[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 10th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20989 63 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 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 2921)
---------------------------------------
Vector Time (GMT): 2014/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1536993
36 A = 6799585
95 meter
Y = 6473137
42 meter E =
0008277
Z = -1381382
83 I = 51
32595
XDOT = -5033
679870 Wp = 159
57026
YDOT = -33
524835 meter/sec RA = 247
07666 deg
ZDOT = -5775
925646 TA = 35
52325
MA = 35
46816
Ha = 226
139 n
mi
Hp = 221
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5042629
13 X = 1471205
46
Y = 21237327
50 feet Y = 6489957
09 meter
Z = -4532095
89 Z = -1374076
63
XDOT = -16514
697736 XDOT = -5004
872669
YDOT = -109
989615 feet/sec YDOT = -89
654221 meter/sec
ZDOT = -18949
887289 ZDOT = -5800
309104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11445180
81 X = -3488491
11
Y = -18593854
58 feet Y = -5667406
88 meter
Z = -4502053
86 Z = -1372226
02
XDOT = 14255
141089 XDOT = 4344
967004
YDOT = -4175
668717 feet/sec YDOT = -1272
743825 meter/sec
ZDOT = -19053
573750 ZDOT = -5807
529279
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 14283
52958587
00016717 00000-0 10270-3 0 9004
2 25544 51
6434 247
8552 0002548 249
4334 110
6544 15
50333708 29227
Satellite: ISS
Catalog Number: 25544
Epoch time: 14283
52958587 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 247
8552 deg
Eccentricity:
0002548
Arg of perigee: 249
4334 deg
Mean anomaly: 110
6544 deg
Mean motion: 15
50333708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2922
Checksum: 315
Coasting Arc #2 (Orbit 2937)
---------------------------------------
Vector Time (GMT): 2014/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1709472
66 A = 6798853
37 meter
Y = -6321195
51 meter E =
0011281
Z = 1808515
64 I = 51
33706
XDOT = 5201
456490 Wp = 64
85860
YDOT = 208
774815 meter/sec RA = 242
10115 deg
ZDOT = 5623
405804 TA = 315
07541
MA = 315
16664
Ha = 226
021 n
mi
Hp = 221
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5608506
10 X = -1647445
90
Y = -20738830
41 feet Y = -6339964
98 meter
Z = 5933450
25 Z = 1800362
27
XDOT = 17065
145963 XDOT = 5171
418067
YDOT = 684
956742 feet/sec YDOT = 266
773382 meter/sec
ZDOT = 18449
494108 ZDOT = 5648
601288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12142430
75 X = 3701012
89
Y = 17734550
71 feet Y = 5405491
06 meter
Z = 5899775
08 Z = 1798251
45
XDOT = -14940
985967 XDOT = -4554
012523
YDOT = 4031
340947 feet/sec YDOT = 1228
752720 meter/sec
ZDOT = 18556
613416 ZDOT = 5656
055769
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 14284
56092738
00016717 00000-0 10270-3 0 9017
2 25544 51
6434 242
7434 0002648 249
8713 110
2153 15
50390981 29381
Satellite: ISS
Catalog Number: 25544
Epoch time: 14284
56092738 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 242
7434 deg
Eccentricity:
0002648
Arg of perigee: 249
8713 deg
Mean anomaly: 110
2153 deg
Mean motion: 15
50390981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2938
Checksum: 312
Coasting Arc #3 (Orbit 2952)
---------------------------------------
Vector Time (GMT): 2014/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1821795
85 A = 6798042
29 meter
Y = 6145093
52 meter E =
0005166
Z = -2257714
85 I = 51
35057
XDOT = -5404
492502 Wp = 162
28168
YDOT = -384
285493 meter/sec RA = 237
12553 deg
ZDOT = -5415
055391 TA = 42
89500
MA = 42
85471
Ha = 225
950 n
mi
Hp = 221
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5977020
50 X = 1763912
04
Y = 20161067
99 feet Y = 6165142
22 meter
Z = -7407200
