[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 8th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 261)
---------------------------------------
Vector Time (GMT): 2013/219/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -47622
15 A = 6790747
06 meter
Y = -4743654
19 meter E =
0003607
Z = 4858335
26 I = 51
42827
XDOT = 6862
437831 Wp = 145
32653
YDOT = 2406
285376 meter/sec RA = 214
66698 deg
ZDOT = 2412
959129 TA = 280
89931
MA = 280
93989
Ha = 225
689 n
mi
Hp = 222
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -156240
67 X = -18174
02
Y = -15563169
90 feet Y = -4744022
11 meter
Z = 15939420
15 Z = 4858175
41
XDOT = 22514
559813 XDOT = 6823
298937
YDOT = 7894
637060 feet/sec YDOT = 2482
806645 meter/sec
ZDOT = 7916
532574 ZDOT = 2446
200489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5189768
16 X = -1581841
33
Y = -14673283
47 feet Y = -4472416
80 meter
Z = 15939348
86 Z = 4858313
53
XDOT = 22739
554041 XDOT = 6931
016072
YDOT = 721
296672 feet/sec YDOT = 219
851226 meter/sec
ZDOT = 8055
440432 ZDOT = 2455
298244
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 13219
22907326
00016717 00000-0 10270-3 0 9004
2 25544 51
6480 215
4317 0004058 278
4817 81
5874 15
50220882 2629
Satellite: ISS
Catalog Number: 25544
Epoch time: 13219
22907326 = yrday
fracday
Element set: 900
Inclination: 51
6480 deg
RA of node: 215
4317 deg
Eccentricity:
0004058
Arg of perigee: 278
4817 deg
Mean anomaly: 81
5874 deg
Mean motion: 15
50220882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 262
Checksum: 297
Coasting Arc #2 (Orbit 276)
---------------------------------------
Vector Time (GMT): 2013/220/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -26287
98 A = 6790188
12 meter
Y = 4585980
73 meter E =
0009290
Z = -5015953
72 I = 51
45219
XDOT = -7056
739801 Wp = 63
57096
YDOT = -2207
861619 meter/sec RA = 209
69601 deg
ZDOT = -1980
424990 TA = 187
10468
MA = 187
11786
Ha = 225
801 n
mi
Hp = 222
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -86246
66 X = -53201
79
Y = 15045868
53 feet Y = 4585536
22 meter
Z = -16456541
08 Z = -5016146
84
XDOT = -23152
033469 XDOT = -7021
906358
YDOT = -7243
640482 feet/sec YDOT = -2286
579810 meter/sec
ZDOT = -6497
457316 ZDOT = -2014
620699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5042987
29 X = 1537102
53
Y = 14174217
93 feet Y = 4320301
62 meter
Z = -16457921
13 Z = -5016374
36
XDOT = -23169
817549 XDOT = -7062
160389
YDOT = 528
668914 feet/sec YDOT = 161
138285 meter/sec
ZDOT = -6640
402685 ZDOT = -2023
994738
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 13220
19605293
00016717 00000-0 10270-3 0 9011
2 25544 51
6482 210
6405 0004095 282
8063 77
2630 15
50194757 2778
Satellite: ISS
Catalog Number: 25544
Epoch time: 13220
19605293 = yrday
fracday
Element set: 901
Inclination: 51
6482 deg
RA of node: 210
6405 deg
Eccentricity:
0004095
Arg of perigee: 282
8063 deg
Mean anomaly: 77
2630 deg
Mean motion: 15
50194757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 277
Checksum: 293
Coasting Arc #3 (Orbit 292)
---------------------------------------
Vector Time (GMT): 2013/221/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 128506
10 A = 6789483
16 meter
Y = -4440739
54 meter E =
0001646
Z = 5134512
05 I = 51
47817
XDOT = 7238
572822 Wp = 175
83711
YDOT = 1987
217006 meter/sec RA = 204
72558 deg
ZDOT = 1535
899718 TA = 259
30774
MA = 259
32628
Ha = 225
766 n
mi
Hp = 222
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 421607
94 X = 153212
22
Y = -14569355
44 feet Y = -4439164
23 meter
Z = 16845511
99 Z = 5135196
44
XDOT = 23748
598496 XDOT = 7208
352482
YDOT = 6519
740833 feet/sec YDOT = 2067
