[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 9th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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
There are no maneuvers
Coasting Arc #1 (Orbit 1015)
---------------------------------------
Vector Time (GMT): 2014/160/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4651880
12 A = 6799499
92 meter
Y = -4935057
01 meter E =
0015757
Z = 398058
10 I = 51
91099
XDOT = 3694
889583 Wp = 118
96104
YDOT = 2983
900256 meter/sec RA = 135
94485 deg
ZDOT = -6013
960149 TA = 56
76957
MA = 56
61863
Ha = 228
048 n
mi
Hp = 218
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15262073
88 X = 4704785
64
Y = -16191131
93 feet Y = -4882740
92 meter
Z = 1305964
88 Z = 420784
66
XDOT = 12122
341152 XDOT = 3690
462626
YDOT = 9789
699004 feet/sec YDOT = 3025
194680 meter/sec
ZDOT = -19730
840384 ZDOT = -5996
021114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22188830
17 X = -6763155
43
Y = -1573626
75 feet Y = -479641
43 meter
Z = 1403107
68 Z = 427667
22
XDOT = -279
165186 XDOT = -85
089549
YDOT = -14058
023902 feet/sec YDOT = -4284
885685 meter/sec
ZDOT = -19655
268189 ZDOT = -5990
925744
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 14160
67793553
00016717 00000-0 10270-3 0 9004
2 25544 51
6454 136
8169 0004123 79
7389 280
4227 15
50610029 10166
Satellite: ISS
Catalog Number: 25544
Epoch time: 14160
67793553 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 136
8169 deg
Eccentricity:
0004123
Arg of perigee: 79
7389 deg
Mean anomaly: 280
4227 deg
Mean motion: 15
50610029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1016
Checksum: 304
Coasting Arc #2 (Orbit 1031)
---------------------------------------
Vector Time (GMT): 2014/161/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4531900
15 A = 6799526
84 meter
Y = 5058956
49 meter E =
0015807
Z = 128043
11 I = 51
93263
XDOT = -3437
809444 Wp = 55
37940
YDOT = -3245
457582 meter/sec RA = 131
00855 deg
ZDOT = 6031
542165 TA = 305
99247
MA = 306
13893
Ha = 228
005 n
mi
Hp = 218
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14868438
81 X = -4588755
73
Y = 16597626
27 feet Y = 5007959
95 meter
Z = 420088
95 Z = 105889
92
XDOT = -11278
902374 XDOT = -3430
562214
YDOT = -10647
826711 feet/sec YDOT = -3283
861535 meter/sec
ZDOT = 19788
524162 ZDOT = 6014
858758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22275922
80 X = 6789701
27
Y = 636839
02 feet Y = 194108
53 meter
Z = 325337
57 Z = 99162
89
XDOT = -719
138136 XDOT = -219
193304
YDOT = 13956
930672 feet/sec YDOT = 4254
072469 meter/sec
ZDOT = 19718
316489 ZDOT = 6010
142866
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 14161
70909150
00016717 00000-0 10270-3 0 9012
2 25544 51
6451 131
7035 0004101 81
7297 278
4319 15
50626168 10324
Satellite: ISS
Catalog Number: 25544
Epoch time: 14161
70909150 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 131
7035 deg
Eccentricity:
0004101
Arg of perigee: 81
7297 deg
Mean anomaly: 278
4319 deg
Mean motion: 15
50626168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1032
Checksum: 280
Coasting Arc #3 (Orbit 1046)
---------------------------------------
Vector Time (GMT): 2014/162/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4415660
03 A = 6799310
12 meter
Y = -5115395
68 meter E =
0013420
Z = -711635
13 I = 51
95270
XDOT = 3188
527169 Wp = 125
90529
YDOT = 3572
371896 meter/sec RA = 126
07362 deg
ZDOT = -5980
791013 TA = 61
73709
MA = 61
60170
Ha = 228
018 n
mi
Hp = 218
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14487073
61 X = 4475990
31
Y = -16782794
24 feet Y = -5065679
52 meter
Z = -2334760
93 Z = -690038
35
XDOT = 10461
047144 XDOT = 3177
