[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 16th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 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
258/12:43:42
120 1
7 1
7 1
7
N/A 0
2 -0
3 227
9
000/00:03:24
239 0
0 -0
0 220
0
Coasting Arc #1 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2013/256/13:04:07
307
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6173747
48 A = 6797151
42 meter
Y = 1225018
28 meter E =
0008899
Z = -2563895
43 I = 51
84106
XDOT = 1110
583022 Wp = 53
07205
YDOT = 5429
469670 meter/sec RA = 29
89078 deg
ZDOT = 5286
289178 TA = 278
25700
MA = 278
35791
Ha = 227
963 n
mi
Hp = 219
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20255077
04 X = 6172044
89
Y = 4019088
84 feet Y = 1294047
39 meter
Z = -8411730
40 Z = -2533908
18
XDOT = 3643
645084 XDOT = 1024
107656
YDOT = 17813
220702 feet/sec YDOT = 5441
405673 meter/sec
ZDOT = 17343
468431 ZDOT = 5291
473956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20666481
55 X = -6299143
58
Y = -1189913
17 feet Y = -362685
54 meter
Z = -8286077
25 Z = -2525596
35
XDOT = -6037
027078 XDOT = -1840
085853
YDOT = -15652
663975 feet/sec YDOT = -4770
931979 meter/sec
ZDOT = 17364
401474 ZDOT = 5292
669569
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 13256
54959776
00016717 00000-0 10270-3 0 9006
2 25544 51
6496 30
4612 0003658 58
3494 301
8014 15
50516749 8417
Satellite: ISS
Catalog Number: 25544
Epoch time: 13256
54959776 = yrday
fracday
Element set: 900
Inclination: 51
6496 deg
RA of node: 30
4612 deg
Eccentricity:
0003658
Arg of perigee: 58
3494 deg
Mean anomaly: 301
8014 deg
Mean motion: 15
50516749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 841
Checksum: 317
Coasting Arc #2 (Orbit 856)
---------------------------------------
Vector Time (GMT): 2013/257/13:04:07
307
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6363125
87 A = 6798064
76 meter
Y = -1166181
49 meter E =
0016591
Z = 2068231
78 I = 51
81708
XDOT = -859
729320 Wp = 101
59901
YDOT = -5214
661925 meter/sec RA = 24
94771 deg
ZDOT = -5550
929432 TA = 55
60723
MA = 55
45046
Ha = 227
955 n
mi
Hp = 219
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20876397
23 X = -6359659
30
Y = -3826054
76 feet Y = -1237318
49 meter
Z = 6785537
34 Z = 2037328
97
XDOT = -2820
634253 XDOT = -774
389182
YDOT = -17108
470881 feet/sec YDOT = -5223
799147 meter/sec
ZDOT = -18211
710736 ZDOT = -5554
898282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21257979
42 X = 6479432
13
Y = 549262
02 feet Y = 167415
07 meter
Z = 6656034
50 Z = 2028759
32
XDOT = 5357
318554 XDOT = 1632
910695
YDOT = 14936
337423 feet/sec YDOT = 4552
595646 meter/sec
ZDOT = -18227
571698 ZDOT = -5555
763854
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 13257
58081486
00016717 00000-0 10270-3 0 9016
2 25544 51
6496 25
3485 0003646 64
0058 296
1468 15
50533899 8576
Satellite: ISS
Catalog Number: 25544
Epoch time: 13257
58081486 = yrday
fracday
Element set: 901
Inclination: 51
6496 deg
RA of node: 25
3485 deg
Eccentricity:
0003646
Arg of perigee: 64
0058 deg
Mean anomaly: 296
1468 deg
Mean motion: 15
50533899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 857
Checksum: 336
Coasting Arc #3 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2013/258/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1457043
31 A = 6788642
07 meter
Y = -3949190
43 meter E =
0016950