94 Z = -2249005
68
XDOT = -17731
274612 XDOT = -5373
488568
YDOT = -1260
779178 feet/sec YDOT = -444
549050 meter/sec
ZDOT = -17765
929762 ZDOT = -5441
234803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12601234
90 X = -3840856
40
Y = -16850383
84 feet Y = -5135996
99 meter
Z = -7371126
49 Z = -2246719
35
XDOT = 15746
235143 XDOT = 4799
452471
YDOT = -3966
898130 feet/sec YDOT = -1209
110550 meter/sec
ZDOT = -17877
215502 ZDOT = -5448
975285
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 14285
52778997
00016717 00000-0 10270-3 0 9023
2 25544 51
6440 237
9504 0002604 257
5877 102
4982 15
50404835 29535
Satellite: ISS
Catalog Number: 25544
Epoch time: 14285
52778997 = yrday
fracday
Element set: 902
Inclination: 51
6440 deg
RA of node: 237
9504 deg
Eccentricity:
0002604
Arg of perigee: 257
5877 deg
Mean anomaly: 102
4982 deg
Mean motion: 15
50404835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2953
Checksum: 332
Coasting Arc #4 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2014/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1910330
61 A = 6797052
01 meter
Y = -5943479
26 meter E =
0010875
Z = 2675384
00 I = 51
36535
XDOT = 5635
504665 Wp = 77
77803
YDOT = 521
563581 meter/sec RA = 232
15079 deg
ZDOT = 5167
063143 TA = 312
50421
MA = 312
59603
Ha = 225
858 n
mi
Hp = 221
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6267488
88 X = -1856723
63
Y = -19499603
87 feet Y = -5964541
91 meter
Z = 8777506
55 Z = 2666234
32
XDOT = 18489
188532 XDOT = 5604
153247
YDOT = 1711
166603 feet/sec YDOT = 584
408474 meter/sec
ZDOT = 16952
306899 ZDOT = 5194
363872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12929584
80 X = 3940937
45
Y = 15906201
80 feet Y = 4848210
31 meter
Z = 8739517
74 Z = 2663805
01
XDOT = -16602
612525 XDOT = -5060
476298
YDOT = 4089
402039 feet/sec YDOT = 1246
449742 meter/sec
ZDOT = 17068
351740 ZDOT = 5202
433610
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 14286
55908499
00016717 00000-0 10270-3 0 9030
2 25544 51
6440 232
8384 0002657 259
0604 101
0248 15
50449466 29694
Satellite: ISS
Catalog Number: 25544
Epoch time: 14286
55908499 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 232
8384 deg
Eccentricity:
0002657
Arg of perigee: 259
0604 deg
Mean anomaly: 101
0248 deg
Mean motion: 15
50449466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 328
Coasting Arc #5 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2014/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1930243
01 A = 6795920
65 meter
Y = 5729452
54 meter E =
0002255
Z = -3103242
43 I = 51
38207
XDOT = -5886
884579 Wp = 131
14778
YDOT = -645
013099 meter/sec RA = 227
17583 deg
ZDOT = -4856
332348 TA = 84
61612
MA = 84
59039
Ha = 225
786 n
mi
Hp = 221
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6332818
27 X = 1881106
23
Y = 18797416
46 feet Y = 5750762
82 meter
Z = -10181241
57 Z = -3093985
19
XDOT = -19313
925783 XDOT = -5855
643555
YDOT = -2116
184708 feet/sec YDOT = -710
669694 meter/sec
ZDOT = -15932
848911 ZDOT = -4884
854446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13005470
98 X = -3964067
55
Y = -15002914
57 feet Y = -4572888
36 meter
Z = -10142751
70 Z = -3091510
72
XDOT = 17501
741762 XDOT = 5334
530889
YDOT = -4326
600540 feet/sec YDOT = -1318
747845 meter/sec
ZDOT = -16054
082521 ZDOT = -4893
284352
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 14287
52590245
00016717 00000-0 10270-3 0 9045
2 25544 51
6442 228
0451 0002639 265
2148 94
8701 15
50480276 29844
Satellite: ISS
Catalog Number: 25544
Epoch time: 14287
52590245 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 228
0451 deg
Eccentricity:
