[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 11th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
176/10:51:33
202 1
4 3
4 3
4
N/A 3
0 -0
0 227
2
000/00:01:06
403 0
6 -0
0 220
9
Coasting Arc #1 (Orbit 1044)
---------------------------------------
Vector Time (GMT): 2014/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2712091
78 A = 6787743
49 meter
Y = -3283826
79 meter E =
0007306
Z = 5279494
60 I = 51
90896
XDOT = 5101
408581 Wp = 74
41781
YDOT = -5654
969689 meter/sec RA = 126
77565 deg
ZDOT = -893
823181 TA = 24
11629
MA = 24
08209
Ha = 228
098 n
mi
Hp = 218
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8897938
91 X = -2700816
14
Y = -10773709
96 feet Y = -3314092
80 meter
Z = 17321176
50 Z = 5266346
42
XDOT = 16736
904792 XDOT = 5168
606550
YDOT = -18553
050161 feet/sec YDOT = -5597
546618 meter/sec
ZDOT = -2932
490752 ZDOT = -868
878445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12301678
66 X = -3749551
66
Y = 6769376
99 feet Y = 2063306
11 meter
Z = 17265964
66 Z = 5262666
03
XDOT = -14495
524137 XDOT = -4418
235757
YDOT = -19109
929216 feet/sec YDOT = -5824
706425 meter/sec
ZDOT = -2825
786499 ZDOT = -861
299725
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 14162
54689137
00016717 00000-0 10270-3 0 9004
2 25544 51
6434 127
5491 0004150 85
6865 274
4760 15
50647249 10455
Satellite: ISS
Catalog Number: 25544
Epoch time: 14162
54689137 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 127
5491 deg
Eccentricity:
0004150
Arg of perigee: 85
6865 deg
Mean anomaly: 274
4760 deg
Mean motion: 15
50647249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1045
Checksum: 313
Coasting Arc #2 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2014/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2548967
24 A = 6788205
65 meter
Y = 3590194
62 meter E =
0017749
Z = -5182263
07 I = 51
92916
XDOT = -4911
246179 Wp = 98
61886
YDOT = 5666
306290 meter/sec RA = 121
83136 deg
ZDOT = 1511
706123 TA = 185
90929
MA = 185
93026
Ha = 227
970 n
mi
Hp = 218
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8362753
40 X = 2533805
43
Y = 11778853
72 feet Y = 3618614
80 meter
Z = -17002175
41 Z = -5169916
71
XDOT = -16113
012397 XDOT = -4981
586540
YDOT = 18590
243734 feet/sec YDOT = 5610
992061 meter/sec
ZDOT = 4959
665758 ZDOT = 1487
677731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13078933
81 X = 3986459
03
Y = -6275024
94 feet Y = -1912627
60 meter
Z = -16950414
76 Z = -5166486
42
XDOT = 15017
366493 XDOT = 4577
293307
YDOT = 18197
296836 feet/sec YDOT = 5546
536076 meter/sec
ZDOT = 4856
821896 ZDOT = 1480
359314
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 14163
51357844
00016717 00000-0 10270-3 0 9010
2 25544 51
6441 122
7549 0004117 88
8072 271
3550 15
50658882 10607
Satellite: ISS
Catalog Number: 25544
Epoch time: 14163
51357844 = yrday
fracday
Element set: 901
Inclination: 51
6441 deg
RA of node: 122
7549 deg
Eccentricity:
0004117
Arg of perigee: 88
8072 deg
Mean anomaly: 271
3550 deg
Mean motion: 15
50658882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 301
Coasting Arc #3 (Orbit 1075)
---------------------------------------
Vector Time (GMT): 2014/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2402067
84 A = 6788855
93 meter
Y = -3909941
97 meter E =
0009789
Z = 4996146
12 I = 51
94816
XDOT = 4733
877068 Wp = 71
10811