396247
YDOT = 11720
380236 feet/sec YDOT = 3607
966622 meter/sec
ZDOT = -19622
017760 ZDOT = -5965
327951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22179699
66 X = -6760372
46
Y = 146398
79 feet Y = 44622
35 meter
Z = -2242338
81 Z = -683464
87
XDOT = 1854
506922 XDOT = 565
253710
YDOT = -14065
327433 feet/sec YDOT = -4287
111802 meter/sec
ZDOT = -19557
037410 ZDOT = -5960
985003
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
67579095
00016717 00000-0 10270-3 0 9021
2 25544 51
6461 126
9093 0004071 86
8980 273
2637 15
50632666 10478
Satellite: ISS
Catalog Number: 25544
Epoch time: 14162
67579095 = yrday
fracday
Element set: 902
Inclination: 51
6461 deg
RA of node: 126
9093 deg
Eccentricity:
0004071
Arg of perigee: 86
8980 deg
Mean anomaly: 273
2637 deg
Mean motion: 15
50632666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 323
Coasting Arc #4 (Orbit 1062)
---------------------------------------
Vector Time (GMT): 2014/163/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4245830
76 A = 6798833
63 meter
Y = 5154001
08 meter E =
0017361
Z = 1238606
57 I = 51
96906
XDOT = -3007
784981 Wp = 65
27217
YDOT = -3902
647749 meter/sec RA = 121
13962 deg
ZDOT = 5871
658375 TA = 308
11529
MA = 308
27169
Ha = 227
986 n
mi
Hp = 218
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13929890
96 X = -4309165
22
Y = 16909452
36 feet Y = 5106167
16 meter
Z = 4063669
85 Z = 1217827
67
XDOT = -9868
060960 XDOT = -2992
444022
YDOT = -12803
962430 feet/sec YDOT = -3936
197836 meter/sec
ZDOT = 19263
971048 ZDOT = 5857
083522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21900929
60 X = 6675403
34
Y = -1017833
42 feet Y = -310235
63 meter
Z = 3974688
89 Z = 1211485
17
XDOT = -2850
613442 XDOT = -868
866977
YDOT = 14401
844506 feet/sec YDOT = 4389
682205 meter/sec
ZDOT = 19202
811571 ZDOT = 5853
016967
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
70692794
00016717 00000-0 10270-3 0 9039
2 25544 51
6463 121
7959 0004087 88
3544 271
8075 15
50653818 10634
Satellite: ISS
Catalog Number: 25544
Epoch time: 14163
70692794 = yrday
fracday
Element set: 903
Inclination: 51
6463 deg
RA of node: 121
7959 deg
Eccentricity:
0004087
Arg of perigee: 88
3544 deg
Mean anomaly: 271
8075 deg
Mean motion: 15
50653818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1063
Checksum: 327
Coasting Arc #5 (Orbit 1077)
---------------------------------------
Vector Time (GMT): 2014/164/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4093586
14 A = 6798090
12 meter
Y = -5114459
09 meter E =
0010502
Z = -1809012
72 I = 51
98303
XDOT = 2845
453360 Wp = 125
45061
YDOT = 4276
796873 meter/sec RA = 116
20647 deg
ZDOT = -5681
555737 TA = 74
29642
MA = 74
18059
Ha = 227
947 n
mi
Hp = 218
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13430400
71 X = 4159260
57
Y = -16779721
43 feet Y = -5068314
49 meter
Z = -5935081
12 Z = -1788967
86
XDOT = 9335
476902 XDOT = 2825
017036
YDOT = 14031
485804 feet/sec YDOT = 4308
503179 meter/sec
ZDOT = -18640
274729 ZDOT = -5667
781843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21451956
41 X = -6538556
31
Y = 1661421
74 feet Y = 506401
35 meter
Z = -5849200
49 Z = -1782836
31
XDOT = 3884
211294 XDOT = 1183
907603
YDOT = -14928
754264 feet/sec YDOT = -4550
284300 meter/sec
ZDOT = -18582
574407 ZDOT = -5663
968679
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
67360930
00016717 00000-0 10270-3 0 9041
2 25544 51
6473 117
0020 0003971 93
9064 266
2541 15
50657802 10781
Satellite: ISS
Catalog Number: 25544
Epoch time: 14164
67360930 = yrday
fracday
Element set: 904
Inclination: 51
6473 deg
RA of node: 117
0020 deg
Eccentricity:
0003971
Arg of perigee: 93
