[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 8th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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 1440)
---------------------------------------
Vector Time (GMT): 2013/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4056869
01 A = 6783794
77 meter
Y = -1945305
67 meter E =
0008757
Z = -5080722
20 I = 51
84469
XDOT = 4967
357519 Wp = 171
02838
YDOT = 5536
895172 meter/sec RA = 36
90727 deg
ZDOT = 1838
380080 TA = 116
78152
MA = 116
69192
Ha = 223
867 n
mi
Hp = 219
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13309937
69 X = 4103000
62
Y = -6382236
44 feet Y = -1899681
17 meter
Z = -16669036
10 Z = -5060902
67
XDOT = 16297
104721 XDOT = 4896
143417
YDOT = 18165
666574 feet/sec YDOT = 5592
045061 meter/sec
ZDOT = 6031
430710 ZDOT = 1862
337741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14080250
17 X = 4291660
25
Y = 4731369
94 feet Y = 1442121
56 meter
Z = -16586284
73 Z = -5055499
59
XDOT = -588
761059 XDOT = -179
454371
YDOT = 23335
343681 feet/sec YDOT = 7112
612754 meter/sec
ZDOT = 6130
396857 ZDOT = 1868
544962
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 13037
51285664
00016717 00000-0 10270-3 0 9008
2 25544 51
6461 37
4459 0012615 244
1469 115
8383 15
52315607 14416
Satellite: ISS
Catalog Number: 25544
Epoch time: 13037
51285664 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 37
4459 deg
Eccentricity:
0012615
Arg of perigee: 244
1469 deg
Mean anomaly: 115
8383 deg
Mean motion: 15
52315607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 298
Coasting Arc #2 (Orbit 1456)
---------------------------------------
Vector Time (GMT): 2013/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4788963
87 A = 6785519
61 meter
Y = 1303771
17 meter E =
0004150
Z = 4629808
01 I = 51
82507
XDOT = -4394
609136 Wp = 252
36329
YDOT = -5515
602411 meter/sec RA = 31
94216 deg
ZDOT = -2995
900451 TA = 227
44529
MA = 227
48033
Ha = 223
526 n
mi
Hp = 219
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15711823
73 X = -4825676
81
Y = 4277464
48 feet Y = 1250012
65 meter
Z = 15189658
82 Z = 4606455
05
XDOT = -14418
008977 XDOT = -4318
052961
YDOT = -18095
808436 feet/sec YDOT = -5564
317605 meter/sec
ZDOT = -9829
069720 ZDOT = -3017
062667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14471767
70 X = -4410994
79
Y = -7659941
54 feet Y = -2334750
18 meter
Z = 15092285
36 Z = 4600128
58
XDOT = 1298
981834 XDOT = 395
929663
YDOT = -21969
955843 feet/sec YDOT = -6696
442541 meter/sec
ZDOT = -9916
403540 ZDOT = -3022
519799
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 13038
54287020
00016717 00000-0 10270-3 0 9011
2 25544 51
6454 32
3246 0012619 248
2674 111
7135 15
52361486 14576
Satellite: ISS
Catalog Number: 25544
Epoch time: 13038
54287020 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 32
3246 deg
Eccentricity:
0012619
Arg of perigee: 248
2674 deg
Mean anomaly: 111
7135 deg
Mean motion: 15
52361486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1457
Checksum: 291
Coasting Arc #3 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2013/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5470555
48 A = 6787979
70 meter
Y = -707209
84 meter E =
0007996
Z = -3955626
93 I = 51
80661
XDOT = 3626
439056 Wp = 224
08760
YDOT = 5410
404700 meter/sec RA = 26
97890 deg
ZDOT = 4037
482811 TA = 88
05410
MA = 87
96253
Ha = 223
141 n
mi
Hp = 219
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17948016
66 X = 5497271
90
Y = -2320242
27 feet Y = -645885
31 meter
Z = -12977778
63 Z = -3928987
30
XDOT = 11897
765931 XDOT = 3546
056784
YDOT = 17750
671588 feet/sec YDOT = 5450
508407 meter/sec
