[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 24th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 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 3344)
---------------------------------------
Vector Time (GMT): 2012/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3795578
56 A = 6794543
17 meter
Y = -4061105
73 meter E =
0024225
Z = -3930847
79 I = 51
57216
XDOT = 6199
600261 Wp = 98
20105
YDOT = 1888
486560 meter/sec RA = 347
19232 deg
ZDOT = 4053
311483 TA = 214
32068
MA = 214
47743
Ha = 233
838 n
mi
Hp = 214
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12452685
55 X = 3859803
70
Y = -13323837
70 feet Y = -4018302
37 meter
Z = -12896482
26 Z = -3912252
82
XDOT = 20339
895868 XDOT = 6158
332026
YDOT = 6195
822046 feet/sec YDOT = 1957
583887 meter/sec
ZDOT = 13298
266021 ZDOT = 4083
328403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11837087
14 X = -3607944
16
Y = 13945114
22 feet Y = 4250470
81 meter
Z = -12819143
53 Z = -3907274
95
XDOT = -19530
294521 XDOT = -5952
833770
YDOT = -4294
534377 feet/sec YDOT = -1308
974078 meter/sec
ZDOT = 13422
166391 ZDOT = 4091
076316
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 12268
50844899
00016717 00000-0 10270-3 0 9003
2 25544 51
6486 347
7080 0017847 96
1252 264
1933 15
50134953 33452
Satellite: ISS
Catalog Number: 25544
Epoch time: 12268
50844899 = yrday
fracday
Element set: 900
Inclination: 51
6486 deg
RA of node: 347
7080 deg
Eccentricity:
0017847
Arg of perigee: 96
1252 deg
Mean anomaly: 264
1933 deg
Mean motion: 15
50134953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 329
Coasting Arc #2 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2012/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3854197
59 A = 6795393
80 meter
Y = 4249438
07 meter E =
0029639
Z = 3614651
88 I = 51
54614
XDOT = -6051
457498 Wp = 93
71613
YDOT = -1725
475542 meter/sec RA = 342
23078 deg
ZDOT = -4394
747857 TA = 43
38403
MA = 43
15111
Ha = 233
803 n
mi
Hp = 214
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12645005
22 X = -3918988
33
Y = 13941725
94 feet Y = 4205976
08 meter
Z = 11859094
09 Z = 3595770
69
XDOT = -19853
863184 XDOT = -6010
364502
YDOT = -5661
008995 feet/sec YDOT = -1792
917338 meter/sec
ZDOT = -14418
464098 ZDOT = -4424
045479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11738946
85 X = 3578031
00
Y = -14775709
85 feet Y = -4503636
36 meter
Z = 11780556
75 Z = 3590713
70
XDOT = 19027
267221 XDOT = 5799
511049
YDOT = 3447
531594 feet/sec YDOT = 1050
807630 meter/sec
ZDOT = -14539
406800 ZDOT = -4431
611193
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 12269
53993328
00016717 00000-0 10270-3 0 9010
2 25544 51
6488 342
5964 0017815 99
2404 261
0762 15
50174947 33617
Satellite: ISS
Catalog Number: 25544
Epoch time: 12269
53993328 = yrday
fracday
Element set: 901
Inclination: 51
6488 deg
RA of node: 342
5964 deg
Eccentricity:
0017815
Arg of perigee: 99
2404 deg
Mean anomaly: 261
0762 deg
Mean motion: 15
50174947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3361
Checksum: 331
Coasting Arc #3 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2012/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3851123
70 A = 6796099
98 meter
Y = -4502397
98 meter E =
0022378
Z = -3352209
49 I = 51
51956
XDOT = 5858
582772 Wp = 98
82795
YDOT = 1560
218211 meter/sec RA = 337
26900 deg
ZDOT = 4658
347736 TA = 222
19140
MA = 222
36384
Ha = 233
710 n
mi
Hp = 214
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12634920
27 X = 3917468
46
Y = -14771646
92 feet Y = -4458961
72 meter
Z = -10998062
63 Z = -3333339
32
XDOT = 19221
072086 XDOT = 5818
071522
