[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 4th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16684 06 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
345/16:37:50
560 1
9 3
1 3
1
N/A -2
5 -0
3 226
4
000/00:07:41
121 0
4 0
2 221
2
347/15:02:13
519 1
5 3
4 3
4
N/A -3
0 -0
3 226
4
000/00:08:27
037 0
4 0
2 223
1
Coasting Arc #1 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2013/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5344226
57 A = 6792856
16 meter
Y = 1643945
27 meter E =
0012452
Z = 3848116
08 I = 51
55198
XDOT = -4432
014527 Wp = 97
88637
YDOT = 4690
959447 meter/sec RA = 343
97671 deg
ZDOT = 4137
955122 TA = 308
49061
MA = 308
60223
Ha = 226
694 n
mi
Hp = 219
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17533551
74 X = 5306753
15
Y = 5393521
23 feet Y = 1703497
88 meter
Z = 12625052
77 Z = 3873987
23
XDOT = -14540
730075 XDOT = -4504
241713
YDOT = 15390
286898 feet/sec YDOT = 4640
993559 meter/sec
ZDOT = 13575
968249 ZDOT = 4116
249661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10355805
48 X = -3156449
51
Y = 15050620
58 feet Y = 4587429
15 meter
Z = 12733561
10 Z = 3881189
42
XDOT = -9230
380217 XDOT = -2813
419890
YDOT = -17795
344180 feet/sec YDOT = -5424
020906 meter/sec
ZDOT = 13483
852753 ZDOT = 4109
878319
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 13338
55606965
00016717 00000-0 10270-3 0 9007
2 25544 51
6480 344
2194 0001219 95
4216 264
7074 15
50731780 21137
Satellite: ISS
Catalog Number: 25544
Epoch time: 13338
55606965 = yrday
fracday
Element set: 900
Inclination: 51
6480 deg
RA of node: 344
2194 deg
Eccentricity:
0001219
Arg of perigee: 95
4216 deg
Mean anomaly: 264
7074 deg
Mean motion: 15
50731780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 298
Coasting Arc #2 (Orbit 2127)
---------------------------------------
Vector Time (GMT): 2013/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5035380
55 A = 6791462
43 meter
Y = -1682250
25 meter E =
0009337
Z = -4244984
10 I = 51
51809
XDOT = 4670
518029 Wp = 72
94991
YDOT = -4869
413435 meter/sec RA = 339
00852 deg
ZDOT = -3614
364550 TA = 159
96792
MA = 159
93125
Ha = 226
737 n
mi
Hp = 219
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16520277
39 X = -4995573
96
Y = -5519193
74 feet Y = -1738336
11 meter
Z = -13927113
18 Z = -4269349
08
XDOT = 15323
221881 XDOT = 4742
179427
YDOT = -15975
765862 feet/sec YDOT = -4816
783704 meter/sec
ZDOT = -11858
151411 ZDOT = -3591
501914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9928195
31 X = 3026113
93
Y = -14211111
65 feet Y = -4331546
83 meter
Z = -14029283
28 Z = -4276125
55
XDOT = 9953
244903 XDOT = 3033
749046
YDOT = 18551
597228 feet/sec YDOT = 5654
526835 meter/sec
ZDOT = -11761
138805 ZDOT = -3584
795108
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 13339
52270547
00016717 00000-0 10270-3 0 9019
2 25544 51
6480 339
4250 0001208 98
6552 261
4736 15
50749365 21285
Satellite: ISS
Catalog Number: 25544
Epoch time: 13339
52270547 = yrday
fracday
Element set: 901
Inclination: 51
6480 deg
RA of node: 339
4250 deg
Eccentricity:
0001208
Arg of perigee: 98
6552 deg
Mean anomaly: 261
4736 deg
Mean motion: 15
50749365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2128
Checksum: 308
Coasting Arc #3 (Orbit 2143)
---------------------------------------
Vector Time (GMT): 2013/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4708781
53 A = 6790179
01 meter
Y = 1746993