YDOT = -5642
788986 meter/sec RA = 116
88928 deg
ZDOT = -2133
532093 TA = 39
61853
MA = 39
54704
Ha = 228
006 n
mi
Hp = 218
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7880799
99 X = -2382437
23
Y = -12827893
60 feet Y = -3936694
45 meter
Z = 16391555
50 Z = 4984524
23
XDOT = 15531
092743 XDOT = 4806
988244
YDOT = -18513
087223 feet/sec YDOT = -5589
442612 meter/sec
ZDOT = -6999
777209 ZDOT = -2110
358770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13928074
50 X = -4245277
11
Y = 5853428
65 feet Y = 1784125
05 meter
Z = 16342921
04 Z = 4981322
33
XDOT = -15389
286551 XDOT = -4690
654541
YDOT = -17292
238580 feet/sec YDOT = -5270
674319 meter/sec
ZDOT = -6900
541444 ZDOT = -2103
285032
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 14164
54470079
00016717 00000-0 10270-3 0 9021
2 25544 51
6449 117
6418 0004089 92
2070 267
9549 15
50684899 10761
Satellite: ISS
Catalog Number: 25544
Epoch time: 14164
54470079 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 117
6418 deg
Eccentricity:
0004089
Arg of perigee: 92
2070 deg
Mean anomaly: 267
9549 deg
Mean motion: 15
50684899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1076
Checksum: 336
Coasting Arc #4 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2014/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2323468
12 A = 6789758
83 meter
Y = 4240369
91 meter E =
0015041
Z = -4780961
46 I = 51
96503
XDOT = -4524
045049 Wp = 105
32520
YDOT = 5539
118749 meter/sec RA = 111
94846 deg
ZDOT = 2717
447439 TA = 191
46271
MA = 191
49700
Ha = 227
876 n
mi
Hp = 218
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7622926
90 X = 2299103
01
Y = 13911974
78 feet Y = 4266216
92 meter
Z = -15685569
09 Z = -4769732
92
XDOT = -14842
667484 XDOT = -4598
848972
YDOT = 18172
961774 feet/sec YDOT = 5488
109305 meter/sec
ZDOT = 8915
509972 ZDOT = 2695
289428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14861565
25 X = 4529805
09
Y = -5679380
33 feet Y = -1731075
12 meter
Z = -15638658
90 Z = -4766663
23
XDOT = 15473
529368 XDOT = 4716
331751
YDOT = 16231
784127 feet/sec YDOT = 4947
447802 meter/sec
ZDOT = 8820
578714 ZDOT = 2688
512392
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 14165
51136705
00016717 00000-0 10270-3 0 9035
2 25544 51
6454 112
8478 0004026 95
1723 264
9888 15
50696917 10912
Satellite: ISS
Catalog Number: 25544
Epoch time: 14165
51136705 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 112
8478 deg
Eccentricity:
0004026
Arg of perigee: 95
1723 deg
Mean anomaly: 264
9888 deg
Mean motion: 15
50696917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 321
Coasting Arc #5 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2014/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2260260
21 A = 6790827
70 meter
Y = -4571421
23 meter E =
0012776
Z = 4474964
82 I = 51
98047
XDOT = 4345
692304 Wp = 78
15631
YDOT = -5388
359791 meter/sec RA = 107
00975 deg
ZDOT = -3299
045762 TA = 44
99521
MA = 44
89177
Ha = 227
900 n
mi
Hp = 218
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7415551
86 X = -2230711
38
Y = -14998101
13 feet Y = -4596532
31 meter
Z = 14681643
11 Z = 4464055
98
XDOT = 14257
520683 XDOT = 4421
648810
YDOT = -17678
345770 feet/sec YDOT = -5339
338311 meter/sec
ZDOT = -10823
640952 ZDOT = -3277
751360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15812953
29 X = -4819788
