184675
28 I = 51
95462
XDOT = 282
036005 Wp = 123
60805
YDOT = -6692
114407 meter/sec RA = 118
33356 deg
ZDOT = 3741
371448 TA = 288
04878
MA = 288
21551
Ha = 220
813 n
mi
Hp = 211
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16001384
58 X = -4921176
09
Y = 7038336
82 feet Y = 2090499
52 meter
Z = 13729249
61 Z = 4160875
81
XDOT = 925
314978 XDOT = 338
673779
YDOT = -21955
755930 feet/sec YDOT = -6688
643362 meter/sec
ZDOT = 12274
840708 ZDOT = 3742
879894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10334512
67 X = 3149959
46
Y = -14197948
30 feet Y = -4327534
64 meter
Z = 13626844
85 Z = 4153462
31
XDOT = 9315
599307 XDOT = 2839
394669
YDOT = 18626
387370 feet/sec YDOT = 5677
322870 meter/sec
ZDOT = 12282
397996 ZDOT = 3743
674909
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 15089
12179477
00016717 00000-0 10270-3 0 9075
2 25544 51
6418 119
0087 0006469 155
0360 205
1107 15
55415954 15734
Satellite: ISS
Catalog Number: 25544
Epoch time: 15089
12179477 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 119
0087 deg
Eccentricity:
0006469
Arg of perigee: 155
0360 deg
Mean anomaly: 205
1107 deg
Mean motion: 15
55415954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1573
Checksum: 313
Coasting Arc #9 (Orbit 1587)
---------------------------------------
Vector Time (GMT): 2015/090/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4400308
77 A = 6774326
26 meter
Y = 1708
64 meter E =
0016303
Z = -5163564
18 I = 51
95567
XDOT = -1817
113162 Wp = 101
91026
YDOT = 7276
925342 meter/sec RA = 113
34831 deg
ZDOT = -1553
513714 TA = 153
20787
MA = 153
12357
Ha = 220
734 n
mi
Hp = 211
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14436708
56 X = 4425045
16
Y = 5605
78 feet Y = 51053
39 meter
Z = -16940827
35 Z = -5142128
36
XDOT = -5961
657356 XDOT = -1890
804064
YDOT = 23874
426975 feet/sec YDOT = 7256
192959 meter/sec
ZDOT = -5096
829771 ZDOT = -1562
520809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12428910
03 X = -3788331
78
Y = 7552939
41 feet Y = 2302135
93 meter
Z = -16848902
60 Z = -5135545
51
XDOT = -6787
155168 XDOT = -2068
724895
YDOT = -22572
958510 feet/sec YDOT = -6880
237754 meter/sec
ZDOT = -5136
648196 ZDOT = -1565
650370
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 15090
08551915
00016717 00000-0 10270-3 0 9084
2 25544 51
6414 114
1945 0006652 156
7410 203
4045 15
55447245 15883
Satellite: ISS
Catalog Number: 25544
Epoch time: 15090
08551915 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 114
1945 deg
Eccentricity:
0006652
Arg of perigee: 156
7410 deg
Mean anomaly: 203
4045 deg
Mean motion: 15
55447245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1588
Checksum: 301
Coasting Arc #10 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2015/091/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3609056
78 A = 6773775
52 meter
Y = -2228965
11 meter E =
0006910
Z = 5276153
35 I = 51
96509
XDOT = 3042
375503 Wp = 132
15850
YDOT = -6991
988241 meter/sec RA = 108
35573 deg
ZDOT = -876
543290 TA = 326
15630
MA = 326
20038
Ha = 220
789 n
mi
Hp = 211
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11840737
45 X = -3609493
24
Y = -7312877
67 feet Y = -2269325
63 meter
Z = 17310214
41 Z = 5258620
56
XDOT = 9981
546925 XDOT = 3124
593366
YDOT = -22939
593967 feet/sec YDOT = -6957
506828 meter/sec
ZDOT = -2875
798195 ZDOT = -861
563367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14008028
62 X = 4269647
12
Y = -202860
36 feet Y = -61831
84 meter
Z = 17235392
32 Z = 5253347
58
XDOT = 3785
945083 XDOT = 1153
956061
YDOT = 23712
755893 feet/sec YDOT = 7227
647996 meter/sec
ZDOT = -2810
401027 ZDOT = -856
610233
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 15091
11346993
00016717 00000-0 10270-3 0 9098
2 25544 51
6410 109
0591 0006682 160
4220 199
7191 15
55437091 16049
Satellite: ISS
Catalog Number: 25544
Epoch time: 15091
11346993 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 109
0591 deg
Eccentricity:
0006682
Arg of perigee: 160
4220 deg
Mean anomaly: 199
7191 deg
Mean motion: 15
55437091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 301
Coasting Arc #11 (Orbit 1618)
---------------------------------------
Vector Time (GMT): 2015/092/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2627054
56 A = 6776638
72 meter
Y = 4303662
