[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 11th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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 1955)
---------------------------------------
Vector Time (GMT): 2013/070/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1984131
79 A = 6790494
61 meter
Y = -5927892
93 meter E =
0020336
Z = 2617583
39 I = 51
37488
XDOT = 5620
450119 Wp = 42
88478
YDOT = 424
249560 meter/sec RA = 231
94738 deg
ZDOT = 5211
833850 TA = 346
74488
MA = 346
79823
Ha = 226
177 n
mi
Hp = 215
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6509618
75 X = -1930412
72
Y = -19448467
60 feet Y = -5949779
99 meter
Z = 8587872
00 Z = 2608076
12
XDOT = 18439
796979 XDOT = 5589
970972
YDOT = 1391
894882 feet/sec YDOT = 486
931322 meter/sec
ZDOT = 17099
192420 ZDOT = 5239
063058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14411279
22 X = -4392557
91
Y = -14615079
17 feet Y = -4454676
13 meter
Z = 8548921
92 Z = 2605711
40
XDOT = 16029
195234 XDOT = 4885
698707
YDOT = -5719
609551 feet/sec YDOT = -1743
336991 meter/sec
ZDOT = 17212
470564 ZDOT = 5246
361028
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 13070
66287488
00016717 00000-0 10270-3 0 9007
2 25544 51
6455 232
6113 0011910 2
7236 357
3979 15
52739648 19562
Satellite: ISS
Catalog Number: 25544
Epoch time: 13070
66287488 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 232
6113 deg
Eccentricity:
0011910
Arg of perigee: 2
7236 deg
Mean anomaly: 357
3979 deg
Mean motion: 15
52739648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1956
Checksum: 323
Coasting Arc #2 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2013/071/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1261111
46 A = 6787853
36 meter
Y = 5603656
60 meter E =
0014335
Z = -3634692
97 I = 51
38588
XDOT = -6119
964592 Wp = 27
75688
YDOT = -1453
167182 meter/sec RA = 226
95795 deg
ZDOT = -4358
316994 TA = 195
42794
MA = 195
47168
Ha = 226
355 n
mi
Hp = 214
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4137504
79 X = 1216012
67
Y = 18384700
12 feet Y = 5617506
43 meter
Z = -11924845
70 Z = -3628677
04
XDOT = -20078
623988 XDOT = -6082
088752
YDOT = -4767
608866 feet/sec YDOT = -1521
393363 meter/sec
ZDOT = -14298
940270 ZDOT = -4387
954778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12082174
21 X = 3682646
70
Y = 14481712
47 feet Y = 4414025
96 meter
Z = -11900384
85 Z = -3627237
30
XDOT = -18925
463577 XDOT = -5768
481298
YDOT = 3923
424192 feet/sec YDOT = 1195
859694 meter/sec
ZDOT = -14422
142084 ZDOT = -4395
868907
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 13071
62828099
00016717 00000-0 10270-3 0 9014
2 25544 51
6458 227
8091 0012003 6
0577 354
0718 15
52727269 19713
Satellite: ISS
Catalog Number: 25544
Epoch time: 13071
62828099 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 227
8091 deg
Eccentricity:
0012003
Arg of perigee: 6
0577 deg
Mean anomaly: 354
0718 deg
Mean motion: 15
52727269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 311
Coasting Arc #3 (Orbit 1986)
---------------------------------------
Vector Time (GMT): 2013/072/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -388075
85 A = 6784898
69 meter
Y = -5108992
08 meter E =
0013752
Z = 4433568
54 I = 51
39913
XDOT = 6529
050115 Wp = 51
22652
YDOT = 2349
407599 meter/sec RA = 221
96391 deg
ZDOT = 3280
399147 TA = 5
62728
MA = 5
61185
Ha = 226
371 n
mi
Hp = 214
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1273214
73 X = -352454
17
Y = -16761785
04 feet Y = -5113131
97 meter
Z = 14545828
55 Z = 4431770
59
XDOT = 21420
768094 XDOT = 6486
358050
YDOT = 7708
030181 feet/sec YDOT = 2422