Z = -5340630
52 I = 51
75548
XDOT = 7181
411791 Wp = 85
06475
YDOT = 2635
347667 meter/sec RA = 20
08088 deg
ZDOT = 11
964588 TA = 185
04081
MA = 185
05789
Ha = 227
894 n
mi
Hp = 220
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4780325
82 X = 1527038
85
Y = -12956661
52 feet Y = -3932505
92 meter
Z = -17521753
69 Z = -5333382
06
XDOT = 23561
062308 XDOT = 7151
350897
YDOT = 8646
153763 feet/sec YDOT = 2715
486696 meter/sec
ZDOT = 39
253899 ZDOT = 46
777706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3699863
37 X = -1127718
36
Y = 13346296
18 feet Y = 4067951
08 meter
Z = -17490735
67 Z = -5331176
23
XDOT = -23271
206244 XDOT = -7093
063663
YDOT = -6215
139105 feet/sec YDOT = -1894
374399 meter/sec
ZDOT = 184
939436 ZDOT = 56
369540
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 13258
54757299
00016717 00000-0 10270-3 0 9026
2 25544 51
6499 20
5549 0002510 54
9089 305
2297 15
50261077 8723
Satellite: ISS
Catalog Number: 25544
Epoch time: 13258
54757299 = yrday
fracday
Element set: 902
Inclination: 51
6499 deg
RA of node: 20
5549 deg
Eccentricity:
0002510
Arg of perigee: 54
9089 deg
Mean anomaly: 305
2297 deg
Mean motion: 15
50261077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 323
Coasting Arc #4 (Orbit 887)
---------------------------------------
Vector Time (GMT): 2013/259/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1635430
43 A = 6788633
48 meter
Y = 3896863
90 meter E =
0005301
Z = 5308888
14 I = 51
72711
XDOT = -7272
909229 Wp = 61
94465
YDOT = -2372
027492 meter/sec RA = 15
12820 deg
ZDOT = -496
513515 TA = 32
80405
MA = 32
77115
Ha = 227
922 n
mi
Hp = 219
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5365585
40 X = -1704673
39
Y = 12784986
55 feet Y = 3878188
88 meter
Z = 17417612
00 Z = 5300774
84
XDOT = -23861
250750 XDOT = -7243
432250
YDOT = -7782
242427 feet/sec YDOT = -2453
193020 meter/sec
ZDOT = -1628
981349 ZDOT = -531
772492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4069399
44 X = 1240352
95
Y = -13300028
75 feet Y = -4053848
76 meter
Z = 17382974
98 Z = 5298330
77
XDOT = 23578
442979 XDOT = 7186
709420
YDOT = 4880
232366 feet/sec YDOT = 1487
494825 meter/sec
ZDOT = -1776
572951 ZDOT = -541
499435
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 13259
57897820
00016717 00000-0 10270-3 0 9036
2 25544 51
6505 15
4429 0002513 56
8004 303
3387 15
50291642 8889
Satellite: ISS
Catalog Number: 25544
Epoch time: 13259
57897820 = yrday
fracday
Element set: 903
Inclination: 51
6505 deg
RA of node: 15
4429 deg
Eccentricity:
0002513
Arg of perigee: 56
8004 deg
Mean anomaly: 303
3387 deg
Mean motion: 15
50291642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 888
Checksum: 309
Coasting Arc #5 (Orbit 902)
---------------------------------------
Vector Time (GMT): 2013/260/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1820149
60 A = 6788898
19 meter
Y = -3898620
32 meter E =
0016446
Z = -5265678
46 I = 51
69822
XDOT = 7293
714132 Wp = 91
81911
YDOT = 2091
357370 meter/sec RA = 10
17518 deg
ZDOT = 974
888383 TA = 187
51418
MA = 187
53885
Ha = 227
913 n
mi
Hp = 219
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5971619
43 X = 1889188
63
Y = -12790749
10 feet Y = -3877880
89 meter
Z = -17275847
96 Z = -5256668
22
XDOT = 23929
508308 XDOT = 7265
050316
YDOT = 6861
408693 feet/sec YDOT = 2172
760169 meter/sec
ZDOT = 3198
452700 ZDOT = 1010
