[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 18th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
018/00:13:20
021 1
0 3
8 3
8
N/A 2
8 -0
4 228
9
000/00:08:40
041 -2
4 -0
1 220
7
Coasting Arc #1 (Orbit 2773)
---------------------------------------
Vector Time (GMT): 2014/016/03:02:39
929
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1145507
46 A = 6794248
80 meter
Y = -5576390
29 meter E =
0016256
Z = 3701704
08 I = 51
91213
XDOT = 6094
928485 Wp = 65
90077
YDOT = -1646
155599 meter/sec RA = 132
24751 deg
ZDOT = -4344
433851 TA = 70
26215
MA = 70
08688
Ha = 228
604 n
mi
Hp = 219
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3758226
58 X = 1189797
38
Y = -18295243
73 feet Y = -5563333
05 meter
Z = 12144698
42 Z = 3707375
98
XDOT = 19996
484531 XDOT = 6133
986683
YDOT = -5400
772963 feet/sec YDOT = -1577
779605 meter/sec
ZDOT = -14253
391900 ZDOT = -4314
731263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9627035
16 X = -2934320
32
Y = 15986190
85 feet Y = 4872590
97 meter
Z = 12169462
01 Z = 3709252
02
XDOT = -19565
447712 XDOT = -5963
548463
YDOT = -974
120592 feet/sec YDOT = -296
911956 meter/sec
ZDOT = -14127
834400 ZDOT = -4306
163925
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 14016
16703742
00016717 00000-0 10270-3 0 9009
2 25544 51
6503 133
0867 0006447 29
3056 330
8455 15
50446164 27740
Satellite: ISS
Catalog Number: 25544
Epoch time: 14016
16703742 = yrday
fracday
Element set: 900
Inclination: 51
6503 deg
RA of node: 133
0867 deg
Eccentricity:
0006447
Arg of perigee: 29
3056 deg
Mean anomaly: 330
8455 deg
Mean motion: 15
50446164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2774
Checksum: 293
Coasting Arc #2 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2014/017/03:02:39
929
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1118041
78 A = 6795230
96 meter
Y = 5802612
85 meter E =
0009925
Z = -3355754
57 I = 51
93625
XDOT = -5835
147685 Wp = 55
12819
YDOT = 1584
905525 meter/sec RA = 127
30950 deg
ZDOT = 4700
006049 TA = 266
02836
MA = 266
14183
Ha = 228
627 n
mi
Hp = 218
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3668116
06 X = -1166543
91
Y = 19037443
75 feet Y = 5789839
13 meter
Z = -11009693
49 Z = -3361303
36
XDOT = -19144
185319 XDOT = -5875
267475
YDOT = 5199
821277 feet/sec YDOT = 1519
428687 meter/sec
ZDOT = 15419
967353 ZDOT = 4671
562849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9509851
52 X = 2898602
74
Y = -16879181
55 feet Y = -5144774
54 meter
Z = -11033976
83 Z = -3363156
14
XDOT = 18661
295493 XDOT = 5687
962866
YDOT = 545
294128 feet/sec YDOT = 166
205650 meter/sec
ZDOT = 15299
719098 ZDOT = 4663
354381
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 14017
13385921
00016717 00000-0 10270-3 0 9013
2 25544 51
6509 128
2942 0006449 31
3468 328
8066 15
50462128 27897
Satellite: ISS
Catalog Number: 25544
Epoch time: 14017
13385921 = yrday
fracday
Element set: 901
Inclination: 51
6509 deg
RA of node: 128
2942 deg
Eccentricity:
0006449
Arg of perigee: 31
3468 deg
Mean anomaly: 328
8066 deg
Mean motion: 15
50462128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 314
Coasting Arc #3 (Orbit 2802)
---------------------------------------
Vector Time (GMT): 2014/018/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5099183
04 A = 6795730
46 meter
Y = -2250528
57 meter E =
0009431
Z = -3898573