YDOT = 5118
826151 feet/sec YDOT = 1625
506530 meter/sec
ZDOT = 15283
293097 ZDOT = 4686
709814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11397033
12 X = -3473815
70
Y = 15800987
20 feet Y = 4816140
90 meter
Z = -10919550
55 Z = -3328279
01
XDOT = -18341
602073 XDOT = -5590
520312
YDOT = -2640
213678 feet/sec YDOT = -804
737129 meter/sec
ZDOT = 15400
382730 ZDOT = 4694
036656
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 12270
50692764
00016717 00000-0 10270-3 0 9020
2 25544 51
6481 337
8057 0017846 102
8233 257
4913 15
50202058 33763
Satellite: ISS
Catalog Number: 25544
Epoch time: 12270
50692764 = yrday
fracday
Element set: 902
Inclination: 51
6481 deg
RA of node: 337
8057 deg
Eccentricity:
0017846
Arg of perigee: 102
8233 deg
Mean anomaly: 257
4913 deg
Mean motion: 15
50202058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 307
Coasting Arc #4 (Orbit 3391)
---------------------------------------
Vector Time (GMT): 2012/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3871732
47 A = 6796937
88 meter
Y = 4706084
91 meter E =
0030882
Z = 2975776
45 I = 51
49553
XDOT = -5658
639027 Wp = 101
92922
YDOT = -1491
642585 meter/sec RA = 332
30434 deg
ZDOT = -4965
962392 TA = 43
96589
MA = 43
72062
Ha = 233
610 n
mi
Hp = 214
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12702534
37 X = -3938524
79
Y = 15439911
13 feet Y = 4662415
69 meter
Z = 9763046
08 Z = 2956804
93
XDOT = -18565
088670 XDOT = -5617
415074
YDOT = -4893
840502 feet/sec YDOT = -1554
691133 meter/sec
ZDOT = -16292
527533 ZDOT = -4993
351488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11114902
94 X = 3387822
42
Y = -16665515
84 feet Y = -5079649
23 meter
Z = 9684101
32 Z = 2951714
08
XDOT = 17653
692105 XDOT = 5380
845354
YDOT = 2168
975130 feet/sec YDOT = 661
103619 meter/sec
ZDOT = -16405
597417 ZDOT = -5000
426093
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 12271
53836311
00016717 00000-0 10270-3 0 9033
2 25544 51
6484 332
6939 0017772 105
8986 254
4125 15
50254069 33923
Satellite: ISS
Catalog Number: 25544
Epoch time: 12271
53836311 = yrday
fracday
Element set: 903
Inclination: 51
6484 deg
RA of node: 332
6939 deg
Eccentricity:
0017772
Arg of perigee: 105
8986 deg
Mean anomaly: 254
4125 deg
Mean motion: 15
50254069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 320
Coasting Arc #5 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2012/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3822709
79 A = 6797641
18 meter
Y = -4964633
70 meter E =
0021085
Z = -2658192
03 I = 51
47081
XDOT = 5434
696797 Wp = 97
66823
YDOT = 1423
945861 meter/sec RA = 327
33908 deg
ZDOT = 5188
845465 TA = 232
38256
MA = 232
57413
Ha = 233
572 n
mi
Hp = 214
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12541698
77 X = 3890854
19
Y = -16288168
30 feet Y = -4921505
10 meter
Z = -8721102
46 Z = -2639455
23
XDOT = 17830
370070 XDOT = 5393
163671
YDOT = 4671
738390 feet/sec YDOT = 1484
488493 meter/sec
ZDOT = 17023
771212 ZDOT = 5215
146009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10559269
68 X = -3218465
40
Y = 17676389
86 feet Y = 5387763
63 meter
Z = -8643108
71 Z = -2634419
54
XDOT = -16868
024076 XDOT = -5141
373738
YDOT = -1752
297681 feet/sec YDOT = -534
100333 meter/sec
ZDOT = 17132
342855 ZDOT = 5221
938102
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 12272
50531236
00016717 00000-0 10270-3 0 9040
2 25544 51
6475 327
9026 0017857 109
4639 250
8443 15
50268021 34079
Satellite: ISS
Catalog Number: 25544
Epoch time: 12272
50531236 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 327
9026 deg
Eccentricity:
0017857
Arg of perigee: 109
4639 deg
