[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 15th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 27986 17 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 3226)
---------------------------------------
Vector Time (GMT): 2014/045/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6690816
07 A = 6800358
51 meter
Y = 1115516
75 meter E =
0015081
Z = -374161
10 I = 51
59702
XDOT = -466
577503 Wp = 136
07373
YDOT = -4755
900185 meter/sec RA = 348
02850 deg
ZDOT = -5991
413575 TA = 47
95640
MA = 47
82815
Ha = 228
174 n
mi
Hp = 219
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21951496
30 X = -6700975
25
Y = 3659831
87 feet Y = 1040638
93 meter
Z = -1227562
65 Z = -406688
11
XDOT = -1530
766086 XDOT = -384
257628
YDOT = -15603
347064 feet/sec YDOT = -4760
657935 meter/sec
ZDOT = -19656
868684 ZDOT = -5993
479779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2283714
84 X = -696076
28
Y = -22128958
38 feet Y = -6744906
51 meter
Z = -1365033
63 Z = -416062
25
XDOT = 14048
724251 XDOT = 4282
051152
YDOT = -265
137727 feet/sec YDOT = -80
813979 meter/sec
ZDOT = -19664
772223 ZDOT = -5993
822574
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 14045
37306583
00016717 00000-0 10270-3 0 9006
2 25544 51
6479 348
4120 0003888 132
9819 227
1658 15
50317062 32271
Satellite: ISS
Catalog Number: 25544
Epoch time: 14045
37306583 = yrday
fracday
Element set: 900
Inclination: 51
6479 deg
RA of node: 348
4120 deg
Eccentricity:
0003888
Arg of perigee: 132
9819 deg
Mean anomaly: 227
1658 deg
Mean motion: 15
50317062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 311
Coasting Arc #2 (Orbit 3242)
---------------------------------------
Vector Time (GMT): 2014/046/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6611898
37 A = 6799881
35 meter
Y = -1346087
00 meter E =
0014218
Z = 803350
01 I = 51
56615
XDOT = 255
388219 Wp = 69
68183
YDOT = 4842
542893 meter/sec RA = 343
07133 deg
ZDOT = 5931
641246 TA = 298
99870
MA = 299
14113
Ha = 228
014 n
mi
Hp = 219
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21692579
96 X = 6622556
88
Y = -4416295
93 feet Y = -1272088
85 meter
Z = 2635662
77 Z = 835494
97
XDOT = 837
887856 XDOT = 172
405479
YDOT = 15887
607916 feet/sec YDOT = 4844
935378 meter/sec
ZDOT = 19460
765243 ZDOT = 5932
679851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3431702
52 X = 1045982
93
Y = 21853153
77 feet Y = 6660841
27 meter
Z = 2771552
14 Z = 844769
09
XDOT = -14311
777922 XDOT = -4362
229911
YDOT = -253
008497 feet/sec YDOT = -77
116990 meter/sec
ZDOT = 19464
322085 ZDOT = 5932
725372
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 14046
40441304
00016717 00000-0 10270-3 0 9013
2 25544 51
6478 343
3011 0003933 139
8893 220
2548 15
50402743 32433
Satellite: ISS
Catalog Number: 25544
Epoch time: 14046
40441304 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 343
3011 deg
Eccentricity:
0003933
Arg of perigee: 139
8893 deg
Mean anomaly: 220
2548 deg
Mean motion: 15
50402743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3243
Checksum: 280
Coasting Arc #3 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2014/047/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6498391
73 A = 6799482
87 meter
Y = 1510488
28 meter E =
0012554
Z = -1285354
32 I = 51
53507
XDOT = -13
775772 Wp = 141
12863
YDOT = -4980
084890 meter/sec RA = 338
11044 deg
ZDOT = -5823
214624 TA = 52
85316
MA = 52
73856
Ha = 227
926 n
mi
Hp = 219
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21320182
83 X = -6508555
66
Y = 4955670
22 feet Y = 1437762
14 meter
Z = -4217041
74 Z = -1316946
81
XDOT = -45
196103 XDOT = 70
200424
YDOT = -16338
861188 feet/sec YDOT = -4979
770023 meter/sec
