[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 22nd 2012
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) : 131 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
116/12:16:23
874 4
5 6
7 6
8
N/A -2
8 -0
9 214
3
000/00:14:47
747 -4
2 -0
1 213
2
Coasting Arc #1 (Orbit 902)
---------------------------------------
Vector Time (GMT): 2012/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908154
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5358207
32 A = 6773509
19 meter
Y = -3101355
90 meter E =
0006314
Z = 2745082
96 I = 51
92192
XDOT = 602
500920 Wp = 75
16067
YDOT = -5632
006052 meter/sec RA = 50
39046 deg
ZDOT = -5175
443436 TA = 73
84648
MA = 73
77699
Ha = 213
591 n
mi
Hp = 210
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17579420
35 X = -5336464
30
Y = -10175052
17 feet Y = -3161152
96 meter
Z = 9006177
69 Z = 2719105
62
XDOT = 1976
709054 XDOT = 690
575908
YDOT = -18477
710144 feet/sec YDOT = -5624
776363 meter/sec
ZDOT = -16979
801298 ZDOT = -5172
302202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20348503
17 X = -6202223
77
Y = -642506
83 feet Y = -195836
08 meter
Z = 8899693
65 Z = 2712626
62
XDOT = -6938
664114 XDOT = -2114
904822
YDOT = -15787
273524 feet/sec YDOT = -4811
960970 meter/sec
ZDOT = -16966
393238 ZDOT = -5171
356659
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 12111
53754606
00016717 00000-0 10270-3 0 9009
2 25544 51
6420 50
8495 0008331 300
9160 59
1176 15
58502468 9030
Satellite: ISS
Catalog Number: 25544
Epoch time: 12111
53754606 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 50
8495 deg
Eccentricity:
0008331
Arg of perigee: 300
9160 deg
Mean anomaly: 59
1176 deg
Mean motion: 15
58502468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 903
Checksum: 283
Coasting Arc #2 (Orbit 918)
---------------------------------------
Vector Time (GMT): 2012/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908154
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4571732
27 A = 6776543
19 meter
Y = 4980486
13 meter E =
0013392
Z = 306228
42 I = 51
91214
XDOT = -3679
306246 Wp = 11
08674
YDOT = 3004
425308 meter/sec RA = 45
41579 deg
ZDOT = 6034
325321 TA = 352
20909
MA = 352
22988
Ha = 213
749 n
mi
Hp = 210
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14999121
61 X = 4514212
06
Y = 16340177
58 feet Y = 5031288
46 meter
Z = 1004686
42 Z = 328298
16
XDOT = -12071
214718 XDOT = -3741
942793
YDOT = 9857
038412 feet/sec YDOT = 2962
931062 meter/sec
ZDOT = 19797
655253 ZDOT = 6016
298831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21054563
35 X = 6417430
91
Y = 6963542
98 feet Y = 2122487
90 meter
Z = 1094933
08 Z = 333735
60
XDOT = -5334
701618 XDOT = -1626
017053
YDOT = 13013
877163 feet/sec YDOT = 3966
629759 meter/sec
ZDOT = 19723
302354 ZDOT = 6011
662558
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 12112
56348189
00016717 00000-0 10270-3 0 9019
2 25544 51
6420 45
7011 0008372 304
5200 55
5164 15
58523088 9192
Satellite: ISS
Catalog Number: 25544
Epoch time: 12112
56348189 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 45
7011 deg
Eccentricity:
0008372
Arg of perigee: 304
5200 deg
Mean anomaly: 55
5164 deg
Mean motion: 15
58523088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 919
Checksum: 285
Coasting Arc #3 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2012/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908154
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2415470