Mean anomaly: 250
8443 deg
Mean motion: 15
50268021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 303
Coasting Arc #6 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2012/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3796054
78 A = 6798371
64 meter
Y = 5163123
51 meter E =
0031644
Z = 2222984
03 I = 51
44900
XDOT = -5207
895832 Wp = 110
57770
YDOT = -1462
768096 meter/sec RA = 322
37143 deg
ZDOT = -5443
811713 TA = 44
64707
MA = 44
39267
Ha = 233
437 n
mi
Hp = 214
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12454247
96 X = -3864306
61
Y = 16939381
60 feet Y = 5120292
34 meter
Z = 7293254
69 Z = 2204376
34
XDOT = -17086
272415 XDOT = -5164
706756
YDOT = -4799
107926 feet/sec YDOT = -1520
765284 meter/sec
ZDOT = -17860
274648 ZDOT = -5469
006540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10069481
99 X = 3069178
11
Y = -18487307
47 feet Y = -5634931
32 meter
Z = 7215781
32 Z = 2199370
15
XDOT = 16124
790041 XDOT = 4914
836004
YDOT = 1703
809415 feet/sec YDOT = 519
321110 meter/sec
ZDOT = -17964
265762 ZDOT = -5475
508204
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 12273
53669914
00016717 00000-0 10270-3 0 9050
2 25544 51
6478 322
7903 0017805 112
6177 247
6859 15
50325988 34234
Satellite: ISS
Catalog Number: 25544
Epoch time: 12273
53669914 = yrday
fracday
Element set: 905
Inclination: 51
6478 deg
RA of node: 322
7903 deg
Eccentricity:
0017805
Arg of perigee: 112
6177 deg
Mean anomaly: 247
6859 deg
Mean motion: 15
50325988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 338
Coasting Arc #7 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2012/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3695639
05 A = 6798949
86 meter
Y = -5405431
52 meter E =
0020735
Z = -1852960
52 I = 51
42710
XDOT = 4979
733832 Wp = 95
76124
YDOT = 1499
383985 meter/sec RA = 317
40298 deg
ZDOT = 5610
193798 TA = 243
85678
MA = 244
07022
Ha = 233
419 n
mi
Hp = 214
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12124800
02 X = 3764810
41
Y = -17734355
38 feet Y = -5363718
06 meter
Z = -6079266
79 Z = -1834838
33
XDOT = 16337
709424 XDOT = 4935
343905
YDOT = 4919
238796 feet/sec YDOT = 1554
823006 meter/sec
ZDOT = 18406
147631 ZDOT = 5634
277397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9295074
06 X = -2833138
57
Y = 19391540
21 feet Y = 5910541
46 meter
Z = -6003781
09 Z = -1829952
48
XDOT = -15373
674057 XDOT = -4685
895853
YDOT = -1693
532311 feet/sec YDOT = -516
188648 meter/sec
ZDOT = 18505
536553 ZDOT = 5640
487541
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 12274
50360277
00016717 00000-0 10270-3 0 9069
2 25544 51
6471 317
9985 0017884 116
1086 244
1908 15
50336368 34385
Satellite: ISS
Catalog Number: 25544
Epoch time: 12274
50360277 = yrday
fracday
Element set: 906
Inclination: 51
6471 deg
RA of node: 317
9985 deg
Eccentricity:
0017884
Arg of perigee: 116
1086 deg
Mean anomaly: 244
1908 deg
Mean motion: 15
50336368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 328
Coasting Arc #8 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2012/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3619737
58 A = 6799473
70 meter
Y = 5573493
57 meter E =
0031678
Z = 1364448
48 I = 51
40768
XDOT = -4755
338398 Wp = 119
38211
YDOT = -1649
260950 meter/sec RA = 312
43251 deg
ZDOT = -5792
194017 TA = 45
70730
MA = 45
44790
Ha = 233
283 n
mi
Hp = 214
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11875779
47 X = -3688420
81
Y = 18285740
05 feet Y = 5532631
54 meter
Z = 4476537
02 Z = 1346696
20
XDOT = -15601
503930 XDOT = -4708
404978
YDOT = -5410
961121 feet/sec YDOT = -1702
176383 meter/sec
ZDOT = -19003