994382 meter/sec
ZDOT = 5039
041069 ZDOT = 1570
990004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4807254
89 X = -1465251
29
Y = -13755694
77 feet Y = -4192735
76 meter
Z = 16848926
00 Z = 5135552
64
XDOT = 23494
874006 XDOT = 7161
237597
YDOT = -1852
360917 feet/sec YDOT = -564
599608 meter/sec
ZDOT = 5185
775015 ZDOT = 1580
624224
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 13221
22748554
00016717 00000-0 10270-3 0 9025
2 25544 51
6488 205
5288 0004042 286
9518 73
1189 15
50252499 2938
Satellite: ISS
Catalog Number: 25544
Epoch time: 13221
22748554 = yrday
fracday
Element set: 902
Inclination: 51
6488 deg
RA of node: 205
5288 deg
Eccentricity:
0004042
Arg of perigee: 286
9518 deg
Mean anomaly: 73
1189 deg
Mean motion: 15
50252499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 293
Checksum: 317
Coasting Arc #4 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2013/222/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -260125
48 A = 6789155
86 meter
Y = 4328742
96 meter E =
0010830
Z = -5233134
71 I = 51
50522
XDOT = -7375
517076 Wp = 70
98795
YDOT = -1742
435459 meter/sec RA = 199
75777 deg
ZDOT = -1073
062378 TA = 188
68395
MA = 188
70270
Ha = 225
919 n
mi
Hp = 222
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -853430
06 X = -283090
29
Y = 14201912
59 feet Y = 4325705
49 meter
Z = -17169077
15 Z = -5234454
29
XDOT = -24197
890670 XDOT = -7350
272042
YDOT = -5716
651770 feet/sec YDOT = -1824
772049 meter/sec
ZDOT = -3520
545859 ZDOT = -1108
830110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4508598
63 X = 1374220
86
Y = 13486555
38 feet Y = 4110702
08 meter
Z = -17175134
25 Z = -5234980
92
XDOT = -23605
460864 XDOT = -7194
944471
YDOT = 3210
633548 feet/sec YDOT = 978
601105 meter/sec
ZDOT = -3670
160727 ZDOT = -1118
664989
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 13222
19444594
00016717 00000-0 10270-3 0 9030
2 25544 51
6489 200
7379 0004102 291
2562 68
8150 15
50225630 3085
Satellite: ISS
Catalog Number: 25544
Epoch time: 13222
19444594 = yrday
fracday
Element set: 903
Inclination: 51
6489 deg
RA of node: 200
7379 deg
Eccentricity:
0004102
Arg of perigee: 291
2562 deg
Mean anomaly: 68
8150 deg
Mean motion: 15
50225630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 289
Coasting Arc #5 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2013/223/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 418276
27 A = 6788699
03 meter
Y = -4235848
83 meter E =
0001105
Z = 5289411
62 I = 51
53392
XDOT = 7492
414352 Wp = 294
41598
YDOT = 1486
492366 meter/sec RA = 194
79049 deg
ZDOT = 598
468264 TA = 149
86182
MA = 149
85546
Ha = 225
883 n
mi
Hp = 222
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1372297
49 X = 439917
09
Y = -13897141
82 feet Y = -4231050
21 meter
Z = 17353712
67 Z = 5291496
27
XDOT = 24581
411917 XDOT = 7472
328049
YDOT = 4876
943459 feet/sec YDOT = 1570
165004 meter/sec
ZDOT = 1963
478557 ZDOT = 634
816536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4145007
10 X = -1263398
16
Y = -13323347
09 feet Y = -4060956
19 meter
Z = 17362961
54 Z = 5292230
68
XDOT = 23595
000454 XDOT = 7191
756138
YDOT = -4585
932746 feet/sec YDOT = -1397
792301 meter/sec
ZDOT = 2115
569291 ZDOT = 644
825520
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 13223
22585773
00016717 00000-0 10270-3 0 9041
2 25544 51
6493 195
6262 0004072 295
1871 64
8858 15
50284434 3241
Satellite: ISS
Catalog Number: 25544
Epoch time: 13223
22585773 = yrday
fracday
Element set: 904
Inclination: 51
6493 deg
RA of node: 195
6262 deg
Eccentricity:
0004072
Arg of perigee: 295
1871 deg
Mean anomaly: 64
8858 deg
Mean motion: 15