86 A = 6771871
47 meter
Y = -5422333
08 meter E =
0005066
Z = -3262634
41 I = 51
87603
XDOT = 6004
054558 Wp = 337
07395
YDOT = 199
168587 meter/sec RA = 40
43599 deg
ZDOT = -4769
036896 TA = 240
68117
MA = 240
73179
Ha = 213
833 n
mi
Hp = 209
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7924773
15 X = -2338808
27
Y = -17789806
68 feet Y = -5448915
80 meter
Z = -10704181
14 Z = -3274182
53
XDOT = 19698
341726 XDOT = 6024
548506
YDOT = 653
440246 feet/sec YDOT = 266
424112 meter/sec
ZDOT = -15646
446509 ZDOT = -4739
819160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15731192
24 X = -4794867
39
Y = -11436843
16 feet Y = -3485949
79 meter
Z = -10751137
34 Z = -3276946
66
XDOT = 16609
612437 XDOT = 5062
609871
YDOT = -8229
153137 feet/sec YDOT = -2508
245876 meter/sec
ZDOT = -15526
394972 ZDOT = -4732
445187
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 12113
52527712
00016717 00000-0 10270-3 0 9028
2 25544 51
6431 40
8748 0008362 308
3362 51
7040 15
58570999 9348
Satellite: ISS
Catalog Number: 25544
Epoch time: 12113
52527712 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 40
8748 deg
Eccentricity:
0008362
Arg of perigee: 308
3362 deg
Mean anomaly: 51
7040 deg
Mean motion: 15
58570999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 934
Checksum: 300
Coasting Arc #4 (Orbit 949)
---------------------------------------
Vector Time (GMT): 2012/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908154
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -644584
48 A = 6765359
36 meter
Y = 4432949
89 meter E =
0003105
Z = 5070899
15 I = 51
83065
XDOT = -6792
773310 Wp = 320
79947
YDOT = -3071
438253 meter/sec RA = 35
42250 deg
ZDOT = 1824
530230 TA = 111
61655
MA = 111
58347
Ha = 213
935 n
mi
Hp = 209
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2114778
48 X = -718740
44
Y = 14543798
86 feet Y = 4425327
16 meter
Z = 16636808
23 Z = 5067587
57
XDOT = -22286
001672 XDOT = -6766
786318
YDOT = -10076
897157 feet/sec YDOT = -3147
253931 meter/sec
ZDOT = 5985
991569 ZDOT = 1791
593804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5623213
87 X = 1713955
59
Y = 13595599
61 feet Y = 4143938
76 meter
Z = 16622782
51 Z = 5066624
11
XDOT = -23325
396038 XDOT = -7109
580712
YDOT = 2505
688023 feet/sec YDOT = 763
733709 meter/sec
ZDOT = 5850
930463 ZDOT = 1783
363605
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 12114
55117101
00016717 00000-0 10270-3 0 9030
2 25544 51
6430 35
7265 0008398 310
9860 49
0568 15
58616920 9503
Satellite: ISS
Catalog Number: 25544
Epoch time: 12114
55117101 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 35
7265 deg
Eccentricity:
0008398
Arg of perigee: 310
9860 deg
Mean anomaly: 49
0568 deg
Mean motion: 15
58616920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 950
Checksum: 297
Coasting Arc #5 (Orbit 964)
---------------------------------------
Vector Time (GMT): 2012/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908154
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3732245
88 A = 6765362
00 meter
Y = -2451536
25 meter E =
0007530
Z = -5087555
00 I = 51
80559
XDOT = 5624
573394 Wp = 66
98291
YDOT = 4908
794718 meter/sec RA = 30
38787 deg
ZDOT = 1765
752366 TA = 220
01939
MA = 220
07490
Ha = 214
151 n
mi
Hp = 209
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12244901
19 X = 3784096
65
Y = -8043097
95 feet Y = -2409510
02 meter
Z = -16691453
41 Z = -5069297
70
XDOT = 18453
