[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 2nd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 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
345/16:37:49
337 1
8 3
0 3
1
N/A -2
4 -0
3 226
4
000/00:09:38
674 0
4 0
3 221
1
347/15:02:18
145 1
5 3
3 3
3
N/A -3
0 -0
3 226
4
000/00:10:36
290 0
4 0
3 223
0
Coasting Arc #1 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2013/333/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -755248
30 A = 6787598
48 meter
Y = 4146122
58 meter E =
0003462
Z = 5317908
79 I = 51
67311
XDOT = -7589
705037 Wp = 76
15983
YDOT = -1044
689110 meter/sec RA = 6
28553 deg
ZDOT = -262
440766 TA = 16
34697
MA = 16
33580
Ha = 226
876 n
mi
Hp = 219
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2477848
77 X = -827388
57
Y = 13602764
37 feet Y = 4137273
41 meter
Z = 17447207
31 Z = 5314064
66
XDOT = -24900
607078 XDOT = -7576
184107
YDOT = -3427
457709 feet/sec YDOT = -1129
486418 meter/sec
ZDOT = -861
026134 ZDOT = -299
278884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11533321
15 X = 3515356
29
Y = 7664630
76 feet Y = 2336179
45 meter
Z = 17430315
96 Z = 5312760
30
XDOT = -12263
754642 XDOT = -3737
992415
YDOT = 20770
928706 feet/sec YDOT = 6330
979070 meter/sec
ZDOT = -1015
767052 ZDOT = -309
605797
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 13334
04491937
00016717 00000-0 10270-3 0 9008
2 25544 51
6500 6
5894 0000916 78
7833 281
3421 15
50623484 20442
Satellite: ISS
Catalog Number: 25544
Epoch time: 13334
04491937 = yrday
fracday
Element set: 900
Inclination: 51
6500 deg
RA of node: 6
5894 deg
Eccentricity:
0000916
Arg of perigee: 78
7833 deg
Mean anomaly: 281
3421 deg
Mean motion: 15
50623484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 294
Coasting Arc #2 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2013/334/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1096652
84 A = 6787758
28 meter
Y = -4148610
84 meter E =
0015282
Z = -5272647
34 I = 51
64161
XDOT = 7549
860414 Wp = 95
71186
YDOT = 873
733000 meter/sec RA = 1
32254 deg
ZDOT = 883
544846 TA = 182
75220
MA = 182
76062
Ha = 226
789 n
mi
Hp = 219
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3597942
38 X = 1168575
70
Y = -13610927
94 feet Y = -4135944
94 meter
Z = -17298711
76 Z = -5267145
30
XDOT = 24769
883249 XDOT = 7535
236889
YDOT = 2866
578083 feet/sec YDOT = 958
078535 meter/sec
ZDOT = 2898
769181 ZDOT = 920
186763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11254386
82 X = -3430337
10
Y = -8506851
98 feet Y = -2592888
48 meter
Z = -17274843
68 Z = -5265372
35
XDOT = 11254
892094 XDOT = 3430
491110
YDOT = -21084
278438 feet/sec YDOT = -6426
488068 meter/sec
ZDOT = 3052
709197 ZDOT = 930
465763
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 13335
01162387
00016717 00000-0 10270-3 0 9011
2 25544 51
6485 1
7947 0000919 80
2623 279
8631 15
50660780 20599
Satellite: ISS
Catalog Number: 25544
Epoch time: 13335
01162387 = yrday
fracday
Element set: 901
Inclination: 51
6485 deg
RA of node: 1
7947 deg
Eccentricity:
0000919
Arg of perigee: 80
2623 deg
Mean anomaly: 279
8631 deg
Mean motion: 15
50660780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 304
Coasting Arc #3 (Orbit 2074)
---------------------------------------
Vector Time (GMT): 2013/335/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1446080
50 A = 6788234
60 meter
Y = 4178197
51 meter E =
0005605
Z = 5147381
91 I = 51
61253
