[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 27th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 ET - UTC (sec) : 66 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
299/12:52:57
996 -2
3 5
8 5
9
N/A -4
3 -0
5 218
8
000/00:01:51
992 3
2 0
4 203
1
Coasting Arc #1 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2011/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3175025
94 A = 6770830
81 meter
Y = -5709174
90 meter E =
0026005
Z = 1711936
53 I = 51
39282
XDOT = 5061
230634 Wp = 21
10112
YDOT = -1108
778685 meter/sec RA = 228
84184 deg
ZDOT = 5686
087165 TA = 357
82802
MA = 357
83929
Ha = 216
399 n
mi
Hp = 202
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10416751
77 X = -3119265
28
Y = -18730888
78 feet Y = -5744368
05 meter
Z = 5616589
66 Z = 1696647
94
XDOT = 16605
087381 XDOT = 5045
630540
YDOT = -3637
725344 feet/sec YDOT = -1052
267598 meter/sec
ZDOT = 18655
141616 ZDOT = 5710
637294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18743120
48 X = 5712903
12
Y = 10428005
75 feet Y = 3178456
15 meter
Z = 5554558
70 Z = 1693029
49
XDOT = -11349
755443 XDOT = -3459
405459
YDOT = 10404
483471 feet/sec YDOT = 3171
286562 meter/sec
ZDOT = 18755
198547 ZDOT = 5716
584517
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 11297
56075329
00016717 00000-0 10270-3 0 9004
2 25544 51
6396 229
4913 0018544 349
7760 10
3016 15
60093073 21110
Satellite: ISS
Catalog Number: 25544
Epoch time: 11297
56075329 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 229
4913 deg
Eccentricity:
0018544
Arg of perigee: 349
7760 deg
Mean anomaly: 10
3016 deg
Mean motion: 15
60093073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 298
Coasting Arc #2 (Orbit 2125)
---------------------------------------
Vector Time (GMT): 2011/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 7361
99 A = 6763037
59 meter
Y = 5029397
00 meter E =
0022925
Z = -4539040
81 I = 51
38915
XDOT = -6446
157358 Wp = 18
40209
YDOT = -2780
387398 meter/sec RA = 223
80077 deg
ZDOT = -3074
105689 TA = 220
62602
MA = 220
79729
Ha = 216
438 n
mi
Hp = 202
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 24153
51 X = -26827
89
Y = 16500646
33 feet Y = 5029287
80 meter
Z = -14891866
18 Z = -4539088
49
XDOT = -21148
810229 XDOT = -6399
653607
YDOT = -9122
005900 feet/sec YDOT = -2852
212508 meter/sec
ZDOT = -10085
648586 ZDOT = -3105
308692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9018775
90 X = -2748922
89
Y = -13817427
06 feet Y = -4211551
77 meter
Z = -14892279
26 Z = -4539166
72
XDOT = 21663
775833 XDOT = 6603
118874
YDOT = -3072
606410 feet/sec YDOT = -936
530434 meter/sec
ZDOT = -10212
643726 ZDOT = -3112
813808
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 11298
52156926
00016717 00000-0 10270-3 0 9015
2 25544 51
6404 224
6579 0018490 353
4604 6
6307 15
60177200 21266
Satellite: ISS
Catalog Number: 25544
Epoch time: 11298
52156926 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 224
6579 deg
Eccentricity:
0018490
Arg of perigee: 353
4604 deg
Mean anomaly: 6
6307 deg
Mean motion: 15
60177200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2126
Checksum: 295
Coasting Arc #3 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2011/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3504015
85 A = 6759919
76 meter
Y = -2516489
96 meter E =
0020412
Z = 5205621
35 I = 51
40222
XDOT = 5395
530427 Wp = 5
81673
YDOT = 5366
788558 meter/sec RA = 218
72257 deg
ZDOT = -1017
140685 TA = 94
05915
MA = 93
82581
Ha = 216
356 n
mi
Hp = 201
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11496115
00 X = 3506606
64
Y = -8256200
65 feet Y = -2477291
15 meter
Z = 17078810
22 Z = 5222650
76
XDOT = 17701
871480 XDOT = 5340
058148
YDOT = 17607
574009 feet/sec YDOT = 5426
814471 meter/sec
ZDOT = -3337
075737 ZDOT = -991
063503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4892694
70 X = -1491293
34
Y = 13191232
