[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 12th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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
119 1
6 1
7 1
7
N/A 0
4 -0
1 227
9
000/00:03:24
237 -0
1 -0
0 220
1
Coasting Arc #1 (Orbit 809)
---------------------------------------
Vector Time (GMT): 2013/254/12:52:24
779
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3124793
99 A = 6787967
15 meter
Y = -2842259
43 meter E =
0017567
Z = -5328603
25 I = 51
85967
XDOT = 5594
354835 Wp = 86
51458
YDOT = 5192
030821 meter/sec RA = 39
83425 deg
ZDOT = 513
723793 TA = 188
36896
MA = 188
39830
Ha = 227
830 n
mi
Hp = 219
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10251948
79 X = 3182229
56
Y = -9324998
13 feet Y = -2806995
19 meter
Z = -17482294
11 Z = -5313283
51
XDOT = 18354
182528 XDOT = 5533
385077
YDOT = 17034
221854 feet/sec YDOT = 5254
249580 meter/sec
ZDOT = 1685
445515 ZDOT = 540
752381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9859443
49 X = -3005158
38
Y = 9854335
44 feet Y = 3003601
44 meter
Z = -17417580
16 Z = -5308878
43
XDOT = -18488
817290 XDOT = -5635
391510
YDOT = -15334
817863 feet/sec YDOT = -4674
052485 meter/sec
ZDOT = 1798
092018 ZDOT = 548
058447
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 13254
55159529
00016717 00000-0 10270-3 0 9003
2 25544 51
6485 40
3659 0003541 54
6967 305
4515 15
50525672 8108
Satellite: ISS
Catalog Number: 25544
Epoch time: 13254
55159529 = yrday
fracday
Element set: 900
Inclination: 51
6485 deg
RA of node: 40
3659 deg
Eccentricity:
0003541
Arg of perigee: 54
6967 deg
Mean anomaly: 305
4515 deg
Mean motion: 15
50525672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 810
Checksum: 305
Coasting Arc #2 (Orbit 825)
---------------------------------------
Vector Time (GMT): 2013/255/12:52:24
779
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3370046
92 A = 6788338
29 meter
Y = 2675725
94 meter E =
0007465
Z = 5245517
35 I = 51
83684
XDOT = -5693
342528 Wp = 56
31075
YDOT = -5017
149194 meter/sec RA = 34
88590 deg
ZDOT = -1093
366715 TA = 44
16903
MA = 44
10945
Ha = 228
013 n
mi
Hp = 219
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11056584
37 X = -3425198
35
Y = 8778628
40 feet Y = 2637731
83 meter
Z = 17209702
60 Z = 5229011
84
XDOT = -18678
945303 XDOT = -5631
505233
YDOT = -16460
463235 feet/sec YDOT = -5080
470069 meter/sec
ZDOT = -3587
161138 ZDOT = -1120
874051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10527374
48 X = 3208743
74
Y = -9533092
15 feet Y = -2905686
49 meter
Z = 17140034
39 Z = 5224282
48
XDOT = 19057
952605 XDOT = 5808
863954
YDOT = 14359
405602 feet/sec YDOT = 4376
746828 meter/sec
ZDOT = -3701
836145 ZDOT = -1128
319657
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 13255
58283097
00016717 00000-0 10270-3 0 9016
2 25544 51
6488 35
2525 0003591 56
9964 303
1532 15
50504236 8267
Satellite: ISS
Catalog Number: 25544
Epoch time: 13255
58283097 = yrday
fracday
Element set: 901
Inclination: 51
6488 deg
RA of node: 35
2525 deg
Eccentricity:
0003591
Arg of perigee: 56
9964 deg
Mean anomaly: 303
1532 deg
Mean motion: 15
50504236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 826
Checksum: 307
Coasting Arc #3 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2013/256/12:52:24
779
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3634639
17 A = 6788743
51 meter
Y = -2571370
62 meter E =
0016184
Z = -5139106
29 I = 51
81307
XDOT = 5725
666022 Wp = 93
75870
YDOT = 4797
432525 meter/sec RA = 29
93818 deg
ZDOT = 1652
531055 TA = 192
17272
MA = 192
21187
Ha = 227
851 n
mi
Hp = 219
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11924669
20 X = 3688087
00
Y = -8436255
30 feet Y = -2530427
