[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 30th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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 1773)
---------------------------------------
Vector Time (GMT): 2014/209/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3691479
88 A = 6796888
83 meter
Y = -5042135
94 meter E =
0006541
Z = -2662642
99 I = 51
30796
XDOT = 2900
331018 Wp = 346
55748
YDOT = -4852
963185 meter/sec RA = 253
74515 deg
ZDOT = 5172
517151 TA = 343
29566
MA = 343
31719
Ha = 225
813 n
mi
Hp = 222
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12111154
45 X = -3621889
20
Y = -16542440
74 feet Y = -5083027
25 meter
Z = -8735705
35 Z = -2680406
45
XDOT = 9515
521712 XDOT = 2929
256493
YDOT = -15921
795226 feet/sec YDOT = -4820
368254 meter/sec
ZDOT = 16970
200628 ZDOT = 5186
676360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2854395
25 X = -870019
67
Y = 20270099
89 feet Y = 6178326
45 meter
Z = -8810245
97 Z = -2685362
97
XDOT = -16357
471526 XDOT = -4985
757321
YDOT = 5093
818599 feet/sec YDOT = 1552
595909 meter/sec
ZDOT = 17031
099112 ZDOT = 5191
079009
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 14209
53493196
00016717 00000-0 10270-3 0 9003
2 25544 51
6456 254
6440 0006626 302
6240 57
4270 15
50486889 17749
Satellite: ISS
Catalog Number: 25544
Epoch time: 14209
53493196 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 254
6440 deg
Eccentricity:
0006626
Arg of perigee: 302
6240 deg
Mean anomaly: 57
4270 deg
Mean motion: 15
50486889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1774
Checksum: 316
Coasting Arc #2 (Orbit 1789)
---------------------------------------
Vector Time (GMT): 2014/210/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3887975
71 A = 6797849
36 meter
Y = 5115237
42 meter E =
0007796
Z = 2212685
32 I = 51
31978
XDOT = -2895
451794 Wp = 92
36488
YDOT = 4558
020076 meter/sec RA = 248
76646 deg
ZDOT = -5433
111666 TA = 62
98302
MA = 62
90345
Ha = 226
156 n
mi
Hp = 222
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12755825
81 X = 3819738
68
Y = 16782275
00 feet Y = 5158333
70 meter
Z = 7259466
29 Z = 2231406
56
XDOT = -9499
513760 XDOT = -2919
813610
YDOT = 14954
134108 feet/sec YDOT = 4525
505150 meter/sec
ZDOT = -17825
169509 ZDOT = -5447
236190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2191740
86 X = 668042
61
Y = -20938114
35 feet Y = -6381937
26 meter
Z = 7338074
43 Z = 2236645
09
XDOT = 15545
081746 XDOT = 4738
140916
YDOT = -4659
734093 feet/sec YDOT = -1420
286951 meter/sec
ZDOT = -17885
864515 ZDOT = -5451
611504
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 14210
56620089
00016717 00000-0 10270-3 0 9012
2 25544 51
6447 249
5311 0006718 307
5871 52
4669 15
50478585 17904
Satellite: ISS
Catalog Number: 25544
Epoch time: 14210
56620089 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 249
5311 deg
Eccentricity:
0006718
Arg of perigee: 307
5871 deg
Mean anomaly: 52
4669 deg
Mean motion: 15
50478585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1790
Checksum: 320
Coasting Arc #3 (Orbit 1804)
---------------------------------------
Vector Time (GMT): 2014/211/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4091858
38 A = 6798544
41 meter
Y = -5128275
69 meter E =
0010153
Z = -1757290
76 I = 51
33520
XDOT = 2933
052795 Wp = 357
85139
YDOT = -4272
290374 meter/sec RA = 243
78921 deg
ZDOT = 5647
023507 TA = 342
79721
MA = 342
83160
Ha = 226
163 n
mi
Hp = 222
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13424732
21 X = -4025672
49
Y = -16825051
48 feet Y = -5173663
41 meter
Z = -5765389
65 Z = -1777007
38
XDOT = 9622
876623 XDOT = 2953
177558
YDOT = -14016