04 meter E =
0009606
Z = 4563764
89 I = 51
48509
XDOT = -4859
878220 Wp = 111
75118
YDOT = 5077
013113 meter/sec RA = 334
03732 deg
ZDOT = 3062
159834 TA = 307
50843
MA = 307
59572
Ha = 226
573 n
mi
Hp = 219
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15448758
29 X = 4666726
76
Y = 5731604
46 feet Y = 1799414
14 meter
Z = 14972981
93 Z = 4586537
72
XDOT = -15944
482350 XDOT = -4931
164451
YDOT = 16656
867169 feet/sec YDOT = 5022
268040 meter/sec
ZDOT = 10046
456148 ZDOT = 3038
378220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9601159
83 X = -2926433
52
Y = 13284022
16 feet Y = 4048969
96 meter
Z = 15068447
02 Z = 4592862
65
XDOT = -10845
511958 XDOT = -3305
712045
YDOT = -19152
324494 feet/sec YDOT = -5837
628506 meter/sec
ZDOT = 9945
546197 ZDOT = 3031
402481
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 13340
55377062
00016717 00000-0 10270-3 0 9025
2 25544 51
6476 334
3113 0001130 98
5354 261
5925 15
50773834 21442
Satellite: ISS
Catalog Number: 25544
Epoch time: 13340
55377062 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 334
3113 deg
Eccentricity:
0001130
Arg of perigee: 98
5354 deg
Mean anomaly: 261
5925 deg
Mean motion: 15
50773834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2144
Checksum: 291
Coasting Arc #4 (Orbit 2158)
---------------------------------------
Vector Time (GMT): 2013/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4367800
81 A = 6789030
81 meter
Y = -1890519
73 meter E =
0012902
Z = -4853532
14 I = 51
45394
XDOT = 4990
682672 Wp = 74
78532
YDOT = -5261
482871 meter/sec RA = 329
06255 deg
ZDOT = -2443
939234 TA = 171
12606
MA = 171
10323
Ha = 226
685 n
mi
Hp = 219
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14330055
16 X = -4322758
85
Y = -6202492
54 feet Y = -1939111
13 meter
Z = -15923661
87 Z = -4874641
21
XDOT = 16373
630813 XDOT = 5061
018803
YDOT = -17262
082911 feet/sec YDOT = -5205
280466 meter/sec
ZDOT = -8018
173339 ZDOT = -2419
524428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9547744
31 X = 2910152
46
Y = -12240810
33 feet Y = -3730998
99 meter
Z = -16012106
14 Z = -4880489
95
XDOT = 11743
788134 XDOT = 3579
506623
YDOT = 19503
946707 feet/sec YDOT = 5944
802956 meter/sec
ZDOT = -7914
574992 ZDOT = -2412
362457
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 13341
52038168
00016717 00000-0 10270-3 0 9035
2 25544 51
6475 329
5169 0001203 100
9569 259
1718 15
50785942 21597
Satellite: ISS
Catalog Number: 25544
Epoch time: 13341
52038168 = yrday
fracday
Element set: 903
Inclination: 51
6475 deg
RA of node: 329
5169 deg
Eccentricity:
0001203
Arg of perigee: 100
9569 deg
Mean anomaly: 259
1718 deg
Mean motion: 15
50785942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2159
Checksum: 316
Coasting Arc #5 (Orbit 2174)
---------------------------------------
Vector Time (GMT): 2013/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4023209
00 A = 6788061
17 meter
Y = 2066943
87 meter E =
0006341
Z = 5057677
61 I = 51
42464
XDOT = -5076
477874 Wp = 120
33151
YDOT = 5453
805319 meter/sec RA = 324
08541 deg
ZDOT = 1804
497400 TA = 312
11891
MA = 312
17279
Ha = 226
486 n
mi
Hp = 219
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13199504
60 X = 3975228
13
Y = 6781311
91 feet Y = 2111665
47 meter
Z = 16593430
47 Z = 5077105
54
XDOT = -16655
111135 XDOT = -5145
851998
YDOT = 17893
062069 feet/sec YDOT = 5396
648940 meter/sec
ZDOT = 5920
267062 ZDOT = 1779