33 feet Y = 4020687
62 meter
Z = 17148300
08 Z = 5226801
87
XDOT = -23552
979767 XDOT = -7178
948233
YDOT = -4449
348182 feet/sec YDOT = -1356
161326 meter/sec
ZDOT = -3231
069566 ZDOT = -984
830004
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 11299
54639967
00016717 00000-0 10270-3 0 9020
2 25544 51
6405 219
5021 0018437 356
7666 3
3367 15
60247685 21420
Satellite: ISS
Catalog Number: 25544
Epoch time: 11299
54639967 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 219
5021 deg
Eccentricity:
0018437
Arg of perigee: 356
7666 deg
Mean anomaly: 3
3367 deg
Mean motion: 15
60247685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 324
Coasting Arc #4 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2011/299/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5404287
89 A = 6767682
00 meter
Y = -162922
03 meter E =
0018991
Z = -4058983
90 I = 51
41989
XDOT = -2695
827329 Wp = 7
46564
YDOT = -6074
509409 meter/sec RA = 218
51580 deg
ZDOT = 3853
656734 TA = 302
36001
MA = 302
54369
Ha = 218
835 n
mi
Hp = 203
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17730603
31 X = -5382346
04
Y = -534521
08 feet Y = -223233
61 meter
Z = -13316876
30 Z = -4085185
34
XDOT = -8844
577850 XDOT = -2646
421491
YDOT = -19929
492811 feet/sec YDOT = -6104
379363 meter/sec
ZDOT = 12643
230755 ZDOT = 3840
680364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12377208
64 X = 3772573
19
Y = -12594062
64 feet Y = -3838670
29 meter
Z = -13423617
00 Z = -4091518
46
XDOT = 19769
327508 XDOT = 6025
691024
YDOT = 6080
103643 feet/sec YDOT = 1853
215590 meter/sec
ZDOT = 12590
629616 ZDOT = 3837
623907
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 11299
54639917
00016717 00000-0 10270-3 0 9036
2 25544 51
6420 219
5011 0021784 347
5856 12
4760 15
59123070 21421
Satellite: ISS
Catalog Number: 25544
Epoch time: 11299
54639917 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 219
5011 deg
Eccentricity:
0021784
Arg of perigee: 347
5856 deg
Mean anomaly: 12
4760 deg
Mean motion: 15
59123070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 301
Coasting Arc #5 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2011/300/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6038099
76 A = 6774063
60 meter
Y = 2842780
13 meter E =
0016546
Z = 1206905
63 I = 51
46579
XDOT = -1103
377224 Wp = 31
09059
YDOT = 4841
797944 meter/sec RA = 213
49216 deg
ZDOT = -5834
599239 TA = 135
75976
MA = 135
62737
Ha = 219
015 n
mi
Hp = 202
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19810038
57 X = 5999999
36
Y = 9326706
47 feet Y = 2910088
85 meter
Z = 3959664
15 Z = 1236146
94
XDOT = -3620
004017 XDOT = -1129
092934
YDOT = 15885
163858 feet/sec YDOT = 4829
315410 meter/sec
ZDOT = -19142
385954 ZDOT = -5840
022151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20137872
08 X = -6138023
41
Y = 8540169
16 feet Y = 2603043
56 meter
Z = 4078681
24 Z = 1243182
04
XDOT = -8887
334209 XDOT = -2708
859467
YDOT = -11727
974933 feet/sec YDOT = -3574
686760 meter/sec
ZDOT = -19164
696417 ZDOT = -5841
399468
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 11300
57191951
00016717 00000-0 10270-3 0 9044
2 25544 51
6418 214
3498 0021655 351
3040 8
7737 15
59163698 21584
Satellite: ISS
Catalog Number: 25544
Epoch time: 11300
57191951 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 214
3498 deg
Eccentricity:
0021655
Arg of perigee: 351
3040 deg
Mean anomaly: 8
7737 deg
Mean motion: 15
59163698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 312
Coasting Arc #6 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2011/301/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4632522
61 A = 6772719
78 meter
Y = -4433086
99 meter E =
0028794
Z = 2119774
73 I = 51
48743
XDOT = 4805
635911 Wp = 23
19176
YDOT = -2385
193299 meter/sec RA = 208
48629 deg
ZDOT = 5514
567803 TA =
45853
MA =
45590
Ha = 219
151 n
mi
Hp = 202
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15198565