22 I = 51
94550
XDOT = -318
053456 Wp = 63
41313
YDOT = 6431
906323 meter/sec RA = 122
98690 deg
ZDOT = -4132
568903 TA = 163
29703
MA = 163
26595
Ha = 228
898 n
mi
Hp = 220
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16729603
14 X = 5142907
64
Y = -7383623
92 feet Y = -2193261
69 meter
Z = -12790594
54 Z = -3873696
40
XDOT = -1043
482468 XDOT = -369
878507
YDOT = 21102
054867 feet/sec YDOT = 6428
059960 meter/sec
ZDOT = -13558
296926 ZDOT = -4134
239681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14974784
08 X = -4564314
19
Y = -10622439
64 feet Y = -3237719
60 meter
Z = -12685284
78 Z = -3866474
80
XDOT = 17818
033752 XDOT = 5430
936688
YDOT = -8932
093326 feet/sec YDOT = -2722
502046 meter/sec
ZDOT = -13566
315834 ZDOT = -4135
013066
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 14018
03622414
00016717 00000-0 10270-3 0 9025
2 25544 51
6493 123
8201 0003528 41
6134 318
5284 15
49771739 28031
Satellite: ISS
Catalog Number: 25544
Epoch time: 14018
03622414 = yrday
fracday
Element set: 902
Inclination: 51
6493 deg
RA of node: 123
8201 deg
Eccentricity:
0003528
Arg of perigee: 41
6134 deg
Mean anomaly: 318
5284 deg
Mean motion: 15
49771739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2803
Checksum: 290
Coasting Arc #4 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2014/019/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4880606
80 A = 6795152
71 meter
Y = 2403644
05 meter E =
0013064
Z = 4059913
67 I = 51
95932
XDOT = 30
179978 Wp = 88
71368
YDOT = -6585
852522 meter/sec RA = 118
05555 deg
ZDOT = 3924
792220 TA = 320
69696
MA = 320
79172
Ha = 229
052 n
mi
Hp = 220
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16012489
50 X = -4926843
56
Y = 7885971
28 feet Y = 2348807
45 meter
Z = 13319926
74 Z = 4036092
49
XDOT = 99
015677 XDOT = 84
757161
YDOT = -21607
127696 feet/sec YDOT = -6585
209884 meter/sec
ZDOT = 12876
614894 ZDOT = 3925
071368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15204329
67 X = 4634279
68
Y = 9491794
80 feet Y = 2893099
06 meter
Z = 13219039
38 Z = 4029163
20
XDOT = -17656
971400 XDOT = -5381
844883
YDOT = 10298
798756 feet/sec YDOT = 3139
073861 meter/sec
ZDOT = 12878
789143 ZDOT = 3925
454931
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 14019
06795355
00016717 00000-0 10270-3 0 9035
2 25544 51
6490 118
7111 0003547 45
1417 315
0021 15
49776591 28194
Satellite: ISS
Catalog Number: 25544
Epoch time: 14019
06795355 = yrday
fracday
Element set: 903
Inclination: 51
6490 deg
RA of node: 118
7111 deg
Eccentricity:
0003547
Arg of perigee: 45
1417 deg
Mean anomaly: 315
0021 deg
Mean motion: 15
49776591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2819
Checksum: 303
Coasting Arc #5 (Orbit 2833)
---------------------------------------
Vector Time (GMT): 2014/020/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4683291
45 A = 6794398
91 meter
Y = -2508984
06 meter E =
0011342
Z = -4247183
91 I = 51
97166
XDOT = 261
808460 Wp = 63
19700
YDOT = 6705
314636 meter/sec RA = 113
12455 deg
ZDOT = -3675
007857 TA = 169
24041
MA = 169
21612
Ha = 228
904 n
mi
Hp = 220
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15365129
43 X = 4731630
53
Y = -8231575
01 feet Y = -2456342
27 meter
Z = -13934330
40 Z = -4224316
05
XDOT = 858
951639 XDOT = 204
660407
YDOT = 21999
063767 feet/sec YDOT = 6707
922774 meter/sec
ZDOT = -12057