668047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9635629
17 X = -2936939
77
Y = 11165195
57 feet Y = 3403151
61 meter
Z = 16674774
54 Z = 5082471
28
XDOT = -12719
154810 XDOT = -3876
798386
YDOT = -19684
604106 feet/sec YDOT = -5999
867331 meter/sec
ZDOT = 5814
900456 ZDOT = 1772
381659
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 13342
55141990
00016717 00000-0 10270-3 0 9048
2 25544 51
6472 324
4033 0001075 100
7808 259
3464 15
50811588 21753
Satellite: ISS
Catalog Number: 25544
Epoch time: 13342
55141990 = yrday
fracday
Element set: 904
Inclination: 51
6472 deg
RA of node: 324
4033 deg
Eccentricity:
0001075
Arg of perigee: 100
7808 deg
Mean anomaly: 259
3464 deg
Mean motion: 15
50811588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2175
Checksum: 295
Coasting Arc #6 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2013/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3689603
56 A = 6787385
99 meter
Y = -2315974
47 meter E =
0015318
Z = -5218490
75 I = 51
39800
XDOT = 5096
048977 Wp = 82
89591
YDOT = -5596
681784 meter/sec RA = 319
10479 deg
ZDOT = -1120
201340 TA = 176
31257
MA = 176
30127
Ha = 226
611 n
mi
Hp = 219
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12104998
56 X = -3638081
52
Y = -7598341
42 feet Y = -2356945
71 meter
Z = -17121032
63 Z = -5236289
49
XDOT = 16719
320792 XDOT = 5163
695211
YDOT = -18361
816875 feet/sec YDOT = -5539
316248 meter/sec
ZDOT = -3675
201246 ZDOT = -1095
281008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10003820
04 X = 3049164
35
Y = -10081394
55 feet Y = -3072809
06 meter
Z = -17195482
24 Z = -5241182
99
XDOT = 13593
651566 XDOT = 4143
344997
YDOT = 19571
834256 feet/sec YDOT = 5965
495081 meter/sec
ZDOT = -3569
436342 ZDOT = -1087
964197
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 13343
51800549
00016717 00000-0 10270-3 0 9058
2 25544 51
6473 319
6087 0001158 103
4456 256
6824 15
50824329 21904
Satellite: ISS
Catalog Number: 25544
Epoch time: 13343
51800549 = yrday
fracday
Element set: 905
Inclination: 51
6473 deg
RA of node: 319
6087 deg
Eccentricity:
0001158
Arg of perigee: 103
4456 deg
Mean anomaly: 256
6824 deg
Mean motion: 15
50824329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 306
Coasting Arc #7 (Orbit 2205)
---------------------------------------
Vector Time (GMT): 2013/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3366196
91 A = 6786957
14 meter
Y = 2597239
59 meter E =
0003677
Z = 5287154
92 I = 51
37394
XDOT = -5081
759650 Wp = 105
85489
YDOT = 5724
377621 meter/sec RA = 314
12256 deg
ZDOT = 422
176969 TA = 340
09579
MA = 340
11013
Ha = 226
422 n
mi
Hp = 219
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11043953
10 X = 3311220
10
Y = 8521127
25 feet Y = 2634574
98 meter
Z = 17346308
80 Z = 5303374
24
XDOT = -16672
439798 XDOT = -5147
444053
YDOT = 18780
766474 feet/sec YDOT = 5667
182871 meter/sec
ZDOT = 1385
095043 ZDOT = 397
330745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10522624
16 X = -3207295
84
Y = 9027599
39 feet Y = 2751612
29 meter
Z = 17414068
13 Z = 5307807
97
XDOT = -14440
151765 XDOT = -4401
358258
YDOT = -19307
666151 feet/sec YDOT = -5884
976643 meter/sec
ZDOT = 1279
628017 ZDOT = 390
030620
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 13344
54901658
00016717 00000-0 10270-3 0 9066
2 25544 51
6471 314
4950 0001052 103
5851 256
5417 15
50849639 22063
Satellite: ISS
Catalog Number: 25544
Epoch time: 13344
54901658 = yrday
fracday