XDOT = -7480
685436 Wp = 58
91265
YDOT = -723
128965 meter/sec RA = 356
35906 deg
ZDOT = -1510
563876 TA = 45
67040
MA = 45
62446
Ha = 226
804 n
mi
Hp = 219
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4744358
60 X = -1517699
68
Y = 13707997
07 feet Y = 4161625
67 meter
Z = 16887735
91 Z = 5140183
19
XDOT = -24542
931219 XDOT = -7464
705192
YDOT = -2372
470359 feet/sec YDOT = -806
693283 meter/sec
ZDOT = -4955
918229 ZDOT = -1546
866396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11082216
89 X = 3377859
71
Y = 9415364
07 feet Y = 2869802
97 meter
Z = 16856723
72 Z = 5137929
39
XDOT = -10263
147323 XDOT = -3128
207304
YDOT = 21249
804642 feet/sec YDOT = 6476
940455 meter/sec
ZDOT = -5108
454762 ZDOT = -1557
057012
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 13336
04276015
00016717 00000-0 10270-3 0 9020
2 25544 51
6486 356
6818 0000872 84
9253 275
1997 15
50670573 20750
Satellite: ISS
Catalog Number: 25544
Epoch time: 13336
04276015 = yrday
fracday
Element set: 902
Inclination: 51
6486 deg
RA of node: 356
6818 deg
Eccentricity:
0000872
Arg of perigee: 84
9253 deg
Mean anomaly: 275
1997 deg
Mean motion: 15
50670573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2075
Checksum: 324
Coasting Arc #4 (Orbit 2089)
---------------------------------------
Vector Time (GMT): 2013/336/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1781190
27 A = 6788903
30 meter
Y = -4266822
08 meter E =
0013349
Z = -4983289
67 I = 51
58273
XDOT = 7329
938922 Wp = 104
32521
YDOT = 588
767393 meter/sec RA = 351
39180 deg
ZDOT = 2117
383816 TA = 186
34667
MA = 186
36360
Ha = 226
748 n
mi
Hp = 219
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5843800
10 X = 1852978
33
Y = -13998760
10 feet Y = -4246501
80 meter
Z = -16349375
54 Z = -4974462
70
XDOT = 24048
356043 XDOT = 7312
524556
YDOT = 1931
651552 feet/sec YDOT = 670
637859 meter/sec
ZDOT = 6946
797295 ZDOT = 2152
950380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11143107
40 X = -3396419
13
Y = -10352950
31 feet Y = -3155579
25 meter
Z = -16311497
24 Z = -4971744
36
XDOT = 9226
915943 XDOT = 2812
363979
YDOT = -21103
592987 feet/sec YDOT = -6432
375143 meter/sec
ZDOT = 7096
262939 ZDOT = 2162
940944
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 13337
00943601
00016717 00000-0 10270-3 0 9030
2 25544 51
6471 351
8864 0000962 90
5448 269
5813 15
50700519 20906
Satellite: ISS
Catalog Number: 25544
Epoch time: 13337
00943601 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 351
8864 deg
Eccentricity:
0000962
Arg of perigee: 90
5448 deg
Mean anomaly: 269
5813 deg
Mean motion: 15
50700519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2090
Checksum: 300
Coasting Arc #5 (Orbit 2105)
---------------------------------------
Vector Time (GMT): 2013/337/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2113156
04 A = 6789841
27 meter
Y = 4377512
37 meter E =
0008602
Z = 4735439
44 I = 51
55589
XDOT = -7148
902487 Wp = 65
61222
YDOT = -497
446795 meter/sec RA = 346
42460 deg
ZDOT = -2722
918484 TA = 51
39500
MA = 51
31800
Ha = 226
746 n
mi
Hp = 219
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6932926
63 X = -2184953
04
Y = 14361917
23 feet Y = 4353479
77 meter
Z = 15536218
64 Z = 4724999
87
XDOT = -23454
404485 XDOT = -7129
581246
YDOT = -1632
043291 feet/sec YDOT = -577
282054 meter/sec
ZDOT = -8933
459592 ZDOT = -2757
600739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11311925