700702 feet/sec YDOT = -4239
378593 meter/sec
ZDOT = 18526
980011 ZDOT = 5661
320490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1356801
99 X = -413553
25
Y = 21459327
88 feet Y = 6540803
14 meter
Z = -5848234
38 Z = -1782541
84
XDOT = -14886
508881 XDOT = -4537
407907
YDOT = 4116
760700 feet/sec YDOT = 1254
788661 meter/sec
ZDOT = 18588
354175 ZDOT = 5665
730353
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 14211
53301230
00016717 00000-0 10270-3 0 9025
2 25544 51
6454 244
7380 0006647 310
8732 49
1842 15
50503488 18053
Satellite: ISS
Catalog Number: 25544
Epoch time: 14211
53301230 = yrday
fracday
Element set: 902
Inclination: 51
6454 deg
RA of node: 244
7380 deg
Eccentricity:
0006647
Arg of perigee: 310
8732 deg
Mean anomaly: 49
1842 deg
Mean motion: 15
50503488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1805
Checksum: 282
Coasting Arc #4 (Orbit 1820)
---------------------------------------
Vector Time (GMT): 2014/212/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284470
62 A = 6799244
18 meter
Y = 5121750
51 meter E =
0007456
Z = 1266837
90 I = 51
35076
XDOT = -3024
503088 Wp = 107
47503
YDOT = 3973
187723 meter/sec RA = 238
81310 deg
ZDOT = -5808
259270 TA = 58
71728
MA = 58
64428
Ha = 226
501 n
mi
Hp = 221
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14056662
15 X = 4220725
80
Y = 16803643
40 feet Y = 5169305
81 meter
Z = 4156292
33 Z = 1287496
14
XDOT = -9922
910394 XDOT = -3040
493117
YDOT = 13035
392792 feet/sec YDOT = 3939
276360 meter/sec
ZDOT = -19055
968734 ZDOT = -5822
990532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 489786
96 X = 149287
07
Y = -21885674
59 feet Y = -6670753
62 meter
Z = 4243147
96 Z = 1293311
50
XDOT = 14361
658194 XDOT = 4377
433418
YDOT = -3401
680646 feet/sec YDOT = -1036
832261 meter/sec
ZDOT = -19119
133483 ZDOT = -5827
511886
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 14212
56427344
00016717 00000-0 10270-3 0 9035
2 25544 51
6443 239
6247 0006723 315
8541 44
2073 15
50481420 18215
Satellite: ISS
Catalog Number: 25544
Epoch time: 14212
56427344 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 239
6247 deg
Eccentricity:
0006723
Arg of perigee: 315
8541 deg
Mean anomaly: 44
2073 deg
Mean motion: 15
50481420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1821
Checksum: 284
Coasting Arc #5 (Orbit 1835)
---------------------------------------
Vector Time (GMT): 2014/213/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4467560
38 A = 6799559
72 meter
Y = -5054636
30 meter E =
0013088
Z = -781368
59 I = 51
36975
XDOT = 3157
576883 Wp = 9
54073
YDOT = -3702
380528 meter/sec RA = 233
83913 deg
ZDOT = 5923
660043 TA = 341
98964
MA = 342
03597
Ha = 226
483 n
mi
Hp = 221
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14657350
33 X = -4406910
64
Y = -16583452
44 feet Y = -5104256
33 meter
Z = -2563545
25 Z = -802923
82
XDOT = 10359
504210 XDOT = 3169
968129
YDOT = -12146
917742 feet/sec YDOT = -3667
001159 meter/sec
ZDOT = 19434
580194 ZDOT = 5939
029063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 495579
42 X = 151052
61
Y = 22116284
37 feet Y = 6741043
48 meter
Z = -2654231
40 Z = -809009
73
XDOT = -14043
464779 XDOT = -4280
448064
YDOT = 2644
737540 feet/sec YDOT = 806
116002 meter/sec
ZDOT = 19500
406364 ZDOT = 5943
723860
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 14213
53107678
00016717 00000-0 10270-3 0 9049
2 25544 51
6449 234
8318 0006698 318
6948 41
3695 15
50521419 18367
Satellite: ISS
Catalog Number: 25544
Epoch time: 14213
53107678 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 234
8318 deg
Eccentricity:
0006698
Arg of perigee: 318
6948 deg
Mean anomaly: 41
3695 deg
Mean motion: 15