250465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4439744
00 X = -1353233
97
Y = 13449067
18 feet Y = 4099275
68 meter
Z = -17237450
19 Z = -5253974
82
XDOT = -23596
473806 XDOT = -7192
205216
YDOT = -3509
358106 feet/sec YDOT = -1069
652351 meter/sec
ZDOT = 3346
511935 ZDOT = 1020
016838
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 13260
54591436
00016717 00000-0 10270-3 0 9040
2 25544 51
6507 10
6520 0002608 60
0806 300
0604 15
50290413 9031
Satellite: ISS
Catalog Number: 25544
Epoch time: 13260
54591436 = yrday
fracday
Element set: 904
Inclination: 51
6507 deg
RA of node: 10
6520 deg
Eccentricity:
0002608
Arg of perigee: 60
0806 deg
Mean anomaly: 300
0604 deg
Mean motion: 15
50290413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 903
Checksum: 255
Coasting Arc #6 (Orbit 918)
---------------------------------------
Vector Time (GMT): 2013/261/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2018313
11 A = 6789218
70 meter
Y = 3914291
57 meter E =
0007304
Z = 5162610
68 I = 51
66949
XDOT = -7299
912591 Wp = 56
80109
YDOT = -1827
903147 meter/sec RA = 5
21881 deg
ZDOT = -1462
564188 TA = 47
30560
MA = 47
24411
Ha = 227
944 n
mi
Hp = 219
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6621762
16 X = -2087012
07
Y = 12842163
93 feet Y = 3891338
10 meter
Z = 16937699
07 Z = 5152638
52
XDOT = -23949
844460 XDOT = -7271
825307
YDOT = -5997
057570 feet/sec YDOT = -1909
378565 meter/sec
ZDOT = -4798
438936 ZDOT = -1497
957930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4841985
90 X = 1475837
30
Y = -13666005
31 feet Y = -4165398
42 meter
Z = 16895266
49 Z = 5149677
22
XDOT = 23530
967250 XDOT = 7172
238818
YDOT = 2199
691473 feet/sec YDOT = 670
465961 meter/sec
ZDOT = -4946
660860 ZDOT = -1507
742230
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 13261
57730347
00016717 00000-0 10270-3 0 9051
2 25544 51
6511 5
5403 0002598 61
6246 298
5167 15
50316553 9198
Satellite: ISS
Catalog Number: 25544
Epoch time: 13261
57730347 = yrday
fracday
Element set: 905
Inclination: 51
6511 deg
RA of node: 5
5403 deg
Eccentricity:
0002598
Arg of perigee: 61
6246 deg
Mean anomaly: 298
5167 deg
Mean motion: 15
50316553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 919
Checksum: 303
Coasting Arc #7 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2013/262/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2203860
22 A = 6789760
36 meter
Y = -3985933
74 meter E =
0015010
Z = -5048967
49 I = 51
64032
XDOT = 7236
959611 Wp = 97
63252
YDOT = 1560
559737 meter/sec RA =
26228 deg
ZDOT = 1929
906992 TA = 191
11641
MA = 191
14961
Ha = 227
932 n
mi
Hp = 219
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7230512
52 X = 2272794
58
Y = -13077210
44 feet Y = -3960904
06 meter
Z = -16564853
99 Z = -5038093
32
XDOT = 23743
305809 XDOT = 7209
596233
YDOT = 5119
946645 feet/sec YDOT = 1641
335296 meter/sec
ZDOT = 6331
715852 ZDOT = 1964
996868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5167704
26 X = -1575116
26
Y = 14075433
94 feet Y = 4290192
27 meter
Z = -16518629
59 Z = -5034878
30
XDOT = -23189
066239 XDOT = -7068
027390
YDOT = -921
990988 feet/sec YDOT = -281
022853 meter/sec
ZDOT = 6478
691889 ZDOT = 1974
705288
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 13262
54422447
00016717 00000-0 10270-3 0 9069
2 25544 51
6509
7496 0002704 65
2361 294
9071 15
50318584 9348
Satellite: ISS