27 X = 3447874
82
Y = 11302957
29 feet Y = 3445141
38 meter
Z = 15491537
40 Z = 4721820
60
XDOT = -8299
486657 XDOT = -2529
683533
YDOT = 20783
104200 feet/sec YDOT = 6334
690160 meter/sec
ZDOT = -9079
224953 ZDOT = -2767
347766
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
04054104
00016717 00000-0 10270-3 0 9047
2 25544 51
6473 346
7729 0000884 94
6365 265
4887 15
50715339 21067
Satellite: ISS
Catalog Number: 25544
Epoch time: 13338
04054104 = yrday
fracday
Element set: 904
Inclination: 51
6473 deg
RA of node: 346
7729 deg
Eccentricity:
0000884
Arg of perigee: 94
6365 deg
Mean anomaly: 265
4887 deg
Mean motion: 15
50715339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2106
Checksum: 318
Coasting Arc #6 (Orbit 2120)
---------------------------------------
Vector Time (GMT): 2013/338/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2406407
80 A = 6790896
27 meter
Y = -4538504
01 meter E =
0010191
Z = -4451816
20 I = 51
52902
XDOT = 6899
078754 Wp = 109
15906
YDOT = 438
706850 meter/sec RA = 341
45458 deg
ZDOT = 3284
912341 TA = 194
06942
MA = 194
09783
Ha = 226
716 n
mi
Hp = 219
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7895038
71 X = 2478605
35
Y = -14890105
02 feet Y = -4511189
90 meter
Z = -14605696
19 Z = -4439951
11
XDOT = 22634
772816 XDOT = 6877
702972
YDOT = 1439
326937 feet/sec YDOT = 515
736889 meter/sec
ZDOT = 10777
271459 ZDOT = 3318
375768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11713036
85 X = -3570133
63
Y = -12179088
85 feet Y = -3712186
28 meter
Z = -14554991
85 Z = -4436361
51
XDOT = 7423
697926 XDOT = 2262
743128
YDOT = -20176
014612 feet/sec YDOT = -6149
649254 meter/sec
ZDOT = 10917
924470 ZDOT = 3327
783378
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
00718821
00016717 00000-0 10270-3 0 9058
2 25544 51
6465 341
9774 0001063 101
5323 258
5947 15
50742360 21218
Satellite: ISS
Catalog Number: 25544
Epoch time: 13339
00718821 = yrday
fracday
Element set: 905
Inclination: 51
6465 deg
RA of node: 341
9774 deg
Eccentricity:
0001063
Arg of perigee: 101
5323 deg
Mean anomaly: 258
5947 deg
Mean motion: 15
50742360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2121
Checksum: 290
Coasting Arc #7 (Orbit 2136)
---------------------------------------
Vector Time (GMT): 2013/339/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2686367
17 A = 6792156
49 meter
Y = 4709774
05 meter E =
0011530
Z = 4082497
44 I = 51
50469
XDOT = -6623
393658 Wp = 79
51942
YDOT = -444
023597 meter/sec RA = 336
48496 deg
ZDOT = -3834
789577 TA = 50
25766
MA = 50
15612
Ha = 226
697 n
mi
Hp = 219
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8813540
58 X = -2758664
94
Y = 15452014
59 feet Y = 4679328
79 meter
Z = 13394020
46 Z = 4069272
09
XDOT = -21730
294154 XDOT = -6599
307824
YDOT = -1456
770331 feet/sec YDOT = -517
955597 meter/sec
ZDOT = -12581
330634 ZDOT = -3866
907013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12193020
53 X = 3716432
66
Y = 13010863
34 feet Y = 3965711
15 meter
Z = 13337568
08 Z = 4065290
75
XDOT = -6750
268815 XDOT = -2057
481935
YDOT = 19399
727168 feet/sec YDOT = 5913
036841 meter/sec
ZDOT = -12716
324203 ZDOT = -3875
935617
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
03826211
00016717 00000-0 10270-3 0 9067
2 25544 51
6468 336
8637 0000978 106
0073 254
1186 15
50758949 21372
Satellite: ISS
Catalog Number: 25544
Epoch time: 13340
03826211 = yrday
fracday