181326 meter/sec
ZDOT = 10762
464392 ZDOT = 3312
012516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9052924
47 X = -2759331
38
Y = -14171292
32 feet Y = -4319409
90 meter
Z = 14538867
71 Z = 4431446
88
XDOT = 21444
459320 XDOT = 6536
271201
YDOT = -2528
129946 feet/sec YDOT = -770
574008 meter/sec
ZDOT = 10893
804420 ZDOT = 3320
431587
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 13072
65803226
00016717 00000-0 10270-3 0 9024
2 25544 51
6467 222
6863 0012072 9
8058 350
3327 15
52783974 19871
Satellite: ISS
Catalog Number: 25544
Epoch time: 13072
65803226 = yrday
fracday
Element set: 902
Inclination: 51
6467 deg
RA of node: 222
6863 deg
Eccentricity:
0012072
Arg of perigee: 9
8058 deg
Mean anomaly: 350
3327 deg
Mean motion: 15
52783974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1987
Checksum: 319
Coasting Arc #4 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2013/073/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -580187
73 A = 6782737
39 meter
Y = 4560783
34 meter E =
0021311
Z = -5004530
18 I = 51
41532
XDOT = -6720
912249 Wp = 44
95951
YDOT = -3060
731314 meter/sec RA = 216
96721 deg
ZDOT = -2000
635378 TA = 205
44543
MA = 205
55050
Ha = 226
561 n
mi
Hp = 214
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1903503
05 X = -606833
63
Y = 14963199
93 feet Y = 4554145
65 meter
Z = -16419062
28 Z = -5007414
02
XDOT = -22050
237037 XDOT = -6676
468447
YDOT = -10041
769403 feet/sec YDOT = -3135
640557 meter/sec
ZDOT = -6563
764365 ZDOT = -2033
176561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5655116
37 X = 1723679
47
Y = 13968920
63 feet Y = 4257727
01 meter
Z = -16431530
58 Z = -5008330
52
XDOT = -23102
742254 XDOT = -7041
715839
YDOT = 1436
189204 feet/sec YDOT = 437
750469 meter/sec
ZDOT = -6698
902962 ZDOT = -2041
825623
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 13073
62341435
00016717 00000-0 10270-3 0 9032
2 25544 51
6469 217
8847 0012169 12
9985 347
1479 15
52760408 20020
Satellite: ISS
Catalog Number: 25544
Epoch time: 13073
62341435 = yrday
fracday
Element set: 903
Inclination: 51
6469 deg
RA of node: 217
8847 deg
Eccentricity:
0012169
Arg of perigee: 12
9985 deg
Mean anomaly: 347
1479 deg
Mean motion: 15
52760408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 316
Coasting Arc #5 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2013/074/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1660553
98 A = 6781256
07 meter
Y = -3918930
51 meter E =
0012172
Z = 5272883
13 I = 51
43653
XDOT = 6728
080490 Wp = 30
87867
YDOT = 3639
147569 meter/sec RA = 211
96697 deg
ZDOT = 595
508208 TA = 53
48047
MA = 53
36844
Ha = 226
515 n
mi
Hp = 214
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5448011
74 X = 1678638
63
Y = -12857383
57 feet Y = -3900259
41 meter
Z = 17299485
33 Z = 5280994
34
XDOT = 22073
754888 XDOT = 6683
993899
YDOT = 11939
460527 feet/sec YDOT = 3714
138769 meter/sec
ZDOT = 1953
767087 ZDOT = 628
085107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1776857
10 X = -541586
04
Y = -13807705
97 feet Y = -4208588
78 meter
Z = 17333648
53 Z = 5283296
07
XDOT = 24069
801968 XDOT = 7336
475640
YDOT = -514
604778 feet/sec YDOT = -156
851536 meter/sec
ZDOT = 2089
006486 ZDOT = 636
729177
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 13074
65313975
00016717 00000-0 10270-3 0 9045
2 25544 51
6472 212
7616 0012254 16
8528 343
3029 15
52829181 20183
Satellite: ISS
Catalog Number: 25544
Epoch time: 13074
65313975 = yrday
fracday
Element set: 904
Inclination: 51
6472 deg
RA of node: 212
7616 deg
Eccentricity:
0012254
Arg of perigee: 16
8528 deg
Mean anomaly: 343
3029 deg
Mean motion: 15