324785 XDOT = 5560
686458
YDOT = 16104
969546 feet/sec YDOT = 4971
334952 meter/sec
ZDOT = 5793
150807 ZDOT = 1792
921577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6179832
24 X = 1883612
87
Y = -13377050
18 feet Y = -4077324
89 meter
Z = -16616192
36 Z = -5064615
43
XDOT = 23186
186611 XDOT = 7067
149679
YDOT = 3397
614701 feet/sec YDOT = 1035
592961 meter/sec
ZDOT = 5904
330831 ZDOT = 1799
640037
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 12115
51292943
00016717 00000-0 10270-3 0 9046
2 25544 51
6435 30
8995 0008422 315
3222 44
7254 15
58622770 9653
Satellite: ISS
Catalog Number: 25544
Epoch time: 12115
51292943 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 30
8995 deg
Eccentricity:
0008422
Arg of perigee: 315
3222 deg
Mean anomaly: 44
7254 deg
Mean motion: 15
58622770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 965
Checksum: 303
Coasting Arc #6 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908154
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5925044
88 A = 6771760
93 meter
Y = 45706
95 meter E =
0009200
Z = 3278581
91 I = 51
80001
XDOT = -2675
719796 Wp = 51
50989
YDOT = -5401
905181 meter/sec RA = 25
37035 deg
ZDOT = -4745
667414 TA = 90
45957
MA = 90
35415
Ha = 214
219 n
mi
Hp = 209
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19439123
63 X = -5941042
44
Y = 149957
20 feet Y = -20640
06 meter
Z = 10756502
32 Z = 3249759
06
XDOT = -8778
608253 XDOT = -2592
062039
YDOT = -17722
786026 feet/sec YDOT = -5431
358904 meter/sec
ZDOT = -15569
774979 ZDOT = -4758
462992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16256040
64 X = -4954841
19
Y = 10778558
34 feet Y = 3285304
58 meter
Z = 10638053
37 Z = 3242478
67
XDOT = -16168
203812 XDOT = -4928
068522
YDOT = -8918
688454 feet/sec YDOT = -2718
416241 meter/sec
ZDOT = -15621
833966 ZDOT = -4761
534993
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 12116
53878418
00016717 00000-0 10270-3 0 9057
2 25544 51
6432 25
7510 0008379 318
9678 41
0846 15
58642437 9818
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53878418 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 25
7510 deg
Eccentricity:
0008379
Arg of perigee: 318
9678 deg
Mean anomaly: 41
0846 deg
Mean motion: 15
58642437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 329
Coasting Arc #7 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:23:47
747
Vector Time (MET): N/A
Weight (LBS) : 907501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2082142
97 A = 6772091
72 meter
Y = -4766155
01 meter E =
0004415
Z = -4339880
05 I = 51
78688
XDOT = 6828
653805 Wp = 2
55628
YDOT = 195
683876 meter/sec RA = 25
33535 deg
ZDOT = -3486
915338 TA = 232
07087
MA = 232
11079
Ha = 214
251 n
mi
Hp = 213
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6831177
72 X = -2007609
67
Y = -15636991
50 feet Y = -4789022
01 meter
Z = -14238451
61 Z = -4349814
18
XDOT = 22403
719832 XDOT = 6842
896976
YDOT = 642
007466 feet/sec YDOT = 272
125797 meter/sec
ZDOT = -11440
010952 ZDOT = -3453
707003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15092170
64 X = -4600093
61
Y = -7890239
07 feet Y = -2404944
87 meter
Z = -14278813
31 Z = -4352182
30
XDOT = 17276
461327 XDOT = 5265
865412
YDOT = -12565
273698 feet/sec YDOT = -3829
895423 meter/sec
ZDOT = -11303
563595 ZDOT = -3445
326184
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 12116
53880259
00016717 00000-0 10270-3 0 9064
2 25544 51
6422 25
7501 0008105 279