16
Y = 5587292
99 feet Y = 1703006
90 meter
Z = 14636145
55 Z = 4461097
16
XDOT = -15356
291598 XDOT = -4680
597679
YDOT = -15256
440916 feet/sec YDOT = -4650
163191 meter/sec
ZDOT = -10732
382757 ZDOT = -3271
230264
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 14166
54246695
00016717 00000-0 10270-3 0 9040
2 25544 51
6462 107
7347 0004022 98
8949 261
2657 15
50722961 11076
Satellite: ISS
Catalog Number: 25544
Epoch time: 14166
54246695 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 107
7347 deg
Eccentricity:
0004022
Arg of perigee: 98
8949 deg
Mean anomaly: 261
2657 deg
Mean motion: 15
50722961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 320
Coasting Arc #6 (Orbit 1121)
---------------------------------------
Vector Time (GMT): 2014/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2268437
02 A = 6792011
68 meter
Y = 4887670
92 meter E =
0011463
Z = -4146566
54 I = 51
99278
XDOT = -4157
602711 Wp = 106
76313
YDOT = 5165
705283 meter/sec RA = 102
07215 deg
ZDOT = 3819
998332 TA = 202
52236
MA = 202
57272
Ha = 227
782 n
mi
Hp = 218
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7442378
66 X = 2233755
91
Y = 16035665
75 feet Y = 4912844
62 meter
Z = -13604220
94 Z = -4135630
52
XDOT = -13640
428842 XDOT = -4233
613991
YDOT = 16947
851979 feet/sec YDOT = 5118
786836 meter/sec
ZDOT = 12532
802926 ZDOT = 3799
617419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16748349
57 X = 5104896
95
Y = -5767308
50 feet Y = -1757875
63 meter
Z = -13558663
01 Z = -4132680
49
XDOT = 14961
883851 XDOT = 4560
382198
YDOT = 14233
576334 feet/sec YDOT = 4338
394066 meter/sec
ZDOT = 12445
445552 ZDOT = 3793
371804
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 14167
50911229
00016717 00000-0 10270-3 0 9050
2 25544 51
6462 102
9407 0003967 102
0351 258
1245 15
50736137 11227
Satellite: ISS
Catalog Number: 25544
Epoch time: 14167
50911229 = yrday
fracday
Element set: 905
Inclination: 51
6462 deg
RA of node: 102
9407 deg
Eccentricity:
0003967
Arg of perigee: 102
0351 deg
Mean anomaly: 258
1245 deg
Mean motion: 15
50736137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1122
Checksum: 281
Coasting Arc #7 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2014/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2284760
62 A = 6793317
59 meter
Y = -5189999
06 meter E =
0015467
Z = 3727405
08 I = 52
00335
XDOT = 4019
915655 Wp = 89
90403
YDOT = -4889
445710 meter/sec RA = 97
13631 deg
ZDOT = -4328
461331 TA = 45
90812
MA = 45
78092
Ha = 227
794 n
mi
Hp = 218
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7495933
79 X = -2244661
47
Y = -17027555
99 feet Y = -5215324
89 meter
Z = 12229019
28 Z = 3716402
98
XDOT = 13188
699656 XDOT = 4095
317908
YDOT = -16041
488549 feet/sec YDOT = -4844
070398 meter/sec
ZDOT = -14200
988620 ZDOT = -4308
750623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17638699
14 X = -5376275
50
Y = 6010047
14 feet Y = 1831862
37 meter
Z = 12183235
40 Z = 3713450
15
XDOT = -14344
905752 XDOT = -4372
327273
YDOT = -13380
781166 feet/sec YDOT = -4078
462099 meter/sec
ZDOT = -14116
512086 ZDOT = -4302
712884
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 14168
54018951
00016717 00000-0 10270-3 0 9066
2 25544 51
6466 97
8272 0003972 105
7585 254
4004 15
50757340 11386
Satellite: ISS
Catalog Number: 25544
Epoch time: 14168
54018951 = yrday