ZDOT = -19105
034855 ZDOT = -5823
077044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4356841
57 X = -1327965
31
Y = -21423873
59 feet Y = -6529996
67 meter
Z = -4350617
92 Z = -1326068
34
XDOT = 14769
675073 XDOT = 4501
796962
YDOT = 849
662537 feet/sec YDOT = 258
977141 meter/sec
ZDOT = -19103
609989 ZDOT = -5822
780325
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 14047
37128447
00016717 00000-0 10270-3 0 9021
2 25544 51
6475 338
5079 0003760 140
1188 220
0239 15
50386824 32582
Satellite: ISS
Catalog Number: 25544
Epoch time: 14047
37128447 = yrday
fracday
Element set: 902
Inclination: 51
6475 deg
RA of node: 338
5079 deg
Eccentricity:
0003760
Arg of perigee: 140
1188 deg
Mean anomaly: 220
0239 deg
Mean motion: 15
50386824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 307
Coasting Arc #4 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2014/048/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6353136
02 A = 6798690
54 meter
Y = -1682089
53 meter E =
0014929
Z = 1721186
30 I = 51
50449
XDOT = -183
943816 Wp = 79
45607
YDOT = 5149
048940 meter/sec RA = 333
14834 deg
ZDOT = 5671
752190 TA = 299
43112
MA = 299
58004
Ha = 227
767 n
mi
Hp = 219
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20843622
11 X = 6363112
51
Y = -5518666
43 feet Y = -1610988
72 meter
Z = 5646936
67 Z = 1752072
85
XDOT = -603
490210 XDOT = -269
059063
YDOT = 16893
205185 feet/sec YDOT = 5146
516702 meter/sec
ZDOT = 18608
110861 ZDOT = 5670
651310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5292814
53 X = 1613249
87
Y = 20866388
10 feet Y = 6360075
09 meter
Z = 5777552
89 Z = 1760998
12
XDOT = -15364
347765 XDOT = -4683
053199
YDOT = -1288
431536 feet/sec YDOT = -392
713932 meter/sec
ZDOT = 18602
597833 ZDOT = 5670
071819
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 14048
40258725
00016717 00000-0 10270-3 0 9030
2 25544 51
6472 333
3967 0003836 147
5776 212
5611 15
50466231 32745
Satellite: ISS
Catalog Number: 25544
Epoch time: 14048
40258725 = yrday
fracday
Element set: 903
Inclination: 51
6472 deg
RA of node: 333
3967 deg
Eccentricity:
0003836
Arg of perigee: 147
5776 deg
Mean anomaly: 212
5611 deg
Mean motion: 15
50466231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 309
Coasting Arc #5 (Orbit 3288)
---------------------------------------
Vector Time (GMT): 2014/049/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6179859
20 A = 6797905
40 meter
Y = 1774546
50 meter E =
0009614
Z = -2198378
84 I = 51
47473
XDOT = 395
473120 Wp = 140
39946
YDOT = -5360
040722 meter/sec RA = 328
18227 deg
ZDOT = -5458
832298 TA = 64
02801
MA = 63
92900
Ha = 227
667 n
mi
Hp = 219
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20275128
60 X = -6188564
39
Y = 5822002
94 feet Y = 1705390
43 meter
Z = -7212529
02 Z = -2228420
68
XDOT = 1297
483989 XDOT = 481
897818
YDOT = -17585
435439 feet/sec YDOT = -5355
135683 meter/sec
ZDOT = -17909
554784 ZDOT = -5456
700642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5950471
56 X = -1813703
73
Y = -20192064
90 feet Y = -6154541
38 meter
Z = -7339586
92 Z = -2237106
09
XDOT = 16123
107503 XDOT = 4914
323167
YDOT = 1730
975055 feet/sec YDOT = 527
601197 meter/sec
ZDOT = -17899
662039 ZDOT = -5455
816990
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 14049
36941646
00016717 00000-0 10270-3 0 9048
2 25544 51
6473 328
6033 0003626 147
8729 212
2644 15
50457381 32890
Satellite: ISS
Catalog Number: 25544
Epoch time: 14049
36941646 = yrday
fracday
Element set: 904
Inclination: 51
6473 deg
RA of node: 328
6033 deg
Eccentricity:
0003626
Arg of perigee: 147
8729 deg
Mean anomaly: 212
2644 deg
Mean motion: 15
50457381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3289