5284 80
4954 15
57291066 9813
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53880259 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 25
7501 deg
Eccentricity:
0008105
Arg of perigee: 279
5284 deg
Mean anomaly: 80
4954 deg
Mean motion: 15
57291066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 311
Coasting Arc #8 (Orbit 996)
---------------------------------------
Vector Time (GMT): 2012/117/12:23:47
747
Vector Time (MET): N/A
Weight (LBS) : 907501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -853638
85 A = 6768146
29 meter
Y = 4135133
05 meter E =
0005472
Z = 5294211
37 I = 51
74562
XDOT = -7316
041612 Wp = 277
43333
YDOT = -2233
012526 meter/sec RA = 20
31607 deg
ZDOT = 565
684646 TA = 167
18453
MA = 167
17061
Ha = 214
500 n
mi
Hp = 213
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2800652
40 X = -925533
65
Y = 13566709
47 feet Y = 4125185
05 meter
Z = 17369459
88 Z = 5289889
83
XDOT = -24002
761193 XDOT = -7293
275860
YDOT = -7326
156580 feet/sec YDOT = -2314
697747 meter/sec
ZDOT = 1855
920755 ZDOT = 530
198536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6506582
51 X = 1983206
35
Y = 12255377
45 feet Y = 3735439
05 meter
Z = 17351296
88 Z = 5288675
29
XDOT = -22201
499536 XDOT = -6767
017059
YDOT = 9371
203831 feet/sec YDOT = 2856
342928 meter/sec
ZDOT = 1710
312642 ZDOT = 521
303293
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 12117
56554504
00016717 00000-0 10270-3 0 9070
2 25544 51
6419 20
6067 0008198 282
7734 77
2504 15
57325788 9979
Satellite: ISS
Catalog Number: 25544
Epoch time: 12117
56554504 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 20
6067 deg
Eccentricity:
0008198
Arg of perigee: 282
7734 deg
Mean anomaly: 77
2504 deg
Mean motion: 15
57325788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 997
Checksum: 333
Coasting Arc #9 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2012/118/12:23:47
747
Vector Time (MET): N/A
Weight (LBS) : 907501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3729121
74 A = 6770168
63 meter
Y = -2933641
68 meter E =
0003284
Z = -4832455
41 I = 51
72376
XDOT = 6202
842861 Wp = 110
95446
YDOT = 3749
527792 meter/sec RA = 15
29005 deg
ZDOT = 2510
624723 TA = 183
68547
MA = 183
68789
Ha = 214
779 n
mi
Hp = 212
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12234651
39 X = 3785124
32
Y = -9624808
66 feet Y = -2891627
14 meter
Z = -15854512
49 Z = -4814203
37
XDOT = 20350
534320 XDOT = 6148
257728
YDOT = 12301
600366 feet/sec YDOT = 3818
586579 meter/sec
ZDOT = 8236
957753 ZDOT = 2540
625546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2980331
71 X = 908405
10
Y = -15356531
02 feet Y = -4680670
66 meter
Z = -15779219
89 Z = -4809506
22
XDOT = 22268
874749 XDOT = 6787
553024
YDOT = -4267
360077 feet/sec YDOT = -1300
691352 meter/sec
ZDOT = 8359
873821 ZDOT = 2548
089541
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 12118
52809991
00016717 00000-0 10270-3 0 9081
2 25544 51
6422 15
7847 0008259 286
8064 73
2184 15
57337811 10122
Satellite: ISS
Catalog Number: 25544
Epoch time: 12118
52809991 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 15
7847 deg
Eccentricity:
0008259
Arg of perigee: 286
8064 deg
Mean anomaly: 73
2184 deg
Mean motion: 15
57337811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 317
Coasting Arc #10 (Orbit 1027)
---------------------------------------
Vector Time (GMT): 2012/119/12:23:47
747
Vector Time (MET): N/A