0002639
Arg of perigee: 265
2148 deg
Mean anomaly: 94
8701 deg
Mean motion: 15
50480276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 313
Coasting Arc #6 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2014/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1915727
75 A = 6794743
39 meter
Y = -5500038
10 meter E =
0009599
Z = 3491837
17 I = 51
40029
XDOT = 6155
611235 Wp = 92
67118
YDOT = 724
665359 meter/sec RA = 222
20170 deg
ZDOT = 4507
391150 TA = 308
47318
MA = 308
55925
Ha = 225
730 n
mi
Hp = 221
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6285196
03 X = -1871045
08
Y = -18044744
41 feet Y = -5521210
91 meter
Z = 11456158
69 Z = 3482639
67
XDOT = 20195
574918 XDOT = 6125
154659
YDOT = 2377
511021 feet/sec YDOT = 793
331431 meter/sec
ZDOT = 14788
028708 ZDOT = 4537
220535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12929723
13 X = 3940979
61
Y = 14100156
33 feet Y = 4297727
65 meter
Z = 11417876
90 Z = 3480168
88
XDOT = -18394
127972 XDOT = -5606
530206
YDOT = 4759
849731 feet/sec YDOT = 1450
802198 meter/sec
ZDOT = 14914
824861 ZDOT = 4546
038618
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 14288
55714986
00016717 00000-0 10270-3 0 9050
2 25544 51
6442 222
9326 0002668 267
0797 93
0049 15
50514198 30007
Satellite: ISS
Catalog Number: 25544
Epoch time: 14288
55714986 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 222
9326 deg
Eccentricity:
0002668
Arg of perigee: 267
0797 deg
Mean anomaly: 93
0049 deg
Mean motion: 15
50514198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 321
Coasting Arc #7 (Orbit 3014)
---------------------------------------
Vector Time (GMT): 2014/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1829097
11 A = 6793427
71 meter
Y = 5273552
36 meter E =
0003852
Z = -3876695
58 I = 51
42049
XDOT = -6423
936040 Wp = 63
57365
YDOT = -779
946105 meter/sec RA = 217
22732 deg
ZDOT = -4093
397455 TA = 163
28815
MA = 163
27546
Ha = 225
654 n
mi
Hp = 221
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6000974
76 X = 1788823
01
Y = 17301680
96 feet Y = 5293780
99 meter
Z = -12718817
53 Z = -3867908
27
XDOT = -21075
905642 XDOT = -6394
852448
YDOT = -2558
878297 feet/sec YDOT = -851
620450 meter/sec
ZDOT = -13429
781677 ZDOT = -4124
533630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12614742
35 X = -3844973
47
Y = -13310047
00 feet Y = -4056902
33 meter
Z = -12682235
85 Z = -3865545
49
XDOT = 19236
186537 XDOT = 5863
189656
YDOT = -5313
528181 feet/sec YDOT = -1619
563390 meter/sec
ZDOT = -13562
142983 ZDOT = -4133
741181
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 14289
52392192
00016717 00000-0 10270-3 0 9060
2 25544 51
6446 218
1389 0002650 272
4920 87
5927 15
50557265 30157
Satellite: ISS
Catalog Number: 25544
Epoch time: 14289
52392192 = yrday
fracday
Element set: 906
Inclination: 51
6446 deg
RA of node: 218
1389 deg
Eccentricity:
0002650
Arg of perigee: 272
4920 deg
Mean anomaly: 87
5927 deg
Mean motion: 15
50557265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3015
Checksum: 321
Coasting Arc #8 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2014/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1701156
63 A = 6792185
07 meter
Y = -5044736
43 meter E =
0007565
Z = 4213363
24 I = 51
44197
XDOT = 6695
803804 Wp = 109
51998
YDOT = 791
476744 meter/sec RA = 212
25386 deg
ZDOT = 3643
266642 TA = 303
00372
MA = 303
07639
Ha = 225
618 n
mi
Hp = 221
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5581222
55 X = -1665086
16
Y = -16550972
52 feet Y = -5063557
78 meter
Z = 13823370
21 Z = 4205187
27
XDOT = 21967
860248 XDOT = 6668
757677
YDOT = 2596
708477 feet/sec YDOT = 866