Element set: 906
Inclination: 51
6471 deg
RA of node: 314
4950 deg
Eccentricity:
0001052
Arg of perigee: 103
5851 deg
Mean anomaly: 256
5417 deg
Mean motion: 15
50849639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2206
Checksum: 303
Coasting Arc #8 (Orbit 2220)
---------------------------------------
Vector Time (GMT): 2013/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3078278
99 A = 6786909
30 meter
Y = -2935008
20 meter E =
0015842
Z = -5302652
14 I = 51
35322
XDOT = 5005
487954 Wp = 93
16611
YDOT = -5779
634206 meter/sec RA = 309
13752 deg
ZDOT = 293
150643 TA = 179
64626
MA = 179
64514
Ha = 226
514 n
mi
Hp = 219
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10099340
52 X = -3019471
23
Y = -9629292
01 feet Y = -2969102
46 meter
Z = -17397152
71 Z = -5317463
54
XDOT = 16422
204572 XDOT = 5068
321025
YDOT = -18962
054483 feet/sec YDOT = -5723
308343 meter/sec
ZDOT = 961
780325 ZDOT = 317
619445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11284052
30 X = 3439379
14
Y = -8076920
96 feet Y = -2461845
51 meter
Z = -17458934
02 Z = -5321483
09
XDOT = 15078
712402 XDOT = 4595
991540
YDOT = 18761
871486 feet/sec YDOT = 5718
618429 meter/sec
ZDOT = 1065
663114 ZDOT = 324
814117
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 13345
51557619
00016717 00000-0 10270-3 0 9079
2 25544 51
6473 309
7001 0001075 106
5201 253
6068 15
50865496 22212
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
51557619 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 309
7001 deg
Eccentricity:
0001075
Arg of perigee: 106
5201 deg
Mean anomaly: 253
6068 deg
Mean motion: 15
50865496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2221
Checksum: 295
Coasting Arc #9 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2013/345/16:41:41
121
Vector Time (MET): N/A
Weight (LBS) : 901651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2079474
43 A = 6789391
98 meter
Y = -3968948
45 meter E =
0011977
Z = -5111705
51 I = 51
35567
XDOT = 5567
352584 Wp = 104
30911
YDOT = -4996
531742 meter/sec RA = 308
15317 deg
ZDOT = 1614
978621 TA = 181
36454
MA = 181
36781
Ha = 226
446 n
mi
Hp = 221
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6822422
67 X = -2010106
72
Y = -13021484
41 feet Y = -3991814
39 meter
Z = -16770687
37 Z = -5121639
17
XDOT = 18265
592468 XDOT = 5614
965932
YDOT = -16392
820675 feet/sec YDOT = -4934
007904 meter/sec
ZDOT = 5298
486288 ZDOT = 1642
139998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 653436
88 X = 199167
56
Y = -14638904
05 feet Y = -4461937
96 meter
Z = -16811780
71 Z = -5124230
76
XDOT = 22904
219803 XDOT = 6981
206196
YDOT = -5193
631584 feet/sec YDOT = -1583
018907 meter/sec
ZDOT = 5413
556619 ZDOT = 1650
052057
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 13345
70888707
00016717 00000-0 10270-3 0 9086
2 25544 51
6507 308
7417 0001533 265
4947 94
6028 15
50311276 22245
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
70888707 = yrday
fracday
Element set: 908
Inclination: 51
6507 deg
RA of node: 308
7417 deg
Eccentricity:
0001533
Arg of perigee: 265
4947 deg
Mean anomaly: 94
6028 deg
Mean motion: 15
50311276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 315
Coasting Arc #10 (Orbit 2239)
---------------------------------------
Vector Time (GMT): 2013/346/16:41:41
121
Vector Time (MET): N/A
Weight (LBS) : 901651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2018071
29 A = 6789840
75 meter
Y = 4168987