112393 ZDOT = -3673
874925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15305981
51 X = -4665263
16
Y = -8500806
60 feet Y = -2591045
85 meter
Z = -13837442
34 Z = -4217652
43
XDOT = 17341
808482 XDOT = 5285
783225
YDOT = -11618
261808 feet/sec YDOT = -3541
246199 meter/sec
ZDOT = -12053
351069 ZDOT = -3673
861406
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 14020
03518455
00016717 00000-0 10270-3 0 9049
2 25544 51
6497 113
9212 0003608 47
1843 312
9610 15
49819684 28341
Satellite: ISS
Catalog Number: 25544
Epoch time: 14020
03518455 = yrday
fracday
Element set: 904
Inclination: 51
6497 deg
RA of node: 113
9212 deg
Eccentricity:
0003608
Arg of perigee: 47
1843 deg
Mean anomaly: 312
9610 deg
Mean motion: 15
49819684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2834
Checksum: 304
Coasting Arc #6 (Orbit 2849)
---------------------------------------
Vector Time (GMT): 2014/021/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4471857
14 A = 6793807
91 meter
Y = 2595731
42 meter E =
0011865
Z = 4397139
17 I = 51
98060
XDOT = -580
459009 Wp = 93
87341
YDOT = -6830
564650 meter/sec RA = 108
19379 deg
ZDOT = 3433
171497 TA = 321
44474
MA = 321
52942
Ha = 229
072 n
mi
Hp = 220
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14671447
30 X = -4521910
44
Y = 8516179
19 feet Y = 2545444
47 meter
Z = 14426309
62 Z = 4375294
18
XDOT = -1904
393073 XDOT = -520
711999
YDOT = -22409
989009 feet/sec YDOT = -6836
721585 meter/sec
ZDOT = 11263
686014 ZDOT = 3430
496992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15301158
03 X = 4663792
97
Y = 7504277
21 feet Y = 2287303
69 meter
Z = 14333717
94 Z = 4368917
23
XDOT = -16953
783284 XDOT = -5167
513145
YDOT = 13018
569779 feet/sec YDOT = 3968
060069 meter/sec
ZDOT = 11253
444780 ZDOT = 3430
049969
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 14021
06688317
00016717 00000-0 10270-3 0 9059
2 25544 51
6493 108
8116 0003646 50
9676 309
1798 15
49823273 28503
Satellite: ISS
Catalog Number: 25544
Epoch time: 14021
06688317 = yrday
fracday
Element set: 905
Inclination: 51
6493 deg
RA of node: 108
8116 deg
Eccentricity:
0003646
Arg of perigee: 50
9676 deg
Mean anomaly: 309
1798 deg
Mean motion: 15
49823273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2850
Checksum: 326
Coasting Arc #7 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2014/022/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4291612
71 A = 6793071
07 meter
Y = -2640694
15 meter E =
0013250
Z = -4569045
77 I = 51
98779
XDOT = 900
828421 Wp = 65
03195
YDOT = 6912
628513 meter/sec RA = 103
26322 deg
ZDOT = -3150
766068 TA = 173
45997
MA = 173
44266
Ha = 228
887 n
mi
Hp = 220
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14080094
19 X = 4343017
32
Y = -8663694
73 feet Y = -2592415
27 meter
Z = -14990307
64 Z = -4548073
01
XDOT = 2955
473821 XDOT = 838
768173
YDOT = 22679
227405 feet/sec YDOT = 6922
355089 meter/sec
ZDOT = -10337
159017 ZDOT = -3146
540894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15212929
15 X = -4636900
81
Y = -6673345
83 feet Y = -2034035
81 meter
Z = -14901383
29 Z = -4541941
63
XDOT = 16391
925439 XDOT = 4996
258874
YDOT = -14335
490637 feet/sec YDOT = -4369
457546 meter/sec
ZDOT = -10320
394512 ZDOT = -3145
656247
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 14022
03408510
00016717 00000-0 10270-3 0 9063
2 25544 51
6497 104