ZDOT = 13246
334681 ZDOT = 4054
903955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14940529
08 X = 4553873
26
Y = 10351978
89 feet Y = 3155283
17 meter
Z = -12866805
67 Z = -3921802
37
XDOT = -2362
224073 XDOT = -720
005897
YDOT = 20006
019128 feet/sec YDOT = 6097
834630 meter/sec
ZDOT = 13318
112616 ZDOT = 4059
360725
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 13039
50849539
00016717 00000-0 10270-3 0 9028
2 25544 51
6453 27
5235 0012521 252
0004 107
9784 15
52356720 14720
Satellite: ISS
Catalog Number: 25544
Epoch time: 13039
50849539 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 27
5235 deg
Eccentricity:
0012521
Arg of perigee: 252
0004 deg
Mean anomaly: 107
9784 deg
Mean motion: 15
52356720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 292
Coasting Arc #4 (Orbit 1487)
---------------------------------------
Vector Time (GMT): 2013/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6029343
31 A = 6790328
57 meter
Y = 203617
20 meter E =
0004374
Z = 3110916
61 I = 51
78720
XDOT = -2699
758417 Wp = 170
09860
YDOT = -5246
389419 meter/sec RA = 22
01822 deg
ZDOT = -4892
259011 TA = 334
21750
MA = 334
23930
Ha = 222
805 n
mi
Hp = 219
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19781310
09 X = -6046283
64
Y = 668035
43 feet Y = 136098
68 meter
Z = 10206419
34 Z = 3081586
31
XDOT = -8857
475121 XDOT = -2617
126948
YDOT = -17212
563712 feet/sec YDOT = -5276
117949 meter/sec
ZDOT = -16050
718541 ZDOT = -4905
172944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15400092
06 X = -4693948
06
Y = -12532406
32 feet Y = -3819877
45 meter
Z = 10084317
13 Z = 3073699
86
XDOT = 3791
641586 XDOT = 1155
692355
YDOT = -17608
792950 feet/sec YDOT = -5367
160091 meter/sec
ZDOT = -16103
760020 ZDOT = -4908
426054
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 13040
53848110
00016717 00000-0 10270-3 0 9038
2 25544 51
6452 22
4020 0012599 256
3359 103
6390 15
52410533 14886
Satellite: ISS
Catalog Number: 25544
Epoch time: 13040
53848110 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 22
4020 deg
Eccentricity:
0012599
Arg of perigee: 256
3359 deg
Mean anomaly: 103
6390 deg
Mean motion: 15
52410533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1488
Checksum: 278
Coasting Arc #5 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2013/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6450371
87 A = 6792508
58 meter
Y = 247100
57 meter E =
0008411
Z = -2102009
94 I = 51
76594
XDOT = 1614
062949 Wp = 288
20532
YDOT = 5054
151990 meter/sec RA = 17
06005 deg
ZDOT = 5531
557778 TA = 48
57917
MA = 48
50693
Ha = 222
398 n
mi
Hp = 219
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21162637
36 X = 6457340
04
Y = 810697
41 feet Y = 319271
52 meter
Z = -6896358
09 Z = -2070658
59
XDOT = 5295
482117 XDOT = 1530
556331
YDOT = 16581
863485 feet/sec YDOT = 5071
734851 meter/sec
ZDOT = 18148
155438 ZDOT = 5539
195421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15702339
80 X = 4786073
17
Y = 14273514
01 feet Y = 4350567
07 meter
Z = -6765909
23 Z = -2062249
13
XDOT = -5670
926727 XDOT = -1728
498467
YDOT = 14880
647371 feet/sec YDOT = 4535
621319 meter/sec
ZDOT = 18179
263586 ZDOT = 5541
039541
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 13041
50408019
00016717 00000-0 10270-3 0 9047
2 25544 51
6453 17
6008 0012456 259
5191 100
4557 15
52417189 15032
Satellite: ISS
Catalog Number: 25544
Epoch time: 13041
50408019 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 17
6008 deg
Eccentricity:
0012456
Arg of perigee: 259
5191 deg
Mean anomaly: 100
4557 deg
Mean motion: 15
52417189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 283