19 meter
Z = -16860584
95 Z = -5121319
63
XDOT = 18784
993511 XDOT = 5663
567004
YDOT = 15739
608022 feet/sec YDOT = 4861
113427 meter/sec
ZDOT = 5421
689814 ZDOT = 1680
194681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11254115
98 X = -3430254
55
Y = 9446560
65 feet Y = 2879311
68 meter
Z = -16785554
18 Z = -5116236
92
XDOT = -19353
492308 XDOT = -5898
944456
YDOT = -13238
191572 feet/sec YDOT = -4035
000791 meter/sec
ZDOT = 5537
049667 ZDOT = 1687
692739
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
54960628
00016717 00000-0 10270-3 0 9026
2 25544 51
6491 30
4605 0003569 60
2855 299
8651 15
50547720 8414
Satellite: ISS
Catalog Number: 25544
Epoch time: 13256
54960628 = yrday
fracday
Element set: 902
Inclination: 51
6491 deg
RA of node: 30
4605 deg
Eccentricity:
0003569
Arg of perigee: 60
2855 deg
Mean anomaly: 299
8651 deg
Mean motion: 15
50547720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 841
Checksum: 314
Coasting Arc #4 (Orbit 856)
---------------------------------------
Vector Time (GMT): 2013/257/12:52:24
779
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3917194
12 A = 6789542
10 meter
Y = 2478214
52 meter E =
0010194
Z = 4955228
96 I = 51
78883
XDOT = -5723
274176 Wp = 59
44317
YDOT = -4593
966165 meter/sec RA = 24
98724 deg
ZDOT = -2218
355727 TA = 52
21023
MA = 52
11796
Ha = 228
050 n
mi
Hp = 219
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12851686
74 X = -3968685
94
Y = 8130625
08 feet Y = 2434122
37 meter
Z = 16257312
87 Z = 4936074
48
XDOT = -18777
146247 XDOT = -5660
701966
YDOT = -15072
067470 feet/sec YDOT = -4657
617728 meter/sec
ZDOT = -7278
069970 ZDOT = -2246
006435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12039923
53 X = 3669768
69
Y = -9430398
70 feet Y = -2874385
52 meter
Z = 16176555
87 Z = 4930614
23
XDOT = 19505
095821 XDOT = 5945
153206
YDOT = 12172
257336 feet/sec YDOT = 3710
104036 meter/sec
ZDOT = -7393
403905 ZDOT = -2253
509510
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
58082787
00016717 00000-0 10270-3 0 9033
2 25544 51
6496 25
3472 0003671 63
1029 297
0497 15
50524961 8570
Satellite: ISS
Catalog Number: 25544
Epoch time: 13257
58082787 = yrday
fracday
Element set: 903
Inclination: 51
6496 deg
RA of node: 25
3472 deg
Eccentricity:
0003671
Arg of perigee: 63
1029 deg
Mean anomaly: 297
0497 deg
Mean motion: 15
50524961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 857
Checksum: 327
Coasting Arc #5 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2013/258/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1446203
66 A = 6788674
31 meter
Y = -3953141
09 meter E =
0016843
Z = -5340606
82 I = 51
75543
XDOT = 7184
257014 Wp = 85
14888
YDOT = 2627
782623 meter/sec RA = 20
08066 deg
ZDOT = 1
748481 TA = 184
85961
MA = 184
87598
Ha = 227
869 n
mi
Hp = 220
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4744762
67 X = 1516244
07
Y = -12969622
99 feet Y = -3936577
54 meter
Z = -17521675
93 Z = -5333410
91
XDOT = 23570
397028 XDOT = 7154
330129
YDOT = 8621
334065 feet/sec YDOT = 2707
954217 meter/sec
ZDOT = 5
736486 ZDOT = 36
575746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3663277
89 X = -1116567
10
Y = 13355995
24 feet Y = 4070907
35 meter
Z = -17490877
82 Z = -5331219
56
XDOT = -23277
762003 XDOT = -7095
061859
YDOT = -6192
228446 feet/sec YDOT = -1887
391230 meter/sec
ZDOT = 151
482543 ZDOT = 46
171879
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
54759039
00016717 00000-0 10270-3 0 9042
2 25544 51
6499 20
5544 0002393 54
5036 305
6337 15
50249915 8721
Satellite: ISS
Catalog Number: 25544
Epoch time: 13258
54759039 = yrday
fracday
Element set: 904
Inclination: 51
6499 deg
RA of node: 20
5544 deg
Eccentricity:
0002393
Arg of perigee: 54
5036 deg
Mean anomaly: 305
6337 deg
Mean motion: 15
50249915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 317
Coasting Arc #6 (Orbit 887)
---------------------------------------
Vector Time (GMT): 2013/259/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1619536
25 A = 6788664
94 meter
Y = 3902110
96 meter E =
0005160
Z = 5310037
27 I = 51
72705
XDOT = -7277
341114 Wp = 62
09311
YDOT = -2361
139490 meter/sec RA = 15
12810 deg
ZDOT = -481
741769 TA = 32
51400
MA = 32
48223
Ha = 227
899 n
mi
Hp = 219
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5313439
14 X = -1688844
64
Y = 12802201
33 feet Y = 3883613
31 meter
Z = 17421382
13 Z = 5302001
03
XDOT = -23875
791057 XDOT = -7248
057315
YDOT = -7746
520636 feet/sec YDOT = -2442
355657 meter/sec
ZDOT = -1580
517616 ZDOT = -517
022746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4015732
69 X = 1223995
32
Y = -13311548
36 feet Y = -4057359
94 meter
Z = 17387067
63 Z = 5299578
21
XDOT = 23588
522283 XDOT = 7189
781592
YDOT = 4847
037173 feet/sec YDOT = 1477
376930 meter/sec
ZDOT = -1728
203188 ZDOT = -526
756332
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
57900351
00016717 00000-0 10270-3 0 9052
2 25544 51
6504 15
4425 0002395 56
3454 303
7925 15
50279116 8880
Satellite: ISS
Catalog Number: 25544
Epoch time: 13259
57900351 = yrday
fracday
Element set: 905
Inclination: 51
6504 deg
RA of node: 15
4425 deg
Eccentricity:
0002395
Arg of perigee: 56
3454 deg
Mean anomaly: 303
7925 deg
Mean motion: 15
50279116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 888
Checksum: 306
Coasting Arc #7 (Orbit 902)
---------------------------------------
Vector Time (GMT): 2013/260/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1798858
98 A = 6788927
53 meter
Y = -3904691
43 meter E =
0016360
Z = -5268466
12 I = 51
69813
XDOT = 7300
454789 Wp = 91
86210
YDOT = 2076
936279 meter/sec RA = 10
17520 deg
ZDOT = 955
401414 TA = 187
28316
MA = 187
30695
Ha = 227
893 n
mi
Hp = 219
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5901768
32 X = 1867981
02
Y = -12810667
42 feet Y = -3884189
62 meter
Z = -17284993
83 Z = -5259559
11
XDOT = 23951
623325 XDOT = 7272
046394
YDOT = 6814
095402 feet/sec YDOT = 2158
415882 meter/sec
ZDOT = 3134
519074 ZDOT = 990
796864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4368016
80 X = -1331371
52
Y = 13460145
84 feet Y = 4102652
45 meter
Z = -17247028
27 Z = -5256894
22
XDOT = -23612
113937 XDOT = -7196
972328
YDOT = -3464
840476 feet/sec YDOT = -1056
083377 meter/sec
ZDOT = 3282
720505 ZDOT = 1000
573210
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
54594810
00016717 00000-0 10270-3 0 9061
2 25544 51
6507 10
6516 0002490 59
6424 300
4973 15
50275931 9036
Satellite: ISS
Catalog Number: 25544
Epoch time: 13260
54594810 = yrday
fracday
Element set: 906
Inclination: 51
6507 deg
RA of node: 10
6516 deg
Eccentricity:
0002490
Arg of perigee: 59
6424 deg
Mean anomaly: 300
4973 deg
Mean motion: 15
50275931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 903
Checksum: 291
Coasting Arc #8 (Orbit 918)
---------------------------------------
Vector Time (GMT): 2013/261/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1990751
50 A = 6789239
86 meter
Y = 3921235
97 meter E =
0007131
Z = 5168169
69 I = 51
66936
XDOT = -7309
434506 Wp = 56
58936
YDOT = -1809
060253 meter/sec RA = 5
21898 deg
ZDOT = -1437
700364 TA = 47
27269
MA = 47
21269
Ha = 227
924 n
mi
Hp = 219
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6531336
94 X = -2059557
17
Y = 12864947
42 feet Y = 3898590
12 meter
Z = 16955937
29 Z = 5158331
16
XDOT = -23981
084337 XDOT = -7281
678001
YDOT = -5935
237052 feet/sec YDOT = -1890