52829181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2018
Checksum: 302
Coasting Arc #6 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2013/075/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2734222
22 A = 6781372
60 meter
Y = 3312162
49 meter E =
0021329
Z = -5263067
64 I = 51
46311
XDOT = -6454
858690 Wp = 62
18653
YDOT = -4027
362850 meter/sec RA = 206
96924 deg
ZDOT = 831
187533 TA = 215
72279
MA = 215
86568
Ha = 226
725 n
mi
Hp = 213
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8970545
35 X = -2745489
75
Y = 10866674
85 feet Y = 3281523
16 meter
Z = -17267282
28 Z = -5276377
95
XDOT = -21177
357908 XDOT = -6413
381804
YDOT = -13213
132709 feet/sec YDOT = -4099
313147 meter/sec
ZDOT = 2726
993218 ZDOT = 799
931563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2030915
82 X = -619023
14
Y = 13874520
72 feet Y = 4228953
92 meter
Z = -17323030
89 Z = -5280059
81
XDOT = -23959
115907 XDOT = -7302
738529
YDOT = -314
556346 feet/sec YDOT = -95
876774 meter/sec
ZDOT = 2597
279797 ZDOT = 791
650882
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 13075
61849724
00016717 00000-0 10270-3 0 9059
2 25544 51
6469 207
9604 0012405 20
4788 339
6859 15
52820085 20339
Satellite: ISS
Catalog Number: 25544
Epoch time: 13075
61849724 = yrday
fracday
Element set: 905
Inclination: 51
6469 deg
RA of node: 207
9604 deg
Eccentricity:
0012405
Arg of perigee: 20
4788 deg
Mean anomaly: 339
6859 deg
Mean motion: 15
52820085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2033
Checksum: 322
Coasting Arc #7 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2013/076/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3831279
88 A = 6782672
52 meter
Y = -2670459
32 meter E =
0018188
Z = 4914779
63 I = 51
49568
XDOT = 5923
066762 Wp = 35
69332
YDOT = 4320
732884 meter/sec RA = 201
97234 deg
ZDOT = -2250
903307 TA = 76
43503
MA = 76
23249
Ha = 226
703 n
mi
Hp = 213
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12569815
90 X = 3836982
13
Y = -8761349
48 feet Y = -2627583
21 meter
Z = 16124605
07 Z = 4933405
71
XDOT = 19432
633734 XDOT = 5885
245458
YDOT = 14175
632820 feet/sec YDOT = 4386
756671 meter/sec
ZDOT = -7384
853369 ZDOT = -2222
221866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5966120
54 X = 1818473
54
Y = -14023237
58 feet Y = -4274282
82 meter
Z = 16202426
31 Z = 4938499
54
XDOT = 23003
124823 XDOT = 7011
352446
YDOT = 1321
057164 feet/sec YDOT = 402
658223 meter/sec
ZDOT = -7265
875108 ZDOT = -2214
638733
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 13076
64819684
00016717 00000-0 10270-3 0 9066
2 25544 51
6469 202
8369 0012479 23
9959 336
1772 15
52862760 20499
Satellite: ISS
Catalog Number: 25544
Epoch time: 13076
64819684 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 202
8369 deg
Eccentricity:
0012479
Arg of perigee: 23
9959 deg
Mean anomaly: 336
1772 deg
Mean motion: 15
52862760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 349
Coasting Arc #8 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2013/077/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4791581
60 A = 6784975
55 meter
Y = 2122676
02 meter E =
0016130
Z = -4316629
76 I = 51
53165
XDOT = -5128
218879 Wp = 60
62955
YDOT = -4479
867349 meter/sec RA = 196
98355 deg
ZDOT = 3507
156128 TA = 245
07659
MA = 245
24430
Ha = 226
813 n
mi
Hp = 213
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15720412
06 X = -4793992
73
Y = 6964160
18 feet Y = 2069079
70 meter
Z = -14162171
12 Z = -4339912
80
XDOT = -16824
865089 XDOT = -5094
779675
YDOT = -14697
727524 feet/sec YDOT = -4537
027059 meter/sec
ZDOT = 11506
417743 ZDOT = 3482
