[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 25th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 185 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 49)
---------------------------------------
Vector Time (GMT): 2013/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2525360
08 A = 6800505
05 meter
Y = -6156244
51 meter E =
0009530
Z = 1384583
32 I = 51
32144
XDOT = 4065
962367 Wp = 68
19254
YDOT = 2972
450157 meter/sec RA = 282
71519 deg
ZDOT = 5771
751746 TA = 306
93409
MA = 307
02135
Ha = 226
938 n
mi
Hp = 222
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8285302
12 X = 2587287
08
Y = -20197652
58 feet Y = -6127658
15 meter
Z = 4542596
19 Z = 1397001
12
XDOT = 13339
771544 XDOT = 4004
384627
YDOT = 9752
133062 feet/sec YDOT = 3017
573739 meter/sec
ZDOT = 18936
193392 ZDOT = 5791
353953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21531742
14 X = -6562875
00
Y = 3534465
24 feet Y = 1077305
01 meter
Z = 4595456
13 Z = 1400695
03
XDOT = 1649
080712 XDOT = 502
639801
YDOT = -14801
237510 feet/sec YDOT = -4511
417193 meter/sec
ZDOT = 19017
777464 ZDOT = 5796
618571
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 13205
56174575
00016717 00000-0 10270-3 0 9008
2 25544 51
6499 283
1451 0004542 224
4310 135
6477 15
50008611 506
Satellite: ISS
Catalog Number: 25544
Epoch time: 13205
56174575 = yrday
fracday
Element set: 900
Inclination: 51
6499 deg
RA of node: 283
1451 deg
Eccentricity:
0004542
Arg of perigee: 224
4310 deg
Mean anomaly: 135
6477 deg
Mean motion: 15
50008611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 50
Checksum: 278
Coasting Arc #2 (Orbit 64)
---------------------------------------
Vector Time (GMT): 2013/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2239639
95 A = 6800008
53 meter
Y = 6176461
95 meter E =
0009019
Z = -1732493
23 I = 51
31275
XDOT = -4149
439499 Wp = 171
48584
YDOT = -3086
964550 meter/sec RA = 277
74041 deg
ZDOT = -5653
696228 TA = 27
58043
MA = 27
53261
Ha = 226
749 n
mi
Hp = 222
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7347900
11 X = -2300124
22
Y = 20263982
77 feet Y = 6151078
74 meter
Z = -5684032
90 Z = -1743519
71
XDOT = -13613
646650 XDOT = -4087
148413
YDOT = -10127
836451 feet/sec YDOT = -3133
017752 meter/sec
ZDOT = -18548
872140 ZDOT = -5673
702226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21015541
09 X = 6405536
92
Y = -4736119
67 feet Y = -1443569
27 meter
Z = -5731061
58 Z = -1746827
57
XDOT = -1622
961963 XDOT = -494
678806
YDOT = 15295
366516 feet/sec YDOT = 4662
027714 meter/sec
ZDOT = -18632
136563 ZDOT = -5679
075224
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 13206
52883458
00016717 00000-0 10270-3 0 9013
2 25544 51
6486 278
3546 0004506 227
9138 132
1630 15
50020383 658
Satellite: ISS
Catalog Number: 25544
Epoch time: 13206
52883458 = yrday
fracday
Element set: 901
Inclination: 51
6486 deg
RA of node: 278
3546 deg
Eccentricity:
0004506
Arg of perigee: 227
9138 deg
Mean anomaly: 132
1630 deg
Mean motion: 15
50020383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 65
Checksum: 295
Coasting Arc #3 (Orbit 80)
---------------------------------------
Vector Time (GMT): 2013/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1945271
45 A = 6799461
85 meter
Y = -6178722
78 meter E =
0009760
Z = 2053930
09 I = 51
30793
XDOT = 4265
543115 Wp = 76
57340
YDOT = 3181
584463 meter/sec RA = 272
76414 deg
ZDOT = 5511
148390 TA = 306
20944
MA = 306
29965
Ha = 226
637 n
mi
Hp = 222
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6382124
16 X = 2004241
41
Y = -20271400
20 feet Y = -6156639
85 meter
Z = 6738615
77 Z = 2063523
00
XDOT = 13994
564025 XDOT = 4202
877680
YDOT = 10438