Element set: 906
Inclination: 51
6468 deg
RA of node: 336
8637 deg
Eccentricity:
0000978
Arg of perigee: 106
0073 deg
Mean anomaly: 254
1186 deg
Mean motion: 15
50758949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2137
Checksum: 313
Coasting Arc #8 (Orbit 2151)
---------------------------------------
Vector Time (GMT): 2013/340/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2908093
96 A = 6793386
34 meter
Y = -4915544
92 meter E =
0006734
Z = -3685309
96 I = 51
48117
XDOT = 6301
111212 Wp = 101
27748
YDOT = 493
026317 meter/sec RA = 331
51360 deg
ZDOT = 4320
062314 TA = 214
85651
MA = 214
90063
Ha = 226
684 n
mi
Hp = 219
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9540990
68 X = 2980746
76
Y = -16127115
89 feet Y = -4882618
29 meter
Z = -12090911
96 Z = -3671006
58
XDOT = 20672
937048 XDOT = 6274
144090
YDOT = 1617
540411 feet/sec YDOT = 563
338282 meter/sec
ZDOT = 14173
432789 ZDOT = 4350
607058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12866468
48 X = -3921699
59
Y = -13676261
93 feet Y = -4168524
64 meter
Z = -12029894
87 Z = -3666711
96
XDOT = 6213
174949 XDOT = 1893
775725
YDOT = -18409
645187 feet/sec YDOT = -5611
259853 meter/sec
ZDOT = 14301
804121 ZDOT = 4359
189896
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
00488032
00016717 00000-0 10270-3 0 9071
2 25544 51
6468 332
0687 0001206 111
3417 248
7862 15
50787488 21528
Satellite: ISS
Catalog Number: 25544
Epoch time: 13341
00488032 = yrday
fracday
Element set: 907
Inclination: 51
6468 deg
RA of node: 332
0687 deg
Eccentricity:
0001206
Arg of perigee: 111
3417 deg
Mean anomaly: 248
7862 deg
Mean motion: 15
50787488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2152
Checksum: 303
Coasting Arc #9 (Orbit 2167)
---------------------------------------
Vector Time (GMT): 2013/341/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3109774
78 A = 6794725
07 meter
Y = 5113667
08 meter E =
0013876
Z = 3203364
48 I = 51
45890
XDOT = -5962
634313 Wp = 95
29501
YDOT = -622
305158 meter/sec RA = 326
54244 deg
ZDOT = -4778
387096 TA = 47
59721
MA = 47
47988
Ha = 226
637 n
mi
Hp = 219
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10202673
16 X = -3182286
88
Y = 16777122
96 feet Y = 5078486
00 meter
Z = 10509725
98 Z = 3188081
60
XDOT = -19562
448532 XDOT = -5932
020304
YDOT = -2041
683588 feet/sec YDOT = -688
811724 meter/sec
ZDOT = -15677
123018 ZDOT = -4807
278691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13559437
80 X = 4132916
64
Y = 14250386
17 feet Y = 4343517
70 meter
Z = 10444561
98 Z = 3183502
49
XDOT = -5958
299971 XDOT = -1816
089831
YDOT = 17288
880600 feet/sec YDOT = 5269
650807 meter/sec
ZDOT = -15798
518150 ZDOT = -4815
388332
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
03592290
00016717 00000-0 10270-3 0 9088
2 25544 51
6466 326
9548 0001117 116
0408 244
0858 15
50805764 21686
Satellite: ISS
Catalog Number: 25544
Epoch time: 13342
03592290 = yrday
fracday
Element set: 908
Inclination: 51
6466 deg
RA of node: 326
9548 deg
Eccentricity:
0001117
Arg of perigee: 116
0408 deg
Mean anomaly: 244
0858 deg
Mean motion: 15
50805764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2168
Checksum: 308
Coasting Arc #10 (Orbit 2182)
---------------------------------------
Vector Time (GMT): 2013/342/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3241528
73 A = 6795873
71 meter
Y = -5325570
56 meter E =
0005634
Z = -2705896
16 I = 51
43851