fracday
Element set: 906
Inclination: 51
6466 deg
RA of node: 97
8272 deg
Eccentricity:
0003972
Arg of perigee: 105
7585 deg
Mean anomaly: 254
4004 deg
Mean motion: 15
50757340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 316
Coasting Arc #8 (Orbit 1152)
---------------------------------------
Vector Time (GMT): 2014/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2367000
37 A = 6794547
58 meter
Y = 5454103
94 meter E =
0008356
Z = -3296786
71 I = 52
01055
XDOT = -3894
019749 Wp = 95
29575
YDOT = 4560
184478 meter/sec RA = 92
20137 deg
ZDOT = 4758
044365 TA = 226
73049
MA = 226
80025
Ha = 227
683 n
mi
Hp = 218
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7765749
23 X = 2321850
06
Y = 17894041
80 feet Y = 5480321
09 meter
Z = -10816229
37 Z = -3285397
42
XDOT = -12775
655343 XDOT = -3967
836296
YDOT = 14961
235165 feet/sec YDOT = 4516
225912 meter/sec
ZDOT = 15610
381776 ZDOT = 4738
948945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18416021
83 X = 5613203
45
Y = -6509712
61 feet Y = -1984160
40 meter
Z = -10768852
90 Z = -3282346
36
XDOT = 13510
744963 XDOT = 4118
075065
YDOT = 12585
868904 feet/sec YDOT = 3836
172842 meter/sec
ZDOT = 15528
564116 ZDOT = 4733
106342
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 14169
50681364
00016717 00000-0 10270-3 0 9078
2 25544 51
6466 93
0328 0003927 109
1784 250
9792 15
50775094 11533
Satellite: ISS
Catalog Number: 25544
Epoch time: 14169
50681364 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 93
0328 deg
Eccentricity:
0003927
Arg of perigee: 109
1784 deg
Mean anomaly: 250
9792 deg
Mean motion: 15
50775094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1153
Checksum: 325
Coasting Arc #9 (Orbit 1168)
---------------------------------------
Vector Time (GMT): 2014/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2443606
14 A = 6795842
18 meter
Y = -5690321
91 meter E =
0017301
Z = 2778495
15 I = 52
01548
XDOT = 3834
997938 Wp = 103
40351
YDOT = -4178
029636 meter/sec RA = 87
26787 deg
ZDOT = -5160
770523 TA = 45
30687
MA = 45
16607
Ha = 227
692 n
mi
Hp = 218
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8017080
52 X = -2393291
07
Y = -18669035
13 feet Y = -5717366
77 meter
Z = 9115797
74 Z = 2766746
24
XDOT = 12582
014231 XDOT = 3906
501916
YDOT = -13707
446313 feet/sec YDOT = -4134
744020 meter/sec
ZDOT = -16931
661821 ZDOT = -5141
967317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19088657
19 X = -5818222
71
Y = 7022671
76 feet Y = 2140510
35 meter
Z = 9066943
76 Z = 2763604
46
XDOT = -12469
449251 XDOT = -3800
688132
YDOT = -12039
365197 feet/sec YDOT = -3669
598512 meter/sec
ZDOT = -16851
142474 ZDOT = -5136
228226
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 14170
53786822
00016717 00000-0 10270-3 0 9089
2 25544 51
6468 87
9187 0003941 112
8943 247
2617 15
50785005 11699
Satellite: ISS
Catalog Number: 25544
Epoch time: 14170
53786822 = yrday
fracday
Element set: 908
Inclination: 51
6468 deg
RA of node: 87
9187 deg
Eccentricity:
0003941
Arg of perigee: 112
8943 deg
Mean anomaly: 247
2617 deg
Mean motion: 15
50785005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1169
Checksum: 332
Coasting Arc #10 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2014/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2573087
88 A = 6796848
55 meter
Y = 5870421
03 meter E =