0213 0003647 52
2518 307
8963 15
49866289 28653
Satellite: ISS
Catalog Number: 25544
Epoch time: 14022
03408510 = yrday
fracday
Element set: 906
Inclination: 51
6497 deg
RA of node: 104
0213 deg
Eccentricity:
0003647
Arg of perigee: 52
2518 deg
Mean anomaly: 307
8963 deg
Mean motion: 15
49866289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 310
Coasting Arc #8 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2014/023/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4104275
47 A = 6792497
72 meter
Y = 2665955
33 meter E =
0010465
Z = 4701925
49 I = 51
99200
XDOT = -1245
100723 Wp = 98
15625
YDOT = -6997
920924 meter/sec RA = 98
33254 deg
ZDOT = 2874
028757 TA = 323
39925
MA = 323
47070
Ha = 229
072 n
mi
Hp = 220
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13465470
71 X = -4156622
02
Y = 8746572
60 feet Y = 2619766
09 meter
Z = 15426264
74 Z = 4681860
46
XDOT = -4084
976125 XDOT = -1180
716878
YDOT = -22959
058150 feet/sec YDOT = -7011
484399 meter/sec
ZDOT = 9429
228205 ZDOT = 2868
136773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15034212
33 X = 4582427
92
Y = 5866203
03 feet Y = 1788018
68 meter
Z = 15341160
29 Z = 4675985
66
XDOT = -15751
113760 XDOT = -4800
939474
YDOT = 15711
332074 feet/sec YDOT = 4788
814016 meter/sec
ZDOT = 9405
452408 ZDOT = 2866
781894
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 14023
06575329
00016717 00000-0 10270-3 0 9071
2 25544 51
6496 98
9114 0003715 56
4698 303
6807 15
49868970 28812
Satellite: ISS
Catalog Number: 25544
Epoch time: 14023
06575329 = yrday
fracday
Element set: 907
Inclination: 51
6496 deg
RA of node: 98
9114 deg
Eccentricity:
0003715
Arg of perigee: 56
4698 deg
Mean anomaly: 303
6807 deg
Mean motion: 15
49868970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 347
Coasting Arc #9 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2014/024/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3956635
58 A = 6791816
67 meter
Y = -2658346
16 meter E =
0015032
Z = -4852372
89 I = 51
99384
XDOT = 1586
061891 Wp = 68
39262
YDOT = 7031
615639 meter/sec RA = 93
40167 deg
ZDOT = -2559
945402 TA = 176
47924
MA = 176
46865
Ha = 228
858 n
mi
Hp = 220
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12981087
87 X = 4009638
88
Y = -8721608
15 feet Y = -2613804
21 meter
Z = -15919858
57 Z = -4833023
46
XDOT = 5203
615128 XDOT = 1519
750239
YDOT = 23069
605116 feet/sec YDOT = 7048
981211 meter/sec
ZDOT = -8398
771003 ZDOT = -2552
401689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14824335
89 X = -4518457
58
Y = -5236522
18 feet Y = -1596091
96 meter
Z = -15837767
80 Z = -4827351
62
XDOT = 14927
111360 XDOT = 4549
783543
YDOT = -16958
813382 feet/sec YDOT = -5169
046319 meter/sec
ZDOT = -8368
040728 ZDOT = -2550
578814
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 14024
03292662
00016717 00000-0 10270-3 0 9086
2 25544 51
6498 94
1208 0003657 57
2611 302
8892 15
49911789 28963
Satellite: ISS
Catalog Number: 25544
Epoch time: 14024
03292662 = yrday
fracday
Element set: 908
Inclination: 51
6498 deg
RA of node: 94
1208 deg
Eccentricity:
0003657
Arg of perigee: 57
2611 deg
Mean anomaly: 302
8892 deg
Mean motion: 15
49911789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 333
Coasting Arc #10 (Orbit 2911)
---------------------------------------
Vector Time (GMT): 2014/025/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3808727