9064 deg
Mean anomaly: 266
2541 deg
Mean motion: 15
50657802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1078
Checksum: 296
Coasting Arc #6 (Orbit 1093)
---------------------------------------
Vector Time (GMT): 2014/165/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3905366
40 A = 6797161
24 meter
Y = 5049929
54 meter E =
0017614
Z = 2312359
09 I = 51
99329
XDOT = -2758
408080 Wp = 77
43147
YDOT = -4640
039383 meter/sec RA = 111
27337 deg
ZDOT = 5443
481782 TA = 308
17734
MA = 308
33587
Ha = 227
943 n
mi
Hp = 218
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12812881
89 X = -3972778
28
Y = 16568010
30 feet Y = 5005879
95 meter
Z = 7586479
97 Z = 2293224
42
XDOT = -9049
895274 XDOT = -2732
759734
YDOT = -15223
226321 feet/sec YDOT = -4670
743086 meter/sec
ZDOT = 17859
192198 ZDOT = 5430
143440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20845435
67 X = 6353688
79
Y = -2318311
04 feet Y = -706621
21 meter
Z = 7504454
10 Z = 2287357
61
XDOT = -4705
171161 XDOT = -1434
136170
YDOT = 15657
253564 feet/sec YDOT = 4772
330886 meter/sec
ZDOT = 17803
400140 ZDOT = 5426
476363
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
70472723
00016717 00000-0 10270-3 0 9051
2 25544 51
6476 111
8886 0004034 94
8213 265
3398 15
50682238 10942
Satellite: ISS
Catalog Number: 25544
Epoch time: 14165
70472723 = yrday
fracday
Element set: 905
Inclination: 51
6476 deg
RA of node: 111
8886 deg
Eccentricity:
0004034
Arg of perigee: 94
8213 deg
Mean anomaly: 265
3398 deg
Mean motion: 15
50682238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1094
Checksum: 317
Coasting Arc #7 (Orbit 1108)
---------------------------------------
Vector Time (GMT): 2014/166/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3751753
47 A = 6795991
95 meter
Y = -4903696
61 meter E =
0008419
Z = -2842274
21 I = 52
00049
XDOT = 2694
637022 Wp = 110
94912
YDOT = 5018
790510 meter/sec RA = 106
34038 deg
ZDOT = -5117
035688 TA = 101
10025
MA = 101
00557
Ha = 227
836 n
mi
Hp = 218
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12308902
45 X = 3820115
66
Y = -16088243
48 feet Y = -4861359
47 meter
Z = -9325046
63 Z = -2823883
44
XDOT = 8840
672644 XDOT = 2663
172269
YDOT = 16465
848131 feet/sec YDOT = 5048
748442 meter/sec
ZDOT = -16788
174831 ZDOT = -5104
021330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20114670
76 X = -6130951
65
Y = 2684247
94 feet Y = 818158
77 meter
Z = -9246187
60 Z = -2818237
98
XDOT = 5465
235609 XDOT = 1665
803814
YDOT = -16514
763511 feet/sec YDOT = -5033
699918 meter/sec
ZDOT = -16733
821325 ZDOT = -5100
468740
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
67139024
00016717 00000-0 10270-3 0 9063
2 25544 51
6481 107
0949 0003834 100
5524 259
6059 15
50688418 11095
Satellite: ISS
Catalog Number: 25544
Epoch time: 14166
67139024 = yrday
fracday
Element set: 906
Inclination: 51
6481 deg
RA of node: 107
0949 deg
Eccentricity:
0003834
Arg of perigee: 100
5524 deg
Mean anomaly: 259
6059 deg
Mean motion: 15
50688418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1109
Checksum: 312
Coasting Arc #8 (Orbit 1124)
---------------------------------------
Vector Time (GMT): 2014/167/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3581415
99 A = 6794763
22 meter
Y = 4731147
69 meter E =
0016533
Z = 3296378
74 I = 52
00432
XDOT = -2704
016646 Wp = 90
84805
YDOT = -5373
344074 meter/sec RA = 101
40642 deg
ZDOT = 4753
520971 TA = 307
19302
MA = 307
34382
Ha = 227
877 n
mi
Hp = 218
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11750052
46 X = -3650067
21
Y = 15522138
08 feet Y = 4690713
75 meter
Z = 10814890
89 Z = 3278814
66
XDOT = -8871
445688 XDOT = -2666
820628