Checksum: 322
Coasting Arc #6 (Orbit 3304)
---------------------------------------
Vector Time (GMT): 2014/050/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5981928
49 A = 6796840
59 meter
Y = -1862273
75 meter E =
0014804
Z = 2623160
19 I = 51
44575
XDOT = -552
899720 Wp = 91
50448
YDOT = 5595
217146 meter/sec RA = 323
21476 deg
ZDOT = 5207
192439 TA = 298
09016
MA = 298
23974
Ha = 227
507 n
mi
Hp = 219
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19625749
64 X = 5989565
92
Y = -6109822
02 feet Y = -1795337
01 meter
Z = 8606168
59 Z = 2652238
02
XDOT = -1813
975460 XDOT = -640
720224
YDOT = 18357
011635 feet/sec YDOT = 5588
543797 meter/sec
ZDOT = 17083
964695 ZDOT = 5204
292645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6569025
74 X = 2002239
04
Y = 19422041
19 feet Y = 5919838
16 meter
Z = 8729165
39 Z = 2660649
61
XDOT = -16982
320803 XDOT = -5176
211381
YDOT = -1966
205526 feet/sec YDOT = -599
299444 meter/sec
ZDOT = 17070
796446 ZDOT = 5203
178757
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 14050
40067507
00016717 00000-0 10270-3 0 9051
2 25544 51
6470 323
4916 0003712 155
2027 204
9302 15
50524847 33050
Satellite: ISS
Catalog Number: 25544
Epoch time: 14050
40067507 = yrday
fracday
Element set: 905
Inclination: 51
6470 deg
RA of node: 323
4916 deg
Eccentricity:
0003712
Arg of perigee: 155
2027 deg
Mean anomaly: 204
9302 deg
Mean motion: 15
50524847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3305
Checksum: 275
Coasting Arc #7 (Orbit 3319)
---------------------------------------
Vector Time (GMT): 2014/051/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5767493
60 A = 6795730
33 meter
Y = 1860734
44 meter E =
0007245
Z = -3074710
80 I = 51
41812
XDOT = 708
227448 Wp = 126
85663
YDOT = -5856
160324 meter/sec RA = 318
24313 deg
ZDOT = -4884
735663 TA = 88
50938
MA = 88
42639
Ha = 227
401 n
mi
Hp = 219
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18922223
10 X = -5772936
25
Y = 6104771
79 feet Y = 1796207
91 meter
Z = -10087633
85 Z = -3102741
66
XDOT = 2323
580865 XDOT = 797
388008
YDOT = -19213
124423 feet/sec YDOT = -5847
742418 meter/sec
ZDOT = -16026
035639 ZDOT = -4881
078091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6867905
44 X = -2093337
58
Y = -18594201
90 feet Y = -5667512
74 meter
Z = -10206206
59 Z = -3110851
77
XDOT = 17941
373908 XDOT = 5468
530767
YDOT = 2138
958233 feet/sec YDOT = 651
954470 meter/sec
ZDOT = -16009
631325 ZDOT = -4879
735628
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 14051
36746197
00016717 00000-0 10270-3 0 9067
2 25544 51
6473 318
6979 0003501 156
3704 203
7608 15
50527398 33205
Satellite: ISS
Catalog Number: 25544
Epoch time: 14051
36746197 = yrday
fracday
Element set: 906
Inclination: 51
6473 deg
RA of node: 318
6979 deg
Eccentricity:
0003501
Arg of perigee: 156
3704 deg
Mean anomaly: 203
7608 deg
Mean motion: 15
50527398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3320
Checksum: 316
Coasting Arc #8 (Orbit 3335)
---------------------------------------
Vector Time (GMT): 2014/052/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5539323
11 A = 6794476
25 meter
Y = -1845049
39 meter E =
0013785
Z = 3467292
76 I = 51
39211
XDOT = -804
459533 Wp = 105
51959
YDOT = 6130
217421 meter/sec RA = 313
27007 deg
ZDOT = 4528
572571 TA = 295
28104
MA = 295
42381
Ha = 227
233 n
mi
Hp = 219
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18173632
24 X = 5542700
29
Y = -6053311
63 feet Y = -1783085
96 meter
Z = 11375632
42 Z = 3494210
18
XDOT = -2639
302931 XDOT = -894
947411
YDOT = 20112
261879 feet/sec YDOT = 6120
715866 meter/sec
ZDOT = 14857
521559 ZDOT = 4524