50521419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1836
Checksum: 330
Coasting Arc #6 (Orbit 1851)
---------------------------------------
Vector Time (GMT): 2014/214/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4626937
10 A = 6799888
69 meter
Y = 4972832
76 meter E =
0006102
Z = 267500
24 I = 51
38858
XDOT = -3338
634192 Wp = 118
38994
YDOT = 3433
369419 meter/sec RA = 228
86588 deg
ZDOT = -5976
736687 TA = 58
72340
MA = 58
66365
Ha = 226
825 n
mi
Hp = 221
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15180239
83 X = 4569686
44
Y = 16315068
11 feet Y = 5024254
05 meter
Z = 877625
47 Z = 289838
03
XDOT = -10953
524252 XDOT = -3347
745929
YDOT = 11264
335364 feet/sec YDOT = 3395
983714 meter/sec
ZDOT = -19608
716164 ZDOT = -5992
977312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1459140
43 X = -444746
00
Y = -22233266
61 feet Y = -6776699
66 meter
Z = 971658
43 Z = 296161
49
XDOT = 13888
693959 XDOT = 4233
273919
YDOT = -1784
632403 feet/sec YDOT = -543
955957 meter/sec
ZDOT = -19678
199432 ZDOT = -5997
915187
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 14214
56233003
00016717 00000-0 10270-3 0 9056
2 25544 51
6439 229
7183 0006826 323
8096 36
2592 15
50488876 18520
Satellite: ISS
Catalog Number: 25544
Epoch time: 14214
56233003 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 229
7183 deg
Eccentricity:
0006826
Arg of perigee: 323
8096 deg
Mean anomaly: 36
2592 deg
Mean motion: 15
50488876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1852
Checksum: 320
Coasting Arc #7 (Orbit 1867)
---------------------------------------
Vector Time (GMT): 2014/215/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4760458
35 A = 6799770
46 meter
Y = -4836303
76 meter E =
0015052
Z = 231167
66 I = 51
40995
XDOT = 3555
957325 Wp = 21
36700
YDOT = -3208
781819 meter/sec RA = 223
89511 deg
ZDOT = 5987
141338 TA = 341
12939
MA = 341
18512
Ha = 226
788 n
mi
Hp = 221
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15618301
69 X = -4707146
82
Y = -15867138
31 feet Y = -4889240
19 meter
Z = 758424
09 Z = 208171
59
XDOT = 11666
526658 XDOT = 3562
490926
YDOT = -10527
499405 feet/sec YDOT = -3168
980343 meter/sec
ZDOT = 19642
852158 ZDOT = 6004
431417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2470771
41 X = 753091
13
Y = 22129849
88 feet Y = 6745178
24 meter
Z = 661563
03 Z = 201644
41
XDOT = -13966
148809 XDOT = -4256
882157
YDOT = 957
568714 feet/sec YDOT = 291
866944 meter/sec
ZDOT = 19716
757430 ZDOT = 6009
667665
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 14215
59357664
00016717 00000-0 10270-3 0 9061
2 25544 51
6440 224
6059 0006778 326
4296 33
6425 15
50539545 18688
Satellite: ISS
Catalog Number: 25544
Epoch time: 14215
59357664 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 224
6059 deg
Eccentricity:
0006778
Arg of perigee: 326
4296 deg
Mean anomaly: 33
6425 deg
Mean motion: 15
50539545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1868
Checksum: 333
Coasting Arc #8 (Orbit 1882)
---------------------------------------
Vector Time (GMT): 2014/216/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4860562
95 A = 6799667
65 meter
Y = 4694154
01 meter E =
0003887
Z = -749997
77 I = 51
43157
XDOT = -3808
054495 Wp = 119
00203
YDOT = 3000
022716 meter/sec RA = 218
92469 deg
ZDOT = -5927
517222 TA = 69
10899
MA = 69
06738
Ha = 227
131 n
mi
Hp = 221
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15946728
85 X = 4811353
83
Y = 15400767
74 feet Y = 4748232
83 meter
Z = -2460622
61 Z = -726505
37
XDOT = -12493
617110 XDOT = -3812
524591
YDOT = 9842
594211 feet/sec YDOT = 2957
413747 meter/sec
ZDOT = -19447
234979 ZDOT = -5946