YDOT = -17629
081609 feet/sec YDOT = -5403
374707 meter/sec
ZDOT = 15595
541244 ZDOT = 4740
475050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19277158
95 X = 5875678
05
Y = -3002567
47 feet Y = -915182
56 meter
Z = 10739557
70 Z = 3273417
19
XDOT = -5967
717313 XDOT = -1818
960237
YDOT = 17518
699980 feet/sec YDOT = 5339
699754 meter/sec
ZDOT = 15541
115253 ZDOT = 4736
931929
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
70248903
00016717 00000-0 10270-3 0 9076
2 25544 51
6480 101
9813 0003942 101
2456 258
9138 15
50709111 11251
Satellite: ISS
Catalog Number: 25544
Epoch time: 14167
70248903 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 101
9813 deg
Eccentricity:
0003942
Arg of perigee: 101
2456 deg
Mean anomaly: 258
9138 deg
Mean motion: 15
50709111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1125
Checksum: 291
Coasting Arc #9 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2014/168/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3463245
57 A = 6793352
68 meter
Y = -4482092
12 meter E =
0009208
Z = -3758543
43 I = 52
00482
XDOT = 2733
662539 Wp = 89
41184
YDOT = 5711
722853 meter/sec RA = 96
47173 deg
ZDOT = -4301
384757 TA = 135
14393
MA = 135
06947
Ha = 227
703 n
mi
Hp = 218
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11362354
23 X = 3531365
62
Y = -14705026
63 feet Y = -4442982
63 meter
Z = -12331179
24 Z = -3741554
56
XDOT = 8968
709118 XDOT = 2690
484185
YDOT = 18739
248206 feet/sec YDOT = 5742
051419 meter/sec
ZDOT = -14112
154715 ZDOT = -4288
209418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18389621
29 X = -5605156
57
Y = 2992371
77 feet Y = 912074
91 meter
Z = -12258320
57 Z = -3736336
11
XDOT = 6331
656017 XDOT = 1929
888754
YDOT = -18552
971796 feet/sec YDOT = -5654
945803 meter/sec
ZDOT = -14057
240517 ZDOT = -4284
646910
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
66913336
00016717 00000-0 10270-3 0 9082
2 25544 51
6478 97
1872 0003695 106
9330 253
2226 15
50724939 11405
Satellite: ISS
Catalog Number: 25544
Epoch time: 14168
66913336 = yrday
fracday
Element set: 908
Inclination: 51
6478 deg
RA of node: 97
1872 deg
Eccentricity:
0003695
Arg of perigee: 106
9330 deg
Mean anomaly: 253
2226 deg
Mean motion: 15
50724939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 321
Coasting Arc #10 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2014/169/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3346477
52 A = 6792054
87 meter
Y = 4211212
19 meter E =
0014304
Z = 4137749
95 I = 52
00293
XDOT = -2825
918900 Wp = 104
60578
YDOT = -6015
684740 meter/sec RA = 91
53560 deg
ZDOT = 3822
452922 TA = 306
08275
MA = 306
21513
Ha = 227
794 n
mi
Hp = 218
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10979256
97 X = -3413419
31
Y = 13816312
96 feet Y = 4173415
09 meter
Z = 13575295
12 Z = 4121331
06
XDOT = -9271
387466 XDOT = -2777
008280
YDOT = -19736
498491 feet/sec YDOT = -6047
012824 meter/sec
ZDOT = 12540
856044 ZDOT = 3808
843365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17462709
84 X = 5322633
96
Y = -2897383
22 feet Y = -883122
41 meter
Z = 13504893
95 Z = 4116291
67
XDOT = -6429
664963 XDOT = -1959
761881
YDOT = 19660
747693 feet/sec YDOT = 5992
595897 meter/sec
ZDOT = 12484
157390 ZDOT = 3805
171173
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
70021299
00016717 00000-0 10270-3 0 9097
2 25544 51
6475 92
0731 0003827 107
9872 252
1696 15
50733209 11565
Satellite: ISS
Catalog Number: 25544
Epoch time: 14169
70021299 = yrday
fracday
Element set: 909
Inclination: 51
6475 deg
RA of node: 92
0731 deg
Eccentricity:
0003827
Arg of perigee: 107
9872 deg
Mean anomaly: 252
1696 deg
Mean motion: 15