Coasting Arc #6 (Orbit 1518)
---------------------------------------
Vector Time (GMT): 2013/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6684225
54 A = 6793823
06 meter
Y = -622953
92 meter E =
0009103
Z = 1004856
46 I = 51
74199
XDOT = -433
432437 Wp = 188
28320
YDOT = -4861
076384 meter/sec RA = 12
10317 deg
ZDOT = -5912
199937 TA = 340
85015
MA = 340
88435
Ha = 222
135 n
mi
Hp = 219
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21929873
81 X = -6681643
95
Y = -2043812
08 feet Y = -697686
62 meter
Z = 3296773
16 Z = 972392
23
XDOT = -1422
022430 XDOT = -350
323484
YDOT = -15948
413332 feet/sec YDOT = -4865
459058 meter/sec
ZDOT = -19396
981421 ZDOT = -5914
103228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15745943
34 X = -4799363
53
Y = -15428345
75 feet Y = -4702559
78 meter
Z = 3161749
87 Z = 963701
36
XDOT = 7922
651684 XDOT = 2414
824233
YDOT = -12051
447366 feet/sec YDOT = -3673
281157 meter/sec
ZDOT = -19404
250894 ZDOT = -5914
415673
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 13042
53403794
00016717 00000-0 10270-3 0 9057
2 25544 51
6462 12
4794 0012563 264
0231 95
9490 15
52448798 15193
Satellite: ISS
Catalog Number: 25544
Epoch time: 13042
53403794 = yrday
fracday
Element set: 905
Inclination: 51
6462 deg
RA of node: 12
4794 deg
Eccentricity:
0012563
Arg of perigee: 264
0231 deg
Mean anomaly: 95
9490 deg
Mean motion: 15
52448798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1519
Checksum: 314
Coasting Arc #7 (Orbit 1534)
---------------------------------------
Vector Time (GMT): 2013/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6717057
79 A = 6794099
83 meter
Y = 971678
56 meter E =
0008432
Z = 162788
37 I = 51
71323
XDOT = -820
179274 Wp = 336
29430
YDOT = 4681
623737 meter/sec RA = 7
14634 deg
ZDOT = 6013
964025 TA = 25
45630
MA = 25
41479
Ha = 221
881 n
mi
Hp = 219
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22037591
18 X = 6704902
29
Y = 3187921
78 feet Y = 1046724
97 meter
Z = 534082
56 Z = 195388
93
XDOT = -2690
876882 XDOT = -901
682826
YDOT = 15359
657931 feet/sec YDOT = 4671
996802 meter/sec
ZDOT = 19730
853102 ZDOT = 6009
781371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15368878
02 X = 4684434
02
Y = 16107535
95 feet Y = 4909576
96 meter
Z = 669618
17 Z = 204099
62
XDOT = -10518
997038 XDOT = -3206
190297
YDOT = 9229
715083 feet/sec YDOT = 2813
217157 meter/sec
ZDOT = 19712
820683 ZDOT = 6008
467744
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 13043
56398028
00016717 00000-0 10270-3 0 9065
2 25544 51
6462 7
3582 0012535 267
1168 92
8550 15
52482851 15352
Satellite: ISS
Catalog Number: 25544
Epoch time: 13043
56398028 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 7
3582 deg
Eccentricity:
0012535
Arg of perigee: 267
1168 deg
Mean anomaly: 92
8550 deg
Mean motion: 15
52482851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1535
Checksum: 311
Coasting Arc #8 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2013/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6533937
90 A = 6793327
54 meter
Y = -1287650
05 meter E =
0009812
Z = -1312648
71 I = 51
68137
XDOT = 2067
994276 Wp = 227
36980
YDOT = -4530
453351 meter/sec RA = 2
18708 deg
ZDOT = -5828
403229 TA = 326
89975
MA = 326
96112
Ha = 221
863 n
mi
Hp = 218
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21436804
13 X = -6512677
12
Y = -4224573
65 feet Y = -1360597
89 meter
Z = -4306590
24 Z = -1344337
68
XDOT = 6784
758124 XDOT = 2146
813397
YDOT = -14863
692096 feet/sec YDOT = -4506
887579 meter/sec
ZDOT = -19122
057838 ZDOT = -5818
165405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14520287
90 X = -4425783
75
Y = -16290893