50284434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 324
Checksum: 316
Coasting Arc #6 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2013/224/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -590394
62 A = 6788658
36 meter
Y = 4184809
45 meter E =
0011503
Z = -5322502
71 I = 51
56292
XDOT = -7555
920283 Wp = 78
51634
YDOT = -1215
589897 meter/sec RA = 189
82624 deg
ZDOT = -115
595513 TA = 190
36699
MA = 190
39073
Ha = 226
082 n
mi
Hp = 222
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1936990
22 X = -611291
08
Y = 13729689
78 feet Y = 4178090
28 meter
Z = -17462279
22 Z = -5325421
65
XDOT = -24789
764709 XDOT = -7541
204190
YDOT = -3988
155831 feet/sec YDOT = -1300
002707 meter/sec
ZDOT = -379
250370 ZDOT = -152
265473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3789529
06 X = 1155048
46
Y = 13321064
10 feet Y = 4060260
34 meter
Z = -17475017
28 Z = -5326385
27
XDOT = -23353
599351 XDOT = -7118
177082
YDOT = 5935
979050 feet/sec YDOT = 1809
286414 meter/sec
ZDOT = -532
734878 ZDOT = -162
377591
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 13224
19279829
00016717 00000-0 10270-3 0 9051
2 25544 51
6487 190
8353 0004122 299
8709 60
2032 15
50256863 3394
Satellite: ISS
Catalog Number: 25544
Epoch time: 13224
19279829 = yrday
fracday
Element set: 905
Inclination: 51
6487 deg
RA of node: 190
8353 deg
Eccentricity:
0004122
Arg of perigee: 299
8709 deg
Mean anomaly: 60
2032 deg
Mean motion: 15
50256863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 319
Coasting Arc #7 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2013/225/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 785226
88 A = 6788503
64 meter
Y = -4157665
58 meter E =
0003086
Z = 5309571
53 I = 51
59372
XDOT = 7593
627548 Wp = 341
88505
YDOT = 947
172898 meter/sec RA = 184
86260 deg
ZDOT = -378
519783 TA = 111
74596
MA = 111
71311
Ha = 226
030 n
mi
Hp = 221
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2576203
67 X = 805868
09
Y = -13640635
11 feet Y = -4148769
18 meter
Z = 17419854
09 Z = 5313436
27
XDOT = 24913
476207 XDOT = 7584
310416
YDOT = 3107
522630 feet/sec YDOT = 1032
037552 meter/sec
ZDOT = -1241
862806 ZDOT = -341
653429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3399140
92 X = -1036058
15
Y = -13437540
96 feet Y = -4095762
49 meter
Z = 17436553
61 Z = 5314661
54
XDOT = 22991
834656 XDOT = 7007
911203
YDOT = -7239
078911 feet/sec YDOT = -2206
471252 meter/sec
ZDOT = -1087
508248 ZDOT = -331
472514
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 13225
22418844
00016717 00000-0 10270-3 0 9069
2 25544 51
6490 185
7236 0004137 303
2993 56
7761 15
50316922 3552
Satellite: ISS
Catalog Number: 25544
Epoch time: 13225
22418844 = yrday
fracday
Element set: 906
Inclination: 51
6490 deg
RA of node: 185
7236 deg
Eccentricity:
0004137
Arg of perigee: 303
2993 deg
Mean anomaly: 56
7761 deg
Mean motion: 15
50316922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 305
Coasting Arc #8 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2013/226/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -975957
43 A = 6788776
97 meter
Y = 4176520
19 meter E =
0011220
Z = -5271861
45 I = 51
62392
XDOT = -7574
557770 Wp = 85
39022
YDOT = -675
596197 meter/sec RA = 179
90189 deg
ZDOT = 869
498487 TA = 192
92710
MA = 192
95589
Ha = 226
272 n
mi
Hp = 221
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3201960
07 X = -996978
48
Y = 13702494
06 feet Y = 4165488
89 meter
Z = -17296133
37 Z = -5276653
60
XDOT = -24850
911320 XDOT = -7570
663919
YDOT = -2216
522957 feet/sec YDOT = -760
277931 meter/sec
ZDOT = 2852
685326 ZDOT = 832
711568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3090587