261211 ZDOT = -5815
181392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8611109
09 X = 2624666
05
Y = -20047643
50 feet Y = -6110521
74 meter
Z = 4402567
59 Z = 1341902
60
XDOT = 14718
960491 XDOT = 4486
339158
YDOT = 2064
986457 feet/sec YDOT = 629
407872 meter/sec
ZDOT = -19098
099247 ZDOT = -5821
100651
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 12275
53494088
00016717 00000-0 10270-3 0 9072
2 25544 51
6472 312
8855 0017898 119
4864 240
8074 15
50388831 34548
Satellite: ISS
Catalog Number: 25544
Epoch time: 12275
53494088 = yrday
fracday
Element set: 907
Inclination: 51
6472 deg
RA of node: 312
8855 deg
Eccentricity:
0017898
Arg of perigee: 119
4864 deg
Mean anomaly: 240
8074 deg
Mean motion: 15
50388831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 344
Coasting Arc #9 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2012/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3470619
98 A = 6799780
54 meter
Y = -5774483
30 meter E =
0021396
Z = -948344
83 I = 51
38917
XDOT = 4551
640712 Wp = 95
13643
YDOT = 1787
671820 meter/sec RA = 307
46142 deg
ZDOT = 5885
601250 TA = 254
58803
MA = 254
82449
Ha = 233
235 n
mi
Hp = 214
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11386548
50 X = 3539540
43
Y = -18945155
17 feet Y = -5735287
40 meter
Z = -3111367
56 Z = -931316
41
XDOT = 14933
204437 XDOT = 4502
720880
YDOT = 5865
065027 feet/sec YDOT = 1838
298198 meter/sec
ZDOT = 19309
715388 ZDOT = 5907
594282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7652656
22 X = -2332529
62
Y = 20747192
25 feet Y = 6323744
20 meter
Z = -3040372
62 Z = -926705
57
XDOT = -14138
695811 XDOT = -4309
474483
YDOT = -2427
826596 feet/sec YDOT = -740
001546 meter/sec
ZDOT = 19400
426561 ZDOT = 5913
250016
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 12276
50179822
00016717 00000-0 10270-3 0 9087
2 25544 51
6470 308
0934 0017911 122
9002 237
3875 15
50411179 34698
Satellite: ISS
Catalog Number: 25544
Epoch time: 12276
50179822 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 308
0934 deg
Eccentricity:
0017911
Arg of perigee: 122
9002 deg
Mean anomaly: 237
3875 deg
Mean motion: 15
50411179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 309
Coasting Arc #10 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2012/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3352631
28 A = 6799996
50 meter
Y = 5885071
42 meter E =
0030728
Z = 416847
73 I = 51
37227
XDOT = -4359
957988 Wp = 127
91642
YDOT = -2040
629175 meter/sec RA = 302
48839 deg
ZDOT = -5973
986245 TA = 47
57364
MA = 47
31413
Ha = 233
113 n
mi
Hp = 214
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10999446
45 X = -3420215
18
Y = 19307977
11 feet Y = 5847202
36 meter
Z = 1367610
66 Z = 400395
82
XDOT = -14304
324106 XDOT = -4307
794402
YDOT = -6694
977608 feet/sec YDOT = -2089
093815 meter/sec
ZDOT = -19599
692405 ZDOT = -5995
040213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6831164
12 X = 2082138
82
Y = -21149562
25 feet Y = -6446386
57 meter
Z = 1298989
88 Z = 395932
12
XDOT = 13710
593739 XDOT = 4178
988972
YDOT = 3159
324676 feet/sec YDOT = 962
962161 meter/sec
ZDOT = -19686
494842 ZDOT = -6000
443628
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 12277
53308738
00016717 00000-0 10270-3 0 9092
2 25544 51
6468 302
9799 0017973 126
5399 233
7410 15
50447037 34859
Satellite: ISS
Catalog Number: 25544
Epoch time: 12277
53308738 = yrday
fracday
Element set: 909
Inclination: 51
6468 deg
RA of node: 302
9799 deg
Eccentricity:
0017973
Arg of perigee: 126
5399 deg
Mean anomaly: 233
7410 deg
Mean motion: 15
50447037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 345