70 meter E =
0004973
Z = 4962758
65 I = 51
33923
XDOT = -5332
991873 Wp = 46
26399
YDOT = 5087
165065 meter/sec RA = 303
17377 deg
ZDOT = -2100
175579 TA = 64
30736
MA = 64
25602
Ha = 226
260 n
mi
Hp = 221
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6620968
80 X = 1947194
77
Y = 13677781
17 feet Y = 4191158
49 meter
Z = 16282016
57 Z = 4972390
43
XDOT = -17496
692498 XDOT = -5379
279130
YDOT = 16690
174099 feet/sec YDOT = 5027
269461 meter/sec
ZDOT = -6890
339827 ZDOT = -2126
195193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -892030
17 X = -271890
79
Y = 15126990
61 feet Y = 4610706
74 meter
Z = 16321808
31 Z = 4974887
17
XDOT = -22237
910524 XDOT = -6778
115128
YDOT = 6258
797132 feet/sec YDOT = 1907
681366 meter/sec
ZDOT = -7000
620504 ZDOT = -2133
789130
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 13346
74025365
00016717 00000-0 10270-3 0 9095
2 25544 51
6506 303
6301 0001631 271
8736 88
2228 15
50363030 22400
Satellite: ISS
Catalog Number: 25544
Epoch time: 13346
74025365 = yrday
fracday
Element set: 909
Inclination: 51
6506 deg
RA of node: 303
6301 deg
Eccentricity:
0001631
Arg of perigee: 271
8736 deg
Mean anomaly: 88
2228 deg
Mean motion: 15
50363030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2240
Checksum: 279
Coasting Arc #11 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2013/347/15:06:27
037
Vector Time (MET): N/A
Weight (LBS) : 901284
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2687344
77 A = 6791205
83 meter
Y = -3603269
15 meter E =
0009241
Z = -5099056
28 I = 51
32189
XDOT = 4676
231565 Wp = 107
13584
YDOT = -5829
273962 meter/sec RA = 298
52738 deg
ZDOT = 1654
601643 TA = 178
94076
MA = 178
93880
Ha = 226
415 n
mi
Hp = 223
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8816747
94 X = -2622082
40
Y = -11821749
17 feet Y = -3632955
49 meter
Z = -16729187
26 Z = -5111953
02
XDOT = 15341
967078 XDOT = 4733
030560
YDOT = -19124
914574 feet/sec YDOT = -5776
663895 meter/sec
ZDOT = 5428
483080 ZDOT = 1677
456153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3889986
03 X = 1185667
74
Y = -14161917
37 feet Y = -4316552
42 meter
Z = -16782806
95 Z = -5115399
56
XDOT = 23463
060754 XDOT = 7151
540918
YDOT = -104
033369 feet/sec YDOT = -31
709371 meter/sec
ZDOT = 5525
578307 ZDOT = 1684
196268
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 13347
64269156
00016717 00000-0 10270-3 0 9105
2 25544 51
6503 299
1559 0004228 272
4774 87
5892 15
49703404 22540
Satellite: ISS
Catalog Number: 25544
Epoch time: 13347
64269156 = yrday
fracday
Element set: 910
Inclination: 51
6503 deg
RA of node: 299
1559 deg
Eccentricity:
0004228
Arg of perigee: 272
4774 deg
Mean anomaly: 87
5892 deg
Mean motion: 15
49703404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 329
Coasting Arc #12 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2013/348/15:06:27
037
Vector Time (MET): N/A
Weight (LBS) : 901284
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2810333
71 A = 6791385
18 meter
Y = 3611751
91 meter E =
0003762
Z = 5018660
98 I = 51
30896
XDOT = -4310
791581 Wp = 7
51811
YDOT = 6033
122551 meter/sec RA = 293
55205 deg
ZDOT = -1924
055084 TA = 101
27417
MA = 101
23189
Ha = 226
255 n
mi
Hp = 223
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9220254
96 X = 2745357
91
Y = 11849579
77 feet Y = 3642815
13 meter
Z = 16465423
17 Z = 5032155
94
XDOT = -14143
016997 XDOT = -4368
588282
YDOT = 19793
709157 feet/sec YDOT = 5984