026902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3403248
37 X = -1037310
10
Y = -21917507
31 feet Y = -6680456
23 meter
Z = -2361619
20 Z = -719821
53
XDOT = 14205
452761 XDOT = 4329
822002
YDOT = -111
076109 feet/sec YDOT = -33
855998 meter/sec
ZDOT = -19526
290069 ZDOT = -5951
613213
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 14216
56037050
00016717 00000-0 10270-3 0 9074
2 25544 51
6432 219
8119 0006987 331
5717 28
5052 15
50501817 18836
Satellite: ISS
Catalog Number: 25544
Epoch time: 14216
56037050 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 219
8119 deg
Eccentricity:
0006987
Arg of perigee: 331
5717 deg
Mean anomaly: 28
5052 deg
Mean motion: 15
50501817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1883
Checksum: 304
Coasting Arc #9 (Orbit 1898)
---------------------------------------
Vector Time (GMT): 2014/217/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4920906
98 A = 6799128
70 meter
Y = -4508574
31 meter E =
0015892
Z = 1243867
75 I = 51
45467
XDOT = 4087
696221 Wp = 33
10285
YDOT = -2847
031728 meter/sec RA = 213
95674 deg
ZDOT = 5829
775534 TA = 340
44525
MA = 340
50614
Ha = 227
100 n
mi
Hp = 221
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16144707
95 X = -4876167
61
Y = -14791910
47 feet Y = -4563352
96 meter
Z = 4080930
92 Z = 1220071
32
XDOT = 13411
076840 XDOT = 4090
909587
YDOT = -9340
655275 feet/sec YDOT = -2801
302735 meter/sec
ZDOT = 19126
560151 ZDOT = 5849
640551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4307503
97 X = 1312927
21
Y = 21487356
61 feet Y = 6549346
29 meter
Z = 3980593
32 Z = 1213284
84
XDOT = -14673
605743 XDOT = -4472
515031
YDOT = -631
235408 feet/sec YDOT = -192
400552 meter/sec
ZDOT = 19211
353123 ZDOT = 5855
620432
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 14217
59160862
00016717 00000-0 10270-3 0 9087
2 25544 51
6428 214
6995 0006895 333
8603 26
2199 15
50552446 18991
Satellite: ISS
Catalog Number: 25544
Epoch time: 14217
59160862 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 214
6995 deg
Eccentricity:
0006895
Arg of perigee: 333
8603 deg
Mean anomaly: 26
2199 deg
Mean motion: 15
50552446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1899
Checksum: 342
Coasting Arc #10 (Orbit 1913)
---------------------------------------
Vector Time (GMT): 2014/218/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4942612
02 A = 6798595
31 meter
Y = 4329742
33 meter E =
0002251
Z = -1748516
41 I = 51
47864
XDOT = -4382
580999 Wp = 72
28532
YDOT = 2720
412858 meter/sec RA = 208
98889 deg
ZDOT = -5657
415083 TA = 126
90350
MA = 126
88287
Ha = 227
414 n
mi
Hp = 220
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16215918
71 X = 4902322
16
Y = 14205191
38 feet Y = 4384788
62 meter
Z = -5736602
39 Z = -1724603
76
XDOT = -14378
546584 XDOT = -4385
193913
YDOT = 8925
239034 feet/sec YDOT = 2671
389685 meter/sec
ZDOT = -18561
073106 ZDOT = -5678
711054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5081676
50 X = -1548895
00
Y = -20977779
45 feet Y = -6394027
18 meter
Z = -5635727
28 Z = -1717769
67
XDOT = 15267
393655 XDOT = 4653
501586
YDOT = 1307
686759 feet/sec YDOT = 398
582924 meter/sec
ZDOT = -18651
932052 ZDOT = -5685
108889
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 14218
55839419
00016717 00000-0 10270-3 0 9096
2 25544 51
6425 209
9053 0007156 339
0970 20
9887 15
50517829 19145
Satellite: ISS
Catalog Number: 25544
Epoch time: 14218
55839419 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 209
9053 deg
Eccentricity:
0007156
Arg of perigee: 339
0970 deg
Mean anomaly: 20
9887 deg
Mean motion: 15
50517829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1914
Checksum: 335