643997 meter/sec
ZDOT = -4716
864711 ZDOT = -1473
141169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4749362
45 X = 1447605
67
Y = -13675782
54 feet Y = -4168378
52 meter
Z = 16914064
33 Z = 5155406
81
XDOT = 23552
932832 XDOT = 7178
933927
YDOT = 2140
752908 feet/sec YDOT = 652
501486 meter/sec
ZDOT = -4865
286948 ZDOT = -1482
939462
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
57734725
00016717 00000-0 10270-3 0 9077
2 25544 51
6510 5
5399 0002480 61
1283 299
0116 15
50300899 9193
Satellite: ISS
Catalog Number: 25544
Epoch time: 13261
57734725 = yrday
fracday
Element set: 907
Inclination: 51
6510 deg
RA of node: 5
5399 deg
Eccentricity:
0002480
Arg of perigee: 61
1283 deg
Mean anomaly: 299
0116 deg
Mean motion: 15
50300899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 919
Checksum: 304
Coasting Arc #9 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2013/262/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2169929
11 A = 6789773
75 meter
Y = -3993186
19 meter E =
0014965
Z = -5057917
96 I = 51
64015
XDOT = 7249
973843 Wp = 97
66625
YDOT = 1536
896524 meter/sec RA =
26259 deg
ZDOT = 1899
872380 TA = 190
78055
MA = 190
81266
Ha = 227
916 n
mi
Hp = 219
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7119190
00 X = 2238990
57
Y = -13101004
57 feet Y = -3968535
24 meter
Z = -16594219
04 Z = -5047208
31
XDOT = 23786
003421 XDOT = 7223
020006
YDOT = 5042
311432 feet/sec YDOT = 1617
819903 meter/sec
ZDOT = 6233
177100 ZDOT = 1935
026477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5054201
56 X = -1540520
64
Y = 14081314
01 feet Y = 4291984
51 meter
Z = -16548683
77 Z = -5044038
81
XDOT = -23219
092755 XDOT = -7077
179472
YDOT = -846
745812 feet/sec YDOT = -258
088124 meter/sec
ZDOT = 6380
426146 ZDOT = 1944
753889
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
54427868
00016717 00000-0 10270-3 0 9083
2 25544 51
6508
7493 0002586 64
7554 295
3864 15
50300736 9345
Satellite: ISS
Catalog Number: 25544
Epoch time: 13262
54427868 = yrday
fracday
Element set: 908
Inclination: 51
6508 deg
RA of node:
7493 deg
Eccentricity:
0002586
Arg of perigee: 64
7554 deg
Mean anomaly: 295
3864 deg
Mean motion: 15
50300736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 934
Checksum: 322
Coasting Arc #10 (Orbit 949)
---------------------------------------
Vector Time (GMT): 2013/263/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2356334
90 A = 6790382
19 meter
Y = 4077818
72 meter E =
0009459
Z = 4886258
76 I = 51
61181
XDOT = -7174
253756 Wp = 60
53979
YDOT = -1295
142736 meter/sec RA = 355
30278 deg
ZDOT = -2370
820509 TA = 52
74172
MA = 52
65549
Ha = 227
927 n
mi
Hp = 219
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7730757
54 X = -2425495
11
Y = 13378670
35 feet Y = 4051082
67 meter
Z = 16031032
67 Z = 4874643
27
XDOT = -23537
577938 XDOT = -7147
721094
YDOT = -4249
155959 feet/sec YDOT = -1375
221779 meter/sec
ZDOT = -7778
282509 ZDOT = -2405
607980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5361150
76 X = 1634078
75
Y = -14546173
83 feet Y = -4433673
78 meter
Z = 15981687
34 Z = 4871218
30
XDOT = 22809
353599 XDOT = 6952
290977
YDOT = -328
344295 feet/sec YDOT = -100
079341 meter/sec
ZDOT = -7924
018520 ZDOT = -2415
240845
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
57566369
00016717 00000-0 10270-3 0 9098
2 25544 51
6510 355
6377 0002530 65
3233 294
8181 15
50323080 9502
Satellite: ISS
Catalog Number: 25544
Epoch time: 13263
57566369 = yrday
fracday
Element set: 909
Inclination: 51
6510 deg
RA of node: 355
6377 deg
Eccentricity:
0002530
Arg of perigee: 65
3233 deg
Mean anomaly: 294
8181 deg
Mean motion: 15
50323080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 950