48 feet Y = -4965464
33 meter
Z = -4438281
41 Z = -1352788
17
XDOT = 13287
519153 XDOT = 4050
035838
YDOT = -6627
100975 feet/sec YDOT = -2019
940377 meter/sec
ZDOT = -19078
850195 ZDOT = -5815
233540
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 13044
52953895
00016717 00000-0 10270-3 0 9072
2 25544 51
6473 2
5573 0012605 271
5296 88
4412 15
52488352 15507
Satellite: ISS
Catalog Number: 25544
Epoch time: 13044
52953895 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 2
5573 deg
Eccentricity:
0012605
Arg of perigee: 271
5296 deg
Mean anomaly: 88
4412 deg
Mean motion: 15
52488352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1550
Checksum: 313
Coasting Arc #9 (Orbit 1565)
---------------------------------------
Vector Time (GMT): 2013/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6131366
73 A = 6791441
48 meter
Y = 1620814
28 meter E =
0004690
Z = 2421198
98 I = 51
64498
XDOT = -3275
618760 Wp = 7
55613
YDOT = 4399
808878 meter/sec RA = 357
22340 deg
ZDOT = 5353
086553 TA = 19
49755
MA = 19
47962
Ha = 221
859 n
mi
Hp = 218
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20116032
56 X = 6101025
37
Y = 5317632
15 feet Y = 1689209
64 meter
Z = 7943566
20 Z = 2450910
35
XDOT = -10746
780708 XDOT = -3350
578395
YDOT = 14435
068497 feet/sec YDOT = 4362
760195 meter/sec
ZDOT = 17562
619925 ZDOT = 5336
991659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13068868
72 X = 3983391
19
Y = 16129500
73 feet Y = 4916271
82 meter
Z = 8066975
78 Z = 2458814
22
XDOT = -16103
894651 XDOT = -4908
467090
YDOT = 4303
609911 feet/sec YDOT = 1311
740301 meter/sec
ZDOT = 17495
061018 ZDOT = 5332
494598
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 13045
55945229
00016717 00000-0 10270-3 0 9089
2 25544 51
6475 357
4362 0012625 274
9058 85
0652 15
52522937 15666
Satellite: ISS
Catalog Number: 25544
Epoch time: 13045
55945229 = yrday
fracday
Element set: 908
Inclination: 51
6475 deg
RA of node: 357
4362 deg
Eccentricity:
0012625
Arg of perigee: 274
9058 deg
Mean anomaly: 85
0652 deg
Mean motion: 15
52522937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1566
Checksum: 329
Coasting Arc #10 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2013/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5534365
69 A = 6788958
21 meter
Y = -1966485
96 meter E =
0007841
Z = -3400479
19 I = 51
60678
XDOT = 4366
396313 Wp = 284
88009
YDOT = -4286
097420 meter/sec RA = 352
25337 deg
ZDOT = -4616
904503 TA = 294
85832
MA = 294
93982
Ha = 222
100 n
mi
Hp = 218
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18157367
76 X = -5495446
29
Y = -6451725
58 feet Y = -2028157
36 meter
Z = -11156427
79 Z = -3427269
64
XDOT = 14325
447222 XDOT = 4436
427253
YDOT = -14061
999410 feet/sec YDOT = -4236
878414 meter/sec
ZDOT = -15147
324486 ZDOT = -4595
522777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11073699
28 X = -3375263
54
Y = -15690580
70 feet Y = -4782489
00 meter
Z = -11267631
06 Z = -3434373
95
XDOT = 18741
713565 XDOT = 5712
474295
YDOT = -2388
458115 feet/sec YDOT = -728
002033 meter/sec
ZDOT = -15057
786682 ZDOT = -4589
613381
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 13046
52498325
00016717 00000-0 10270-3 0 9098
2 25544 51
6479 352
6351 0012633 279
1627 80
8096 15
52540678 15817
Satellite: ISS
Catalog Number: 25544
Epoch time: 13046
52498325 = yrday
fracday
Element set: 909
Inclination: 51
6479 deg
RA of node: 352
6351 deg
Eccentricity:
0012633
Arg of perigee: 279
1627 deg
Mean anomaly: 80
8096 deg
Mean motion: 15
52540678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1581
Checksum: 329
Coasting Arc #11 (Orbit 1596)
---------------------------------------