0008048
Z = -2263182
39 I = 52
01713
XDOT = -3804
178713 Wp = 70
82282
YDOT = 3770
148768 meter/sec RA = 82
33506 deg
ZDOT = 5472
626680 TA = 264
18979
MA = 264
28154
Ha = 227
568 n
mi
Hp = 218
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8441889
37 X = 2518246
09
Y = 19259911
52 feet Y = 5898888
50 meter
Z = -7425139
06 Z = -2250815
39
XDOT = -12480
901291 XDOT = -3872
638952
YDOT = 12369
254488 feet/sec YDOT = 3727
224768 meter/sec
ZDOT = 17954
811941 ZDOT = 5453
980497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19571555
78 X = 5965410
20
Y = -7741128
84 feet Y = -2359496
07 meter
Z = -7373703
73 Z = -2247504
90
XDOT = 11312
707350 XDOT = 3448
113200
YDOT = 11632
770995 feet/sec YDOT = 3545
668599 meter/sec
ZDOT = 17875
022528 ZDOT = 5448
306867
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 14171
50447119
00016717 00000-0 10270-3 0 9091
2 25544 51
6472 83
1242 0003867 116
3313 243
8235 15
50812160 11849
Satellite: ISS
Catalog Number: 25544
Epoch time: 14171
50447119 = yrday
fracday
Element set: 909
Inclination: 51
6472 deg
RA of node: 83
1242 deg
Eccentricity:
0003867
Arg of perigee: 116
3313 deg
Mean anomaly: 243
8235 deg
Mean motion: 15
50812160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1184
Checksum: 284
Coasting Arc #11 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2014/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2677570
38 A = 6797856
92 meter
Y = -6012016
20 meter E =
0017803
Z = 1667399
07 I = 52
01574
XDOT = 3851
037240 Wp = 117
09181
YDOT = -3317
891714 meter/sec RA = 77
40331 deg
ZDOT = -5739
857494 TA = 44
75274
MA = 44
60924
Ha = 227
581 n
mi
Hp = 218
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8784679
71 X = -2618243
36
Y = -19724462
59 feet Y = -6041626
95 meter
Z = 5470469
39 Z = 1654535
29
XDOT = 12634
636613 XDOT = 3915
734951
YDOT = -10885
471504 feet/sec YDOT = -3274
464663 meter/sec
ZDOT = -18831
553458 ZDOT = -5720
992769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19907152
60 X = -6067700
11
Y = 8397192
90 feet Y = 2559464
40 meter
Z = 5416962
63 Z = 1651090
21
XDOT = -10001
002153 XDOT = -3048
305456
YDOT = -11529
698141 feet/sec YDOT = -3514
251993 meter/sec
ZDOT = -18750
909074 ZDOT = -5715
277086
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 14172
53550393
00016717 00000-0 10270-3 0 9106
2 25544 51
6476 78
0099 0003907 120
5045 239
6493 15
50806383 12008
Satellite: ISS
Catalog Number: 25544
Epoch time: 14172
53550393 = yrday
fracday
Element set: 910
Inclination: 51
6476 deg
RA of node: 78
0099 deg
Eccentricity:
0003907
Arg of perigee: 120
5045 deg
Mean anomaly: 239
6493 deg
Mean motion: 15
50806383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 298
Coasting Arc #12 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2014/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2816561
59 A = 6798392
52 meter
Y = 6087878
81 meter E =
0010541
Z = -1091267
16 I = 52
01097
XDOT = -3934
604082 Wp = 59
13206
YDOT = 2871
482314 meter/sec RA = 72
47169 deg
ZDOT = 5911
487413 TA = 289
11214
MA = 289
22625
Ha = 227
428 n
mi
Hp = 218
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9240687
64 X = 2753577
27
Y = 19973355
68 feet Y = 6119023
37 meter
Z = -3580272
83 Z = -1077736
94
XDOT = -12908
806044 XDOT = -3995
137490
YDOT = 9420
873733 feet/sec YDOT = 2827
143940 meter/sec
ZDOT = 19394
