[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 26th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 31215 34 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 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
087/22:41:40
105 -1
4 3
3 3
3
N/A 2
8 -0
2 226
2
000/00:07:20
211 -1
0 -0
1 221
2
087/22:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
2
000/00:00:00
000 0
0 0
0 221
1
Coasting Arc #1 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2014/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4070863
87 A = 6788770
35 meter
Y = 2484176
75 meter E =
0011857
Z = -4842700
05 I = 51
76304
XDOT = -5710
725617 Wp = 54
30309
YDOT = 4423
893509 meter/sec RA = 158
24850 deg
ZDOT = -2528
811141 TA = 190
80822
MA = 190
83372
Ha = 225
981 n
mi
Hp = 220
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13355852
60 X = 4066306
87
Y = 8150186
18 feet Y = 2529673
87 meter
Z = -15888123
52 Z = -4822935
73
XDOT = -18735
976433 XDOT = -5747
486058
YDOT = 14514
086314 feet/sec YDOT = 4359
826763 meter/sec
ZDOT = -8296
624478 ZDOT = -2556
642571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13603627
05 X = 4146385
53
Y = 7898268
82 feet Y = 2407392
34 meter
Z = -15804919
58 Z = -4817339
49
XDOT = -17835
712595 XDOT = -5436
325199
YDOT = 13864
999639 feet/sec YDOT = 4226
051890 meter/sec
ZDOT = -8414
863999 ZDOT = -2564
850547
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 14083
52065586
00016717 00000-0 10270-3 0 9000
2 25544 51
6479 159
2138 0003658 339
4999 20
6005 15
50962556 38199
Satellite: ISS
Catalog Number: 25544
Epoch time: 14083
52065586 = yrday
fracday
Element set: 900
Inclination: 51
6479 deg
RA of node: 159
2138 deg
Eccentricity:
0003658
Arg of perigee: 339
4999 deg
Mean anomaly: 20
6005 deg
Mean motion: 15
50962556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3819
Checksum: 333
Coasting Arc #2 (Orbit 3834)
---------------------------------------
Vector Time (GMT): 2014/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3629128
91 A = 6787480
88 meter
Y = -2652900
53 meter E =
0003567
Z = 5082236
64 I = 51
78872
XDOT = 5884
649328 Wp = 82
95900
YDOT = -4563
844165 meter/sec RA = 153
29204 deg
ZDOT = 1819
146504 TA = 349
45876
MA = 349
46623
Ha = 226
065 n
mi
Hp = 219
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11906590
91 X = -3623881
54
Y = -8703741
88 feet Y = -2693453
95 meter
Z = 16674004
74 Z = 5064619
98
XDOT = 19306
592282 XDOT = 5926
409137
YDOT = -14973
242011 feet/sec YDOT = -4497
804577 meter/sec
ZDOT = 5968
328424 ZDOT = 1847
834951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12313855
31 X = -3753263
10
Y = -8267827
78 feet Y = -2520033
91 meter
Z = 16599893
22 Z = 5059647
45
XDOT = 18118
868391 XDOT = 5522
631085
YDOT = -14753
512552 feet/sec YDOT = -4496
870626 meter/sec
ZDOT = 6090
225726 ZDOT = 1856
300801
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 14084
55156240
00016717 00000-0 10270-3 0 9013
2 25544 51
6486 154
0988 0003740 344
0784 16
0249 15
51043554 38355
Satellite: ISS
Catalog Number: 25544
Epoch time: 14084
55156240 = yrday
fracday
Element set: 901
Inclination: 51
6486 deg
RA of node: 154
0988 deg
Eccentricity:
0003740
Arg of perigee: 344
0784 deg
Mean anomaly: 16
0249 deg
Mean motion: 15
51043554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3835
Checksum: 302
Coasting Arc #3 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2014/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3191456