Checksum: 304
Coasting Arc #11 (Orbit 964)
---------------------------------------
Vector Time (GMT): 2013/264/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2511717
36 A = 6791145
42 meter
Y = -4214579
64 meter E =
0012813
Z = -4707606
85 I = 51
58282
XDOT = 7038
086263 Wp = 101
30437
YDOT = 1061
802820 meter/sec RA = 350
34270 deg
ZDOT = 2808
584158 TA = 196
60953
MA = 196
65154
Ha = 227
939 n
mi
Hp = 219
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8240542
51 X = 2581527
54
Y = -13827361
02 feet Y = -4186102
30 meter
Z = -15444904
35 Z = -4695234
92
XDOT = 23090
834197 XDOT = 7012
046384
YDOT = 3483
605051 feet/sec YDOT = 1140
361940 meter/sec
ZDOT = 9214
514955 ZDOT = 2842
711489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5520522
52 X = -1682655
27
Y = 15173871
72 feet Y = 4624996
10 meter
Z = -15392367
33 Z = -4691593
56
XDOT = -22166
736146 XDOT = -6756
421177
YDOT = 1414
065538 feet/sec YDOT = 431
007176 meter/sec
ZDOT = 9357
506747 ZDOT = 2852
168056
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
54258205
00016717 00000-0 10270-3 0 9105
2 25544 51
6501 350
8468 0002684 69
6974 290
4465 15
50323727 9650
Satellite: ISS
Catalog Number: 25544
Epoch time: 13264
54258205 = yrday
fracday
Element set: 910
Inclination: 51
6501 deg
RA of node: 350
8468 deg
Eccentricity:
0002684
Arg of perigee: 69
6974 deg
Mean anomaly: 290
4465 deg
Mean motion: 15
50323727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 965
Checksum: 319
Coasting Arc #12 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2013/265/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2669314
03 A = 6791987
74 meter
Y = 4359499
28 meter E =
0011775
Z = 4465050
48 I = 51
55590
XDOT = -6886
302939 Wp = 68
88746
YDOT = -872
828907 meter/sec RA = 345
37946 deg
ZDOT = -3253
510816 TA = 53
97847
MA = 53
86939
Ha = 227
922 n
mi
Hp = 219
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8757591
97 X = -2739554
78
Y = 14302819
16 feet Y = 4329257
09 meter
Z = 14649115
75 Z = 4451911
93
XDOT = -22592
857410 XDOT = -6860
226106
YDOT = -2863
611899 feet/sec YDOT = -949
690491 meter/sec
ZDOT = -10674
248083 ZDOT = -3286
900795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5659998
66 X = 1725167
59
Y = -15838605
01 feet Y = -4827606
81 meter
Z = 14593342
72 Z = 4448050
86
XDOT = 21471
917094 XDOT = 6544
640330
YDOT = -2324
499800 feet/sec YDOT = -708
507539 meter/sec
ZDOT = -10814
167221 ZDOT = -3296
158169
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
57395275
00016717 00000-0 10270-3 0 9119
2 25544 51
6503 345
7349 0002584 69
2950 290
8478 15
50345208 9816
Satellite: ISS
Catalog Number: 25544
Epoch time: 13265
57395275 = yrday
fracday
Element set: 911
Inclination: 51
6503 deg
RA of node: 345
7349 deg
Eccentricity:
0002584
Arg of perigee: 69
2950 deg
Mean anomaly: 290
8478 deg
Mean motion: 15
50345208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 329
Coasting Arc #13 (Orbit 995)
---------------------------------------
Vector Time (GMT): 2013/266/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2779634
42 A = 6792905
41 meter
Y = -4548555
09 meter E =
0010283
Z = -4220452
48 I = 51
52829
XDOT = 6687
960866 Wp = 100
28965
YDOT = 702
234894 meter/sec RA = 340
41564 deg
ZDOT = 3653
745610 TA = 207
25755
MA = 207
31155
Ha = 227
965 n
mi
Hp = 219
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9119535
49 X = 2850792
82
Y = -14923081
00 feet Y = -4517073
99 meter
Z = -13846628
87 Z = -4206775
82
XDOT = 21942
128827 XDOT = 6661
862140
YDOT = 2303
920256 feet/sec YDOT = 776
878355 meter/sec
ZDOT = 11987
354363 ZDOT = 3686
172030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5594265
11 X = -1705132
01