269236 feet/sec YDOT = 3228
933974 meter/sec
ZDOT = 18081
195506 ZDOT = 5531
717540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20400025
73 X = -6217927
84
Y = 5911481
38 feet Y = 1801819
53 meter
Z = 6779635
34 Z = 2066432
85
XDOT = 1465
769510 XDOT = 446
766547
YDOT = -15851
130909 feet/sec YDOT = -4831
424701 meter/sec
ZDOT = 18166
809281 ZDOT = 5537
243469
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 13207
56038719
00016717 00000-0 10270-3 0 9021
2 25544 51
6487 273
2439 0004399 232
7358 127
3392 15
50032805 813
Satellite: ISS
Catalog Number: 25544
Epoch time: 13207
56038719 = yrday
fracday
Element set: 902
Inclination: 51
6487 deg
RA of node: 273
2439 deg
Eccentricity:
0004399
Arg of perigee: 232
7358 deg
Mean anomaly: 127
3392 deg
Mean motion: 15
50032805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 81
Checksum: 308
Coasting Arc #4 (Orbit 95)
---------------------------------------
Vector Time (GMT): 2013/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1680056
34 A = 6798768
78 meter
Y = 6134513
24 meter E =
0006214
Z = -2391496
57 I = 51
30477
XDOT = -4405
681299 Wp = 175
65173
YDOT = -3284
729029 meter/sec RA = 267
78758 deg
ZDOT = -5337
722906 TA = 31
15153
MA = 31
11471
Ha = 226
448 n
mi
Hp = 222
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5511995
87 X = -1736911
84
Y = 20126355
79 feet Y = 6115407
94 meter
Z = -7846117
37 Z = -2399796
01
XDOT = -14454
334970 XDOT = -4342
694410
YDOT = -10776
670043 feet/sec YDOT = -3333
643861 meter/sec
ZDOT = -17512
214258 ZDOT = -5358
972121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19678828
88 X = 5998107
04
Y = -6901898
53 feet Y = -2103698
67 meter
Z = -7881709
48 Z = -2402345
05
XDOT = -1255
884596 XDOT = -382
793625
YDOT = 16492
413479 feet/sec YDOT = 5026
887628 meter/sec
ZDOT = -17600
665221 ZDOT = -5364
682759
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 13208
52746070
00016717 00000-0 10270-3 0 9035
2 25544 51
6482 268
4527 0004307 236
5157 123
5582 15
50051765 961
Satellite: ISS
Catalog Number: 25544
Epoch time: 13208
52746070 = yrday
fracday
Element set: 903
Inclination: 51
6482 deg
RA of node: 268
4527 deg
Eccentricity:
0004307
Arg of perigee: 236
5157 deg
Mean anomaly: 123
5582 deg
Mean motion: 15
50051765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 96
Checksum: 300
Coasting Arc #5 (Orbit 111)
---------------------------------------
Vector Time (GMT): 2013/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1414668
58 A = 6798100
90 meter
Y = -6071908
36 meter E =
0009559
Z = 2700883
31 I = 51
30456
XDOT = 4576
671612 Wp = 86
15227
YDOT = 3360
967119 meter/sec RA = 262
81041 deg
ZDOT = 5143
504827 TA = 304
46635
MA = 304
55662
Ha = 226
366 n
mi
Hp = 222
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4641301
13 X = 1469340
81
Y = -19920959
19 feet Y = -6055783
02 meter
Z = 8861165
70 Z = 2707888
20
XDOT = 15015
326812 XDOT = 4513
762884
YDOT = 11026
795009 feet/sec YDOT = 3411
794476 meter/sec
ZDOT = 16875
015838 ZDOT = 5165
584963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18880653
44 X = -5754823
17
Y = 7834016
28 feet Y = 2387808
16 meter
Z = 8891325
17 Z = 2710075
91
XDOT = 890
903509 XDOT = 271
547389
YDOT = -17166
048687 feet/sec YDOT = -5232
211640 meter/sec
ZDOT = 16966
939576 ZDOT = 5171
523183
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 13209
55899737
00016717 00000-0 10270-3 0 9049
2 25544 51
6480 263
3419 0004205 241
0722 119
0008 15
50054802 1126
Satellite: ISS
Catalog Number: 25544
Epoch time: 13209
55899737 = yrday
fracday
Element set: 904
Inclination: 51
6480 deg
RA of node: 263
3419 deg
Eccentricity:
0004205
Arg of perigee: 241
0722 deg
Mean anomaly: 119