22 A = 6786724
07 meter
Y = 2890860
64 meter E =
0014583
Z = -5258144
01 I = 51
81292
XDOT = -5974
613770 Wp = 66
73206
YDOT = 4663
482456 meter/sec RA = 148
33656 deg
ZDOT = -1059
121750 TA = 193
10761
MA = 193
14555
Ha = 226
093 n
mi
Hp = 219
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10470656
90 X = 3184434
93
Y = 9484450
93 feet Y = 2926509
70 meter
Z = -17251128
64 Z = -5242657
88
XDOT = -19601
751215 XDOT = -6021
173006
YDOT = 15300
139292 feet/sec YDOT = 4596
410046 meter/sec
ZDOT = -3474
808892 ZDOT = -1088
258943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11065266
14 X = 3372693
12
Y = 8910133
84 feet Y = 2715808
80 meter
Z = -17186049
71 Z = -5238307
95
XDOT = -18093
048020 XDOT = -5514
761036
YDOT = 15507
367610 feet/sec YDOT = 4726
645647 meter/sec
ZDOT = -3598
631189 ZDOT = -1096
862786
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 14085
51800982
00016717 00000-0 10270-3 0 9020
2 25544 51
6480 149
3039 0003832 349
3236 10
7833 15
51053552 38501
Satellite: ISS
Catalog Number: 25544
Epoch time: 14085
51800982 = yrday
fracday
Element set: 902
Inclination: 51
6480 deg
RA of node: 149
3039 deg
Eccentricity:
0003832
Arg of perigee: 349
3236 deg
Mean anomaly: 10
7833 deg
Mean motion: 15
51053552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3850
Checksum: 295
Coasting Arc #4 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2014/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2732311
98 A = 6786092
15 meter
Y = -3187613
05 meter E =
0003853
Z = 5329580
18 I = 51
83805
XDOT = 6024
604668 Wp = 32
25012
YDOT = -4732
829613 meter/sec RA = 143
38163 deg
ZDOT = 261
022175 TA = 55
28597
MA = 55
24968
Ha = 226
134 n
mi
Hp = 219
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8964278
14 X = -2722353
49
Y = -10458048
06 feet Y = -3218111
14 meter
Z = 17485499
27 Z = 5316331
70
XDOT = 19765
763346 XDOT = 6075
812521
YDOT = -15527
656212 feet/sec YDOT = -4665
172265 meter/sec
ZDOT = 856
371965 ZDOT = 290
413627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9783936
32 X = -2982143
79
Y = -9795116
72 feet Y = -2985551
57 meter
Z = 17429917
25 Z = 5312638
78
XDOT = 17909
104657 XDOT = 5458
695099
YDOT = -16160
601718 feet/sec YDOT = -4925
751404 meter/sec
ZDOT = 981
291262 ZDOT = 299
097577
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 14086
54885353
00016717 00000-0 10270-3 0 9030
2 25544 51
6484 144
1890 0003893 353
8375 6
2728 15
51138561 38668
Satellite: ISS
Catalog Number: 25544
Epoch time: 14086
54885353 = yrday
fracday
Element set: 903
Inclination: 51
6484 deg
RA of node: 144
1890 deg
Eccentricity:
0003893
Arg of perigee: 353
8375 deg
Mean anomaly: 6
2728 deg
Mean motion: 15
51138561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3866
Checksum: 332
Coasting Arc #5 (Orbit 3880)
---------------------------------------
Vector Time (GMT): 2014/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2309130
52 A = 6786136
40 meter
Y = 3538234
51 meter E =
0014916
Z = -5322809
88 I = 51
86230
XDOT = -5988
873727 Wp = 78
80463
YDOT = 4732
690889 meter/sec RA = 138
42747 deg
ZDOT = 552
012222 TA = 196
43292
MA = 196
48132
Ha = 226
197 n
mi
Hp = 219
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7575887
52 X = 2295249
95
Y = 11608380
93 feet Y = 3563978
30 meter
Z = -17463287
00 Z = -5311626
73
XDOT = -19648
535849 XDOT = -6044
032123
YDOT = 15527