Y = 16618450
54 feet Y = 5065303
73 meter
Z = -13788571
52 Z = -4202756
60
XDOT = -20610
519939 XDOT = -6282
086477
YDOT = 3104
837991 feet/sec YDOT = 946
354620 meter/sec
ZDOT = 12123
251648 ZDOT = 3695
167102
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
54085810
00016717 00000-0 10270-3 0 9129
2 25544 51
6491 340
9433 0002797 74
5996 285
5463 15
50345920 9960
Satellite: ISS
Catalog Number: 25544
Epoch time: 13266
54085810 = yrday
fracday
Element set: 912
Inclination: 51
6491 deg
RA of node: 340
9433 deg
Eccentricity:
0002797
Arg of perigee: 74
5996 deg
Mean anomaly: 285
5463 deg
Mean motion: 15
50345920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 996
Checksum: 333
Coasting Arc #14 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2013/267/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2888542
02 A = 6793893
33 meter
Y = 4738149
23 meter E =
0013878
Z = 3909818
78 I = 51
50349
XDOT = -6477
607042 Wp = 79
27329
YDOT = -588
744165 meter/sec RA = 335
44947 deg
ZDOT = -4057
322698 TA = 53
34136
MA = 53
21386
Ha = 227
932 n
mi
Hp = 219
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9476843
89 X = -2960303
40
Y = 15545109
01 feet Y = 4705446
80 meter
Z = 12827489
45 Z = 3895611
66
XDOT = -21251
991606 XDOT = -6450
832561
YDOT = -1931
575345 feet/sec YDOT = -661
031522 meter/sec
ZDOT = -13311
426176 ZDOT = -4088
725565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5497090
06 X = 1675513
05
Y = -17400763
84 feet Y = -5303752
82 meter
Z = 12767180
13 Z = 3891436
50
XDOT = 19736
033005 XDOT = 6015
542860
YDOT = -3664
326760 feet/sec YDOT = -1116
886796 meter/sec
ZDOT = -13443
043425 ZDOT = -4097
439636
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
57221456
00016717 00000-0 10270-3 0 9132
2 25544 51
6495 335
8312 0002693 73
7519 286
3928 15
50365576 10124
Satellite: ISS
Catalog Number: 25544
Epoch time: 13267
57221456 = yrday
fracday
Element set: 913
Inclination: 51
6495 deg
RA of node: 335
8312 deg
Eccentricity:
0002693
Arg of perigee: 73
7519 deg
Mean anomaly: 286
3928 deg
Mean motion: 15
50365576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 320
Coasting Arc #15 (Orbit 1026)
---------------------------------------
Vector Time (GMT): 2013/268/12:45:24
237
Vector Time (MET): N/A
Weight (LBS) : 913889
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2937629
46 A = 6794859
96 meter
Y = -4960105
22 meter E =
0008126
Z = -3604010
17 I = 51
47854
XDOT = 6239
037623 Wp = 90
26627
YDOT = 499
130253 meter/sec RA = 330
48242 deg
ZDOT = 4407
098545 TA = 227
08013
MA = 227
14835
Ha = 227
991 n
mi
Hp = 219
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9637891
94 X = 3010383
57
Y = -16273311
09 feet Y = -4926848
27 meter
Z = -11824180
33 Z = -3589562
21
XDOT = 20469
283539 XDOT = 6211
583866
YDOT = 1637
566448 feet/sec YDOT = 568
745975 meter/sec
ZDOT = 14458
984727 ZDOT = 4437
340751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5157616
41 X = -1572041
48
Y = 18236109
30 feet Y = 5558366
12 meter
Z = -11762829
85 Z = -3585310
54
XDOT = -18776
843985 XDOT = -5723
182047
YDOT = 4079
398052 feet/sec YDOT = 1243
400526 meter/sec
ZDOT = 14585
744921 ZDOT = 4445
735052
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
53910682
00016717 00000-0 10270-3 0 9146
2 25544 51
6489 331
0391 0002922 79
5713 280
5767 15
50368459 10273
Satellite: ISS
Catalog Number: 25544
Epoch time: 13268
53910682 = yrday
fracday
Element set: 914
Inclination: 51
6489 deg
RA of node: 331
0391 deg
Eccentricity:
0002922
Arg of perigee: 79
5713 deg
Mean anomaly: 280
5767 deg
Mean motion: 15
50368459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1027
Checksum: 323
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