02 A = 6791305
07 meter
Y = 2631584
70 meter E =
0008952
Z = 4961913
10 I = 51
99334
XDOT = -1946
516661 Wp = 100
66975
YDOT = -7066
558422 meter/sec RA = 88
47074 deg
ZDOT = 2248
619489 TA = 327
44990
MA = 327
50507
Ha = 229
055 n
mi
Hp = 220
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12495823
54 X = -3861974
16
Y = 8633808
07 feet Y = 2588695
32 meter
Z = 16279242
44 Z = 4943281
62
XDOT = -6386
209518 XDOT = -1878
275171
YDOT = -23184
246790 feet/sec YDOT = -7087
944072 meter/sec
ZDOT = 7377
360529 ZDOT = 2239
329333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14546646
15 X = 4433817
75
Y = 4653096
57 feet Y = 1418263
84 meter
Z = 16200177
78 Z = 4937814
19
XDOT = -14026
276993 XDOT = -4275
209227
YDOT = 18239
070165 feet/sec YDOT = 5559
268586 meter/sec
ZDOT = 7339
276506 ZDOT = 2237
011479
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 14025
06456490
00016717 00000-0 10270-3 0 9092
2 25544 51
6500 89
0108 0003750 61
8375 298
3154 15
49912075 29129
Satellite: ISS
Catalog Number: 25544
Epoch time: 14025
06456490 = yrday
fracday
Element set: 909
Inclination: 51
6500 deg
RA of node: 89
0108 deg
Eccentricity:
0003750
Arg of perigee: 61
8375 deg
Mean anomaly: 298
3154 deg
Mean motion: 15
49912075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2912
Checksum: 305
Coasting Arc #11 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2014/026/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3706776
73 A = 6790718
99 meter
Y = -2583432
54 meter E =
0016566
Z = -5084527
15 I = 51
98968
XDOT = 2296
032252 Wp = 72
95307
YDOT = 7042
931157 meter/sec RA = 83
53891 deg
ZDOT = -1905
021906 TA = 178
62143
MA = 178
61686
Ha = 228
825 n
mi
Hp = 220
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12161340
98 X = 3760088
58
Y = -8475828
55 feet Y = -2541682
79 meter
Z = -16681519
53 Z = -5066390
85
XDOT = 7532
914212 XDOT = 2226
359898
YDOT = 23106
729517 feet/sec YDOT = 7068
217341 meter/sec
ZDOT = -6250
071871 ZDOT = -1894
037242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14293386
11 X = -4356624
09
Y = -4242548
53 feet Y = -1293128
79 meter
Z = -16604543
75 Z = -5061064
94
XDOT = 12947
403770 XDOT = 3946
368669
YDOT = -19341
207477 feet/sec YDOT = -5895
200039 meter/sec
ZDOT = -6204
842966 ZDOT = -1891
236136
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 14026
03171017
00016717 00000-0 10270-3 0 9101
2 25544 51
6497 84
2199 0003658 62
7874 297
3649 15
49955823 29274
Satellite: ISS
Catalog Number: 25544
Epoch time: 14026
03171017 = yrday
fracday
Element set: 910
Inclination: 51
6497 deg
RA of node: 84
2199 deg
Eccentricity:
0003658
Arg of perigee: 62
7874 deg
Mean anomaly: 297
3649 deg
Mean motion: 15
49955823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 339
Coasting Arc #12 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2014/027/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3610606
93 A = 6790317
39 meter
Y = 2518239
14 meter E =
0007503
Z = 5164076
68 I = 51
98427
XDOT = -2659
068560 Wp = 99
97983
YDOT = -7019
596812 meter/sec RA = 78
60718 deg
ZDOT = 1560
724938 TA = 335
02775
MA = 335
06403
Ha = 229
024 n
mi
Hp = 219
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11845823
25 X = -3663583
26
Y = 8261939
44 feet Y = 2477566
63 meter
Z = 16942508
78 Z = 5146408
45
XDOT = -8723
978215 XDOT = -2587
957656
YDOT = -23030