Coasting Arc #11 (Orbit 1929)
---------------------------------------
Vector Time (GMT): 2014/219/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4914528
98 A = 6797703
46 meter
Y = -4122719
02 meter E =
0015571
Z = 2219003
24 I = 51
50339
XDOT = 4694
408548 Wp = 44
40795
YDOT = -2654
965146 meter/sec RA = 204
02333 deg
ZDOT = 5451
918661 TA = 340
28173
MA = 340
34187
Ha = 227
418 n
mi
Hp = 220
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16123782
74 X = -4878841
59
Y = -13525981
03 feet Y = -4177477
03 meter
Z = 7280194
37 Z = 2195215
94
XDOT = 15401
602849 XDOT = 4697
264772
YDOT = -8710
515571 feet/sec YDOT = -2602
453560 meter/sec
ZDOT = 17886
872249 ZDOT = 5474
729926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5755899
84 X = 1754398
27
Y = 20279295
57 feet Y = 6181129
29 meter
Z = 7179801
58 Z = 2188403
52
XDOT = -16060
378793 XDOT = -4895
203456
YDOT = -1823
275579 feet/sec YDOT = -555
734397 meter/sec
ZDOT = 17984
167322 ZDOT = 5481
574200
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 14219
58962369
00016717 00000-0 10270-3 0 9103
2 25544 51
6422 204
7926 0007041 341
3526 18
7366 15
50559948 19303
Satellite: ISS
Catalog Number: 25544
Epoch time: 14219
58962369 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 204
7926 deg
Eccentricity:
0007041
Arg of perigee: 341
3526 deg
Mean anomaly: 18
7366 deg
Mean motion: 15
50559948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1930
Checksum: 320
Coasting Arc #12 (Orbit 1944)
---------------------------------------
Vector Time (GMT): 2014/220/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4848474
30 A = 6796810
36 meter
Y = 3936508
87 meter E =
0004783
Z = -2690170
43 I = 51
52932
XDOT = -4997
545343 Wp = 29
07269
YDOT = 2621
074671 meter/sec RA = 199
05783 deg
ZDOT = -5171
431019 TA = 181
27832
MA = 181
27954
Ha = 227
666 n
mi
Hp = 220
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15907067
90 X = 4817162
75
Y = 12915055
36 feet Y = 3990552
68 meter
Z = -8826018
46 Z = -2666693
53
XDOT = -16396
146137 XDOT = -5001
362683
YDOT = 8599
326348 feet/sec YDOT = 2565
167779 meter/sec
ZDOT = -16966
637200 ZDOT = -5195
717106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6265896
56 X = -1909845
27
Y = -19552797
34 feet Y = -5959692
63 meter
Z = -8726896
49 Z = -2659958
05
XDOT = 16910
449892 XDOT = 5154
305127
YDOT = 2200
030328 feet/sec YDOT = 670
569244 meter/sec
ZDOT = -17070
203135 ZDOT = -5202
997916
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 14220
55640025
00016717 00000-0 10270-3 0 9115
2 25544 51
6425 199
9983 0007302 346
2722 13
8229 15
50534625 19451
Satellite: ISS
Catalog Number: 25544
Epoch time: 14220
55640025 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 199
9983 deg
Eccentricity:
0007302
Arg of perigee: 346
2722 deg
Mean anomaly: 13
8229 deg
Mean motion: 15
50534625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1945
Checksum: 300
Coasting Arc #13 (Orbit 1960)
---------------------------------------
Vector Time (GMT): 2014/221/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4727367
08 A = 6795671
82 meter
Y = -3739475
86 meter E =
0014173
Z = 3118585
76 I = 51
55586
XDOT = 5306
765791 Wp = 54
66191
YDOT = -2647
341476 meter/sec RA = 194
09458 deg
ZDOT = 4862
363374 TA = 341
26239
MA = 341
31451
Ha = 227
718 n
mi
Hp = 220
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15509734
52 X = -4700348
81
Y = -12268621
59 feet Y = -3792189
33 meter
Z = 10231580
59 Z = 3095686
92
XDOT = 17410
648919 XDOT = 5312
355285
YDOT = -8685
503531 feet/sec YDOT = -2587
966662 meter/sec
ZDOT = 15952
635741 ZDOT = 4888
155840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6618045