201080 feet/sec YDOT = 4665
411132 meter/sec
ZDOT = 1811
063721 ZDOT = 522
784595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8668103
06 X = 2642037
81
Y = 10892430
32 feet Y = 3320012
76 meter
Z = -17416484
24 Z = -5308544
40
XDOT = -17435
944654 XDOT = -5314
475930
YDOT = 16550
813384 feet/sec YDOT = 5044
687920 meter/sec
ZDOT = 1686
825780 ZDOT = 514
144498
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 14087
51524220
00016717 00000-0 10270-3 0 9042
2 25544 51
6481 139
3933 0004005 359
0643 1
0500 15
51147164 38818
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
51524220 = yrday
fracday
Element set: 904
Inclination: 51
6481 deg
RA of node: 139
3933 deg
Eccentricity:
0004005
Arg of perigee: 359
0643 deg
Mean anomaly: 1
0500 deg
Mean motion: 15
51147164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3881
Checksum: 274
Coasting Arc #6 (Orbit 3887)
---------------------------------------
Vector Time (GMT): 2014/087/22:45:20
211
Vector Time (MET): N/A
Weight (LBS) : 900591
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3749823
79 A = 6788113
37 meter
Y = 2120836
70 meter E =
0012831
Z = -5256845
36 I = 51
87489
XDOT = -4838
088045 Wp = 66
02648
YDOT = 5827
830472 meter/sec RA = 136
22479 deg
ZDOT = -1096
959654 TA = 193
45846
MA = 193
49271
Ha = 226
217 n
mi
Hp = 221
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12302571
49 X = 3751365
42
Y = 6958125
65 feet Y = 2162777
47 meter
Z = -17246867
99 Z = -5238625
87
XDOT = -15872
992275 XDOT = -4897
567918
YDOT = 19120
178714 feet/sec YDOT = 5773
395132 meter/sec
ZDOT = -3598
948995 ZDOT = -1120
607675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10490377
70 X = -3197467
12
Y = -9610531
07 feet Y = -2929289
87 meter
Z = -17170116
52 Z = -5233451
52
XDOT = 19101
918495 XDOT = 5822
264757
YDOT = -14223
335602 feet/sec YDOT = -4335
272691 meter/sec
ZDOT = -3699
748521 ZDOT = -1127
683349
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 14087
96621635
00016717 00000-0 10270-3 0 9050
2 25544 51
6492 137
1556 0003915 323
5029 36
5855 15
50585234 38886
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
96621635 = yrday
fracday
Element set: 905
Inclination: 51
6492 deg
RA of node: 137
1556 deg
Eccentricity:
0003915
Arg of perigee: 323
5029 deg
Mean anomaly: 36
5855 deg
Mean motion: 15
50585234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3888
Checksum: 330
Coasting Arc #7 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2014/088/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3310764
34 A = 6787589
46 meter
Y = -2573096
12 meter E =
0002773
Z = 5337173
61 I = 51
89508
XDOT = 4919
918946 Wp = 6
79944
YDOT = -5871
476183 meter/sec RA = 131
27439 deg
ZDOT = 223
913721 TA = 81
08829
MA = 81
05690
Ha = 226
324 n
mi
Hp = 220
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10862087
72 X = -3307671
66
Y = -8441916
41 feet Y = -2610101
11 meter
Z = 17510412
11 Z = 5321098
26
XDOT = 16141
466358 XDOT = 4984
121753
YDOT = -19263
373304 feet/sec YDOT = -5816
099479 meter/sec
ZDOT = 734
625070 ZDOT = 247
970874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8964219
03 X = 2732293
96
Y = 10547858
48 feet Y = 3214987
27 meter
Z = 17442789
15 Z = 5316562
13
XDOT = -19038
315873 XDOT = -5802
878678
YDOT = 14810
054602 feet/sec YDOT = 4514
104643 meter/sec
ZDOT = 837
172584 ZDOT = 255
170204
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 14088