325369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9355722
48 X = -2851624
21
Y = 14329680
68 feet Y = 4367686
67 meter
Z = -14259336
64 Z = -4346245
81
XDOT = -21121
126842 XDOT = -6437
719461
YDOT = -2499
481655 feet/sec YDOT = -761
842009 meter/sec
ZDOT = 11403
475849 ZDOT = 3475
779439
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 13077
61352910
00016717 00000-0 10270-3 0 9079
2 25544 51
6462 198
0354 0012514 28
0038 332
1785 15
52877574 20642
Satellite: ISS
Catalog Number: 25544
Epoch time: 13077
61352910 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 198
0354 deg
Eccentricity:
0012514
Arg of perigee: 28
0038 deg
Mean anomaly: 332
1785 deg
Mean motion: 15
52877574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 305
Coasting Arc #9 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2013/078/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5656629
90 A = 6787914
02 meter
Y = -1560949
35 meter E =
0021835
Z = 3406734
00 I = 51
57113
XDOT = 4059
146576 Wp = 60
30121
YDOT = 4595
311667 meter/sec RA = 192
00024 deg
ZDOT = -4601
559586 TA = 79
83892
MA = 79
59270
Ha = 226
919 n
mi
Hp = 213
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18558497
04 X = 5657115
44
Y = -5121224
91 feet Y = -1497690
36 meter
Z = 11176948
83 Z = 3434214
58
XDOT = 13317
410025 XDOT = 4029
812160
YDOT = 15076
481847 feet/sec YDOT = 4640
539201 meter/sec
ZDOT = -15096
980269 ZDOT = -4581
912345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12506567
47 X = 3812001
77
Y = -14548389
43 feet Y = -4434349
10 meter
Z = 11291548
92 Z = 3441664
11
XDOT = 18472
431795 XDOT = 5630
397211
YDOT = 4143
014097 feet/sec YDOT = 1262
790697 meter/sec
ZDOT = -15015
623564 ZDOT = -4576
762062
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 13078
64320249
00016717 00000-0 10270-3 0 9084
2 25544 51
6461 192
9117 0012667 31
1798 329
0103 15
52893269 20804
Satellite: ISS
Catalog Number: 25544
Epoch time: 13078
64320249 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 192
9117 deg
Eccentricity:
0012667
Arg of perigee: 31
1798 deg
Mean anomaly: 329
0103 deg
Mean motion: 15
52893269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2080
Checksum: 312
Coasting Arc #10 (Orbit 2094)
---------------------------------------
Vector Time (GMT): 2013/079/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6269997
84 A = 6790561
26 meter
Y = 1101708
41 meter E =
0018221
Z = -2347972
63 I = 51
60939
XDOT = -2825
495563 Wp = 38
47221
YDOT = -4656
513126 meter/sec RA = 187
02575 deg
ZDOT = 5396
719766 TA = 295
32856
MA = 295
51718
Ha = 227
004 n
mi
Hp = 213
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20570859
06 X = -6270445
64
Y = 3614528
92 feet Y = 1031590
65 meter
Z = -7703322
28 Z = -2378432
69
XDOT = -9269
998566 XDOT = -2799
431070
YDOT = -15277
274035 feet/sec YDOT = -4687
963396 meter/sec
ZDOT = 17705
773510 ZDOT = 5383
057568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14784254
41 X = -4506240
74
Y = 14685996
16 feet Y = 4476291
63 meter
Z = -7830298
50 Z = -2386674
98
XDOT = -15351
641381 XDOT = -4679
180293
YDOT = -6106
808803 feet/sec YDOT = -1861
355323 meter/sec
ZDOT = 17649
339364 ZDOT = 5379
518638
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 13079
60850937
00016717 00000-0 10270-3 0 9094
2 25544 51
6455 188
1093 0012696 34
3237 325
8733 15
52873400 20956
Satellite: ISS
Catalog Number: 25544
Epoch time: 13079
60850937 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 188
1093 deg
Eccentricity:
0012696
Arg of perigee: 34
3237 deg
Mean anomaly: 325
8733 deg
Mean motion: 15
52873400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2095
Checksum: 324