444354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7091400
67 X = 2161458
92
Y = 17720945
67 feet Y = 5401344
24 meter
Z = 11489500
61 Z = 3501999
79
XDOT = -18945
783775 XDOT = -5774
674895
YDOT = -2078
862143 feet/sec YDOT = -633
637181 meter/sec
ZDOT = 14839
090663 ZDOT = 4522
954834
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 14052
39867660
00016717 00000-0 10270-3 0 9071
2 25544 51
6474 313
5858 0003593 163
1297 196
9974 15
50584166 33362
Satellite: ISS
Catalog Number: 25544
Epoch time: 14052
39867660 = yrday
fracday
Element set: 907
Inclination: 51
6474 deg
RA of node: 313
5858 deg
Eccentricity:
0003593
Arg of perigee: 163
1297 deg
Mean anomaly: 196
9974 deg
Mean motion: 15
50584166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3336
Checksum: 347
Coasting Arc #9 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2014/053/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5310462
21 A = 6793189
58 meter
Y = 1735314
15 meter E =
0007255
Z = -3869542
55 I = 51
36766
XDOT = 886
236435 Wp = 101
92412
YDOT = -6407
198674 meter/sec RA = 308
29287 deg
ZDOT = -4097
594609 TA = 124
86922
MA = 124
80099
Ha = 227
137 n
mi
Hp = 219
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17422776
27 X = -5310675
35
Y = 5693287
90 feet Y = 1675927
71 meter
Z = -12695349
58 Z = -3895340
46
XDOT = 2907
599852 XDOT = 977
721940
YDOT = -21020
993026 feet/sec YDOT = -6396
776966 meter/sec
ZDOT = -13443
551868 ZDOT = -4093
066786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6979034
41 X = -2127209
69
Y = -16866448
37 feet Y = -5140893
46 meter
Z = -12804474
20 Z = -3902803
74
XDOT = 19957
505313 XDOT = 6083
047619
YDOT = 1912
781287 feet/sec YDOT = 583
015736 meter/sec
ZDOT = -13423
394356 ZDOT = -4091
450600
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 14053
36542170
00016717 00000-0 10270-3 0 9086
2 25544 51
6476 308
7917 0003401 165
1701 194
9550 15
50596439 33517
Satellite: ISS
Catalog Number: 25544
Epoch time: 14053
36542170 = yrday
fracday
Element set: 908
Inclination: 51
6476 deg
RA of node: 308
7917 deg
Eccentricity:
0003401
Arg of perigee: 165
1701 deg
Mean anomaly: 194
9550 deg
Mean motion: 15
50596439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 307
Coasting Arc #10 (Orbit 3366)
---------------------------------------
Vector Time (GMT): 2014/054/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5081263
04 A = 6791880
74 meter
Y = -1605965
50 meter E =
0011940
Z = 4206073
95 I = 51
34570
XDOT = -910
553711 Wp = 121
14079
YDOT = 6683
777982 meter/sec RA = 303
31455 deg
ZDOT = 3638
272955 TA = 291
35890
MA = 291
48628
Ha = 226
944 n
mi
Hp = 219
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16670810
50 X = 5078412
12
Y = -5268915
68 feet Y = -1549159
26 meter
Z = 13799455
21 Z = 4230750
91
XDOT = -2987
380940 XDOT = -1002
898912
YDOT = 21928
405453 feet/sec YDOT = 6673
079463 meter/sec
ZDOT = 11936
591060 ZDOT = 3633
624983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6775458
34 X = 2065159
70
Y = 16027447
37 feet Y = 4885165
96 meter
Z = 13903828
77 Z = 4237887
01
XDOT = -20949
611700 XDOT = -6385
441646
YDOT = -1519
628541 feet/sec YDOT = -463
182779 meter/sec
ZDOT = 11915
887579 ZDOT = 3631
962534
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 14054
39659249
00016717 00000-0 10270-3 0 9097
2 25544 51
6480 303
6794 0003496 171
5431 188
5779 15
50647886 33676
Satellite: ISS
Catalog Number: 25544
Epoch time: 14054
39659249 = yrday
fracday
Element set: 909
Inclination: 51
6480 deg
RA of node: 303
6794 deg
Eccentricity:
0003496
Arg of perigee: 171
5431 deg
Mean anomaly: 188
5779 deg
Mean motion: 15
50647886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3367
Checksum: 357