99740194
00016717 00000-0 10270-3 0 9067
2 25544 51
6490 132
0426 0003902 326
9741 33
1166 15
50623839 39049
Satellite: ISS
Catalog Number: 25544
Epoch time: 14088
99740194 = yrday
fracday
Element set: 906
Inclination: 51
6490 deg
RA of node: 132
0426 deg
Eccentricity:
0003902
Arg of perigee: 326
9741 deg
Mean anomaly: 33
1166 deg
Mean motion: 15
50623839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 310
Coasting Arc #8 (Orbit 3918)
---------------------------------------
Vector Time (GMT): 2014/089/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3106923
53 A = 6787474
76 meter
Y = 2835974
68 meter E =
0013101
Z = -5337639
39 I = 51
91415
XDOT = -4774
253406 Wp = 78
11288
YDOT = 5968
899125 meter/sec RA = 126
32871 deg
ZDOT = 395
829331 TA = 195
63437
MA = 195
67487
Ha = 226
284 n
mi
Hp = 220
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10193318
65 X = 3100908
81
Y = 9304378
87 feet Y = 2870683
88 meter
Z = -17511940
26 Z = -5322561
33
XDOT = -15663
561043 XDOT = -4842
566972
YDOT = 19583
002380 feet/sec YDOT = 5915
128455 meter/sec
ZDOT = 1298
652660 ZDOT = 372
469728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8322267
03 X = -2536626
99
Y = -11109925
51 feet Y = -3386305
29 meter
Z = -17448572
72 Z = -5318324
96
XDOT = 18333
376930 XDOT = 5588
013288
YDOT = -15598
543091 feet/sec YDOT = -4754
435934 meter/sec
ZDOT = 1199
027398 ZDOT = 365
463551
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 14089
96410989
00016717 00000-0 10270-3 0 9072
2 25544 51
6482 127
2484 0004001 330
7539 29
3387 15
50673981 39190
Satellite: ISS
Catalog Number: 25544
Epoch time: 14089
96410989 = yrday
fracday
Element set: 907
Inclination: 51
6482 deg
RA of node: 127
2484 deg
Eccentricity:
0004001
Arg of perigee: 330
7539 deg
Mean anomaly: 29
3387 deg
Mean motion: 15
50673981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3919
Checksum: 336
Coasting Arc #9 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2014/090/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2908399
86 A = 6787622
20 meter
Y = -3147617
93 meter E =
0005684
Z = 5263278
88 I = 51
93272
XDOT = 4625
928526 Wp = 13
66144
YDOT = -6020
844649 meter/sec RA = 121
38437 deg
ZDOT = -1038
851736 TA = 86
28591
MA = 86
22092
Ha = 226
344 n
mi
Hp = 220
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9541994
28 X = -2898553
89
Y = -10326830
48 feet Y = -3180085
76 meter
Z = 17267975
32 Z = 5249174
48
XDOT = 15176
930858 XDOT = 4697
957614
YDOT = -19753
427326 feet/sec YDOT = -5968
711949 meter/sec
ZDOT = -3408
306222 ZDOT = -1016
203650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7690157
68 X = 2343960
06
Y = 11857304
93 feet Y = 3614106
54 meter
Z = 17208772
43 Z = 5245233
84
XDOT = -17561
111280 XDOT = -5352
626718
YDOT = 16222
487994 feet/sec YDOT = 4944
614341 meter/sec
ZDOT = -3311
666300 ZDOT = -1009
395888
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 14090
99523396
00016717 00000-0 10270-3 0 9085
2 25544 51
6482 122
1349 0003997 334
1540 25
9411 15
50721910 39351
Satellite: ISS
Catalog Number: 25544
Epoch time: 14090
99523396 = yrday
fracday
Element set: 908
Inclination: 51
6482 deg
RA of node: 122
1349 deg
Eccentricity:
0003997
Arg of perigee: 334
1540 deg
Mean anomaly: 25
9411 deg
Mean motion: 15
50721910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 310
Coasting Arc #10 (Orbit 3949)
---------------------------------------