0008 deg
Mean motion: 15
50054802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 112
Checksum: 279
Coasting Arc #6 (Orbit 126)
---------------------------------------
Vector Time (GMT): 2013/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1187650
29 A = 6797245
36 meter
Y = 5970451
21 meter E =
0003276
Z = -3020575
49 I = 51
30731
XDOT = -4767
254051 Wp = 170
95967
YDOT = -3432
945547 meter/sec RA = 257
83312 deg
ZDOT = -4915
021338 TA = 43
75453
MA = 43
72858
Ha = 226
193 n
mi
Hp = 222
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3896490
46 X = -1239651
89
Y = 19588094
51 feet Y = 5956879
51 meter
Z = -9910024
57 Z = -3026471
02
XDOT = -15640
597279 XDOT = -4704
636146
YDOT = -11262
944707 feet/sec YDOT = -3485
905691 meter/sec
ZDOT = -16125
398089 ZDOT = -4938
028078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18028673
13 X = 5495139
57
Y = -8563703
50 feet Y = -2610216
83 meter
Z = -9935522
07 Z = -3028347
13
XDOT = -440
370372 XDOT = -134
224889
YDOT = 17877
763047 feet/sec YDOT = 5449
142177 meter/sec
ZDOT = -16221
196868 ZDOT = -4944
220805
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 13210
52605567
00016717 00000-0 10270-3 0 9055
2 25544 51
6486 258
5506 0004132 245
1555 114
9167 15
50082589 1272
Satellite: ISS
Catalog Number: 25544
Epoch time: 13210
52605567 = yrday
fracday
Element set: 905
Inclination: 51
6486 deg
RA of node: 258
5506 deg
Eccentricity:
0004132
Arg of perigee: 245
1555 deg
Mean anomaly: 114
9167 deg
Mean motion: 15
50082589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 127
Checksum: 301
Coasting Arc #7 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2013/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 968723
30 A = 6796492
78 meter
Y = -5852603
57 meter E =
0008900
Z = 3310207
27 I = 51
31138
XDOT = 4984
299179 Wp = 96
76498
YDOT = 3472
581988 meter/sec RA = 252
85579 deg
ZDOT = 4669
167936 TA = 301
86353
MA = 301
95012
Ha = 226
148 n
mi
Hp = 222
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3178226
05 X = 1018016
43
Y = -19201455
30 feet Y = -5841495
25 meter
Z = 10860260
09 Z = 3315032
64
XDOT = 16352
687594 XDOT = 4922
416200
YDOT = 11392
985524 feet/sec YDOT = 3527
973328 meter/sec
ZDOT = 15318
792440 ZDOT = 4693
230883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17131236
14 X = -5221600
77
Y = 9212015
50 feet Y = 2807822
32 meter
Z = 10881257
94 Z = 3316607
42
XDOT = -175
544375 XDOT = -53
505926
YDOT = -18585
386231 feet/sec YDOT = -5664
825723 meter/sec
ZDOT = 15419
015002 ZDOT = 4699
715773
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 13211
55757677
00016717 00000-0 10270-3 0 9060
2 25544 51
6478 253
4398 0004002 249
5927 110
4794 15
50077102 1433
Satellite: ISS
Catalog Number: 25544
Epoch time: 13211
55757677 = yrday
fracday
Element set: 906
Inclination: 51
6478 deg
RA of node: 253
4398 deg
Eccentricity:
0004002
Arg of perigee: 249
5927 deg
Mean anomaly: 110
4794 deg
Mean motion: 15
50077102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 143
Checksum: 307
Coasting Arc #8 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2013/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -795232
98 A = 6795541
52 meter
Y = 5706372
38 meter E =
0001521
Z = -3604260
74 I = 51
31956
XDOT = -5212
871857 Wp = 105
71728
YDOT = -3496
394754 meter/sec RA = 247
87868 deg
ZDOT = -4387
399227 TA = 117
07749
MA = 117
06198
Ha = 225
997 n
mi
Hp = 222
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2609032
09 X = -841475
42
Y = 18721694
16 feet Y = 5697221
25 meter
Z = -11825002
44 Z = -3608235
85
XDOT = -17102
597955 XDOT = -5152
074384
YDOT = -11471
111397 feet/sec YDOT = -3554
348178 meter/sec
ZDOT = -14394