00 X = -4592904
40
Y = -14544248
66 feet Y = -4484669
20 meter
Z = 6954641
49 Z = 2097365
56
XDOT = 15766
522017 XDOT = 4805
160993
YDOT = -7825
437332 feet/sec YDOT = -2331
456439 meter/sec
ZDOT = 18092
414051 ZDOT = 5537
912995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20967761
11 X = 6390973
59
Y = -2035585
91 feet Y = -620446
59 meter
Z = 6863524
57 Z = 2092002
29
XDOT = -4454
285474 XDOT = -1357
666213
YDOT = 15436
416322 feet/sec YDOT = 4705
019695 meter/sec
ZDOT = 18187
651862 ZDOT = 5543
596288
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 11301
59740088
00016717 00000-0 10270-3 0 9059
2 25544 51
6418 209
1981 0021770 355
1551 4
9390 15
59215374 21740
Satellite: ISS
Catalog Number: 25544
Epoch time: 11301
59740088 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 209
1981 deg
Eccentricity:
0021770
Arg of perigee: 355
1551 deg
Mean anomaly: 4
9390 deg
Mean motion: 15
59215374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2174
Checksum: 303
Coasting Arc #7 (Orbit 2188)
---------------------------------------
Vector Time (GMT): 2011/302/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1593603
44 A = 6765288
98 meter
Y = 4698388
60 meter E =
0026758
Z = -4619605
93 I = 51
49054
XDOT = -7056
098283 Wp = 20
01785
YDOT = -513
909643 meter/sec RA = 203
45549 deg
ZDOT = -2937
191264 TA = 220
54135
MA = 220
74097
Ha = 219
124 n
mi
Hp = 202
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5228357
73 X = 1563388
36
Y = 15414660
76 feet Y = 4716040
42 meter
Z = -15156187
42 Z = -4611937
32
XDOT = -23149
928749 XDOT = -7035
558576
YDOT = -1686
055260 feet/sec YDOT = -592
700338 meter/sec
ZDOT = -9636
454278 ZDOT = -2971
420612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15246570
37 X = -4647154
65
Y = -5781826
98 feet Y = -1762300
86 meter
Z = -15125147
17 Z = -4610144
86
XDOT = 15657
673914 XDOT = 4772
459009
YDOT = -15546
856893 feet/sec YDOT = -4738
681981 meter/sec
ZDOT = -9775
932569 ZDOT = -2979
704247
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 11302
55875259
00016717 00000-0 10270-3 0 9066
2 25544 51
6418 204
3688 0021709 358
3191 1
7888 15
59308250 21897
Satellite: ISS
Catalog Number: 25544
Epoch time: 11302
55875259 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 204
3688 deg
Eccentricity:
0021709
Arg of perigee: 358
3191 deg
Mean anomaly: 1
7888 deg
Mean motion: 15
59308250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2189
Checksum: 327
Coasting Arc #8 (Orbit 2204)
---------------------------------------
Vector Time (GMT): 2011/303/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2241729
32 A = 6762315
87 meter
Y = -3643210
26 meter E =
0023477
Z = 5237156
07 I = 51
50936
XDOT = 6996
968047 Wp = 8
92086
YDOT = 3042
949269 meter/sec RA = 198
39241 deg
ZDOT = -854
915792 TA = 89
39238
MA = 89
12338
Ha = 219
039 n
mi
Hp = 201
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7354754
97 X = 2256860
25
Y = -11952789
56 feet Y = -3618057
41 meter
Z = 17182270
56 Z = 5248083
20
XDOT = 22955
931913 XDOT = 6966
574242
YDOT = 9983
429359 feet/sec YDOT = 3121
023735 meter/sec
ZDOT = -2804
841837 ZDOT = -820
997738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4765820
86 X = 1452622
20
Y = 13141928
02 feet Y = 4005659
66 meter
Z = 17226975
93 Z = 5250782
26
XDOT = -21221
358315 XDOT = -6468
270015
YDOT = 11291
244095 feet/sec YDOT = 3441
571200 meter/sec
ZDOT = -2666
727602 ZDOT = -812
818573
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 11303
58415759
00016717 00000-0 10270-3 0 9076
2 25544 51
6414 199
2160 0021620 1
8404 358
2827 15
59383673 22053
Satellite: ISS
Catalog Number: 25544
Epoch time: 11303
58415759 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 199
2160 deg
Eccentricity:
0021620
Arg of perigee: 1
8404 deg
Mean anomaly: 358
2827 deg
Mean motion: 15
59383673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2205