643744 ZDOT = 5892
226827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20010632
47 X = 6099240
78
Y = -9181495
79 feet Y = -2798519
92 meter
Z = -3523963
94 Z = -1074104
21
XDOT = 8699
871466 XDOT = 2651
720823
YDOT = 11609
399837 feet/sec YDOT = 3538
545070 meter/sec
ZDOT = 19312
392077 ZDOT = 5886
417105
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 14173
50208568
00016717 00000-0 10270-3 0 9119
2 25544 51
6483 73
2155 0003764 123
4433 236
7078 15
50846761 12157
Satellite: ISS
Catalog Number: 25544
Epoch time: 14173
50208568 = yrday
fracday
Element set: 911
Inclination: 51
6483 deg
RA of node: 73
2155 deg
Eccentricity:
0003764
Arg of perigee: 123
4433 deg
Mean anomaly: 236
7078 deg
Mean motion: 15
50846761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1215
Checksum: 300
Coasting Arc #13 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2014/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2907775
88 A = 6798870
30 meter
Y = -6120619
08 meter E =
0016647
Z = 446684
30 I = 52
00252
XDOT = 4097
761561 Wp = 129
73059
YDOT = -2396
130644 meter/sec RA = 67
54048 deg
ZDOT = -6019
266761 TA = 45
48143
MA = 45
34553
Ha = 227
436 n
mi
Hp = 218
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9539947
12 X = -2841287
47
Y = -20080771
25 feet Y = -6152763
99 meter
Z = 1465499
66 Z = 432719
39
XDOT = 13444
099611 XDOT = 4153
490894
YDOT = -7861
321011 feet/sec YDOT = -2349
994492 meter/sec
ZDOT = -19748
250528 ZDOT = -5999
225241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19953577
75 X = -6081850
50
Y = 9811713
19 feet Y = 2990610
18 meter
Z = 1407364
03 Z = 428964
56
XDOT = -7324
997764 XDOT = -2232
659318
YDOT = -12008
393206 feet/sec YDOT = -3660
158249 meter/sec
ZDOT = -19662
764290 ZDOT = -5993
210556
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 14174
53309677
00016717 00000-0 10270-3 0 9127
2 25544 51
6487 68
1015 0003825 128
6988 231
4505 15
50826436 12311
Satellite: ISS
Catalog Number: 25544
Epoch time: 14174
53309677 = yrday
fracday
Element set: 912
Inclination: 51
6487 deg
RA of node: 68
1015 deg
Eccentricity:
0003825
Arg of perigee: 128
6988 deg
Mean anomaly: 231
4505 deg
Mean motion: 15
50826436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 312
Coasting Arc #14 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2014/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3012943
44 A = 6798772
65 meter
Y = 6087678
05 meter E =
0013320
Z = 160745
87 I = 51
99037
XDOT = -4297
054445 Wp = 62
71373
YDOT = 1957
438098 meter/sec RA = 62
60826 deg
ZDOT = 6033
906495 TA = 299
00696
MA = 299
14039
Ha = 227
259 n
mi
Hp = 218
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9884985
05 X = 2943864
86
Y = 19972697
02 feet Y = 6120984
46 meter
Z = 527381
45 Z = 175215
42
XDOT = -14097
947654 XDOT = -4347
934461
YDOT = 6422
041003 feet/sec YDOT = 1909
100358 meter/sec
ZDOT = 19796
281152 ZDOT = 6012
908626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19663920
34 X = 5993562
92
Y = -10482584
91 feet Y = -3195091
88 meter
Z = 587653
94 Z = 179116
92
XDOT = 6087
701331 XDOT = 1855
531366
YDOT = 12586
703699 feet/sec YDOT = 3836
427287 meter/sec
ZDOT = 19706
810883 ZDOT = 6006
635957
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 14175
56409479
00016717 00000-0 10270-3 0 9133
2 25544 51
6490 62
9874 0003616 130
9870 229
1595 15
50880723 12473