354419 ZDOT = -4412
575190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16236781
23 X = 4948970
92
Y = -9657311
23 feet Y = -2943548
46 meter
Z = -11842416
92 Z = -3609568
68
XDOT = 892
947863 XDOT = 272
170509
YDOT = 19273
357987 feet/sec YDOT = 5874
519515 meter/sec
ZDOT = -14499
243039 ZDOT = -4419
369278
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 13212
52461980
00016717 00000-0 10270-3 0 9078
2 25544 51
6489 248
6486 0004014 253
7971 106
2738 15
50109544 1581
Satellite: ISS
Catalog Number: 25544
Epoch time: 13212
52461980 = yrday
fracday
Element set: 907
Inclination: 51
6489 deg
RA of node: 248
6486 deg
Eccentricity:
0004014
Arg of perigee: 253
7971 deg
Mean anomaly: 106
2738 deg
Mean motion: 15
50109544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 158
Checksum: 313
Coasting Arc #9 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2013/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 637174
65 A = 6794740
51 meter
Y = -5547967
31 meter E =
0007754
Z = 3866341
54 I = 51
32781
XDOT = 5461
257870 Wp = 108
52040
YDOT = 3484
725726 meter/sec RA = 242
90155 deg
ZDOT = 4091
167220 TA = 298
29018
MA = 298
36840
Ha = 225
984 n
mi
Hp = 222
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2090468
01 X = 680384
45
Y = -18201992
50 feet Y = -5540600
68 meter
Z = 12684847
58 Z = 3869541
42
XDOT = 17917
512696 XDOT = 5402
011468
YDOT = 11432
827184 feet/sec YDOT = 3545
465428 meter/sec
ZDOT = 13422
464632 ZDOT = 4117
553535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15334032
55 X = -4673813
12
Y = 10009546
96 feet Y = 3050909
91 meter
Z = 12698990
55 Z = 3870652
32
XDOT = -1770
077477 XDOT = -539
519615
YDOT = -19918
284876 feet/sec YDOT = -6071
093230 meter/sec
ZDOT = 13532
434091 ZDOT = 4124
685911
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 13213
55612524
00016717 00000-0 10270-3 0 9085
2 25544 51
6475 243
5377 0003870 258
4360 101
6356 15
50101187 1740
Satellite: ISS
Catalog Number: 25544
Epoch time: 13213
55612524 = yrday
fracday
Element set: 908
Inclination: 51
6475 deg
RA of node: 243
5377 deg
Eccentricity:
0003870
Arg of perigee: 258
4360 deg
Mean anomaly: 101
6356 deg
Mean motion: 15
50101187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 174
Checksum: 289
Coasting Arc #10 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2013/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -528400
34 A = 6793780
59 meter
Y = 5373938
68 meter E =
0003713
Z = -4126862
05 I = 51
34058
XDOT = -5710
147489 Wp = 58
85174
YDOT = -3448
019327 meter/sec RA = 237
92519 deg
ZDOT = -3759
472966 TA = 172
19159
MA = 172
18580
Ha = 225
864 n
mi
Hp = 222
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1733596
93 X = -568406
73
Y = 17631032
43 feet Y = 5367806
37 meter
Z = -13539573
67 Z = -4129525
75
XDOT = -18734
079689 XDOT = -5652
904359
YDOT = -11312
399366 feet/sec YDOT = -3511
553492 meter/sec
ZDOT = -12334
228890 ZDOT = -3787
073142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14490044
45 X = 4416565
55
Y = -10177216
18 feet Y = -3102015
49 meter
Z = -13551442
75 Z = -4130479
75
XDOT = 2744
974422 XDOT = 836
668204
YDOT = 20482
272040 feet/sec YDOT = 6242
996518 meter/sec
ZDOT = -12449
299730 ZDOT = -3794
546558
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 13214
52315297
00016717 00000-0 10270-3 0 9091
2 25544 51
6483 238
7467 0003964 262
4674 97
6026 15
50131462 1895
Satellite: ISS
Catalog Number: 25544
Epoch time: 13214
52315297 = yrday
fracday
Element set: 909
Inclination: 51
6483 deg
RA of node: 238
7467 deg
Eccentricity:
0003964
Arg of perigee: 262
4674 deg
Mean anomaly: 97
6026 deg
Mean motion: 15
50131462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 189