Vector Time (GMT): 2013/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4751270
41 A = 6786183
80 meter
Y = 2368079
55 meter E =
0002816
Z = 4229834
25 I = 51
56782
XDOT = -5309
183937 Wp = 266
40341
YDOT = 4158
010885 meter/sec RA = 347
27629 deg
ZDOT = 3637
730300 TA = 146
29962
MA = 146
28172
Ha = 222
249 n
mi
Hp = 218
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15588157
51 X = 4703889
76
Y = 7769289
87 feet Y = 2420946
58 meter
Z = 13877408
96 Z = 4252800
01
XDOT = -17418
582469 XDOT = -5372
956017
YDOT = 13641
767996 feet/sec YDOT = 4098
283905 meter/sec
ZDOT = 11934
810697 ZDOT = 3611
783909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8462304
74 X = 2579310
48
Y = 15135709
80 feet Y = 4613364
35 meter
Z = 13972640
65 Z = 4258860
87
XDOT = -21030
897723 XDOT = -6410
217626
YDOT = 846
520593 feet/sec YDOT = 258
019477 meter/sec
ZDOT = 11826
301919 ZDOT = 3604
656825
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 13047
55486706
00016717 00000-0 10270-3 0 9104
2 25544 51
6481 347
5139 0012670 282
3774 77
5960 15
52572442 15971
Satellite: ISS
Catalog Number: 25544
Epoch time: 13047
55486706 = yrday
fracday
Element set: 910
Inclination: 51
6481 deg
RA of node: 347
5139 deg
Eccentricity:
0012670
Arg of perigee: 282
3774 deg
Mean anomaly: 77
5960 deg
Mean motion: 15
52572442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1597
Checksum: 329
Coasting Arc #12 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2013/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3844122
80 A = 6783812
81 meter
Y = -2806234
86 meter E =
0007193
Z = -4836026
84 I = 51
53051
XDOT = 6048
679216 Wp = 352
51280
YDOT = -3999
678205 meter/sec RA = 342
29155 deg
ZDOT = -2479
730928 TA = 253
03728
MA = 253
11613
Ha = 222
576 n
mi
Hp = 218
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12611951
46 X = -3788965
36
Y = -9206807
28 feet Y = -2848914
09 meter
Z = -15866229
79 Z = -4854566
91
XDOT = 19844
748084 XDOT = 6105
000633
YDOT = -13122
303822 feet/sec YDOT = -3931
723283 meter/sec
ZDOT = -8135
600156 ZDOT = -2450
210352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5433482
01 X = -1656125
32
Y = -14555490
33 feet Y = -4436513
45 meter
Z = -15942987
23 Z = -4859422
51
XDOT = 22771
178223 XDOT = 6940
655122
YDOT = 302
121393 feet/sec YDOT = 92
086600 meter/sec
ZDOT = -8012
246065 ZDOT = -2442
132601
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 13048
52037067
00016717 00000-0 10270-3 0 9115
2 25544 51
6482 342
7123 0012628 286
6291 73
3474 15
52589750 16128
Satellite: ISS
Catalog Number: 25544
Epoch time: 13048
52037067 = yrday
fracday
Element set: 911
Inclination: 51
6482 deg
RA of node: 342
7123 deg
Eccentricity:
0012628
Arg of perigee: 286
6291 deg
Mean anomaly: 73
3474 deg
Mean motion: 15
52589750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 307
Coasting Arc #13 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2013/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2826308
60 A = 6782143
94 meter
Y = 3309522
76 meter E =
0009035
Z = 5208844
75 I = 51
49649
XDOT = -6567
793936 Wp = 283
36932
YDOT = 3762
218227 meter/sec RA = 337
30115 deg
ZDOT = 1177
053833 TA = 155
32836
MA = 155
28512
Ha = 222
815 n
mi
Hp = 218
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9272666
01 X = 2763787
95
Y = 10858014
31 feet Y = 3340778
96 meter
Z = 17089385
67 Z = 5222422
52
XDOT = -21547
880369 XDOT = -6615
093458
YDOT = 12343
235652 feet/sec YDOT = 3688
508611 meter/sec
ZDOT = 3861
725173 ZDOT = 1145
033480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1971094
98 X = 600789
75
Y = 14073909
16 feet Y = 4289727
51 meter
Z = 17145430
23 Z = 5225927
13