202685 meter/sec
ZDOT = 11952
974547 ZDOT = 3675
728471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12149685
23 X = 3703224
06
Y = 12586079
55 feet Y = 3836237
05 meter
Z = 13789345
56 Z = 4202992
53
XDOT = -20011
000375 XDOT = -6099
352914
YDOT = 6042
021423 feet/sec YDOT = 1841
608130 meter/sec
ZDOT = 12090
988454 ZDOT = 3685
333281
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 14290
55512113
00016717 00000-0 10270-3 0 9073
2 25544 51
6445 213
0259 0002686 274
2959 85
7885 15
50586063 30316
Satellite: ISS
Catalog Number: 25544
Epoch time: 14290
55512113 = yrday
fracday
Element set: 907
Inclination: 51
6445 deg
RA of node: 213
0259 deg
Eccentricity:
0002686
Arg of perigee: 274
2959 deg
Mean anomaly: 85
7885 deg
Mean motion: 15
50586063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3031
Checksum: 313
Coasting Arc #9 (Orbit 3045)
---------------------------------------
Vector Time (GMT): 2014/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1504467
52 A = 6790885
32 meter
Y = 4836229
40 meter E =
0007449
Z = -4531257
75 I = 51
46580
XDOT = -6942
787227 Wp = 59
71979
YDOT = -774
228348 meter/sec RA = 207
28050 deg
ZDOT = -3131
666697 TA = 178
75122
MA = 178
74935
Ha = 225
548 n
mi
Hp = 221
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4935917
06 X = 1472287
51
Y = 15866894
37 feet Y = 4852872
93 meter
Z = -14866331
22 Z = -4524027
86
XDOT = -22778
173317 XDOT = -6918
400813
YDOT = -2540
119252 feet/sec YDOT = -851
731073 meter/sec
ZDOT = -10274
497037 ZDOT = -3165
334845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11489989
97 X = -3502148
94
Y = -12041343
78 feet Y = -3670201
58 meter
Z = -14836292
95 Z = -4522102
09
XDOT = 20640
890414 XDOT = 6291
343398
YDOT = -6860
800934 feet/sec YDOT = -2091
172125 meter/sec
ZDOT = -10417
660224 ZDOT = -3175
302836
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 14291
52184796
00016717 00000-0 10270-3 0 9084
2 25544 51
6453 208
2320 0002667 279
6876 80
3974 15
50634231 30463
Satellite: ISS
Catalog Number: 25544
Epoch time: 14291
52184796 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 208
2320 deg
Eccentricity:
0002667
Arg of perigee: 279
6876 deg
Mean anomaly: 80
3974 deg
Mean motion: 15
50634231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3046
Checksum: 321
Coasting Arc #10 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2014/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1264630
57 A = 6789754
38 meter
Y = -4639642
99 meter E =
0004952
Z = 4791144
83 I = 51
49042
XDOT = 7177
805254 Wp = 128
29542
YDOT = 719
994636 meter/sec RA = 202
30811 deg
ZDOT = 2586
994671 TA = 296
12318
MA = 296
17411
Ha = 225
509 n
mi
Hp = 221
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4149050
43 X = -1235929
18
Y = -15221925
81 feet Y = -4653623
88 meter
Z = 15718979
09 Z = 4785071
59
XDOT = 23549
229837 XDOT = 7156
653672
YDOT = 2362
187126 feet/sec YDOT = 800
143538 meter/sec
ZDOT = 8487
515326 ZDOT = 2621
812448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10706066
77 X = 3263209
15
Y = 11622902
35 feet Y = 3542660
64 meter
Z = 15693827
56 Z = 4783478
64
XDOT = -21151
494420 XDOT = -6446
975499
YDOT = 7801
400486 feet/sec YDOT = 2377
866868 meter/sec
ZDOT = 8635
592025 ZDOT = 2632
128449
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 14292
55299894
00016717 00000-0 10270-3 0 9095
2 25544 51
6452 203
1185 0002729 281
3640 78
7204 15
50662673 30629
Satellite: ISS
Catalog Number: 25544
Epoch time: 14292
55299894 = yrday
fracday
Element set: 909
Inclination: 51
6452 deg
RA of node: 203
1185 deg
Eccentricity:
0002729
Arg of perigee: 281
3640 deg
Mean anomaly: 78
7204 deg