Checksum: 303
Coasting Arc #9 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2011/304/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5360063
94 A = 6767997
62 meter
Y = 1767240
59 meter E =
0021661
Z = -3724468
33 I = 51
55747
XDOT = -4460
174422 Wp = 21
41891
YDOT = -4554
075015 meter/sec RA = 193
34240 deg
ZDOT = 4285
564169 TA = 293
89448
MA = 294
12127
Ha = 219
115 n
mi
Hp = 201
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17585511
61 X = -5361334
20
Y = 5798033
43 feet Y = 1707294
04 meter
Z = -12219384
28 Z = -3750510
86
XDOT = -14633
118181 XDOT = -4429
737095
YDOT = -14941
190993 feet/sec YDOT = -4603
781321 meter/sec
ZDOT = 14060
249898 ZDOT = 4263
970235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6163422
34 X = 1878611
13
Y = -17385966
40 feet Y = -5299242
56 meter
Z = -12325630
20 Z = -3756852
09
XDOT = 19559
698938 XDOT = 5961
796236
YDOT = -2907
978045 feet/sec YDOT = -886
351708 meter/sec
ZDOT = 13972
425183 ZDOT = 4258
795196
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 11304
54544169
00016717 00000-0 10270-3 0 9082
2 25544 51
6411 194
3858 0021638 5
1988 354
9389 15
59402609 22207
Satellite: ISS
Catalog Number: 25544
Epoch time: 11304
54544169 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 194
3858 deg
Eccentricity:
0021638
Arg of perigee: 5
1988 deg
Mean anomaly: 354
9389 deg
Mean motion: 15
59402609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 323
Coasting Arc #10 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2011/305/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6735582
62 A = 6773761
19 meter
Y = 500316
63 meter E =
0018969
Z = 607000
81 I = 51
60653
XDOT = 192
428016 Wp = 47
10046
YDOT = 4805
450696 meter/sec RA = 188
33183 deg
ZDOT = -5965
194534 TA = 126
34174
MA = 126
16651
Ha = 219
236 n
mi
Hp = 201
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22098368
16 X = 6726538
64
Y = 1641458
76 feet Y = 575587
47 meter
Z = 1991472
48 Z = 639700
59
XDOT = 631
325511 XDOT = 167
656307
YDOT = 15765
914358 feet/sec YDOT = 4807
464075 meter/sec
ZDOT = -19570
848210 ZDOT = -5964
319853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14559583
95 X = -4437761
19
Y = 16688381
67 feet Y = 5086618
73 meter
Z = 2124772
25 Z = 647630
58
XDOT = -11847
448102 XDOT = -3611
102182
YDOT = -7793
558779 feet/sec YDOT = -2375
476716 meter/sec
ZDOT = -19567
497492 ZDOT = -5964
173235
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 11305
57077478
00016717 00000-0 10270-3 0 9091
2 25544 51
6409 189
2329 0021435 9
2695 350
8852 15
59433351 22360
Satellite: ISS
Catalog Number: 25544
Epoch time: 11305
57077478 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 189
2329 deg
Eccentricity:
0021435
Arg of perigee: 9
2695 deg
Mean anomaly: 350
8852 deg
Mean motion: 15
59433351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 325
Coasting Arc #11 (Orbit 2251)
---------------------------------------
Vector Time (GMT): 2011/306/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5640643
70 A = 6770615
65 meter
Y = -2500601
39 meter E =
0029787
Z = 2738667
37 I = 51
62621
XDOT = 4215
223255 Wp = 37
43208
YDOT = -3848
687755 meter/sec RA = 183
33130 deg
ZDOT = 5161
522174 TA = 353
73143
MA = 353
76861
Ha = 219
354 n
mi
Hp = 201
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18506048
89 X = -5625566
31
Y = -8204072
80 feet Y = -2563594
19 meter
Z = 8985129
17 Z = 2711301
56
XDOT = 13829
472620 XDOT = 4232
872814
YDOT = -12626
928329 feet/sec YDOT = -3801
451805 meter/sec
ZDOT = 16934
127868 ZDOT = 5182
042800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17522301
72 X = 5340797
56
Y = -10234277
13 feet Y = -3119407
67 meter
Z = 8873652
95 Z = 2704689
42
XDOT = 1443
102605 XDOT = 439
857674
YDOT = 17243
954462 feet/sec YDOT = 5255
957320 meter/sec
ZDOT = 17017
974383 ZDOT = 5187
078592
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 11306
59606889