70 X = 942011
13
Y = 13702059
35 feet Y = 4176387
69 meter
Z = -17316724
81 Z = -5278137
72
XDOT = -22409
970457 XDOT = -6830
558995
YDOT = 8454
965471 feet/sec YDOT = 2577
073475 meter/sec
ZDOT = 2698
613792 ZDOT = 822
537484
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 13226
19110857
00016717 00000-0 10270-3 0 9070
2 25544 51
6478 180
9322 0004144 308
7635 51
3145 15
50289518 3706
Satellite: ISS
Catalog Number: 25544
Epoch time: 13226
19110857 = yrday
fracday
Element set: 907
Inclination: 51
6478 deg
RA of node: 180
9322 deg
Eccentricity:
0004144
Arg of perigee: 308
7635 deg
Mean anomaly: 51
3145 deg
Mean motion: 15
50289518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 300
Coasting Arc #9 (Orbit 385)
---------------------------------------
Vector Time (GMT): 2013/227/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1184155
84 A = 6788953
78 meter
Y = -4221391
69 meter E =
0005242
Z = 5184064
72 I = 51
65622
XDOT = 7526
502474 Wp = 4
84526
YDOT = 422
053110 meter/sec RA = 174
94237 deg
ZDOT = -1370
337421 TA = 98
36611
MA = 98
30667
Ha = 226
212 n
mi
Hp = 221
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3885025
71 X = 1206089
71
Y = -13849710
28 feet Y = -4208027
17 meter
Z = 17008086
35 Z = 5189870
41
XDOT = 24693
249586 XDOT = 7527
880287
YDOT = 1384
688682 feet/sec YDOT = 506
226958 meter/sec
ZDOT = -4495
857680 ZDOT = -1333
771200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2778057
48 X = -846751
92
Y = -14083479
90 feet Y = -4292644
67 meter
Z = 17032935
49 Z = 5191638
74
XDOT = 21727
094967 XDOT = 6622
418546
YDOT = -9558
562195 feet/sec YDOT = -2913
449757 meter/sec
ZDOT = -4342
660897 ZDOT = -1323
643041
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 13227
22247635
00016717 00000-0 10270-3 0 9081
2 25544 51
6482 175
8203 0004193 311
7246 48
3546 15
50349939 3860
Satellite: ISS
Catalog Number: 25544
Epoch time: 13227
22247635 = yrday
fracday
Element set: 908
Inclination: 51
6482 deg
RA of node: 175
8203 deg
Eccentricity:
0004193
Arg of perigee: 311
7246 deg
Mean anomaly: 48
3546 deg
Mean motion: 15
50349939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 386
Checksum: 315
Coasting Arc #10 (Orbit 400)
---------------------------------------
Vector Time (GMT): 2013/228/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1369069
11 A = 6789529
31 meter
Y = 4311171
45 meter E =
0009997
Z = -5071988
82 I = 51
68756
XDOT = -7424
314485 Wp = 90
42571
YDOT = -177
953104 meter/sec RA = 169
98538 deg
ZDOT = 1855
862765 TA = 197
55514
MA = 197
58972
Ha = 226
469 n
mi
Hp = 221
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4491696
55 X = -1392537
69
Y = 14144263
28 feet Y = 4295730
57 meter
Z = -16640383
25 Z = -5078696
45
XDOT = -24357
987156 XDOT = -7430
787979
YDOT = -583
835644 feet/sec YDOT = -261
012740 meter/sec
ZDOT = 6088
788599 ZDOT = 1819
780715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2614934
39 X = 797032
00
Y = 14575440
57 feet Y = 4442594
28 meter
Z = -16669028
97 Z = -5080720
03
XDOT = -20862
379847 XDOT = -6358
853377
YDOT = 10521
690098 feet/sec YDOT = 3207
011142 meter/sec
ZDOT = 5937
570117 ZDOT = 1809
771372
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 13228
18937554
00016717 00000-0 10270-3 0 9094
2 25544 51
6473 171
0281 0004157 317
9442 42
1390 15
50325769 4012
Satellite: ISS
Catalog Number: 25544
Epoch time: 13228
18937554 = yrday
fracday
Element set: 909
Inclination: 51
6473 deg
RA of node: 171
0281 deg
Eccentricity:
0004157
Arg of perigee: 317
9442 deg
Mean anomaly: 42
1390 deg
Mean motion: 15
50325769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 401
Checksum: 300
Coasting Arc #11 (Orbit 416)