Mean motion: 15
50662673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 318
Coasting Arc #11 (Orbit 3076)
---------------------------------------
Vector Time (GMT): 2014/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 967516
63 A = 6788700
95 meter
Y = 4480301
71 meter E =
0010471
Z = -5017338
41 I = 51
51752
XDOT = -7363
282638 Wp = 67
45103
YDOT = -640
382944 meter/sec RA = 197
33641 deg
ZDOT = -1991
139999 TA = 183
13725
MA = 183
14382
Ha = 225
457 n
mi
Hp = 221
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3174267
15 X = 941717
97
Y = 14699152
60 feet Y = 4490976
26 meter
Z = -16461084
02 Z = -5012701
48
XDOT = -24157
751436 XDOT = -7345
901988
YDOT = -2100
993911 feet/sec YDOT = -722
627001 meter/sec
ZDOT = -6532
611545 ZDOT = -2026
868080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9802416
25 X = -2987776
47
Y = -11431580
91 feet Y = -3484345
86 meter
Z = -16442017
51 Z = -5011526
94
XDOT = 21439
663903 XDOT = 6534
809558
YDOT = -8766
967268 feet/sec YDOT = -2672
171623 meter/sec
ZDOT = -6684
586893 ZDOT = -2037
462085
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 14293
51968088
00016717 00000-0 10270-3 0 9102
2 25544 51
6461 198
3246 0002732 286
8309 73
2542 15
50710085 30770
Satellite: ISS
Catalog Number: 25544
Epoch time: 14293
51968088 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 198
3246 deg
Eccentricity:
0002732
Arg of perigee: 286
8309 deg
Mean anomaly: 73
2542 deg
Mean motion: 15
50710085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3077
Checksum: 316
Coasting Arc #12 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2014/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -631064
41 A = 6787887
45 meter
Y = -4345976
33 meter E =
0001971
Z = 5175347
97 I = 51
54512
XDOT = 7521
430280 Wp = 149
42039
YDOT = 537
745244 meter/sec RA = 192
36577 deg
ZDOT = 1366
816435 TA = 287
40393
MA = 287
42549
Ha = 225
399 n
mi
Hp = 220
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2070421
30 X = -607560
47
Y = -14258452
53 feet Y = -4352901
26 meter
Z = 16979488
09 Z = 5172339
90
XDOT = 24676
608530 XDOT = 7508
218385
YDOT = 1764
256051 feet/sec YDOT = 621
781045 meter/sec
ZDOT = 4484
305889 ZDOT = 1403
323049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8821424
84 X = 2688770
29
Y = 11409873
60 feet Y = 3477729
47 meter
Z = 16967332
65 Z = 5171642
99
XDOT = -21576
353343 XDOT = -6576
472499
YDOT = 9772
837491 feet/sec YDOT = 2978
760867 meter/sec
ZDOT = 4639
622619 ZDOT = 1414
156974
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 14294
55078393
00016717 00000-0 10270-3 0 9119
2 25544 51
6459 193
2108 0002819 288
5741 71
5103 15
50741980 30933
Satellite: ISS
Catalog Number: 25544
Epoch time: 14294
55078393 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 193
2108 deg
Eccentricity:
0002819
Arg of perigee: 288
5741 deg
Mean anomaly: 71
5103 deg
Mean motion: 15
50741980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 316
Coasting Arc #13 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2014/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 256996
09 A = 6787303
71 meter
Y = 4262284
39 meter E =
0012145
Z = -5286384
96 I = 51
57472
XDOT = -7609
622227 Wp = 77
93772
YDOT = -421
133502 meter/sec RA = 187
39632 deg
ZDOT = -708
390204 TA = 185
27133
MA = 185
28413
Ha = 225
383 n
mi
Hp = 220
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 843163
02 X = 234995
29
Y = 13983872
66 feet Y = 4265034
68 meter
Z = -17343782
68 Z = -5285190
40
XDOT = -24965
952188 XDOT = -7600
906232
YDOT = -1381
671596 feet/sec YDOT = -506
180576 meter/sec
ZDOT = -2324
114841 ZDOT = -745