173268 feet/sec YDOT = -7048
934669 meter/sec
ZDOT = 5120
488641 ZDOT = 1547
980151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13999018
93 X = 4266900
97
Y = 3891828
88 feet Y = 1186229
44 meter
Z = 16867510
57 Z = 5141217
22
XDOT = -11803
718866 XDOT = -3597
773510
YDOT = 20448
341514 feet/sec YDOT = 6232
654494 meter/sec
ZDOT = 5067
835496 ZDOT = 1544
676259
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 14027
06331886
00016717 00000-0 10270-3 0 9118
2 25544 51
6500 79
1101 0003750 67
4880 292
6667 15
49952711 29436
Satellite: ISS
Catalog Number: 25544
Epoch time: 14027
06331886 = yrday
fracday
Element set: 911
Inclination: 51
6500 deg
RA of node: 79
1101 deg
Eccentricity:
0003750
Arg of perigee: 67
4880 deg
Mean anomaly: 292
6667 deg
Mean motion: 15
49952711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 308
Coasting Arc #13 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2014/028/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3563731
28 A = 6789867
73 meter
Y = -2444947
57 meter E =
0017729
Z = -5252424
94 I = 51
97508
XDOT = 3001
352348 Wp = 78
46056
YDOT = 6933
321798 meter/sec RA = 73
67359 deg
ZDOT = -1190
949294 TA = 180
13847
MA = 180
13896
Ha = 228
796 n
mi
Hp = 220
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11692031
75 X = 3616320
57
Y = -8021481
54 feet Y = -2404801
39 meter
Z = -17232365
30 Z = -5234985
47
XDOT = 9846
956523 XDOT = 2929
384491
YDOT = 22747
118759 feet/sec YDOT = 6966
482491 meter/sec
ZDOT = -3907
313956 ZDOT = -1176
543876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13782576
36 X = -4200929
28
Y = -3692460
07 feet Y = -1125461
83 meter
Z = -17158336
57 Z = -5229860
99
XDOT = 10504
292138 XDOT = 3201
708244
YDOT = -21328
505626 feet/sec YDOT = -6500
928515 meter/sec
ZDOT = -3847
642770 ZDOT = -1172
761516
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 14028
03043638
00016717 00000-0 10270-3 0 9122
2 25544 51
6489 74
3186 0003662 69
2831 290
8711 15
49997898 29581
Satellite: ISS
Catalog Number: 25544
Epoch time: 14028
03043638 = yrday
fracday
Element set: 912
Inclination: 51
6489 deg
RA of node: 74
3186 deg
Eccentricity:
0003662
Arg of perigee: 69
2831 deg
Mean anomaly: 290
8711 deg
Mean motion: 15
49997898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 347
Coasting Arc #14 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2014/029/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3527318
74 A = 6789620
89 meter
Y = 2358033
09 meter E =
0006416
Z = 5295171
64 I = 51
96476
XDOT = -3349
843673 Wp = 94
39056
YDOT = -6847
820451 meter/sec RA = 68
74011 deg
ZDOT = 816
666254 TA = 347
82924
MA = 347
84473
Ha = 228
981 n
mi
Hp = 219
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11572568
03 X = -3579146
35
Y = 7736329
04 feet Y = 2318298
39 meter
Z = 17372610
37 Z = 5277910
98
XDOT = -10990
300765 XDOT = -3276
987870
YDOT = -22466
602530 feet/sec YDOT = -6884
873211 meter/sec
ZDOT = 2679
351228 ZDOT = 800
570235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13552404
41 X = 4130772
86
Y = 3556365
36 feet Y = 1083980
16 meter
Z = 17299344
19 Z = 5272840
11
XDOT = -9162
759025 XDOT = -2792
808951
YDOT = 22187
435036 feet/sec YDOT = 6762
730199 meter/sec
ZDOT = 2612
531923 ZDOT = 796
299730
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 14029
06201539
00016717 00000-0 10270-3 0 9133
2 25544 51