Coasting Arc #11 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2014/055/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4869745
22 A = 6790634
87 meter
Y = 1385212
53 meter E =
0009642
Z = -4533894
77 I = 51
32566
XDOT = 914
474124 Wp = 89
09507
YDOT = -6936
233923 meter/sec RA = 298
33224 deg
ZDOT = -3107
000226 TA = 149
60906
MA = 149
55313
Ha = 226
880 n
mi
Hp = 219
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15976854
38 X = -4862849
16
Y = 4544660
54 feet Y = 1330794
24 meter
Z = -14874982
85 Z = -4557534
28
XDOT = 3000
243188 XDOT = 1007
061270
YDOT = -22756
672976 feet/sec YDOT = -6925
490168 meter/sec
ZDOT = -10193
570296 ZDOT = -3102
332655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6253513
24 X = -1906070
84
Y = -15291290
25 feet Y = -4660785
27 meter
Z = -14974943
89 Z = -4564362
90
XDOT = 21841
033036 XDOT = 6657
146869
YDOT = 1012
328804 feet/sec YDOT = 308
557820 meter/sec
ZDOT = -10172
751564 ZDOT = -3100
654677
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 14055
36329649
00016717 00000-0 10270-3 0 9105
2 25544 51
6482 298
8853 0003325 173
7776 186
3416 15
50664449 33821
Satellite: ISS
Catalog Number: 25544
Epoch time: 14055
36329649 = yrday
fracday
Element set: 910
Inclination: 51
6482 deg
RA of node: 298
8853 deg
Eccentricity:
0003325
Arg of perigee: 173
7776 deg
Mean anomaly: 186
3416 deg
Mean motion: 15
50664449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 340
Coasting Arc #12 (Orbit 3397)
---------------------------------------
Vector Time (GMT): 2014/056/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4671787
58 A = 6789458
07 meter
Y = -1144310
82 meter E =
0009424
Z = 4789152
47 I = 51
30850
XDOT = -869
888363 Wp = 137
52045
YDOT = 7174
068248 meter/sec RA = 293
34920 deg
ZDOT = 2552
950699 TA = 287
16583
MA = 287
26899
Ha = 226
640 n
mi
Hp = 219
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15327387
08 X = 4660972
58
Y = -3754300
59 feet Y = -1092128
09 meter
Z = 15712442
47 Z = 4811820
72
XDOT = -2853
964445 XDOT = -962
446934
YDOT = 23536
969316 feet/sec YDOT = 7163
823223 meter/sec
ZDOT = 8375
822504 ZDOT = 2548
499753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5648743
75 X = 1721737
10
Y = 14631978
06 feet Y = 4459826
91 meter
Z = 15808267
71 Z = 4818360
00
XDOT = -22649
232191 XDOT = -6903
485972
YDOT = -318
241148 feet/sec YDOT = -96
999902 meter/sec
ZDOT = 8355
890888 ZDOT = 2546
875543
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 14056
39442345
00016717 00000-0 10270-3 0 9119
2 25544 51
6484 293
7729 0003411 180
3174 179
7975 15
50715305 33982
Satellite: ISS
Catalog Number: 25544
Epoch time: 14056
39442345 = yrday
fracday
Element set: 911
Inclination: 51
6484 deg
RA of node: 293
7729 deg
Eccentricity:
0003411
Arg of perigee: 180
3174 deg
Mean anomaly: 179
7975 deg
Mean motion: 15
50715305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3398
Checksum: 325
Coasting Arc #13 (Orbit 3412)
---------------------------------------
Vector Time (GMT): 2014/057/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4509696
99 A = 6788494
90 meter
Y = 823255
66 meter E =
0012388
Z = -5017626
07 I = 51
29411
XDOT = 807
331066 Wp = 90
06607
YDOT = -7360
321490 meter/sec RA = 288
36254 deg
ZDOT = -1937
413863 TA = 161
02918
MA = 160
98299
Ha = 226
623 n
mi
Hp = 219
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14795593
81 X = -4494194
18
Y = 2700970
00 feet Y = 772911
65 meter
Z = -16462027
78 Z = -5039495
46
XDOT = 2648
723971 XDOT = 898
986957
YDOT = -24148
036385 feet/sec YDOT = -7350
781062 meter/sec
ZDOT = -6356
344696 ZDOT = -1933
268890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4780124
44 X = -1456981
93
Y = -14152893