XDOT = 5606
109049 Wp = 67
35900
YDOT = 798
288424 meter/sec RA = 321
57028 deg
ZDOT = 5155
432638 TA = 262
03275
MA = 262
09670
Ha = 226
636 n
mi
Hp = 219
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10634936
78 X = 3313984
05
Y = -17472344
37 feet Y = -5288916
50 meter
Z = -8877612
07 Z = -2689973
29
XDOT = 18392
746223 XDOT = 5571
722025
YDOT = 2619
056510 feet/sec YDOT = 860
787048 meter/sec
ZDOT = 16914
149074 ZDOT = 5182
583148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14375169
74 X = -4381551
74
Y = -14592460
04 feet Y = -4447781
82 meter
Z = -8809727
54 Z = -2685204
95
XDOT = 5894
043529 XDOT = 1796
504468
YDOT = -16065
075105 feet/sec YDOT = -4896
634892 meter/sec
ZDOT = 17028
189321 ZDOT = 5190
192105
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
00251167
00016717 00000-0 10270-3 0 9092
2 25544 51
6474 322
1603 0001339 119
4539 240
6746 15
50834539 21830
Satellite: ISS
Catalog Number: 25544
Epoch time: 13343
00251167 = yrday
fracday
Element set: 909
Inclination: 51
6474 deg
RA of node: 322
1603 deg
Eccentricity:
0001339
Arg of perigee: 119
4539 deg
Mean anomaly: 240
6746 deg
Mean motion: 15
50834539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2183
Checksum: 296
Coasting Arc #11 (Orbit 2198)
---------------------------------------
Vector Time (GMT): 2013/343/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3351991
04 A = 6796977
06 meter
Y = 5507562
74 meter E =
0015096
Z = 2128787
38 I = 51
41803
XDOT = -5247
145893 Wp = 110
99718
YDOT = -1062
523137 meter/sec RA = 316
59768 deg
ZDOT = -5486
984823 TA = 45
35726
MA = 45
23427
Ha = 226
547 n
mi
Hp = 219
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10997345
94 X = -3423669
81
Y = 18069431
55 feet Y = 5469677
79 meter
Z = 6984210
56 Z = 2112329
72
XDOT = -17215
045581 XDOT = -5208
220150
YDOT = -3485
968297 feet/sec YDOT = -1120
982243 meter/sec
ZDOT = -18001
918709 ZDOT = -5512
380571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15126930
59 X = 4610688
44
Y = 14818806
05 feet Y = 4516772
08 meter
Z = 6914053
06 Z = 2107403
37
XDOT = -6160
805569 XDOT = -1877
813537
YDOT = 14778
422798 feet/sec YDOT = 4504
463269 meter/sec
ZDOT = -18108
531503 ZDOT = -5519
480402
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
03352253
00016717 00000-0 10270-3 0 9106
2 25544 51
6466 317
0460 0001239 123
6959 236
4310 15
50859156 21996
Satellite: ISS
Catalog Number: 25544
Epoch time: 13344
03352253 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 317
0460 deg
Eccentricity:
0001239
Arg of perigee: 123
6959 deg
Mean anomaly: 236
4310 deg
Mean motion: 15
50859156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2199
Checksum: 296
Coasting Arc #12 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2013/344/23:55:48
514
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3390479
48 A = 6797786
82 meter
Y = -5680833
60 meter E =
0008341
Z = -1552139
13 I = 51
40045
XDOT = 4900
670068 Wp = 47
24566
YDOT = 1367
094267 meter/sec RA = 311
62447 deg
ZDOT = 5726
596301 TA = 295
76069
MA = 295
84675
Ha = 226
560 n
mi
Hp = 219
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11123620
35 X = 3461291
76
Y = -18637905
50 feet Y = -5642523
10 meter
Z = -5092319
97 Z = -1535496
57
XDOT = 16078
313872 XDOT = 4857
200239
YDOT = 4485
217413 feet/sec YDOT = 1421
653426 meter/sec
ZDOT = 18788
045606 ZDOT = 5750
297942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15911689