Satellite: ISS
Catalog Number: 25544
Epoch time: 14175
56409479 = yrday
fracday
Element set: 913
Inclination: 51
6490 deg
RA of node: 62
9874 deg
Eccentricity:
0003616
Arg of perigee: 130
9870 deg
Mean anomaly: 229
1595 deg
Mean motion: 15
50880723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 330
Coasting Arc #15 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2014/176/10:52:06
403
Vector Time (MET): N/A
Weight (LBS) : 887988
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4376911
00 A = 6789472
58 meter
Y = -632602
83 meter E =
0014008
Z = -5164134
65 I = 51
93884
XDOT = 2871
847072 Wp = 109
51061
YDOT = 6912
388915 meter/sec RA = 57
88744 deg
ZDOT = 1586
253914 TA = 175
76159
MA = 175
74971
Ha = 227
193 n
mi
Hp = 220
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14359944
23 X = 4408745
32
Y = -2075468
59 feet Y = -583478
65 meter
Z = -16942698
98 Z = -5142794
99
XDOT = 9422
070446 XDOT = 2786
632208
YDOT = 22678
441322 feet/sec YDOT = 6944
027060 meter/sec
ZDOT = 5204
245126 ZDOT = 1599
998974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1559589
55 X = 475362
90
Y = -14530921
86 feet Y = -4429024
98 meter
Z = -16852020
87 Z = -5136495
96
XDOT = 23235
519948 XDOT = 7082
186480
YDOT = -3611
840856 feet/sec YDOT = -1100
889093 meter/sec
ZDOT = 5261
279773 ZDOT = 1603
638075
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 14176
46621077
00016717 00000-0 10270-3 0 9144
2 25544 51
6489 58
5125 0001895 180
7458 179
3690 15
50267761 12612
Satellite: ISS
Catalog Number: 25544
Epoch time: 14176
46621077 = yrday
fracday
Element set: 914
Inclination: 51
6489 deg
RA of node: 58
5125 deg
Eccentricity:
0001895
Arg of perigee: 180
7458 deg
Mean anomaly: 179
3690 deg
Mean motion: 15
50267761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 330
Coasting Arc #16 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2014/177/10:52:06
403
Vector Time (MET): N/A
Weight (LBS) : 887988
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4533898
22 A = 6789892
16 meter
Y = 526026
01 meter E =
0005046
Z = 5023242
46 I = 51
92323
XDOT = -3058
614536 Wp = 72
06014
YDOT = -6721
569594 meter/sec RA = 52
94878 deg
ZDOT = -2053
578871 TA = 37
85570
MA = 37
82023
Ha = 227
164 n
mi
Hp = 220
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14874994
17 X = -4563844
62
Y = 1725807
11 feet Y = 475156
86 meter
Z = 16480454
25 Z = 5001144
82
XDOT = -10034
824593 XDOT = -2973
249493
YDOT = -22052
393680 feet/sec YDOT = -6755
295380 meter/sec
ZDOT = -6737
463487 ZDOT = -2068
230801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1767628
34 X = -538773
12
Y = 14973471
48 feet Y = 4563914
11 meter
Z = 16386576
09 Z = 4994628
39
XDOT = -22669
243809 XDOT = -6909
585513
YDOT = 4775
418731 feet/sec YDOT = 1455
547629 meter/sec
ZDOT = -6798
374027 ZDOT = -2072
144403
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 14177
49760641
00016717 00000-0 10270-3 0 9150
2 25544 51
6487 53
4012 0001815 188
9116 171
2003 15
50315215 12776
Satellite: ISS
Catalog Number: 25544
Epoch time: 14177
49760641 = yrday
fracday
Element set: 915
Inclination: 51
6487 deg
RA of node: 53
4012 deg
Eccentricity:
0001815
Arg of perigee: 188
9116 deg
Mean anomaly: 171
2003 deg
Mean motion: 15
50315215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 290
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