Vector Time (GMT): 2014/091/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2764334
80 A = 6788068
92 meter
Y = 3479013
77 meter E =
0011639
Z = -5141361
84 I = 51
94892
XDOT = -4447
264089 Wp = 86
05117
YDOT = 6001
098292 meter/sec RA = 116
44010 deg
ZDOT = 1673
671985 TA = 200
04679
MA = 200
09255
Ha = 226
338 n
mi
Hp = 220
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9069339
90 X = 2750201
59
Y = 11414087
18 feet Y = 3509846
72 meter
Z = -16867985
05 Z = -5127967
68
XDOT = -14590
761446 XDOT = -4522
169443
YDOT = 19688
642690 feet/sec YDOT = 5950
947506 meter/sec
ZDOT = 5491
049821 ZDOT = 1651
884927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7251650
83 X = -2210303
17
Y = -12721592
36 feet Y = -3877541
35 meter
Z = -16811837
50 Z = -5124248
07
XDOT = 16630
540314 XDOT = 5068
988688
YDOT = -16595
889427 feet/sec YDOT = -5058
427097 meter/sec
ZDOT = 5398
036100 ZDOT = 1645
321403
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 14091
96188456
00016717 00000-0 10270-3 0 9098
2 25544 51
6471 117
3398 0004033 337
8157 22
2819 15
50761174 39500
Satellite: ISS
Catalog Number: 25544
Epoch time: 14091
96188456 = yrday
fracday
Element set: 909
Inclination: 51
6471 deg
RA of node: 117
3398 deg
Eccentricity:
0004033
Arg of perigee: 337
8157 deg
Mean anomaly: 22
2819 deg
Mean motion: 15
50761174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3950
Checksum: 322
Coasting Arc #11 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2014/092/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2632116
56 A = 6788749
13 meter
Y = -3848263
24 meter E =
0008477
Z = 4933439
50 I = 51
96508
XDOT = 4282
104888 Wp = 30
80278
YDOT = -5916
352354 meter/sec RA = 111
49800 deg
ZDOT = -2321
510641 TA = 81
86474
MA = 81
76858
Ha = 226
348 n
mi
Hp = 220
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8635553
02 X = -2612854
11
Y = -12625535
57 feet Y = -3877589
08 meter
Z = 16185825
12 Z = 4920700
07
XDOT = 14048
900550 XDOT = 4359
221892
YDOT = -19410
604836 feet/sec YDOT = -5868
036147 meter/sec
ZDOT = -7616
504729 ZDOT = -2300
520674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6864514
91 X = 2092304
15
Y = 13732391
08 feet Y = 4185632
80 meter
Z = 16132505
38 Z = 4917187
64
XDOT = -15697
148081 XDOT = -4784
490735
YDOT = 16723
248717 feet/sec YDOT = 5097
246209 meter/sec
ZDOT = -7526
855794 ZDOT = -2294
185646
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 14092
99294654
00016717 00000-0 10270-3 0 9102
2 25544 51
6475 112
2259 0004050 340
8493 19
2505 15
50819235 39667
Satellite: ISS
Catalog Number: 25544
Epoch time: 14092
99294654 = yrday
fracday
Element set: 910
Inclination: 51
6475 deg
RA of node: 112
2259 deg
Eccentricity:
0004050
Arg of perigee: 340
8493 deg
Mean anomaly: 19
2505 deg
Mean motion: 15
50819235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 313
Coasting Arc #12 (Orbit 3980)
---------------------------------------
Vector Time (GMT): 2014/093/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2562771
36 A = 6789715
36 meter
Y = 4211120
75 meter E =
0008834
Z = -4676392
17 I = 51
97798
XDOT = -4106
869416 Wp = 88
01285
YDOT = 5755
382020 meter/sec RA = 106
55602 deg
ZDOT = 2937
178565 TA = 211
10346
MA = 211
15579
Ha = 226
374 n
mi
Hp = 220
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8408042
52 X = 2538207
81
Y = 13816012
95 feet Y = 4239641
59 meter
Z = -15342493
98 Z = -4664002
47
XDOT = -13473