27 X = -4849882
89
Y = -14786556
26 feet Y = -4506942
35 meter
Z = -5021361
59 Z = -1530511
01
XDOT = 6629
021607 XDOT = 2020
525786
YDOT = -13518
973366 feet/sec YDOT = -4120
583082 meter/sec
ZDOT = 18887
480087 ZDOT = 5756
903930
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
00008145
00016717 00000-0 10270-3 0 9113
2 25544 51
6478 312
2516 0001422 126
3890 233
7392 15
50882574 22144
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
00008145 = yrday
fracday
Element set: 911
Inclination: 51
6478 deg
RA of node: 312
2516 deg
Eccentricity:
0001422
Arg of perigee: 126
3890 deg
Mean anomaly: 233
7392 deg
Mean motion: 15
50882574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 281
Coasting Arc #13 (Orbit 2224)
---------------------------------------
Vector Time (GMT): 2013/345/16:42:38
674
Vector Time (MET): N/A
Weight (LBS) : 901645
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1752513
77 A = 6789788
84 meter
Y = -4250055
91 meter E =
0011380
Z = -5007182
84 I = 51
35702
XDOT = 5707
886821 Wp = 107
54269
YDOT = -4694
885603 meter/sec RA = 308
14520 deg
ZDOT = 1987
607983 TA = 181
87633
MA = 181
88060
Ha = 226
442 n
mi
Hp = 221
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5749717
11 X = -1680534
71
Y = -13943752
98 feet Y = -4269250
97 meter
Z = -16427765
24 Z = -5015521
82
XDOT = 18726
662798 XDOT = 5750
306501
YDOT = -15403
167990 feet/sec YDOT = -4630
819277 meter/sec
ZDOT = 6521
023567 ZDOT = 2015
439467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1978373
15 X = 603008
13
Y = -14914560
45 feet Y = -4545958
02 meter
Z = -16462104
70 Z = -5017649
51
XDOT = 22767
657036 XDOT = 6939
581865
YDOT = -4306
248366 feet/sec YDOT = -1312
544502 meter/sec
ZDOT = 6638
860164 ZDOT = 2023
524578
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
70888195
00016717 00000-0 10270-3 0 9122
2 25544 51
6505 308
7397 0001470 262
3977 97
7007 15
50330843 22252
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
70888195 = yrday
fracday
Element set: 912
Inclination: 51
6505 deg
RA of node: 308
7397 deg
Eccentricity:
0001470
Arg of perigee: 262
3977 deg
Mean anomaly: 97
7007 deg
Mean motion: 15
50330843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2225
Checksum: 318
Coasting Arc #14 (Orbit 2240)
---------------------------------------
Vector Time (GMT): 2013/346/16:42:38
674
Vector Time (MET): N/A
Weight (LBS) : 901645
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1697862
00 A = 6790344
19 meter
Y = 4460816
60 meter E =
0005860
Z = 4827161
18 I = 51
34096
XDOT = -5472
957189 Wp = 52
74161
YDOT = 4762
199709 meter/sec RA = 303
16593 deg
ZDOT = -2470
218946 TA = 61
66693
MA = 61
60783
Ha = 226
266 n
mi
Hp = 221
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5570413
40 X = 1624404
69
Y = 14635225
06 feet Y = 4479392
19 meter
Z = 15837142
96 Z = 4835231
14
XDOT = -17955
896290 XDOT = -5513
802620
YDOT = 15624
014792 feet/sec YDOT = 4700
769370 meter/sec
ZDOT = -8104
392868 ZDOT = -2496
905305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2206855
28 X = -672649
49
Y = 15469234
92 feet Y = 4715022
80 meter
Z = 15870317
45 Z = 4837272
76
XDOT = -22072
535678 XDOT = -6727
708875
YDOT = 5300
260878 feet/sec YDOT = 1615
519516 meter/sec
ZDOT = -8217
421857 ZDOT = -2504
670182
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
74023327
00016717 00000-0 10270-3 0 9136
2 25544 51
6504 303
6279 0001543 269
2888 90
8086 15
50386017 22415