80 X = 2017180
36
Y = 18688021
66 feet Y = 5696109
00 meter
Z = 10134865
47 Z = 3089106
99
XDOT = -17910
007082 XDOT = -5458
970158
YDOT = -2382
163303 feet/sec YDOT = -726
083375 meter/sec
ZDOT = 16062
616594 ZDOT = 4895
885538
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 14221
58762093
00016717 00000-0 10270-3 0 9120
2 25544 51
6428 194
8855 0007184 348
7570 11
3420 15
50566333 19617
Satellite: ISS
Catalog Number: 25544
Epoch time: 14221
58762093 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 194
8855 deg
Eccentricity:
0007184
Arg of perigee: 348
7570 deg
Mean anomaly: 11
3420 deg
Mean motion: 15
50566333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1961
Checksum: 311
Coasting Arc #14 (Orbit 1975)
---------------------------------------
Vector Time (GMT): 2014/222/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4575656
08 A = 6794560
49 meter
Y = 3576950
70 meter E =
0008752
Z = -3537471
83 I = 51
58318
XDOT = -5581
756146 Wp = 28
89720
YDOT = 2703
818538 meter/sec RA = 189
13152 deg
ZDOT = -4483
073847 TA = 192
70233
MA = 192
72440
Ha = 227
890 n
mi
Hp = 220
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15011995
02 X = 4552501
22
Y = 11735402
56 feet Y = 3627989
16 meter
Z = -11605878
71 Z = -3515300
72
XDOT = -18312
848247 XDOT = -5589
799203
YDOT = 8870
795729 feet/sec YDOT = 2641
354756 meter/sec
ZDOT = -14708
247530 ZDOT = -4510
208133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6797526
47 X = -2071886
07
Y = -17861653
15 feet Y = -5444231
88 meter
Z = -11512213
90 Z = -3508922
80
XDOT = 18874
053234 XDOT = 5752
811426
YDOT = 2377
578489 feet/sec YDOT = 724
685923 meter/sec
ZDOT = -14823
948664 ZDOT = -4518
339553
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 14222
55438833
00016717 00000-0 10270-3 0 9131
2 25544 51
6435 190
0913 0007413 353
1782 6
9267 15
50551152 19766
Satellite: ISS
Catalog Number: 25544
Epoch time: 14222
55438833 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 190
0913 deg
Eccentricity:
0007413
Arg of perigee: 353
1782 deg
Mean anomaly: 6
9267 deg
Mean motion: 15
50551152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1976
Checksum: 301
Coasting Arc #15 (Orbit 1991)
---------------------------------------
Vector Time (GMT): 2014/223/12:42:29
731
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4368563
10 A = 6793311
88 meter
Y = -3421146
60 meter E =
0011957
Z = 3905651
79 I = 51
61098
XDOT = 5853
322654 Wp = 62
57970
YDOT = -2813
182839 meter/sec RA = 184
17078 deg
ZDOT = 4078
671392 TA = 344
67231
MA = 344
70850
Ha = 227
973 n
mi
Hp = 219
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14332556
10 X = -4348954
35
Y = -11224234
25 feet Y = -3469888
94 meter
Z = 12813818
20 Z = 3884478
12
XDOT = 19203
814481 XDOT = 5864
532850
YDOT = -9229
602491 feet/sec YDOT = -2747
664412 meter/sec
ZDOT = 13381
467823 ZDOT = 4107
132678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6781665
61 X = 2067051
68
Y = 16961702
63 feet Y = 5169926
96 meter
Z = 12724354
26 Z = 3878383
18
XDOT = -19926
598444 XDOT = -6073
627206
YDOT = -2172
903644 feet/sec YDOT = -662
301031 meter/sec
ZDOT = 13502
833794 ZDOT = 4115
663740
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 14223
58559992
00016717 00000-0 10270-3 0 9146
2 25544 51
6443 184
9787 0007298 355
9567 4
1524 15
50576599 19924
Satellite: ISS
Catalog Number: 25544
Epoch time: 14223
58559992 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 184
9787 deg
Eccentricity:
0007298
Arg of perigee: 355
9567 deg
Mean anomaly: 4
1524 deg
Mean motion: 15
50576599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1992
Checksum: 364
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