[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 28th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 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 1827)
---------------------------------------
Vector Time (GMT): 2015/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4446645
99 A = 6781499
99 meter
Y = -3816597
35 meter E =
0011342
Z = 3397993
86 I = 51
55159
XDOT = 5625
101835 Wp = 47
59850
YDOT = -2442
293868 meter/sec RA = 193
22719 deg
ZDOT = 4615
553647 TA = 352
23181
MA = 352
24936
Ha = 220
285 n
mi
Hp = 213
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14588733
57 X = -4420143
27
Y = -12521644
83 feet Y = -3866174
73 meter
Z = 11148273
81 Z = 3376457
39
XDOT = 18455
058513 XDOT = 5629
573863
YDOT = -8012
775156 feet/sec YDOT = -2379
365585 meter/sec
ZDOT = 15142
892544 ZDOT = 4642
889509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10976221
68 X = 3345552
37
Y = -15849289
54 feet Y = -4830863
45 meter
Z = 11055737
15 Z = 3369788
68
XDOT = 8668
402070 XDOT = 2642
128951
YDOT = 16654
401312 feet/sec YDOT = 5076
261520 meter/sec
ZDOT = 15261
617458 ZDOT = 4651
741001
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 15362
55724360
00016717 00000-0 10270-3 0 9006
2 25544 51
6379 194
0437 0008652 331
2741 28
7935 15
55161676 18289
Satellite: ISS
Catalog Number: 25544
Epoch time: 15362
55724360 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 194
0437 deg
Eccentricity:
0008652
Arg of perigee: 331
2741 deg
Mean anomaly: 28
7935 deg
Mean motion: 15
55161676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 319
Coasting Arc #2 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2015/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2614554
82 A = 6777045
13 meter
Y = 4141911
12 meter E =
0013149
Z = -4694666
54 I = 51
56753
XDOT = -7018
642661 Wp = 30
44171
YDOT = 1237
769323 meter/sec RA = 188
22475 deg
ZDOT = -2809
153802 TA = 211
60612
MA = 211
68515
Ha = 220
404 n
mi
Hp = 213
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8577935
76 X = 2590849
16
Y = 13588947
24 feet Y = 4171016
50 meter
Z = -15402449
28 Z = -4682023
13
XDOT = -23027
042850 XDOT = -7018
316487
YDOT = 4060
922977 feet/sec YDOT = 1159
284191 meter/sec
ZDOT = -9216
383864 ZDOT = -2843
247549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12467920
84 X = -3800222
27
Y = 10220182
68 feet Y = 3115111
68 meter
Z = -15348443
86 Z = -4678205
69
XDOT = -5998
359199 XDOT = -1828
299884
YDOT = -21418
240510 feet/sec YDOT = -6528
279708 meter/sec
ZDOT = -9364
162464 ZDOT = -2854
196719
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 15363
52113948
00016717 00000-0 10270-3 0 9019
2 25544 51
6373 189
2304 0008569 336
2635 23
8122 15
55166188 18430
Satellite: ISS
Catalog Number: 25544
Epoch time: 15363
52113948 = yrday
fracday
Element set: 901
Inclination: 51
6373 deg
RA of node: 189
2304 deg
Eccentricity:
0008569
Arg of perigee: 336
2635 deg
Mean anomaly: 23
8122 deg
Mean motion: 15
55166188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 313
Coasting Arc #3 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2015/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -411355
10 A = 6774566
75 meter
Y = -4219069
05 meter E =
0006830
Z = 5284006
88 I = 51
59103
XDOT = 7649
054510 Wp = 358
38463
YDOT = -29
992674 meter/sec RA = 183
21137 deg
ZDOT = 578
225387 TA = 86
13426
MA = 86
05617
Ha = 220
580 n
mi
Hp = 213
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1349590
22 X = -389813
16
Y = -13842090
05 feet Y = -4223548
84 meter
Z = 17335980
58 Z = 5282060
80
XDOT = 25095
323195 XDOT = 7646
012646
YDOT = -98
401161 feet/sec YDOT = 55
527081 meter/sec
ZDOT = 1897
064919 ZDOT = 615
375013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13516078
76 X = 4119700
80
Y = -3317717
36 feet Y = -1011240
25 meter
Z = 17328284
39 Z = 5281661
08
XDOT = 3245
122722 XDOT = 989
113406
YDOT = 23853
662591 feet/sec YDOT = 7270
596358 meter/sec
ZDOT = 2057
880111 ZDOT = 627
241858
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 15364
54928679
00016717 00000-0 10270-3 0 9028
2 25544 51
6375 184
0955 0008571 340
3501 19
7321 15
55128037 18591
Satellite: ISS
Catalog Number: 25544
Epoch time: 15364
54928679 = yrday
fracday
Element set: 902
Inclination: 51
6375 deg
RA of node: 184
0955 deg
Eccentricity:
0008571
Arg of perigee: 340
3501 deg
Mean anomaly: 19
7321 deg
Mean motion: 15
55128037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 323
Coasting Arc #4 (Orbit 1873)
---------------------------------------
Vector Time (GMT): 2015/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1821075
65 A = 6775202
32 meter
Y = 4091432
07 meter E =
0011928
Z = -5092005
34 I = 51
62585
XDOT = -7377
862871 Wp = 64
64458
YDOT = -1139
406173 meter/sec RA = 178
19772 deg
ZDOT = 1731
224408 TA = 222
05722
MA = 222
14884
Ha = 220
584 n
mi
Hp = 213
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5974657
64 X = -1841957
00
Y = 13423333
57 feet Y = 4070950
99 meter
Z = -16706054
27 Z = -5100902
25
XDOT = -24205
586848 XDOT = -7372
982933
YDOT = -3738
209228 feet/sec YDOT = -1221
883078 meter/sec
ZDOT = 5679
870106 ZDOT = 1695
396513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14158283
84 X = -4315444
91
Y = -3756785
39 feet Y = -1145068
19 meter
Z = -16745274
84 Z = -5103959
77
XDOT = -268
536830 XDOT = -81
850026
YDOT = -23495
512164 feet/sec YDOT = -7161
432108 meter/sec
ZDOT = 5524
959827 ZDOT = 1684
007755
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 15365
51316428
00016717 00000-0 10270-3 0 9030
2 25544 51
6376 179
2818 0008473 343
9099 16
1784 15
55188213 18741
Satellite: ISS
Catalog Number: 25544
Epoch time: 15365
51316428 = yrday
fracday
Element set: 903
Inclination: 51
6376 deg
RA of node: 179
2818 deg
Eccentricity:
0008473
Arg of perigee: 343
9099 deg
Mean anomaly: 16
1784 deg
Mean motion: 15
55188213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1874
Checksum: 335
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