00016717 00000-0 10270-3 0 9100
2 25544 51
6405 184
0791 0021619 12
6387 347
5306 15
59505787 22520
Satellite: ISS
Catalog Number: 25544
Epoch time: 11306
59606889 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 184
0791 deg
Eccentricity:
0021619
Arg of perigee: 12
6387 deg
Mean anomaly: 347
5306 deg
Mean motion: 15
59505787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2252
Checksum: 324
Coasting Arc #12 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2011/307/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2532632
11 A = 6763138
09 meter
Y = 3858675
85 meter E =
0029979
Z = -4966735
01 I = 51
63141
XDOT = -7105
704031 Wp = 36
87641
YDOT = 1899
034992 meter/sec RA = 178
29897 deg
ZDOT = -2131
204232 TA = 212
23992
MA = 212
42354
Ha = 219
268 n
mi
Hp = 200
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8309160
45 X = 2513423
11
Y = 12659697
66 feet Y = 3886889
76 meter
Z = -16295062
38 Z = -4954478
14
XDOT = -23312
677266 XDOT = -7116
058204
YDOT = 6230
429763 feet/sec YDOT = 1819
516703 meter/sec
ZDOT = -6992
139868 ZDOT = -2165
749235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15192560
49 X = -4630692
44
Y = -342248
08 feet Y = -104317
21 meter
Z = -16245249
22 Z = -4951551
96
XDOT = 8171
667917 XDOT = 2490
724381
YDOT = -21544
368871 feet/sec YDOT = -6566
723632 meter/sec
ZDOT = -7133
099360 ZDOT = -2174
168685
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 11307
55724798
00016717 00000-0 10270-3 0 9118
2 25544 51
6397 179
2477 0021504 15
8873 344
2952 15
59574945 22674
Satellite: ISS
Catalog Number: 25544
Epoch time: 11307
55724798 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 179
2477 deg
Eccentricity:
0021504
Arg of perigee: 15
8873 deg
Mean anomaly: 344
2952 deg
Mean motion: 15
59574945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 346
Coasting Arc #13 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2011/308/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1589288
59 A = 6762414
33 meter
Y = -4207269
04 meter E =
0025998
Z = 5046337
42 I = 51
66056
XDOT = 7436
204864 Wp = 26
85835
YDOT = 578
651047 meter/sec RA = 173
24156 deg
ZDOT = -1833
106790 TA = 81
00386
MA = 80
70971
Ha = 219
184 n
mi
Hp = 200
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5214201
40 X = 1611702
52
Y = -13803376
10 feet Y = -4189371
12 meter
Z = 16556225
12 Z = 5054112
87
XDOT = 24396
997586 XDOT = 7438
086591
YDOT = 1898
461439 feet/sec YDOT = 661
817700 meter/sec
ZDOT = -6014
129887 ZDOT = -1796
976773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8604900
09 X = 2622773
55
Y = 11942343
35 feet Y = 3640026
25 meter
Z = 16588122
51 Z = 5056059
74
XDOT = -14330
306979 XDOT = -4367
877567
YDOT = 18594
718020 feet/sec YDOT = 5667
670053 meter/sec
ZDOT = -5866
803420 ZDOT = -1788
201682
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 11308
58247048
00016717 00000-0 10270-3 0 9121
2 25544 51
6401 174
0939 0021418 19
5697 340
6276 15
59643359 22838
Satellite: ISS
Catalog Number: 25544
Epoch time: 11308
58247048 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 174
0939 deg
Eccentricity:
0021418
Arg of perigee: 19
5697 deg
Mean anomaly: 340
6276 deg
Mean motion: 15
59643359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2283
Checksum: 323
Coasting Arc #14 (Orbit 2297)
---------------------------------------
Vector Time (GMT): 2011/309/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4992973
27 A = 6769353
98 meter
Y = 3448806
23 meter E =
0024650
Z = -2984251
25 I = 51
71299
XDOT = -5019
180317 Wp = 31
21924
YDOT = -2979
149645 meter/sec RA = 168
20861 deg
ZDOT = 4993
699736 TA = 294
57078
MA = 294
82747
Ha = 219
187 n
mi
Hp = 200
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16381145
88 X = -5016670
25
Y = 11314981
08 feet Y = 3392839
11 meter
Z = -9790850
57 Z = -3008565
17
XDOT = -16467
127025 XDOT = -5009
752669
YDOT = -9774
113007 feet/sec YDOT = -3035