Weight (LBS) : 907501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5882315
98 A = 6776074
27 meter
Y = 1388419
28 meter E =
0005563
Z = 3060780
06 I = 51
71387
XDOT = -3654
239746 Wp = 74
81618
YDOT = -4611
587851 meter/sec RA = 10
28179 deg
ZDOT = -4922
080688 TA = 70
04338
MA = 69
98347
Ha = 214
862 n
mi
Hp = 212
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19298936
94 X = -5912273
04
Y = 4555181
35 feet Y = 1322472
07 meter
Z = 10041929
34 Z = 3032131
12
XDOT = -11988
975543 XDOT = -3578
489951
YDOT = -15129
881401 feet/sec YDOT = -4652
028255 meter/sec
ZDOT = -16148
558687 ZDOT = -4939
648946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11331202
17 X = -3453750
42
Y = 16344900
75 feet Y = 4981925
75 meter
Z = 9924065
00 Z = 3024855
01
XDOT = -17770
487707 XDOT = -5416
444653
YDOT = -2453
196436 feet/sec YDOT = -747
734274 meter/sec
ZDOT = -16220
298078 ZDOT = -4943
946854
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 12119
55480701
00016717 00000-0 10270-3 0 9090
2 25544 51
6421 10
6415 0008193 290
8489 69
1788 15
57354527 10283
Satellite: ISS
Catalog Number: 25544
Epoch time: 12119
55480701 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 10
6415 deg
Eccentricity:
0008193
Arg of perigee: 290
8489 deg
Mean anomaly: 69
1788 deg
Mean motion: 15
57354527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1028
Checksum: 317
Coasting Arc #11 (Orbit 1042)
---------------------------------------
Vector Time (GMT): 2012/120/12:23:47
747
Vector Time (MET): N/A
Weight (LBS) : 907501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6751257
98 A = 6779760
57 meter
Y = 263821
26 meter E =
0011783
Z = -456152
13 I = 51
69695
XDOT = 218
065609 Wp = 359
05646
YDOT = 4781
146338 meter/sec RA = 5
29458 deg
ZDOT = 6002
015702 TA = 356
01934
MA = 356
02871
Ha = 215
017 n
mi
Hp = 212
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22149796
51 X = 6750022
00
Y = 865555
31 feet Y = 339311
09 meter
Z = -1496562
12 Z = -423357
67
XDOT = 715
438350 XDOT = 135
429069
YDOT = 15686
175649 feet/sec YDOT = 4783
122880 meter/sec
ZDOT = 19691
652564 ZDOT = 6002
874302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16792998
01 X = 5118505
79
Y = -14482507
06 feet Y = -4414268
15 meter
Z = -1361828
41 Z = -415085
30
XDOT = 10080
526501 XDOT = 3072
544477
YDOT = 9839
951064 feet/sec YDOT = 2999
217084 meter/sec
ZDOT = 19694
709959 ZDOT = 6002
947595
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 12120
51732641
00016717 00000-0 10270-3 0 9103
2 25544 51
6424 5
8187 0008380 294
1781 65
8497 15
57401271 10434
Satellite: ISS
Catalog Number: 25544
Epoch time: 12120
51732641 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 5
8187 deg
Eccentricity:
0008380
Arg of perigee: 294
1781 deg
Mean anomaly: 65
8497 deg
Mean motion: 15
57401271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1043
Checksum: 291
Coasting Arc #12 (Orbit 1058)
---------------------------------------
Vector Time (GMT): 2012/121/12:23:47
747
Vector Time (MET): N/A
Weight (LBS) : 907501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6109472
71 A = 6777580
72 meter
Y = -1838868
94 meter E =
0003487
Z = -2283078
17 I = 51
65909
XDOT = 3320
133845 Wp = 265
37193
YDOT = -4278
228365 meter/sec RA =
31067 deg
ZDOT = -5431
913025 TA = 300
06755
MA = 300
10213
Ha = 215
182 n
mi
Hp = 212
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20044201
81 X = -6077365
29
Y = -6033034
59 feet Y = -1907009
37 meter