22 meter E =
0014799
Z = -4542443
26 I = 51
98488
XDOT = -3923
857768 Wp = 132
00259
YDOT = 5756
053399 meter/sec RA = 103
36760 deg
ZDOT = 3181
178563 TA = 169
83221
MA = 169
80224
Ha = 220
490 n
mi
Hp = 211
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8618945
39 X = 2600800
23
Y = 14119626
69 feet Y = 4332892
19 meter
Z = -14903029
06 Z = -4529745
94
XDOT = -12873
549107 XDOT = -4003
384674
YDOT = 18884
689629 feet/sec YDOT = 5711
730068 meter/sec
ZDOT = 10436
937542 ZDOT = 3161
923204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15030767
32 X = -4581377
88
Y = -7023170
04 feet Y = -2140662
23 meter
Z = -14849291
87 Z = -4526064
16
XDOT = -55
505218 XDOT = -16
917990
YDOT = -21792
540297 feet/sec YDOT = -6642
366282 meter/sec
ZDOT = 10353
398386 ZDOT = 3155
715828
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 15092
07715112
00016717 00000-0 10270-3 0 9109
2 25544 51
6414 104
2441 0006771 163
6877 196
4496 15
55511196 16193
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
07715112 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 104
2441 deg
Eccentricity:
0006771
Arg of perigee: 163
6877 deg
Mean anomaly: 196
4496 deg
Mean motion: 15
55511196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1619
Checksum: 306
Coasting Arc #12 (Orbit 1629)
---------------------------------------
Vector Time (GMT): 2015/092/18:35:10
200
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2561773
62 A = 6778416
86 meter
Y = 4633763
20 meter E =
0011666
Z = -4244838
31 I = 51
99653
XDOT = -3865
680129 Wp = 135
66335
YDOT = 5500
746188 meter/sec RA = 99
85195 deg
ZDOT = 3669
749158 TA = 171
79303
MA = 171
77393
Ha = 220
261 n
mi
Hp = 212
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8404769
08 X = 2530387
28
Y = 15202635
18 feet Y = 4662234
51 meter
Z = -13926634
87 Z = -4232470
60
XDOT = -12682
677588 XDOT = -3944
729792
YDOT = 18047
067546 feet/sec YDOT = 5457
076182 meter/sec
ZDOT = 12039
859441 ZDOT = 3650
777557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11666213
60 X = 3555861
91
Y = -12927207
85 feet Y = -3940212
95 meter
Z = -13874371
19 Z = -4228908
34
XDOT = 20248
092248 XDOT = 6171
618517
YDOT = 5432
069435 feet/sec YDOT = 1655
694764 meter/sec
ZDOT = 11957
572344 ZDOT = 3644
668051
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 15092
78383853
00016717 00000-0 10270-3 0 9111
2 25544 51
6446 100
7182 0005606 173
9919 186
1303 15
55277117 16306
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
78383853 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 100
7182 deg
Eccentricity:
0005606
Arg of perigee: 173
9919 deg
Mean anomaly: 186
1303 deg
Mean motion: 15
55277117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1630
Checksum: 311
Coasting Arc #13 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2015/093/18:35:10
200
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1560597
91 A = 6783003
34 meter
Y = -6035118
66 meter E =
0016047
Z = 2649593
58 I = 52
01618
XDOT = 4409
852678 Wp = 122
52070
YDOT = -3451
933817 meter/sec RA = 94
88528 deg
ZDOT = -5250
640243 TA = 27
72360
MA = 27
63815
Ha = 220
245 n
mi
Hp = 212
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5120071
89 X = -1505866
61
Y = -19800258
06 feet Y = -6052263
87 meter
Z = 8692892
32 Z = 2642146
27
XDOT = 14468
020597 XDOT = 4473
631085
YDOT = -11325
242183 feet/sec YDOT = -3402
264127 meter/sec
ZDOT = -17226
509985 ZDOT = -5229
062480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16890300
10 X = -5148163
47
Y = 11555070
22 feet Y = 3521985
40 meter
Z = 8661977
09 Z = 2640170
62
XDOT = -14740
036112 XDOT = -4492
763007
YDOT = -8666
104980 feet/sec YDOT = -2641
428798 meter/sec
ZDOT = -17133
382418 ZDOT = -5222
254961
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 15093
81190278
00016717 00000-0 10270-3 0 9124
2 25544 51
6443 95
5841 0005681 177
3625 182
7559 15
55287127 16465
Satellite: ISS
Catalog Number: 25544
Epoch time: 15093
81190278 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 95
5841 deg
Eccentricity:
0005681
Arg of perigee: 177
3625 deg
Mean anomaly: 182
7559 deg
Mean motion: 15
55287127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 333
Coasting Arc #14 (Orbit 1660)
---------------------------------------
Vector Time (GMT): 2015/094/18:35:10
200