---------------------------------------
Vector Time (GMT): 2013/229/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1565468
79 A = 6790036
64 meter
Y = -4425853
14 meter E =
0007376
Z = 4905500
12 I = 51
72044
XDOT = 7293
194308 Wp = 24
49548
YDOT = -31
747041 meter/sec RA = 165
03057 deg
ZDOT = -2348
265670 TA = 88
52771
MA = 88
44322
Ha = 226
422 n
mi
Hp = 221
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5136052
45 X = 1591014
03
Y = -14520515
56 feet Y = -4408204
38 meter
Z = 16094160
51 Z = 4913166
85
XDOT = 23927
802847 XDOT = 7304
414345
YDOT = -104
156959 feet/sec YDOT = 49
872877 meter/sec
ZDOT = -7704
283695 ZDOT = -2312
809225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2474412
26 X = -754200
86
Y = -15167350
97 feet Y = -4623008
58 meter
Z = 16126845
88 Z = 4915462
62
XDOT = 19934
873176 XDOT = 6076
149344
YDOT = -11313
025166 feet/sec YDOT = -3448
210071 meter/sec
ZDOT = -7555
640121 ZDOT = -2302
959109
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 13229
22072063
00016717 00000-0 10270-3 0 9107
2 25544 51
6478 165
9162 0004216 320
7880 39
2965 15
50383228 4177
Satellite: ISS
Catalog Number: 25544
Epoch time: 13229
22072063 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 165
9162 deg
Eccentricity:
0004216
Arg of perigee: 320
7880 deg
Mean anomaly: 39
2965 deg
Mean motion: 15
50383228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 417
Checksum: 298
Coasting Arc #12 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2013/230/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1720317
70 A = 6790861
36 meter
Y = 4578903
28 meter E =
0008018
Z = -4717611
03 I = 51
75268
XDOT = -7116
840759 Wp = 90
87993
YDOT = 220
568571 meter/sec RA = 160
07799 deg
ZDOT = 2813
317997 TA = 206
99785
MA = 207
03959
Ha = 226
656 n
mi
Hp = 221
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5644086
96 X = -1748475
68
Y = 15022648
56 feet Y = 4559508
23 meter
Z = -15477726
49 Z = -4726036
36
XDOT = -23349
215087 XDOT = -7132
444353
YDOT = 723
650167 feet/sec YDOT = 140
896263 meter/sec
ZDOT = 9230
045923 ZDOT = 2778
707762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2535309
71 X = 772762
40
Y = 15811250
43 feet Y = 4819269
13 meter
Z = -15513615
60 Z = -4728550
03
XDOT = -18887
210774 XDOT = -5756
821844
YDOT = 11929
523511 feet/sec YDOT = 3636
118766 meter/sec
ZDOT = 9084
905964 ZDOT = 2769
079338
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 13230
18759851
00016717 00000-0 10270-3 0 9112
2 25544 51
6480 161
1235 0004167 327
1476 32
9415 15
50366537 4327
Satellite: ISS
Catalog Number: 25544
Epoch time: 13230
18759851 = yrday
fracday
Element set: 911
Inclination: 51
6480 deg
RA of node: 161
1235 deg
Eccentricity:
0004167
Arg of perigee: 327
1476 deg
Mean anomaly: 32
9415 deg
Mean motion: 15
50366537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 293
Coasting Arc #13 (Orbit 447)
---------------------------------------
Vector Time (GMT): 2013/231/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1880815
28 A = 6791658
21 meter
Y = -4752201
60 meter E =
0009402
Z = 4471150
22 I = 51
78457
XDOT = 6915
259866 Wp = 42
67191
YDOT = -359
255658 meter/sec RA = 155
12835 deg
ZDOT = -3279
995811 TA = 80
39521
MA = 80
28899
Ha = 226
642 n
mi
Hp = 221
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6170653
80 X = 1912096
47
Y = -15591212
60 feet Y = -4730994
19 meter
Z = 14669128
01 Z = 4480362
87
XDOT = 22687
860453 XDOT = 6934
696176
YDOT = -1178
660294 feet/sec YDOT = -281
816189 meter/sec
ZDOT = -10761
141111 ZDOT = -3246
355610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2635721
01 X = -803367
76
Y = -16524642