Catalog Number: 25544
Epoch time: 13262
54422447 = yrday
fracday
Element set: 906
Inclination: 51
6509 deg
RA of node:
7496 deg
Eccentricity:
0002704
Arg of perigee: 65
2361 deg
Mean anomaly: 294
9071 deg
Mean motion: 15
50318584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 934
Checksum: 301
Coasting Arc #8 (Orbit 949)
---------------------------------------
Vector Time (GMT): 2013/263/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2397334
26 A = 6790384
42 meter
Y = 4070236
09 meter E =
0009666
Z = 4872495
42 I = 51
61204
XDOT = -7157
051372 Wp = 60
96685
YDOT = -1324
824792 meter/sec RA = 355
30233 deg
ZDOT = -2406
471539 TA = 52
68564
MA = 52
59758
Ha = 227
942 n
mi
Hp = 219
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7865269
89 X = -2466339
78
Y = 13353792
93 feet Y = 4043042
42 meter
Z = 15985877
37 Z = 4860681
14
XDOT = -23481
139671 XDOT = -7130
014894
YDOT = -4346
538033 feet/sec YDOT = -1404
708655 meter/sec
ZDOT = -7895
247830 ZDOT = -2441
174214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5497661
14 X = 1675687
11
Y = -14545230
94 feet Y = -4433386
39 meter
Z = 15935699
24 Z = 4857201
13
XDOT = 22770
233158 XDOT = 6940
367067
YDOT = -232
392473 feet/sec YDOT = -70
833226 meter/sec
ZDOT = -8040
623620 ZDOT = -2450
782079
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 13263
57559729
00016717 00000-0 10270-3 0 9078
2 25544 51
6510 355
6378 0002649 65
8946 294
2481 15
50341955 9508
Satellite: ISS
Catalog Number: 25544
Epoch time: 13263
57559729 = yrday
fracday
Element set: 907
Inclination: 51
6510 deg
RA of node: 355
6378 deg
Eccentricity:
0002649
Arg of perigee: 65
8946 deg
Mean anomaly: 294
2481 deg
Mean motion: 15
50341955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 950
Checksum: 340
Coasting Arc #9 (Orbit 964)
---------------------------------------
Vector Time (GMT): 2013/264/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2559593
10 A = 6791160
39 meter
Y = -4207220
36 meter E =
0012805
Z = -4688340
59 I = 51
58312
XDOT = 7016
169372 Wp = 101
17606
YDOT = 1098
134251 meter/sec RA = 350
34212 deg
ZDOT = 2849
226743 TA = 197
17747
MA = 197
22085
Ha = 227
950 n
mi
Hp = 219
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8397615
16 X = 2629223
84
Y = -13803216
41 feet Y = -4178208
64 meter
Z = -15381694
86 Z = -4675736
53
XDOT = 23018
928385 XDOT = 6989
527422
YDOT = 3602
802662 feet/sec YDOT = 1176
444922 meter/sec
ZDOT = 9347
856770 ZDOT = 2883
246136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5678916
61 X = -1730933
78
Y = 15180313
07 feet Y = 4626959
42 meter
Z = -15328185
20 Z = -4672030
85
XDOT = -22117
823226 XDOT = -6741
512519
YDOT = 1294
646734 feet/sec YDOT = 394
608324 meter/sec
ZDOT = 9490
390269 ZDOT = 2892
670954
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 13264
54250317
00016717 00000-0 10270-3 0 9088
2 25544 51
6501 350
8469 0002801 70
2323 289
9129 15
50344901 9655
Satellite: ISS
Catalog Number: 25544
Epoch time: 13264
54250317 = yrday
fracday
Element set: 908
Inclination: 51
6501 deg
RA of node: 350
8469 deg
Eccentricity:
0002801
Arg of perigee: 70
2323 deg
Mean anomaly: 289
9129 deg
Mean motion: 15
50344901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 965
Checksum: 297
Coasting Arc #10 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2013/265/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2724524
63 A = 6792023