Coasting Arc #11 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2012/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3166879
07 A = 6799903
40 meter
Y = -6019473
93 meter E =
0022726
Z = 34744
63 I = 51
35716
XDOT = 4207
831733 Wp = 97
52981
YDOT = 2267
777572 meter/sec RA = 297
51511 deg
ZDOT = 5978
070793 TA = 262
84491
MA = 263
10336
Ha = 233
008 n
mi
Hp = 214
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10390023
19 X = 3233785
92
Y = -19748930
23 feet Y = -5983685
82 meter
Z = 113991
57 Z = 50292
42
XDOT = 13805
222222 XDOT = 4153
119611
YDOT = 7440
215130 feet/sec YDOT = 2314
526708 meter/sec
ZDOT = 19613
093152 ZDOT = 5998
379533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5765703
13 X = -1757386
32
Y = 21557144
71 feet Y = 6570617
71 meter
Z = 178886
88 Z = 54524
72
XDOT = -13419
470320 XDOT = -4090
254553
YDOT = -3811
272967 feet/sec YDOT = -1161
676000 meter/sec
ZDOT = 19696
792591 ZDOT = 6003
582382
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 12278
56435065
00016717 00000-0 10270-3 0 9102
2 25544 51
6469 297
8680 0017914 130
2025 230
0697 15
50494796 35014
Satellite: ISS
Catalog Number: 25544
Epoch time: 12278
56435065 = yrday
fracday
Element set: 910
Inclination: 51
6469 deg
RA of node: 297
8680 deg
Eccentricity:
0017914
Arg of perigee: 130
2025 deg
Mean anomaly: 230
0697 deg
Mean motion: 15
50494796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 320
Coasting Arc #12 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2012/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3023962
30 A = 6799715
80 meter
Y = 6047480
97 meter E =
0028677
Z = -593602
09 I = 51
34293
XDOT = -4075
764825 Wp = 135
48772
YDOT = -2603
273267 meter/sec RA = 292
53968 deg
ZDOT = -5953
495814 TA = 50
94259
MA = 50
68776
Ha = 232
892 n
mi
Hp = 214
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9921136
16 X = -3088478
11
Y = 19840816
83 feet Y = 6013304
37 meter
Z = -1947513
41 Z = -608449
69
XDOT = -13371
931841 XDOT = -4017
430363
YDOT = -8540
922791 feet/sec YDOT = -2648
525232 meter/sec
ZDOT = -19532
466581 ZDOT = -5973
154141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4905881
60 X = 1495312
71
Y = -21628082
23 feet Y = -6592239
46 meter
Z = -2009514
47 Z = -612500
01
XDOT = 13326
281944 XDOT = 4061
850737
YDOT = 4787
528097 feet/sec YDOT = 1459
238564 meter/sec
ZDOT = -19613
445378 ZDOT = -5978
178151
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 12279
53113729
00016717 00000-0 10270-3 0 9111
2 25544 51
6463 293
0738 0017967 133
6907 226
5736 15
50509654 35164
Satellite: ISS
Catalog Number: 25544
Epoch time: 12279
53113729 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 293
0738 deg
Eccentricity:
0017967
Arg of perigee: 133
6907 deg
Mean anomaly: 226
5736 deg
Mean motion: 15
50509654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 329
Coasting Arc #13 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2012/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2823033
02 A = 6799161
53 meter
Y = -6093523
18 meter E =
0024186
Z = 1065339
21 I = 51
33107
XDOT = 3996
584273 Wp = 103
48017
YDOT = 2895
523710 meter/sec RA = 287
56423 deg
ZDOT = 5853
160644 TA = 268
09583
MA = 268
37284
Ha = 232
734 n
mi
Hp = 214
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9261919
34 X = 2885787
00
Y = -19991873
96 feet Y = -6061603
32 meter
Z = 3495207
39 Z = 1079206
36
XDOT = 13112
153127 XDOT = 3935
475164
YDOT = 9499
749705 feet/sec YDOT = 2939
874678 meter/sec
ZDOT = 19203
282952 ZDOT = 5872
427525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3848039
26 X = -1172882
37
Y = 21685071
37 feet Y = 6609609