Satellite: ISS
Catalog Number: 25544
Epoch time: 13346
74023327 = yrday
fracday
Element set: 913
Inclination: 51
6504 deg
RA of node: 303
6279 deg
Eccentricity:
0001543
Arg of perigee: 269
2888 deg
Mean anomaly: 90
8086 deg
Mean motion: 15
50386017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2241
Checksum: 305
Coasting Arc #15 (Orbit 2254)
---------------------------------------
Vector Time (GMT): 2013/347/15:07:36
290
Vector Time (MET): N/A
Weight (LBS) : 901270
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2340669
56 A = 6791705
81 meter
Y = -4012509
29 meter E =
0008504
Z = -4962536
02 I = 51
32371
XDOT = 4906
371266 Wp = 112
28561
YDOT = -5480
501032 meter/sec RA = 298
51775 deg
ZDOT = 2116
897441 TA = 178
46326
MA = 178
46064
Ha = 226
402 n
mi
Hp = 223
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7679362
07 X = -2271519
92
Y = -13164400
57 feet Y = -4038297
17 meter
Z = -16281286
16 Z = -4973739
22
XDOT = 16097
018588 XDOT = 4957
007368
YDOT = -17980
646431 feet/sec YDOT = -5425
351887 meter/sec
ZDOT = 6945
201577 ZDOT = 2140
855014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5575486
89 X = 1699408
40
Y = -14130604
99 feet Y = -4307008
40 meter
Z = -16327714
83 Z = -4976687
48
XDOT = 23035
462072 XDOT = 7021
208839
YDOT = 945
589455 feet/sec YDOT = 288
215666 meter/sec
ZDOT = 7046
876010 ZDOT = 2147
887808
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
64265575
00016717 00000-0 10270-3 0 9140
2 25544 51
6501 299
1536 0004126 271
8130 88
2548 15
49733581 22555
Satellite: ISS
Catalog Number: 25544
Epoch time: 13347
64265575 = yrday
fracday
Element set: 914
Inclination: 51
6501 deg
RA of node: 299
1536 deg
Eccentricity:
0004126
Arg of perigee: 271
8130 deg
Mean anomaly: 88
2548 deg
Mean motion: 15
49733581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2255
Checksum: 319
Coasting Arc #16 (Orbit 2270)
---------------------------------------
Vector Time (GMT): 2013/348/15:07:36
290
Vector Time (MET): N/A
Weight (LBS) : 901270
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2481220
98 A = 6791977
75 meter
Y = 4045972
04 meter E =
0004370
Z = 4858393
36 I = 51
31107
XDOT = -4559
906874 Wp = 24
45899
YDOT = 5672
719200 meter/sec RA = 293
54236 deg
ZDOT = -2390
665679 TA = 89
13177
MA = 89
08170
Ha = 226
262 n
mi
Hp = 223
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8140488
77 X = 2412192
64
Y = 13274186
49 feet Y = 4073332
27 meter
Z = 15939610
76 Z = 4870279
69
XDOT = -14960
324391 XDOT = -4611
388263
YDOT = 18611
283465 feet/sec YDOT = 5621
439770 meter/sec
ZDOT = -7843
391334 ZDOT = -2412
942067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5121411
33 X = -1561006
17
Y = 14651575
86 feet Y = 4465800
32 meter
Z = 15988910
10 Z = 4873419
80
XDOT = -22776
486853 XDOT = -6942
273193
YDOT = 717
829860 feet/sec YDOT = 218
794541 meter/sec
ZDOT = -7938
027400 ZDOT = -2419
510751
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
67440216
00016717 00000-0 10270-3 0 9152
2 25544 51
6500 294
0447 0004191 276
2817 83
7856 15
49780502 22717
Satellite: ISS
Catalog Number: 25544
Epoch time: 13348
67440216 = yrday
fracday
Element set: 915
Inclination: 51
6500 deg
RA of node: 294
0447 deg
Eccentricity:
0004191
Arg of perigee: 276
2817 deg
Mean anomaly: 83
7856 deg
Mean motion: 15
49780502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2271
Checksum: 313
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