336312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7818324
25 X = -2383025
23
Y = -11631324
00 feet Y = -3545227
56 meter
Z = -17339334
59 Z = -5285029
18
XDOT = 21448
606137 XDOT = 6537
535151
YDOT = -10712
878322 feet/sec YDOT = -3265
285312 meter/sec
ZDOT = -2481
332487 ZDOT = -756
310142
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 14295
51742140
00016717 00000-0 10270-3 0 9125
2 25544 51
6463 188
4167 0002862 293
7288 66
3562 15
50782704 31088
Satellite: ISS
Catalog Number: 25544
Epoch time: 14295
51742140 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 188
4167 deg
Eccentricity:
0002862
Arg of perigee: 293
7288 deg
Mean anomaly: 66
3562 deg
Mean motion: 15
50782704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 317
Coasting Arc #14 (Orbit 3123)
---------------------------------------
Vector Time (GMT): 2014/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 147184
34 A = 6786991
50 meter
Y = -4212864
58 meter E =
0001159
Z = 5319357
96 I = 51
60499
XDOT = 7657
361708 Wp = 347
80587
YDOT = 302
122595 meter/sec RA = 182
42837 deg
ZDOT = 28
510690 TA = 101
92865
MA = 101
91565
Ha = 225
302 n
mi
Hp = 220
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 482888
27 X = 168442
23
Y = -13821734
19 feet Y = -4211099
29 meter
Z = 17451961
82 Z = 5320125
03
XDOT = 25122
577783 XDOT = 7653
275685
YDOT = 991
215863 feet/sec YDOT = 387
729333 meter/sec
ZDOT = 93
539009 ZDOT = 65
700082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6797657
23 X = 2071925
92
Y = 12038659
05 feet Y = 3669383
28 meter
Z = 17455859
56 Z = 5320545
99
XDOT = -21166
650619 XDOT = -6451
595109
YDOT = 11591
934622 feet/sec YDOT = 3533
221673 meter/sec
ZDOT = 251
823869 ZDOT = 76
755915
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 14296
54847693
00016717 00000-0 10270-3 0 9139
2 25544 51
6461 183
3027 0002961 295
9057 64
1789 15
50822362 31243
Satellite: ISS
Catalog Number: 25544
Epoch time: 14296
54847693 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 183
3027 deg
Eccentricity:
0002961
Arg of perigee: 295
9057 deg
Mean anomaly: 64
1789 deg
Mean motion: 15
50822362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3124
Checksum: 326
Coasting Arc #15 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2014/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -562662
14 A = 6787038
66 meter
Y = 4220746
35 meter E =
0011994
Z = -5295493
64 I = 51
63636
XDOT = -7623
403449 Wp = 88
95549
YDOT = -186
979504 meter/sec RA = 177
46181 deg
ZDOT = 662
492112 TA = 187
37310
MA = 187
39076
Ha = 225
334 n
mi
Hp = 220
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1846004
41 X = -584093
17
Y = 13847593
02 feet Y = 4214334
05 meter
Z = -17373666
78 Z = -5298279
43
XDOT = -25011
166170 XDOT = -7623
964269
YDOT = -613
449816 feet/sec YDOT = -272
232425 meter/sec
ZDOT = 2173
530550 ZDOT = 625
456323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5860826
08 X = -1786379
79
Y = -12664116
63 feet Y = -3860022
75 meter
Z = -17386164
90 Z = -5299303
06
XDOT = 20627
288917 XDOT = 6287
197662
YDOT = -12306
809779 feet/sec YDOT = -3751
115621 meter/sec
ZDOT = 2015
867075 ZDOT = 614
436284
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 14297
51507046
00016717 00000-0 10270-3 0 9143
2 25544 51
6458 178
5080 0003030 300
3657 59
7194 15
50851016 31393
Satellite: ISS
Catalog Number: 25544
Epoch time: 14297
51507046 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 178
5080 deg
Eccentricity:
0003030
Arg of perigee: 300
3657 deg
Mean anomaly: 59
7194 deg
Mean motion: 15
50851016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 300
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