75 meter
Z = 3553156
68 Z = 1083002
16
XDOT = -13403
175030 XDOT = -4085
287749
YDOT = -5600
384793 feet/sec YDOT = -1706
997285 meter/sec
ZDOT = 19282
617932 ZDOT = 5877
341946
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 12280
56234935
00016717 00000-0 10270-3 0 9120
2 25544 51
6463 287
9618 0017880 137
5232 222
7306 15
50582131 35321
Satellite: ISS
Catalog Number: 25544
Epoch time: 12280
56234935 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 287
9618 deg
Eccentricity:
0017880
Arg of perigee: 137
5232 deg
Mean anomaly: 222
7306 deg
Mean motion: 15
50582131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 305
Coasting Arc #14 (Orbit 3546)
---------------------------------------
Vector Time (GMT): 2012/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2681619
60 A = 6798507
49 meter
Y = 6019959
52 meter E =
0025708
Z = -1630536
78 I = 51
31991
XDOT = -3942
607258 Wp = 141
00217
YDOT = -3281
390728 meter/sec RA = 282
58623 deg
ZDOT = -5699
496675 TA = 56
91622
MA = 56
66965
Ha = 232
613 n
mi
Hp = 214
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8797964
58 X = -2740815
87
Y = 19750523
36 feet Y = 5989640
89 meter
Z = -5349530
12 Z = -1643708
26
XDOT = -12935
063182 XDOT = -3877
933854
YDOT = -10765
717610 feet/sec YDOT = -3325
118153 meter/sec
ZDOT = -18699
136074 ZDOT = -5718
492611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3082417
00 X = 939520
70
Y = -21386769
91 feet Y = -6518687
47 meter
Z = -5404591
05 Z = -1647319
35
XDOT = 13699
584638 XDOT = 4175
633398
YDOT = 6663
292000 feet/sec YDOT = 2030
971402 meter/sec
ZDOT = -18777
317560 ZDOT = -5723
326392
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 12281
52908882
00016717 00000-0 10270-3 0 9137
2 25544 51
6455 283
1672 0017883 140
8208 219
4242 15
50582702 35475
Satellite: ISS
Catalog Number: 25544
Epoch time: 12281
52908882 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 283
1672 deg
Eccentricity:
0017883
Arg of perigee: 140
8208 deg
Mean anomaly: 219
4242 deg
Mean motion: 15
50582702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3547
Checksum: 316
Coasting Arc #15 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2012/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2494827
20 A = 6797520
47 meter
Y = -5963245
86 meter E =
0025285
Z = 2101992
01 I = 51
31147
XDOT = 3947
650302 Wp = 112
63840
YDOT = 3606
099081 meter/sec RA = 277
60837 deg
ZDOT = 5482
299564 TA = 270
70120
MA = 270
99092
Ha = 232
423 n
mi
Hp = 214
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8185128
60 X = 2551112
94
Y = -19564454
91 feet Y = -5935032
29 meter
Z = 6896299
24 Z = 2114248
98
XDOT = 12951
608604 XDOT = 3880
400730
YDOT = 11831
033730 feet/sec YDOT = 3649
868515 meter/sec
ZDOT = 17986
547125 ZDOT = 5501
313661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2171621
49 X = -661910
23
Y = 21079339
00 feet Y = 6424982
53 meter
Z = 6947567
68 Z = 2117618
63
XDOT = -14164
645147 XDOT = -4317
383841
YDOT = -7480
455177 feet/sec YDOT = -2280
042738 meter/sec
ZDOT = 18064
778325 ZDOT = 5506
144433
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 12282
56024879
00016717 00000-0 10270-3 0 9148
2 25544 51
6451 278
0549 0017807 144
9481 215
2846 15
50667959 35631
Satellite: ISS
Catalog Number: 25544
Epoch time: 12282
56024879 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 278
0549 deg
Eccentricity:
0017807
Arg of perigee: 144
9481 deg
Mean anomaly: 215
2846 deg
Mean motion: 15
50667959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 343
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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