07 meter
Y = 4352218
71 meter E =
0012010
Z = 4438621
53 I = 51
55627
XDOT = -6858
822339 Wp = 69
50113
YDOT = -917
375238 meter/sec RA = 345
37874 deg
ZDOT = -3299
214837 TA = 53
88560
MA = 53
77448
Ha = 227
932 n
mi
Hp = 219
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8938729
10 X = -2794551
47
Y = 14278932
78 feet Y = 4321360
31 meter
Z = 14562406
60 Z = 4425215
30
XDOT = -22502
697961 XDOT = -6832
027401
YDOT = -3009
761279 feet/sec YDOT = -993
925507 meter/sec
ZDOT = -10824
195661 ZDOT = -3332
469567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5841593
50 X = 1780517
70
Y = -15853024
82 feet Y = -4832001
97 meter
Z = 14505511
87 Z = 4421280
02
XDOT = 21412
371096 XDOT = 6526
490710
YDOT = -2175
761798 feet/sec YDOT = -663
172196 meter/sec
ZDOT = -10963
540716 ZDOT = -3341
687210
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 13265
57385950
00016717 00000-0 10270-3 0 9095
2 25544 51
6503 345
7349 0002703 69
9482 290
1960 15
50367426 9811
Satellite: ISS
Catalog Number: 25544
Epoch time: 13265
57385950 = yrday
fracday
Element set: 909
Inclination: 51
6503 deg
RA of node: 345
7349 deg
Eccentricity:
0002703
Arg of perigee: 69
9482 deg
Mean anomaly: 290
1960 deg
Mean motion: 15
50367426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 330
Coasting Arc #11 (Orbit 995)
---------------------------------------
Vector Time (GMT): 2013/266/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2841719
81 A = 6792955
98 meter
Y = -4541768
33 meter E =
0010232
Z = -4186207
32 I = 51
52873
XDOT = 6654
774370 Wp = 99
78929
YDOT = 755
836604 meter/sec RA = 340
41482 deg
ZDOT = 3703
467206 TA = 208
35865
MA = 208
41438
Ha = 227
971 n
mi
Hp = 219
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9323227
71 X = 2912631
35
Y = -14900814
74 feet Y = -4509594
34 meter
Z = -13734275
98 Z = -4172229
65
XDOT = 21833
249247 XDOT = 6627
837187
YDOT = 2479
778884 feet/sec YDOT = 830
104269 meter/sec
ZDOT = 12150
482959 ZDOT = 3735
730365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5797035
13 X = -1766936
31
Y = 16642629
66 feet Y = 5072673
52 meter
Z = -13674957
15 Z = -4168126
94
XDOT = -20541
456628 XDOT = -6261
035980
YDOT = 2923
470947 feet/sec YDOT = 891
073945 meter/sec
ZDOT = 12285
687307 ZDOT = 3744
677491
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 13266
54075033
00016717 00000-0 10270-3 0 9103
2 25544 51
6492 340
9432 0002913 75
1814 284
9660 15
50370260 9963
Satellite: ISS
Catalog Number: 25544
Epoch time: 13266
54075033 = yrday
fracday
Element set: 910
Inclination: 51
6492 deg
RA of node: 340
9432 deg
Eccentricity:
0002913
Arg of perigee: 75
1814 deg
Mean anomaly: 284
9660 deg
Mean motion: 15
50370260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 996
Checksum: 300
Coasting Arc #12 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2013/267/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2957711
21 A = 6793963
33 meter
Y = 4731406
23 meter E =
0014123
Z = 3865949
70 I = 51
50401
XDOT = -6437
823008 Wp = 80
06835
YDOT = -653
316259 meter/sec RA = 335
44854 deg
ZDOT = -4110
577483 TA = 53
24055
MA = 53
11097
Ha = 227
937 n
mi
Hp = 219
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9703776
94 X = -3029178
94
Y = 15522986
32 feet Y = 4697931
95 meter
Z = 12683562
00 Z = 3851407
26
XDOT = -21121
466562 XDOT = -6410
070725
YDOT = -2143
426045 feet/sec YDOT = -725
153263 meter/sec