Checksum: 320
Coasting Arc #11 (Orbit 204)
---------------------------------------
Vector Time (GMT): 2013/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 440951
54 A = 6792977
57 meter
Y = -5193631
51 meter E =
0006154
Z = 4353600
83 I = 51
35330
XDOT = 5970
482476 Wp = 121
90391
YDOT = 3375
617350 meter/sec RA = 232
94858 deg
ZDOT = 3415
472648 TA = 293
26090
MA = 293
32568
Ha = 225
866 n
mi
Hp = 222
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1446691
42 X = 477846
84
Y = -17039473
45 feet Y = -5188494
49 meter
Z = 14283467
28 Z = 4355832
18
XDOT = 19588
197101 XDOT = 5915
700692
YDOT = 11074
860073 feet/sec YDOT = 3442
076548 meter/sec
ZDOT = 11205
618924 ZDOT = 3444
343372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13676317
58 X = -4168541
60
Y = 10252235
24 feet Y = 3124881
30 meter
Z = 14293495
69 Z = 4356657
49
XDOT = -3857
303390 XDOT = -1175
706073
YDOT = -20967
033502 feet/sec YDOT = -6390
751812 meter/sec
ZDOT = 11326
035330 ZDOT = 3452
175568
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 13215
55464234
00016717 00000-0 10270-3 0 9103
2 25544 51
6466 233
6353 0003858 267
4903 92
5806 15
50126304 2054
Satellite: ISS
Catalog Number: 25544
Epoch time: 13215
55464234 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 233
6353 deg
Eccentricity:
0003858
Arg of perigee: 267
4903 deg
Mean anomaly: 92
5806 deg
Mean motion: 15
50126304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 205
Checksum: 291
Coasting Arc #12 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2013/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -402474
20 A = 6792097
35 meter
Y = 5011912
73 meter E =
0006421
Z = -4572805
54 I = 51
37010
XDOT = -6218
372781 Wp = 57
15927
YDOT = -3272
263683 meter/sec RA = 227
97329 deg
ZDOT = -3038
883506 TA = 182
30057
MA = 182
30352
Ha = 225
808 n
mi
Hp = 222
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1320453
42 X = -436275
57
Y = 16443283
25 feet Y = 5007223
26 meter
Z = -15002642
83 Z = -4574842
52
XDOT = -20401
485501 XDOT = -6166
557666
YDOT = -10735
773239 feet/sec YDOT = -3341
511588 meter/sec
ZDOT = -9970
090242 ZDOT = -3068
965538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12969506
19 X = 3953105
49
Y = -10180443
84 feet Y = -3102999
28 meter
Z = -15011826
19 Z = -4575604
62
XDOT = 5043
697515 XDOT = 1537
319002
YDOT = 21313
633798 feet/sec YDOT = 6496
395582 meter/sec
ZDOT = -10095
609808 ZDOT = -3077
141869
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 13216
52165483
00016717 00000-0 10270-3 0 9116
2 25544 51
6469 228
8441 0003962 271
2342 88
8354 15
50149726 2203
Satellite: ISS
Catalog Number: 25544
Epoch time: 13216
52165483 = yrday
fracday
Element set: 911
Inclination: 51
6469 deg
RA of node: 228
8441 deg
Eccentricity:
0003962
Arg of perigee: 271
2342 deg
Mean anomaly: 88
8354 deg
Mean motion: 15
50149726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 220
Checksum: 303
Coasting Arc #13 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2013/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 389429
56 A = 6791354
56 meter
Y = -4830781
92 meter E =
0004230
Z = 4756461
48 I = 51
38763
XDOT = 6468
385578 Wp = 138
16131
YDOT = 3136
310852 meter/sec RA = 222
99783 deg
ZDOT = 2651
267468 TA = 285
53004
MA = 285
57674
Ha = 225
810 n
mi
Hp = 222
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1277656
04 X = 420314
35
Y = -15849022
04 feet Y = -4826254
57 meter
Z = 15605188
59 Z = 4758428
09
XDOT = 21221
737462 XDOT = 6419
955053
YDOT = 10289
733766 feet/sec YDOT = 3208
373542 meter/sec
ZDOT = 8698
384080 ZDOT = 2682
572137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12328588