Coasting Arc #11 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2013/080/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6678316
46 A = 6792286
61 meter
Y = -609389
71 meter E =
0019619
Z = 1072651
76 I = 51
64629
XDOT = 1389
694628 Wp = 82
48502
YDOT = 4707
796996 meter/sec RA = 182
05749 deg
ZDOT = -5882
740618 TA = 85
89555
MA = 85
67134
Ha = 227
128 n
mi
Hp = 212
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21910487
08 X = 6679423
83
Y = -1999310
08 feet Y = -534702
28 meter
Z = 3519198
69 Z = 1105096
89
XDOT = 4559
365577 XDOT = 1365
524276
YDOT = 15445
528203 feet/sec YDOT = 4723
201738 meter/sec
ZDOT = -19300
330110 ZDOT = -5876
048816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16581610
01 X = 5054074
73
Y = -14427298
92 feet Y = -4397440
71 meter
Z = 3654408
25 Z = 1113863
63
XDOT = 11777
828206 XDOT = 3589
882037
YDOT = 8578
763459 feet/sec YDOT = 2614
807102 meter/sec
ZDOT = -19272
927568 ZDOT = -5874
388323
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 13080
63815655
00016717 00000-0 10270-3 0 9109
2 25544 51
6456 182
9854 0012879 38
3501 321
8564 15
52930849 21113
Satellite: ISS
Catalog Number: 25544
Epoch time: 13080
63815655 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 182
9854 deg
Eccentricity:
0012879
Arg of perigee: 38
3501 deg
Mean anomaly: 321
8564 deg
Mean motion: 15
52930849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 316
Coasting Arc #12 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2013/081/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6774649
10 A = 6792947
75 meter
Y = 182372
84 meter E =
0025436
Z = 204140
93 I = 51
67844
XDOT = 66
187974 Wp = 44
64330
YDOT = -4764
485971 meter/sec RA = 177
09378 deg
ZDOT = 6016
222365 TA = 317
55608
MA = 317
75251
Ha = 227
305 n
mi
Hp = 212
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22226539
06 X = -6777176
58
Y = 598336
07 feet Y = 106600
33 meter
Z = 669753
70 Z = 171224
44
XDOT = 217
152145 XDOT = 90
235640
YDOT = -15631
515653 feet/sec YDOT = -4763
610713 meter/sec
ZDOT = 19738
262354 ZDOT = 6016
602818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17443673
79 X = -5316831
77
Y = 13793483
49 feet Y = 4204253
77 meter
Z = 532609
04 Z = 162339
24
XDOT = -8279
075921 XDOT = -2523
462341
YDOT = -11301
789013 feet/sec YDOT = -3444
785291 meter/sec
ZDOT = 19740
322782 ZDOT = 6016
850384
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 13081
66779229
00016717 00000-0 10270-3 0 9110
2 25544 51
6455 177
8622 0013061 41
6812 318
5333 15
52884084 21277
Satellite: ISS
Catalog Number: 25544
Epoch time: 13081
66779229 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 177
8622 deg
Eccentricity:
0013061
Arg of perigee: 41
6812 deg
Mean anomaly: 318
5333 deg
Mean motion: 15
52884084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2127
Checksum: 311
Coasting Arc #13 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2013/082/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6610306
07 A = 6791745
25 meter
Y = 318801
38 meter E =
0014624
Z = -1546080
87 I = 51
70639
XDOT = -1566
864179 Wp = 80
21585
YDOT = 4802
112273 meter/sec RA = 172
13158 deg
ZDOT = -5752
993999 TA = 116
63350
MA = 116
48363
Ha = 227
286 n
mi
Hp = 212
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21687355
86 X = 6613760
25
Y = 1045936
28 feet Y = 392741
11 meter
Z = -5072443
80 Z = -1513960
54
XDOT = -5140
630509 XDOT = -1592
499725
YDOT = 15754
961527 feet/sec YDOT = 4784
446564 meter/sec
ZDOT = -18874
652229 ZDOT = -5760
668477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17806252
05 X = 5427345
63
Y = -12478468
19 feet Y = -3803437
10 meter
Z = -4938652