50733209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 316
Coasting Arc #11 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2014/170/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3296756
87 A = 6790654
59 meter
Y = -3878147
67 meter E =
0012263
Z = -4506410
86 I = 51
99771
XDOT = 2926
989062 Wp = 81
23173
YDOT = 6273
148215 meter/sec RA = 86
59796 deg
ZDOT = -3263
032143 TA = 156
03840
MA = 155
98128
Ha = 227
569 n
mi
Hp = 218
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10816131
46 X = 3361768
85
Y = -12723581
58 feet Y = -3840917
36 meter
Z = -14784812
54 Z = -4490238
09
XDOT = 9602
982488 XDOT = 2872
474494
YDOT = 20581
194930 feet/sec YDOT = 6305
575134 meter/sec
ZDOT = -10705
486033 ZDOT = -3248
945178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16577242
73 X = -5052743
58
Y = 2473420
31 feet Y = 753898
51 meter
Z = -14715506
29 Z = -4485286
32
XDOT = 6349
090987 XDOT = 1935
202933
YDOT = -20677
292696 feet/sec YDOT = -6302
438814 meter/sec
ZDOT = -10646
814836 ZDOT = -3245
149162
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
66683876
00016717 00000-0 10270-3 0 9101
2 25544 51
6467 87
2784 0003596 113
5246 246
6283 15
50762790 11715
Satellite: ISS
Catalog Number: 25544
Epoch time: 14170
66683876 = yrday
fracday
Element set: 910
Inclination: 51
6467 deg
RA of node: 87
2784 deg
Eccentricity:
0003596
Arg of perigee: 113
5246 deg
Mean anomaly: 246
6283 deg
Mean motion: 15
50762790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 330
Coasting Arc #12 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2014/171/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3262796
45 A = 6789543
07 meter
Y = 3532727
30 meter E =
0011293
Z = 4786436
88 I = 51
99133
XDOT = -3073
115830 Wp = 117
09970
YDOT = -6490
693011 meter/sec RA = 81
65927 deg
ZDOT = 2685
854637 TA = 306
45108
MA = 306
55512
Ha = 227
695 n
mi
Hp = 218
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10704712
78 X = -3325308
74
Y = 11590312
66 feet Y = 3495890
69 meter
Z = 15703533
09 Z = 4770435
09
XDOT = -10082
401018 XDOT = -3013
354070
YDOT = -21294
924576 feet/sec YDOT = -6524
724642 meter/sec
ZDOT = 8811
859044 ZDOT = 2671
070457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15723998
50 X = 4792674
74
Y = -1956947
96 feet Y = -596477
74 meter
Z = 15635005
61 Z = 4765549
71
XDOT = -6033
638742 XDOT = -1839
053089
YDOT = 21689
915287 feet/sec YDOT = 6611
086180 meter/sec
ZDOT = 8750
278605 ZDOT = 2667
084919
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
69789939
00016717 00000-0 10270-3 0 9113
2 25544 51
6469 82
1642 0003714 115
4833 244
6703 15
50756308 11879
Satellite: ISS
Catalog Number: 25544
Epoch time: 14171
69789939 = yrday
fracday
Element set: 911
Inclination: 51
6469 deg
RA of node: 82
1642 deg
Eccentricity:
0003714
Arg of perigee: 115
4833 deg
Mean anomaly: 244
6703 deg
Mean motion: 15
50756308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 326
Coasting Arc #13 (Orbit 1201)
---------------------------------------
Vector Time (GMT): 2014/172/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3304937
33 A = 6788429
04 meter
Y = -3147299
31 meter E =
0015420
Z = -5039099
60 I = 51
98155
XDOT = 3209
431968 Wp = 84
40939
YDOT = 6637
824076 meter/sec RA = 76
71843 deg
ZDOT = -2044
805404 TA = 165
78239
MA = 165
73894
Ha = 227
451 n
mi
Hp = 218
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10842970
25 X = 3364363
96
Y = -10325785
15 feet Y = -3110008
63 meter
Z = -16532479
00 Z = -5022900
55
XDOT = 10529
632440 XDOT = 3144
900829
YDOT = 21777
638043 feet/sec YDOT = 6673
353386 meter/sec
ZDOT = -6708
679147 ZDOT = -2029
370472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15004937