6490 69
2086 0003726 73
8940 286
2621 15
49992181 29745
Satellite: ISS
Catalog Number: 25544
Epoch time: 14029
06201539 = yrday
fracday
Element set: 913
Inclination: 51
6490 deg
RA of node: 69
2086 deg
Eccentricity:
0003726
Arg of perigee: 73
8940 deg
Mean anomaly: 286
2621 deg
Mean motion: 15
49992181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 322
Coasting Arc #15 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2014/030/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3540127
33 A = 6789347
93 meter
Y = -2277207
80 meter E =
0018395
Z = -5342917
72 I = 51
95054
XDOT = 3666
457154 Wp = 84
66125
YDOT = 6698
538267 meter/sec RA = 63
80390 deg
ZDOT = -425
251594 TA = 181
28750
MA = 181
29224
Ha = 228
768 n
mi
Hp = 219
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11614590
97 X = 3591281
99
Y = -7471154
21 feet Y = -2237333
73 meter
Z = -17529257
61 Z = -5325596
50
XDOT = 12029
058905 XDOT = 3593
345789
YDOT = 21976
831585 feet/sec YDOT = 6739
130151 meter/sec
ZDOT = -1395
182395 ZDOT = -407
618375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13446087
52 X = -4098367
48
Y = -3534325
07 feet Y = -1077262
28 meter
Z = -17455744
54 Z = -5320510
94
XDOT = 7705
022736 XDOT = 2348
490930
YDOT = -22778
141577 feet/sec YDOT = -6942
777553 meter/sec
ZDOT = -1321
849430 ZDOT = -402
899706
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 14030
02910506
00016717 00000-0 10270-3 0 9143
2 25544 51
6474 64
4164 0003683 76
8357 283
3204 15
50038501 29898
Satellite: ISS
Catalog Number: 25544
Epoch time: 14030
02910506 = yrday
fracday
Element set: 914
Inclination: 51
6474 deg
RA of node: 64
4164 deg
Eccentricity:
0003683
Arg of perigee: 76
8357 deg
Mean anomaly: 283
3204 deg
Mean motion: 15
50038501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 295
Coasting Arc #16 (Orbit 3004)
---------------------------------------
Vector Time (GMT): 2014/031/00:17:40
041
Vector Time (MET): N/A
Weight (LBS) : 911249
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3566180
05 A = 6789294
08 meter
Y = 2187058
64 meter E =
0006097
Z = 5342069
48 I = 51
93595
XDOT = -3980
979741 Wp = 84
39201
YDOT = -6552
300458 meter/sec RA = 58
86776 deg
ZDOT = 25
522069 TA = 5
36901
MA = 5
36247
Ha = 228
932 n
mi
Hp = 219
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11700065
79 X = -3616320
54
Y = 7175389
24 feet Y = 2146899
04 meter
Z = 17526474
66 Z = 5324624
14
XDOT = -13060
957156 XDOT = -3907
538555
YDOT = -21497
048746 feet/sec YDOT = -6596
407684 meter/sec
ZDOT = 83
733822 ZDOT = 6
361999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13350317
48 X = 4069176
77
Y = 3568763
00 feet Y = 1087758
96 meter
Z = 17452450
21 Z = 5319506
82
XDOT = -6238
293008 XDOT = -1901
431709
YDOT = 23326
434071 feet/sec YDOT = 7109
897105 meter/sec
ZDOT = 3
930780 ZDOT = 1
198102
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 14031
06065393
00016717 00000-0 10270-3 0 9154
2 25544 51
6474 59
3058 0003707 81
2735 278
8836 15
50032195 30053
Satellite: ISS
Catalog Number: 25544
Epoch time: 14031
06065393 = yrday
fracday
Element set: 915
Inclination: 51
6474 deg
RA of node: 59
3058 deg
Eccentricity:
0003707
Arg of perigee: 81
2735 deg
Mean anomaly: 278
8836 deg
Mean motion: 15
50032195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3005
Checksum: 301
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