00 X = -3757753
62
Y = 10027626
63 feet Y = 3056420
60 meter
Z = 15614046
16 Z = 4759161
27
XDOT = -6329
944290 XDOT = -1929
367020
YDOT = -21552
939065 feet/sec YDOT = -6569
335827 meter/sec
ZDOT = 8829
059217 ZDOT = 2691
097249
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 13217
55312771
00016717 00000-0 10270-3 0 9125
2 25544 51
6456 223
7323 0003942 276
4864 83
5838 15
50151046 2360
Satellite: ISS
Catalog Number: 25544
Epoch time: 13217
55312771 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 223
7323 deg
Eccentricity:
0003942
Arg of perigee: 276
4864 deg
Mean anomaly: 83
5838 deg
Mean motion: 15
50151046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 236
Checksum: 299
Coasting Arc #14 (Orbit 250)
---------------------------------------
Vector Time (GMT): 2013/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -420348
65 A = 6790629
70 meter
Y = 4662719
81 meter E =
0008775
Z = -4927019
01 I = 51
40843
XDOT = -6692
409499 Wp = 62
03686
YDOT = -2967
546185 meter/sec RA = 218
02401 deg
ZDOT = -2236
424997 TA = 186
00830
MA = 186
01884
Ha = 225
840 n
mi
Hp = 222
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1379096
62 X = -448523
34
Y = 15297637
16 feet Y = 4657861
77 meter
Z = -16164760
55 Z = -4929129
32
XDOT = -21956
724077 XDOT = -6647
864642
YDOT = -9736
043913 feet/sec YDOT = -3042
135834 meter/sec
ZDOT = -7337
352353 ZDOT = -2268
827294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11828604
17 X = 3605358
55
Y = -9782574
50 feet Y = -2981728
71 meter
Z = -16174190
96 Z = -4929893
40
XDOT = 7648
710256 XDOT = 2331
326886
YDOT = 21608
763126 feet/sec YDOT = 6586
351001 meter/sec
ZDOT = -7472
663704 ZDOT = -2277
667897
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 13218
52012492
00016717 00000-0 10270-3 0 9131
2 25544 51
6456 218
9407 0003983 280
1658 79
9044 15
50167511 2516
Satellite: ISS
Catalog Number: 25544
Epoch time: 13218
52012492 = yrday
fracday
Element set: 913
Inclination: 51
6456 deg
RA of node: 218
9407 deg
Eccentricity:
0003983
Arg of perigee: 280
1658 deg
Mean anomaly: 79
9044 deg
Mean motion: 15
50167511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 251
Checksum: 301
Coasting Arc #15 (Orbit 266)
---------------------------------------
Vector Time (GMT): 2013/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 478784
90 A = 6790020
98 meter
Y = -4502355
04 meter E =
0002174
Z = 5060042
96 I = 51
43070
XDOT = 6909
160497 Wp = 162
64776
YDOT = 2772
613567 meter/sec RA = 213
05070 deg
ZDOT = 1811
048155 TA = 269
74262
MA = 269
76753
Ha = 225
842 n
mi
Hp = 222
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1570816
61 X = 504515
82
Y = -14771506
03 feet Y = -4496857
10 meter
Z = 16601190
82 Z = 5062431
30
XDOT = 22667
849399 XDOT = 6868
845624
YDOT = 9096
501205 feet/sec YDOT = 2849
650760 meter/sec
ZDOT = 5941
759038 ZDOT = 1844
513626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11423323
45 X = -3481828
99
Y = 9477423
17 feet Y = 2888718
58 meter
Z = 16611758
58 Z = 5063264
02
XDOT = -9017
850135 XDOT = -2748
640721
YDOT = -21541
827686 feet/sec YDOT = -6565
949079 meter/sec
ZDOT = 6081
564750 ZDOT = 1853
660936
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
55158100
00016717 00000-0 10270-3 0 9143
2 25544 51
6450 213
8288 0004054 285
2863 74
7839 15
50175349 2675
Satellite: ISS
Catalog Number: 25544
Epoch time: 13219
55158100 = yrday
fracday
Element set: 914
Inclination: 51
6450 deg
RA of node: 213
8288 deg
Eccentricity:
0004054
Arg of perigee: 285
2863 deg
Mean anomaly: 74
7839 deg
Mean motion: 15
50175349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 267
Checksum: 312
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