XDOT = -23804
768080 XDOT = -7255
693311
YDOT = -1192
673353 feet/sec YDOT = -363
526838 meter/sec
ZDOT = 3728
006632 ZDOT = 1136
296421
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 13049
55022452
00016717 00000-0 10270-3 0 9122
2 25544 51
6483 337
5909 0012763 289
8902 70
0874 15
52629840 16287
Satellite: ISS
Catalog Number: 25544
Epoch time: 13049
55022452 = yrday
fracday
Element set: 912
Inclination: 51
6483 deg
RA of node: 337
5909 deg
Eccentricity:
0012763
Arg of perigee: 289
8902 deg
Mean anomaly: 70
0874 deg
Mean motion: 15
52629840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1628
Checksum: 323
Coasting Arc #14 (Orbit 1642)
---------------------------------------
Vector Time (GMT): 2013/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1784345
81 A = 6781737
13 meter
Y = -3834116
96 meter E =
0005710
Z = -5304333
36 I = 51
46756
XDOT = 6850
194441 Wp = 34
37661
YDOT = -3432
395318 meter/sec RA = 332
30595 deg
ZDOT = 181
377937 TA = 237
32948
MA = 237
38458
Ha = 223
108 n
mi
Hp = 218
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5854152
91 X = -1715572
67
Y = -12579123
89 feet Y = -3853686
31 meter
Z = -17402668
51 Z = -5312834
22
XDOT = 22474
391209 XDOT = 6887
186023
YDOT = -11261
139496 feet/sec YDOT = -3355
585302 meter/sec
ZDOT = 595
071972 ZDOT = 214
745015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1604308
37 X = 488993
19
Y = -13737442
26 feet Y = -4187172
40 meter
Z = -17437523
05 Z = -5314957
03
XDOT = 24051
654352 XDOT = 7330
944246
YDOT = 1896
291731 feet/sec YDOT = 577
989720 meter/sec
ZDOT = 734
345480 ZDOT = 223
828502
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 13050
51570109
00016717 00000-0 10270-3 0 9138
2 25544 51
6487 332
7888 0012672 293
9689 66
0136 15
52627037 16430
Satellite: ISS
Catalog Number: 25544
Epoch time: 13050
51570109 = yrday
fracday
Element set: 913
Inclination: 51
6487 deg
RA of node: 332
7888 deg
Eccentricity:
0012672
Arg of perigee: 293
9689 deg
Mean anomaly: 66
0136 deg
Mean motion: 15
52627037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1643
Checksum: 322
Coasting Arc #15 (Orbit 1658)
---------------------------------------
Vector Time (GMT): 2013/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 726013
44 A = 6782463
91 meter
Y = 4389934
90 meter E =
0011383
Z = 5127302
83 I = 51
44354
XDOT = -6893
291060 Wp = 319
78244
YDOT = 2956
830247 meter/sec RA = 327
30968 deg
ZDOT = -1548
942588 TA = 145
24298
MA = 145
16856
Ha = 223
401 n
mi
Hp = 218
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2381933
84 X = 651963
70
Y = 14402673
55 feet Y = 4397639
81 meter
Z = 16821859
67 Z = 5130649
63
XDOT = -22615
784318 XDOT = -6918
318435
YDOT = 9700
886636 feet/sec YDOT = 2879
605135 meter/sec
ZDOT = -5081
832639 ZDOT = -1582
489868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5282755
56 X = -1610183
89
Y = 13592426
37 feet Y = 4142971
56 meter
Z = 16835201
69 Z = 5131369
48
XDOT = -23405
803677 XDOT = -7134
088961
YDOT = -2602
460026 feet/sec YDOT = -793
229816 meter/sec
ZDOT = -5221
788784 ZDOT = -1591
601221
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 13051
54552628
00016717 00000-0 10270-3 0 9149
2 25544 51
6486 327
6673 0012774 297
7371 62
2485 15
52664027 16599
Satellite: ISS
Catalog Number: 25544
Epoch time: 13051
54552628 = yrday
fracday
Element set: 914
Inclination: 51
6486 deg
RA of node: 327
6673 deg
Eccentricity:
0012774
Arg of perigee: 297
7371 deg
Mean anomaly: 62
2485 deg
Mean motion: 15
52664027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1659
Checksum: 332
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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