981025 XDOT = -4185
190164
YDOT = 18882
486942 feet/sec YDOT = 5709
018688 meter/sec
ZDOT = 9636
412616 ZDOT = 2917
037099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6720755
43 X = -2048486
25
Y = -14764656
22 feet Y = -4500267
22 meter
Z = -15290712
46 Z = -4660609
16
XDOT = 14699
600551 XDOT = 4480
438248
YDOT = -16564
454462 feet/sec YDOT = -5048
845720 meter/sec
ZDOT = 9550
358091 ZDOT = 2910
949146
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 14093
95953910
00016717 00000-0 10270-3 0 9117
2 25544 51
6463 107
4303 0003987 345
0464 15
0568 15
50849807 39811
Satellite: ISS
Catalog Number: 25544
Epoch time: 14093
95953910 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 107
4303 deg
Eccentricity:
0003987
Arg of perigee: 345
0464 deg
Mean anomaly: 15
0568 deg
Mean motion: 15
50849807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3981
Checksum: 322
Coasting Arc #13 (Orbit 3996)
---------------------------------------
Vector Time (GMT): 2014/094/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2505746
03 A = 6790839
92 meter
Y = -4594699
21 meter E =
0010884
Z = 4324302
87 I = 51
99089
XDOT = 3965
341934 Wp = 50
94530
YDOT = -5514
568267 meter/sec RA = 101
61668 deg
ZDOT = -3548
996207 TA = 75
11298
MA = 74
99247
Ha = 226
335 n
mi
Hp = 219
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8220951
54 X = -2475187
05
Y = -15074472
48 feet Y = -4622548
91 meter
Z = 14187345
38 Z = 4312204
78
XDOT = 13009
652015 XDOT = 4043
952366
YDOT = -18092
415575 feet/sec YDOT = -5469
785981 meter/sec
ZDOT = -11643
688344 ZDOT = -3529
541684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6645606
25 X = 2025580
78
Y = 15877330
72 feet Y = 4839410
40 meter
Z = 14136860
34 Z = 4308915
03
XDOT = -13788
927277 XDOT = -4202
865034
YDOT = 16101
866617 feet/sec YDOT = 4907
848945 meter/sec
ZDOT = -11560
558881 ZDOT = -3523
658347
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 14094
99053784
00016717 00000-0 10270-3 0 9123
2 25544 51
6469 102
3162 0004031 347
4367 12
6683 15
50916343 39971
Satellite: ISS
Catalog Number: 25544
Epoch time: 14094
99053784 = yrday
fracday
Element set: 912
Inclination: 51
6469 deg
RA of node: 102
3162 deg
Eccentricity:
0004031
Arg of perigee: 347
4367 deg
Mean anomaly: 12
6683 deg
Mean motion: 15
50916343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3997
Checksum: 318
Coasting Arc #14 (Orbit 4011)
---------------------------------------
Vector Time (GMT): 2014/095/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2510428
18 A = 6792147
06 meter
Y = 4943213
69 meter E =
0006113
Z = -3927059
71 I = 51
99959
XDOT = -3837
731769 Wp = 70
46374
YDOT = 5203
815240 meter/sec RA = 96
67752 deg
ZDOT = 4104
191490 TA = 242
35456
MA = 242
41663
Ha = 226
384 n
mi
Hp = 219
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8236312
94 X = 2474041
95
Y = 16217892
68 feet Y = 4971083
19 meter
Z = -12884054
17 Z = -3914953
07
XDOT = -12590
983495 XDOT = -3915
573703
YDOT = 17072
884647 feet/sec YDOT = 5160
464303 meter/sec
ZDOT = 13465
195177 ZDOT = 4085
358825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6821886
49 X = -2079311
00
Y = -16900193
50 feet Y = -5151178
98 meter
Z = -12833591
46 Z = -3911678
68
XDOT = 12929
374729 XDOT = 3940
873417
YDOT = -15365
119677 feet/sec YDOT = -4683
288478 meter/sec
ZDOT = 13384
728872 ZDOT = 4079
665360
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 14095
95707101