593536 meter/sec
ZDOT = -6312
516680 ZDOT = -1945
136592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3411067
18 X = -1039693
28
Y = 14558106
36 feet Y = 4437310
82 meter
Z = 16521560
53 Z = 5035771
65
XDOT = -23189
660558 XDOT = -7068
208538
YDOT = 1846
347192 feet/sec YDOT = 562
766624 meter/sec
ZDOT = -6402
189074 ZDOT = -1951
387230
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 13348
67445978
00016717 00000-0 10270-3 0 9118
2 25544 51
6502 294
0471 0004325 276
8950 83
1709 15
49751127 22700
Satellite: ISS
Catalog Number: 25544
Epoch time: 13348
67445978 = yrday
fracday
Element set: 911
Inclination: 51
6502 deg
RA of node: 294
0471 deg
Eccentricity:
0004325
Arg of perigee: 276
8950 deg
Mean anomaly: 83
1709 deg
Mean motion: 15
49751127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 322
Coasting Arc #13 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2013/349/15:06:27
037
Vector Time (MET): N/A
Weight (LBS) : 901284
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2955009
85 A = 6791766
65 meter
Y = -3620517
96 meter E =
0008038
Z = -4935786
17 I = 51
29942
XDOT = 3931
276146 Wp = 109
18541
YDOT = -6192
537667 meter/sec RA = 288
57536 deg
ZDOT = 2189
098171 TA = 182
30911
MA = 182
31283
Ha = 226
387 n
mi
Hp = 223
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9694914
22 X = -2890327
92
Y = -11878339
76 feet Y = -3653200
62 meter
Z = -16193524
19 Z = -4949984
68
XDOT = 12897
887618 XDOT = 3989
596176
YDOT = -20316
724629 feet/sec YDOT = -6148
249760 meter/sec
ZDOT = 7182
080612 ZDOT = 2208
337142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2874465
72 X = 876137
15
Y = -14996873
28 feet Y = -4571046
98 meter
Z = -16252623
84 Z = -4953799
75
XDOT = 22718
267984 XDOT = 6924
528081
YDOT = -3516
633757 feet/sec YDOT = -1071
869969 meter/sec
ZDOT = 7264
029899 ZDOT = 2214
076313
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 13349
64173202
00016717 00000-0 10270-3 0 9125
2 25544 51
6509 289
2572 0004298 280
2987 79
7679 15
49745049 22852
Satellite: ISS
Catalog Number: 25544
Epoch time: 13349
64173202 = yrday
fracday
Element set: 912
Inclination: 51
6509 deg
RA of node: 289
2572 deg
Eccentricity:
0004298
Arg of perigee: 280
2987 deg
Mean anomaly: 79
7679 deg
Mean motion: 15
49745049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 351
Coasting Arc #14 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2013/350/15:06:27
037
Vector Time (MET): N/A
Weight (LBS) : 901284
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3101544
03 A = 6792043
15 meter
Y = 3633915
35 meter E =
0005039
Z = 4827896
13 I = 51
29193
XDOT = -3560
289087 Wp = 22
31267
YDOT = 6319
578541 meter/sec RA = 283
59844 deg
ZDOT = -2464
058664 TA = 92
05911
MA = 92
00140
Ha = 226
303 n
mi
Hp = 223
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10175669
38 X = 3037225
57
Y = 11922294
47 feet Y = 3668238
66 meter
Z = 15839554
23 Z = 4842807
36
XDOT = -11680
738476 XDOT = -3618
721635
YDOT = 20733
525397 feet/sec YDOT = 6279
438666 meter/sec
ZDOT = -8084
181969 ZDOT = -2481
495554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2330935
32 X = -710469
09
Y = 15436350
39 feet Y = 4704999
60 meter
Z = 15901655
84 Z = 4846824
70
XDOT = -22133
706758 XDOT = -6746
353820
YDOT = 5080
513128 feet/sec YDOT = 1548
540402 meter/sec
ZDOT = -8158
571496 ZDOT = -2486
732592
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 13350
67347476
00016717 00000-0 10270-3 0 9137