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 521370
72 A = 6785598
77 meter
Y = 6732353
41 meter E =
0007179
Z = -657619
97 I = 52
02789
XDOT = -4679
975324 Wp = 69
43719
YDOT = 942
882378 meter/sec RA = 89
93109 deg
ZDOT = 5997
557876 TA = 283
49986
MA = 283
57985
Ha = 219
950 n
mi
Hp = 212
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1710533
86 X = 449243
70
Y = 22087773
67 feet Y = 6737780
35 meter
Z = -2157545
84 Z = -655263
35
XDOT = -15354
249752 XDOT = -4719
305216
YDOT = 3093
446122 feet/sec YDOT = 890
328757 meter/sec
ZDOT = 19677
027153 ZDOT = 5974
727581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20049848
33 X = 6111193
77
Y = -9425380
31 feet Y = -2872855
92 meter
Z = -2148595
73 Z = -654891
98
XDOT = 7682
805968 XDOT = 2341
719259
YDOT = 11921
275747 feet/sec YDOT = 3633
604848 meter/sec
ZDOT = 19578
951317 ZDOT = 5967
664361
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 15094
77569017
00016717 00000-0 10270-3 0 9132
2 25544 51
6450 90
7703 0005592 182
0580 178
0551 15
55347659 16615
Satellite: ISS
Catalog Number: 25544
Epoch time: 15094
77569017 = yrday
fracday
Element set: 913
Inclination: 51
6450 deg
RA of node: 90
7703 deg
Eccentricity:
0005592
Arg of perigee: 182
0580 deg
Mean anomaly: 178
0551 deg
Mean motion: 15
55347659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1661
Checksum: 321
Coasting Arc #15 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2015/095/18:35:10
200
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 581814
85 A = 6784874
65 meter
Y = -6588281
99 meter E =
0013101
Z = -1480867
41 I = 52
02494
XDOT = 4705
449752 Wp = 160
09552
YDOT = 1716
002428 meter/sec RA = 84
98121 deg
ZDOT = -5812
678588 TA = 35
99621
MA = 35
90805
Ha = 219
913 n
mi
Hp = 212
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1908841
38 X = 662636
93
Y = -21615098
40 feet Y = -6581324
04 meter
Z = -4858488
89 Z = -1477843
90
XDOT = 15437
827271 XDOT = 4714
147460
YDOT = 5629
929227 feet/sec YDOT = 1768
669750 meter/sec
ZDOT = -19070
467809 ZDOT = -5789
799229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20800841
00 X = -6340096
34
Y = 6190162
94 feet Y = 1886761
66 meter
Z = -4844374
56 Z = -1476565
37
XDOT = -71
964759 XDOT = -21
934858
YDOT = -15020
116265 feet/sec YDOT = -4578
131437 meter/sec
ZDOT = -18972
642118 ZDOT = -5782
861318
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 15095
80370853
00016717 00000-0 10270-3 0 9146
2 25544 51
6455 85
6358 0005735 186
5939 173
5140 15
55343030 16775
Satellite: ISS
Catalog Number: 25544
Epoch time: 15095
80370853 = yrday
fracday
Element set: 914
Inclination: 51
6455 deg
RA of node: 85
6358 deg
Eccentricity:
0005735
Arg of perigee: 186
5939 deg
Mean anomaly: 173
5140 deg
Mean motion: 15
55343030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 325
Coasting Arc #16 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2015/096/18:35:10
200
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1671198
55 A = 6780884
66 meter
Y = 5645299
59 meter E =
0012759
Z = 3359679
02 I = 52
00862
XDOT = -4448
375913 Wp = 113
89825
YDOT = -4122
232575 meter/sec RA = 80
02230 deg
ZDOT = 4694
819283 TA = 285
06985
MA = 285
21100
Ha = 219
669 n
mi
Hp = 212
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5482934
88 X = -1750521
72
Y = 18521324
10 feet Y = 5626167
99 meter
Z = 11022568
96 Z = 3351367
27
XDOT = -14594
409163 XDOT = -4424
755513
YDOT = -13524
385088 feet/sec YDOT = -4171
844645 meter/sec
ZDOT = 15402
950404 ZDOT = 4673
267452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19230866
12 X = 5861567
99
Y = -2020466
94 feet Y = -615838
32 meter
Z = 10985925
06 Z = 3348509
96
XDOT = -6957
837017 XDOT = -2120
748723
YDOT = 17368
370003 feet/sec YDOT = 5293
879177 meter/sec
ZDOT = 15311
246634 ZDOT = 4666
867974
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 15096
83170273
00016717 00000-0 10270-3 0 9155
2 25544 51
6457 80
5011 0005490 189
5801 170
5248 15
55397692 16933
Satellite: ISS
Catalog Number: 25544
Epoch time: 15096
83170273 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 80
5011 deg
Eccentricity:
0005490
Arg of perigee: 189
5801 deg
Mean anomaly: 170
5248 deg
Mean motion: 15
55397692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 322
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