224261 meter/sec
ZDOT = 16383
529317 ZDOT = 4969
339251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -631027
31 X = -192337
12
Y = -19849880
79 feet Y = -6050243
66 meter
Z = -9890173
37 Z = -3014524
84
XDOT = 15757
871397 XDOT = 4802
999202
YDOT = -8551
489384 feet/sec YDOT = -2606
493964 meter/sec
ZDOT = 16284
302872 ZDOT = 4963
455515
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 11309
54358434
00016717 00000-0 10270-3 0 9131
2 25544 51
6389 169
2618 0021371 23
0076 337
2032 15
59677059 22984
Satellite: ISS
Catalog Number: 25544
Epoch time: 11309
54358434 = yrday
fracday
Element set: 913
Inclination: 51
6389 deg
RA of node: 169
2618 deg
Eccentricity:
0021371
Arg of perigee: 23
0076 deg
Mean anomaly: 337
2032 deg
Mean motion: 15
59677059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2298
Checksum: 319
Coasting Arc #15 (Orbit 2313)
---------------------------------------
Vector Time (GMT): 2011/310/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6572458
26 A = 6772988
79 meter
Y = -1605162
75 meter E =
0020251
Z = -458281
48 I = 51
75471
XDOT = 745
493810 Wp = 58
41341
YDOT = 4711
680934 meter/sec RA = 163
21507 deg
ZDOT = -5996
201878 TA = 126
52306
MA = 126
33641
Ha = 219
276 n
mi
Hp = 199
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21563183
26 X = 6592145
31
Y = -5266282
00 feet Y = -1531555
44 meter
Z = -1503548
17 Z = -426304
03
XDOT = 2445
845833 XDOT = 721
880438
YDOT = 15458
270781 feet/sec YDOT = 4719
885211 meter/sec
ZDOT = -19672
578341 ZDOT = -5992
637770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6937201
32 X = -2114458
96
Y = 21093962
53 feet Y = 6429439
78 meter
Z = -1373039
66 Z = -418502
49
XDOT = -12937
304868 XDOT = -3943
290524
YDOT = -5491
095943 feet/sec YDOT = -1673
686043 meter/sec
ZDOT = -19658
253343 ZDOT = -5991
835619
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 11310
56873668
00016717 00000-0 10270-3 0 9147
2 25544 51
6386 164
1079 0021385 26
8713 333
3546 15
59735353 23148
Satellite: ISS
Catalog Number: 25544
Epoch time: 11310
56873668 = yrday
fracday
Element set: 914
Inclination: 51
6386 deg
RA of node: 164
1079 deg
Eccentricity:
0021385
Arg of perigee: 26
8713 deg
Mean anomaly: 333
3546 deg
Mean motion: 15
59735353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2314
Checksum: 319
Coasting Arc #16 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2011/311/12:53:53
992
Vector Time (MET): N/A
Weight (LBS) : 870885
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5607487
48 A = 6767289
04 meter
Y = -859837
50 meter E =
0028593
Z = 3654404
27 I = 51
76365
XDOT = 3649
745102 Wp = 52
61550
YDOT = -5172
692607 meter/sec RA = 158
21522 deg
ZDOT = 4376
906598 TA = 350
97118
MA = 351
02249
Ha = 219
328 n
mi
Hp = 199
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18397268
62 X = -5615208
65
Y = -2820989
18 feet Y = -922586
90 meter
Z = 11989515
33 Z = 3627143
80
XDOT = 11974
229338 XDOT = 3686
053239
YDOT = -16970
776270 feet/sec YDOT = -5131
675750 meter/sec
ZDOT = 14359
929785 ZDOT = 4394
725817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11914433
37 X = 3631519
29
Y = -14391559
65 feet Y = -4386547
38 meter
Z = 11878351
68 Z = 3620521
59
XDOT = 7394
687675 XDOT = 2253
900803
YDOT = 18051
707484 feet/sec YDOT = 5502
160441 meter/sec
ZDOT = 14432
858766 ZDOT = 4399
135352
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 11311
59385222
00016717 00000-0 10270-3 0 9156
2 25544 51
6375 158
9525 0021261 30
3998 329
8386 15
59792880 23309
Satellite: ISS
Catalog Number: 25544
Epoch time: 11311
59385222 = yrday
fracday
Element set: 915
Inclination: 51
6375 deg
RA of node: 158
9525 deg
Eccentricity:
0021261
Arg of perigee: 30
3998 deg
Mean anomaly: 329
8386 deg
Mean motion: 15
59792880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 329
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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