2 25544 51
6509 284
1483 0004396 284
8218 75
2446 15
49795773 23014
Satellite: ISS
Catalog Number: 25544
Epoch time: 13350
67347476 = yrday
fracday
Element set: 913
Inclination: 51
6509 deg
RA of node: 284
1483 deg
Eccentricity:
0004396
Arg of perigee: 284
8218 deg
Mean anomaly: 75
2446 deg
Mean motion: 15
49795773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 335
Coasting Arc #15 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2013/351/15:06:27
037
Vector Time (MET): N/A
Weight (LBS) : 901284
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3272800
26 A = 6792528
82 meter
Y = -3637703
36 meter E =
0006522
Z = -4717417
71 I = 51
28724
XDOT = 3184
213101 Wp = 109
70950
YDOT = -6404
149497 meter/sec RA = 278
62069 deg
ZDOT = 2730
206604 TA = 187
48272
MA = 187
49246
Ha = 226
429 n
mi
Hp = 222
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10737533
65 X = -3208963
47
Y = -11934722
30 feet Y = -3673944
45 meter
Z = -15477092
22 Z = -4733162
02
XDOT = 10446
893377 XDOT = 3242
326460
YDOT = -21010
989163 feet/sec YDOT = -6368
216963 meter/sec
ZDOT = 8957
370748 ZDOT = 2745
815689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1695348
85 X = 516742
33
Y = -15900399
64 feet Y = -4846441
81 meter
Z = -15542705
44 Z = -4737416
62
XDOT = 21385
062566 XDOT = 6518
167070
YDOT = -6537
944087 feet/sec YDOT = -1992
765358 meter/sec
ZDOT = 9024
083155 ZDOT = 2750
540546
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 13351
64072334
00016717 00000-0 10270-3 0 9144
2 25544 51
6511 279
3584 0004406 287
9539 72
1131 15
49785435 23164
Satellite: ISS
Catalog Number: 25544
Epoch time: 13351
64072334 = yrday
fracday
Element set: 914
Inclination: 51
6511 deg
RA of node: 279
3584 deg
Eccentricity:
0004406
Arg of perigee: 287
9539 deg
Mean anomaly: 72
1131 deg
Mean motion: 15
49785435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 312
Coasting Arc #16 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2013/352/15:06:27
037
Vector Time (MET): N/A
Weight (LBS) : 901284
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3446012
07 A = 6792902
06 meter
Y = 3645963
80 meter E =
0006303
Z = 4579392
97 I = 51
28530
XDOT = -2825
367406 Wp = 34
75425
YDOT = 6454
942850 meter/sec RA = 273
64306 deg
ZDOT = -3005
975335 TA = 85
47347
MA = 85
40147
Ha = 226
420 n
mi
Hp = 222
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11305813
87 X = 3382740
60
Y = 11961823
49 feet Y = 3684145
05 meter
Z = 15024255
15 Z = 4595980
03
XDOT = -9269
578103 XDOT = -2882
735858
YDOT = 21177
634022 feet/sec YDOT = 6423
027341 meter/sec
ZDOT = -9862
123802 ZDOT = -3019
839340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1050513
82 X = -320196
61
Y = 16362149
44 feet Y = 4987183
15 meter
Z = 15093421
68 Z = 4600474
93
XDOT = -20549
661514 XDOT = -6263
536829
YDOT = 7854
322342 feet/sec YDOT = 2393
997450 meter/sec
ZDOT = -9921
499000 ZDOT = -3024
072895
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 13352
67244094
00016717 00000-0 10270-3 0 9153
2 25544 51
6511 274
2496 0004501 292
5590 67
5084 15
49838157 23328
Satellite: ISS
Catalog Number: 25544
Epoch time: 13352
67244094 = yrday
fracday
Element set: 915
Inclination: 51
6511 deg
RA of node: 274
2496 deg
Eccentricity:
0004501
Arg of perigee: 292
5590 deg
Mean anomaly: 67
5084 deg
Mean motion: 15
49838157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 315
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