00016717 00000-0 10270-3 0 9130
2 25544 51
6456 97
5203 0003866 352
6998 7
4096 15
50942071 40127
Satellite: ISS
Catalog Number: 25544
Epoch time: 14095
95707101 = yrday
fracday
Element set: 913
Inclination: 51
6456 deg
RA of node: 97
5203 deg
Eccentricity:
0003866
Arg of perigee: 352
6998 deg
Mean anomaly: 7
4096 deg
Mean motion: 15
50942071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4012
Checksum: 311
Coasting Arc #15 (Orbit 4027)
---------------------------------------
Vector Time (GMT): 2014/096/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2519442
18 A = 6793467
04 meter
Y = -5291071
14 meter E =
0012629
Z = 3429981
10 I = 52
00790
XDOT = 3765
132097 Wp = 71
93434
YDOT = -4806
658281 meter/sec RA = 91
74104 deg
ZDOT = -4631
322130 TA = 68
20280
MA = 68
06847
Ha = 226
302 n
mi
Hp = 219
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8265886
41 X = -2476750
76
Y = -17359157
29 feet Y = -5319006
21 meter
Z = 11253218
83 Z = 3417846
07
XDOT = 12352
795594 XDOT = 3841
098924
YDOT = -15769
876250 feet/sec YDOT = -4764
129746 meter/sec
ZDOT = -15194
626410 ZDOT = -4612
846739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7047634
59 X = 2148119
02
Y = 17920117
87 feet Y = 5462051
93 meter
Z = 11202695
05 Z = 3414581
45
XDOT = -12258
252008 XDOT = -3736
315212
YDOT = 14307
103817 feet/sec YDOT = 4360
805243 meter/sec
ZDOT = -15115
720300 ZDOT = -4607
271547
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 14096
98800473
00016717 00000-0 10270-3 0 9141
2 25544 51
6462 92
4057 0003943 354
3938 5
7169 15
51016873 40286
Satellite: ISS
Catalog Number: 25544
Epoch time: 14096
98800473 = yrday
fracday
Element set: 914
Inclination: 51
6462 deg
RA of node: 92
4057 deg
Eccentricity:
0003943
Arg of perigee: 354
3938 deg
Mean anomaly: 5
7169 deg
Mean motion: 15
51016873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4028
Checksum: 321
Coasting Arc #16 (Orbit 4042)
---------------------------------------
Vector Time (GMT): 2014/097/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2578190
25 A = 6794814
59 meter
Y = 5576703
08 meter E =
0007125
Z = -2898127
55 I = 52
01151
XDOT = -3729
432453 Wp = 36
16756
YDOT = 4357
457365 meter/sec RA = 86
80459 deg
ZDOT = 5079
022806 TA = 291
05916
MA = 291
13534
Ha = 226
372 n
mi
Hp = 219
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8458629
43 X = 2529716
87
Y = 18296269
95 feet Y = 5605262
79 meter
Z = -9508292
48 Z = -2885721
25
XDOT = -12235
670777 XDOT = -3802
553628
YDOT = 14296
119965 feet/sec YDOT = 4315
344036 meter/sec
ZDOT = 16663
460651 ZDOT = 5060
727768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7484094
56 X = -2281152
02
Y = -18742177
82 feet Y = -5712615
80 meter
Z = -9456671
23 Z = -2882393
39
XDOT = 11751
393551 XDOT = 3581
824754
YDOT = -13041
099716 feet/sec YDOT = -3974
927194 meter/sec
ZDOT = 16585
377424 ZDOT = 5055
223039
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 14097
95447666
00016717 00000-0 10270-3 0 9151
2 25544 51
6450 87
6094 0003703 1
0411 359
0748 15
51038050 40432
Satellite: ISS
Catalog Number: 25544
Epoch time: 14097
95447666 = yrday
fracday
Element set: 915
Inclination: 51
6450 deg
RA of node: 87
6094 deg
Eccentricity:
0003703
Arg of perigee: 1
0411 deg
Mean anomaly: 359
0748 deg
Mean motion: 15
51038050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4043
Checksum: 297
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