ZDOT = -13486
146599 ZDOT = -4141
784700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5721734
86 X = 1743984
79
Y = -17434157
70 feet Y = -5313931
27 meter
Z = 12621847
40 Z = 3847139
09
XDOT = 19657
350649 XDOT = 5991
560478
YDOT = -3443
238177 feet/sec YDOT = -1049
498996 meter/sec
ZDOT = -13616
933415 ZDOT = -4150
441305
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 13267
57209023
00016717 00000-0 10270-3 0 9116
2 25544 51
6496 335
8310 0002811 74
4556 285
6905 15
50391213 10128
Satellite: ISS
Catalog Number: 25544
Epoch time: 13267
57209023 = yrday
fracday
Element set: 911
Inclination: 51
6496 deg
RA of node: 335
8310 deg
Eccentricity:
0002811
Arg of perigee: 74
4556 deg
Mean anomaly: 285
6905 deg
Mean motion: 15
50391213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 288
Coasting Arc #13 (Orbit 1026)
---------------------------------------
Vector Time (GMT): 2013/268/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3013256
17 A = 6794943
25 meter
Y = -4953565
92 meter E =
0008110
Z = -3550017
17 I = 51
47912
XDOT = 6193
076823 Wp = 88
91691
YDOT = 575
628722 meter/sec RA = 330
48142 deg
ZDOT = 4462
481474 TA = 229
21518
MA = 229
28557
Ha = 227
992 n
mi
Hp = 219
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9886011
06 X = 3085669
24
Y = -16251856
71 feet Y = -4919465
17 meter
Z = -11647037
96 Z = -3535202
65
XDOT = 20318
493513 XDOT = 6164
502022
YDOT = 1888
545675 feet/sec YDOT = 644
724216 meter/sec
ZDOT = 14640
687251 ZDOT = 4492
497677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5401742
04 X = -1646450
97
Y = 18279446
94 feet Y = 5571575
43 meter
Z = -11584151
10 Z = -3530849
26
XDOT = -18692
068868 XDOT = -5697
342591
YDOT = 3815
396116 feet/sec YDOT = 1162
932736 meter/sec
ZDOT = 14766
487925 ZDOT = 4500
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 13268
53896590
00016717 00000-0 10270-3 0 9125
2 25544 51
6489 331
0388 0003036 80
1755 279
9739 15
50395701 10271
Satellite: ISS
Catalog Number: 25544
Epoch time: 13268
53896590 = yrday
fracday
Element set: 912
Inclination: 51
6489 deg
RA of node: 331
0388 deg
Eccentricity:
0003036
Arg of perigee: 80
1755 deg
Mean anomaly: 279
9739 deg
Mean motion: 15
50395701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1027
Checksum: 330
Coasting Arc #14 (Orbit 1042)
---------------------------------------
Vector Time (GMT): 2013/269/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3066060
24 A = 6795982
50 meter
Y = 5165138
92 meter E =
0015796
Z = 3164809
76 I = 51
45667
XDOT = -5941
983311 Wp = 91
43886
YDOT = -567
360850 meter/sec RA = 325
51285 deg
ZDOT = -4810
172042 TA = 51
97820
MA = 51
83572
Ha = 227
965 n
mi
Hp = 219
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10059252
75 X = -3138963
96
Y = 16945993
85 feet Y = 5130444
90 meter
Z = 10383234
12 Z = 3149737
55
XDOT = -19494
695903 XDOT = -5911
830676
YDOT = -1861
420112 feet/sec YDOT = -633
639659 meter/sec
ZDOT = -15781
404338 ZDOT = -4838
964551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5053957
01 X = 1540446
10
Y = -19082391
39 feet Y = -5816312
90 meter
Z = 10319238
42 Z = 3145303
87
XDOT = 17765
628332 XDOT = 5414
963516
YDOT = -3930
691746 feet/sec YDOT = -1198
074844 meter/sec
ZDOT = -15902
072391 ZDOT = -4846
951665
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 13269
57028964
00016717 00000-0 10270-3 0 9133
2 25544 51