54 X = -4573504
96
Y = 1153431
69 feet Y = 351565
98 meter
Z = -16463175
55 Z = -5017975
91
XDOT = 5547
240069 XDOT = 1690
798773
YDOT = -22488
687710 feet/sec YDOT = -6854
552014 meter/sec
ZDOT = -6644
376260 ZDOT = -2025
205884
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
66450724
00016717 00000-0 10270-3 0 9129
2 25544 51
6459 77
3690 0003560 120
7395 239
4107 15
50797331 12027
Satellite: ISS
Catalog Number: 25544
Epoch time: 14172
66450724 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 77
3690 deg
Eccentricity:
0003560
Arg of perigee: 120
7395 deg
Mean anomaly: 239
4107 deg
Mean motion: 15
50797331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1202
Checksum: 300
Coasting Arc #14 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2014/173/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3371252
51 A = 6787733
30 meter
Y = 2762208
93 meter E =
0008044
Z = 5198858
35 I = 51
97155
XDOT = -3368
291421 Wp = 124
16852
YDOT = -6745
342083 meter/sec RA = 71
77729 deg
ZDOT = 1393
734627 TA = 312
45525
MA = 312
52323
Ha = 227
586 n
mi
Hp = 218
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11060539
74 X = -3427144
13
Y = 9062365
26 feet Y = 2724196
34 meter
Z = 17056621
89 Z = 5182345
73
XDOT = -11050
824871 XDOT = -3299
383482
YDOT = -22130
387413 feet/sec YDOT = -6782
623351 meter/sec
ZDOT = 4572
620166 ZDOT = 1377
538473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14380070
96 X = 4383045
63
Y = -279328
13 feet Y = -85139
21 meter
Z = 16986049
83 Z = 5177347
99
XDOT = -4893
690244 XDOT = -1491
596786
YDOT = 23215
318000 feet/sec YDOT = 7076
028926 meter/sec
ZDOT = 4505
119895 ZDOT = 1373
160544
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
69554900
00016717 00000-0 10270-3 0 9135
2 25544 51
6463 72
2550 0003633 123
8517 236
2980 15
50781289 12188
Satellite: ISS
Catalog Number: 25544
Epoch time: 14173
69554900 = yrday
fracday
Element set: 913
Inclination: 51
6463 deg
RA of node: 72
2550 deg
Eccentricity:
0003633
Arg of perigee: 123
8517 deg
Mean anomaly: 236
2980 deg
Mean motion: 15
50781289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 307
Coasting Arc #15 (Orbit 1232)
---------------------------------------
Vector Time (GMT): 2014/174/15:28:33
488
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3514454
08 A = 6787140
26 meter
Y = -2364297
71 meter E =
0017379
Z = -5318087
96 I = 51
95823
XDOT = 3494
665898 Wp = 92
75004
YDOT = 6769
139474 meter/sec RA = 66
83353 deg
ZDOT = -702
744406 TA = 170
56832
MA = 170
53564
Ha = 227
347 n
mi
Hp = 218
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11530361
15 X = 3566464
68
Y = -7756882
27 feet Y = -2324705
35 meter
Z = -17447795
14 Z = -5300889
12
XDOT = 11465
439297 XDOT = 3422
125828
YDOT = 22208
462840 feet/sec YDOT = 6807
813568 meter/sec
ZDOT = -2305
591884 ZDOT = -685
943066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13965471
75 X = -4256675
79
Y = -800397
81 feet Y = -243961
25 meter
Z = -17374376
77 Z = -5295710
04
XDOT = 4124
034102 XDOT = 1257
005594
YDOT = -23629
091393 feet/sec YDOT = -7202
147057 meter/sec
ZDOT = -2235
540777 ZDOT = -681
392829
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
66213967
00016717 00000-0 10270-3 0 9149
2 25544 51
6452 67
4596 0003586 128
4824 231
6649 15
50827416 12332
Satellite: ISS
Catalog Number: 25544
Epoch time: 14174
66213967 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 67
4596 deg
Eccentricity:
0003586
Arg of perigee: 128
4824 deg
Mean anomaly: 231
6649 deg
Mean motion: 15
50827416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1233
Checksum: 325
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