92 Z = -1505301
41
XDOT = 4769
977634 XDOT = 1453
889183
YDOT = 14230
787773 feet/sec YDOT = 4337
544113 meter/sec
ZDOT = -18907
103910 ZDOT = -5762
885272
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 13082
63305969
00016717 00000-0 10270-3 0 9125
2 25544 51
6461 173
0586 0013067 45
7054 314
5168 15
52964569 21426
Satellite: ISS
Catalog Number: 25544
Epoch time: 13082
63305969 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 173
0586 deg
Eccentricity:
0013067
Arg of perigee: 45
7054 deg
Mean anomaly: 314
5168 deg
Mean motion: 15
52964569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 315
Coasting Arc #14 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2013/083/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6146456
35 A = 6789683
20 meter
Y = -810673
19 meter E =
0025886
Z = 2732160
33 I = 51
72898
XDOT = 2949
374262 Wp = 64
41477
YDOT = -4853
349744 meter/sec RA = 167
16825 deg
ZDOT = 5167
902651 TA = 326
49324
MA = 326
65672
Ha = 227
480 n
mi
Hp = 212
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20165539
21 X = -6150206
42
Y = -2659688
95 feet Y = -879427
32 meter
Z = 8963780
60 Z = 2702292
61
XDOT = 9676
424743 XDOT = 2978
322146
YDOT = -15923
063464 feet/sec YDOT = -4820
205403 meter/sec
ZDOT = 16955
061190 ZDOT = 5182
301337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17431336
79 X = -5313071
45
Y = 10587046
46 feet Y = 3226931
76 meter
Z = 8839413
15 Z = 2694253
13
XDOT = -1733
673000 XDOT = -528
423530
YDOT = -17136
609299 feet/sec YDOT = -5223
238514 meter/sec
ZDOT = 17015
537153 ZDOT = 5186
335724
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 13083
66266797
00016717 00000-0 10270-3 0 9135
2 25544 51
6456 167
9353 0013224 49
5316 310
6987 15
52950542 21581
Satellite: ISS
Catalog Number: 25544
Epoch time: 13083
66266797 = yrday
fracday
Element set: 913
Inclination: 51
6456 deg
RA of node: 167
9353 deg
Eccentricity:
0013224
Arg of perigee: 49
5316 deg
Mean anomaly: 310
6987 deg
Mean motion: 15
52950542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 330
Coasting Arc #15 (Orbit 2172)
---------------------------------------
Vector Time (GMT): 2013/084/14:29:23
810
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5451247
24 A = 6786592
54 meter
Y = 1406148
92 meter E =
0018784
Z = -3812025
73 I = 51
74987
XDOT = -4183
597934 Wp = 60
82557
YDOT = 4827
692050 meter/sec RA = 162
20101 deg
ZDOT = -4208
561819 TA = 164
73243
MA = 164
67567
Ha = 227
377 n
mi
Hp = 212
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17884669
42 X = 5453635
96
Y = 4613349
48 feet Y = 1467120
98 meter
Z = -12506646
09 Z = -3785538
56
XDOT = -13725
715005 XDOT = -4216
827293
YDOT = 15838
884678 feet/sec YDOT = 4780
721990 meter/sec
ZDOT = -13807
617515 ZDOT = -4228
966732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16758939
12 X = 5108124
65
Y = -7938981
80 feet Y = -2419801
65 meter
Z = -12396415
51 Z = -3778427
45
XDOT = -938
779795 XDOT = -286
140082
YDOT = 19676
900742 feet/sec YDOT = 5997
519346 meter/sec
ZDOT = -13893
123434 ZDOT = -4234
624023
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 13084
62791216
00016717 00000-0 10270-3 0 9142
2 25544 51
6466 163
1317 0013201 53
0290 307
2069 15
52998134 21735
Satellite: ISS
Catalog Number: 25544
Epoch time: 13084
62791216 = yrday
fracday
Element set: 914
Inclination: 51
6466 deg
RA of node: 163
1317 deg
Eccentricity:
0013201
Arg of perigee: 53
0290 deg
Mean anomaly: 307
2069 deg
Mean motion: 15
52998134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2173
Checksum: 291
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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