6492 325
9266 0002981 79
8420 280
3067 15
50410807 10437
Satellite: ISS
Catalog Number: 25544
Epoch time: 13269
57028964 = yrday
fracday
Element set: 913
Inclination: 51
6492 deg
RA of node: 325
9266 deg
Eccentricity:
0002981
Arg of perigee: 79
8420 deg
Mean anomaly: 280
3067 deg
Mean motion: 15
50410807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1043
Checksum: 314
Coasting Arc #15 (Orbit 1057)
---------------------------------------
Vector Time (GMT): 2013/270/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3050979
53 A = 6796876
41 meter
Y = -5394789
76 meter E =
0007715
Z = -2792562
51 I = 51
43513
XDOT = 5684
461567 Wp = 68
94579
YDOT = 583
982745 meter/sec RA = 320
54339 deg
ZDOT = 5096
459854 TA = 259
35993
MA = 259
44682
Ha = 228
000 n
mi
Hp = 219
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10009775
36 X = 3124644
07
Y = -17699441
46 feet Y = -5360260
11 meter
Z = -9161950
50 Z = -2777561
70
XDOT = 18649
808291 XDOT = 5652
751531
YDOT = 1915
953887 feet/sec YDOT = 647
373118 meter/sec
ZDOT = 16720
668811 ZDOT = 5123
997499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4450084
50 X = -1356385
75
Y = 19870234
36 feet Y = 6056447
43 meter
Z = -9098225
20 Z = -2773139
04
XDOT = -16846
519071 XDOT = -5134
819013
YDOT = 3914
652621 feet/sec YDOT = 1193
186119 meter/sec
ZDOT = 16836
070451 ZDOT = 5131
634273
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 13270
53714984
00016717 00000-0 10270-3 0 9146
2 25544 51
6493 321
1342 0003149 85
2805 274
8705 15
50421917 10583
Satellite: ISS
Catalog Number: 25544
Epoch time: 13270
53714984 = yrday
fracday
Element set: 914
Inclination: 51
6493 deg
RA of node: 321
1342 deg
Eccentricity:
0003149
Arg of perigee: 85
2805 deg
Mean anomaly: 274
8705 deg
Mean motion: 15
50421917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1058
Checksum: 303
Coasting Arc #16 (Orbit 1072)
---------------------------------------
Vector Time (GMT): 2013/271/12:45:24
239
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3034706
67 A = 6797823
53 meter
Y = 5601366
42 meter E =
0016772
Z = 2351104
95 I = 51
41482
XDOT = -5429
585168 Wp = 102
85451
YDOT = -676
095540 meter/sec RA = 315
57286 deg
ZDOT = -5368
752948 TA = 50
85466
MA = 50
70572
Ha = 227
999 n
mi
Hp = 219
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9956386
70 X = -3108537
89
Y = 18377186
43 feet Y = 5567017
80 meter
Z = 7713598
92 Z = 2336182
75
XDOT = -17813
599633 XDOT = -5395
541351
YDOT = -2218
161222 feet/sec YDOT = -736
622742 meter/sec
ZDOT = -17614
018858 ZDOT = -5395
046706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3839008
73 X = 1170129
86
Y = -20569078
44 feet Y = -6269455
11 meter
Z = 7650179
71 Z = 2331774
78
XDOT = 16023
860151 XDOT = 4884
072574
YDOT = -3636
795915 feet/sec YDOT = -1108
495395 meter/sec
ZDOT = -17724
189154 ZDOT = -5402
332854
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 13271
56845761
00016717 00000-0 10270-3 0 9159
2 25544 51
6490 316
0220 0003160 85
9435 274
2077 15
50425418 10730
Satellite: ISS
Catalog Number: 25544
Epoch time: 13271
56845761 = yrday
fracday
Element set: 915
Inclination: 51
6490 deg
RA of node: 316
0220 deg
Eccentricity:
0003160
Arg of perigee: 85
9435 deg
Mean anomaly: 274
2077 deg
Mean motion: 15
50425418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1073
Checksum: 293
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