08 feet Y = -4313801
81 meter
Z = -16554432
08 Z = -5045790
90
XDOT = 23252
360897 XDOT = 7087
319601
YDOT = -456
309114 feet/sec YDOT = -139
083018 meter/sec
ZDOT = -6337
688974 ZDOT = -1931
727599
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 14057
36108657
00016717 00000-0 10270-3 0 9123
2 25544 51
6485 288
9787 0003256 182
2651 177
8486 15
50731542 34136
Satellite: ISS
Catalog Number: 25544
Epoch time: 14057
36108657 = yrday
fracday
Element set: 912
Inclination: 51
6485 deg
RA of node: 288
9787 deg
Eccentricity:
0003256
Arg of perigee: 182
2651 deg
Mean anomaly: 177
8486 deg
Mean motion: 15
50731542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3413
Checksum: 333
Coasting Arc #14 (Orbit 3428)
---------------------------------------
Vector Time (GMT): 2014/058/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4373162
10 A = 6787661
30 meter
Y = -486776
04 meter E =
0006417
Z = 5166761
18 I = 51
28258
XDOT = -712
408984 Wp = 152
26807
YDOT = 7518
849295 meter/sec RA = 283
37540 deg
ZDOT = 1305
122434 TA = 285
09056
MA = 285
16154
Ha = 226
325 n
mi
Hp = 220
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14347644
68 X = 4353182
44
Y = -1597034
26 feet Y = -437983
76 meter
Z = 16951316
21 Z = 5187956
40
XDOT = -2337
299816 XDOT = -802
773213
YDOT = 24668
140731 feet/sec YDOT = 7510
377550 meter/sec
ZDOT = 4281
897748 ZDOT = 1301
441534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3860817
85 X = 1176777
28
Y = 13800614
62 feet Y = 4206427
34 meter
Z = 17040823
61 Z = 5194043
04
XDOT = -23721
737677 XDOT = -7230
385644
YDOT = 1344
585827 feet/sec YDOT = 409
829760 meter/sec
ZDOT = 4265
192146 ZDOT = 1300
030566
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 14058
39216947
00016717 00000-0 10270-3 0 9130
2 25544 51
6480 283
8657 0003316 189
2934 170
8156 15
50784652 34293
Satellite: ISS
Catalog Number: 25544
Epoch time: 14058
39216947 = yrday
fracday
Element set: 913
Inclination: 51
6480 deg
RA of node: 283
8657 deg
Eccentricity:
0003316
Arg of perigee: 189
2934 deg
Mean anomaly: 170
8156 deg
Mean motion: 15
50784652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3429
Checksum: 337
Coasting Arc #15 (Orbit 3443)
---------------------------------------
Vector Time (GMT): 2014/059/08:11:53
155
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4287181
68 A = 6787198
81 meter
Y = 89946
74 meter E =
0014108
Z = -5272991
70 I = 51
27506
XDOT = 610
541772 Wp = 97
60796
YDOT = -7602
541113 meter/sec RA = 278
38539 deg
ZDOT = -629
368605 TA = 166
36017
MA = 166
32200
Ha = 226
351 n
mi
Hp = 219
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14065556
68 X = -4262254
93
Y = 295100
84 feet Y = 42143
47 meter
Z = -17299841
54 Z = -5293757
22
XDOT = 2003
089804 XDOT = 698
566919
YDOT = -24942
720186 feet/sec YDOT = -7595
221541 meter/sec
ZDOT = -2064
857629 ZDOT = -626
188043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2765896
78 X = -843045
34
Y = -13683458
07 feet Y = -4170718
02 meter
Z = -17387474
71 Z = -5299702
29
XDOT = 23906
925469 XDOT = 7286
830883
YDOT = -2240
780391 feet/sec YDOT = -682
989863 meter/sec
ZDOT = -2050
267979 ZDOT = -624
921680
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 14059
35879124
00016717 00000-0 10270-3 0 9140
2 25544 51
6482 279
0711 0003180 191
2487 168
8594 15
50797704 34440
Satellite: ISS
Catalog Number: 25544
Epoch time: 14059
35879124 = yrday
fracday
Element set: 914
Inclination: 51
6482 deg
RA of node: 279
0711 deg
Eccentricity:
0003180
Arg of perigee: 191
2487 deg
Mean anomaly: 168
8594 deg
Mean motion: 15
50797704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3444
Checksum: 334
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