32 feet Y = -5036710
98 meter
Z = 14708343
42 Z = 4483103
07
XDOT = 17831
350805 XDOT = 5434
995725
YDOT = -12328
295785 feet/sec YDOT = -3757
664555 meter/sec
ZDOT = -10620
033072 ZDOT = -3236
986080
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 13231
21892104
00016717 00000-0 10270-3 0 9127
2 25544 51
6481 156
0118 0004224 330
3226 29
7685 15
50416115 4482
Satellite: ISS
Catalog Number: 25544
Epoch time: 13231
21892104 = yrday
fracday
Element set: 912
Inclination: 51
6481 deg
RA of node: 156
0118 deg
Eccentricity:
0004224
Arg of perigee: 330
3226 deg
Mean anomaly: 29
7685 deg
Mean motion: 15
50416115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 448
Checksum: 273
Coasting Arc #14 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2013/232/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1984659
94 A = 6792644
01 meter
Y = 4952382
63 meter E =
0005902
Z = -4208462
01 I = 51
81634
XDOT = -6682
994403 Wp = 79
55483
YDOT = 468
623703 meter/sec RA = 150
18094 deg
ZDOT = 3708
544414 TA = 228
45501
MA = 228
50565
Ha = 226
822 n
mi
Hp = 220
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6511351
51 X = -2019447
94
Y = 16247974
52 feet Y = 4929994
26 meter
Z = -13807290
06 Z = -4218187
75
XDOT = -21925
834657 XDOT = -6705
752669
YDOT = 1537
479339 feet/sec YDOT = 393
763096 meter/sec
ZDOT = 12167
140467 ZDOT = 3676
024457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2965809
93 X = 903978
87
Y = 17217826
01 feet Y = 5247993
37 meter
Z = -13848684
86 Z = -4221079
14
XDOT = -16732
577809 XDOT = -5100
089716
YDOT = 12544
414504 feet/sec YDOT = 3823
537541 meter/sec
ZDOT = 12030
701721 ZDOT = 3666
957884
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 13232
18577732
00016717 00000-0 10270-3 0 9132
2 25544 51
6491 151
2192 0004186 335
9750 24
1205 15
50410009 4632
Satellite: ISS
Catalog Number: 25544
Epoch time: 13232
18577732 = yrday
fracday
Element set: 913
Inclination: 51
6491 deg
RA of node: 151
2192 deg
Eccentricity:
0004186
Arg of perigee: 335
9750 deg
Mean anomaly: 24
1205 deg
Mean motion: 15
50410009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 278
Coasting Arc #15 (Orbit 478)
---------------------------------------
Vector Time (GMT): 2013/233/04:14:00
403
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2089598
34 A = 6793640
21 meter
Y = -5164658
69 meter E =
0011144
Z = 3883899
13 I = 51
84542
XDOT = 6432
823353 Wp = 59
51643
YDOT = -514
489186 meter/sec RA = 145
23627 deg
ZDOT = -4130
771230 TA = 73
82683
MA = 73
70421
Ha = 226
851 n
mi
Hp = 220
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6855637
61 X = 2128328
83
Y = -16944418
27 feet Y = -5141074
70 meter
Z = 12742451
22 Z = 3894144
37
XDOT = 21105
063495 XDOT = 6458
164147
YDOT = -1687
956648 feet/sec YDOT = -442
411820 meter/sec
ZDOT = -13552
399049 ZDOT = -4099
460210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3337648
56 X = -1017315
28
Y = -17940458
84 feet Y = -5468251
85 meter
Z = 12786054
10 Z = 3897189
29
XDOT = 15690
973873 XDOT = 4782
608836
YDOT = -12517
633259 feet/sec YDOT = -3815
374617 meter/sec
ZDOT = -13421
013218 ZDOT = -4090
724829
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 13233
21707733
00016717 00000-0 10270-3 0 9144
2 25544 51
6484 146
1073 0004249 339
5952 20
5028 15
50447927 4798
Satellite: ISS
Catalog Number: 25544
Epoch time: 13233
21707733 = yrday
fracday
Element set: 914
Inclination: 51
6484 deg
RA of node: 146
1073 deg
Eccentricity:
0004249
Arg of perigee: 339
5952 deg
Mean anomaly: 20
5028 deg
Mean motion: 15
50447927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 479
Checksum: 306
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