Z = -7490413
94 Z = -2312679
87
XDOT = 10892
827577 XDOT = 3394
114273
YDOT = -14036
182299 feet/sec YDOT = -4240
687040 meter/sec
ZDOT = -17821
236959 ZDOT = -5415
604078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18577208
04 X = -5662333
01
Y = 9550949
25 feet Y = 2911129
33 meter
Z = -7611868
59 Z = -2320097
55
XDOT = -1140
279831 XDOT = -347
557292
YDOT = -16384
930615 feet/sec YDOT = -4994
126851 meter/sec
ZDOT = -17753
801766 ZDOT = -5411
358778
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 12121
54399702
00016717 00000-0 10270-3 0 9115
2 25544 51
6422
6754 0008487 297
0669 62
9619 15
57387315 10593
Satellite: ISS
Catalog Number: 25544
Epoch time: 12121
54399702 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node:
6754 deg
Eccentricity:
0008487
Arg of perigee: 297
0669 deg
Mean anomaly: 62
9619 deg
Mean motion: 15
57387315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1059
Checksum: 322
Coasting Arc #13 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2012/122/12:23:47
747
Vector Time (MET): N/A
Weight (LBS) : 907501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4063253
68 A = 6771458
47 meter
Y = 3161456
22 meter E =
0002048
Z = 4396492
44 I = 51
60832
XDOT = -6118
200748 Wp = 49
68781
YDOT = 3180
237729 meter/sec RA = 355
30280 deg
ZDOT = 3367
861963 TA = 6
26180
MA = 6
25924
Ha = 215
329 n
mi
Hp = 211
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13330884
77 X = 4006242
28
Y = 10372231
70 feet Y = 3206575
41 meter
Z = 14424187
81 Z = 4416093
14
XDOT = -20072
837100 XDOT = -6169
668552
YDOT = 10433
850817 feet/sec YDOT = 3111
532560 meter/sec
ZDOT = 11049
415888 ZDOT = 3338
014634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16699617
32 X = 5090043
36
Y = -2024259
34 feet Y = -616994
25 meter
Z = 14504414
11 Z = 4420945
42
XDOT = -7016
674674 XDOT = -2138
682441
YDOT = 20399
412729 feet/sec YDOT = 6217
741000 meter/sec
ZDOT = 10926
465010 ZDOT = 3330
386535
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 12122
57064970
00016717 00000-0 10270-3 0 9126
2 25544 51
6421 355
5309 0008463 302
6491 57
3847 15
57417220 10758
Satellite: ISS
Catalog Number: 25544
Epoch time: 12122
57064970 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 355
5309 deg
Eccentricity:
0008463
Arg of perigee: 302
6491 deg
Mean anomaly: 57
3847 deg
Mean motion: 15
57417220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 298
Coasting Arc #14 (Orbit 1089)
---------------------------------------
Vector Time (GMT): 2012/123/12:23:47
747
Vector Time (MET): N/A
Weight (LBS) : 907501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1124780
30 A = 6767624
61 meter
Y = -4070699
79 meter E =
0009663
Z = -5295236
17 I = 51
56483
XDOT = 7493
992516 Wp = 53
76536
YDOT = -1582
965524 meter/sec RA = 350
26853 deg
ZDOT = -369
804280 TA = 212
67504
MA = 212
73485
Ha = 215
425 n
mi
Hp = 211
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3690224
08 X = -1053453
91
Y = -13355314
28 feet Y = -4082879
17 meter
Z = -17372822
09 Z = -5300526
97
XDOT = 24586
589620 XDOT = 7512
933033
YDOT = -5193
456443 feet/sec YDOT = -1499
057173 meter/sec
ZDOT = -1213
268635 ZDOT = -333
352256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12094038
20 X = -3686262
84
Y = -6706306
53 feet Y = -2044082
23 meter
Z = -17394160
33 Z = -5301740
07
XDOT = 12870
860889 XDOT = 3923
038399
YDOT = -20409
565251 feet/sec YDOT = -6220
835489 meter/sec
ZDOT = -1063
345418 ZDOT = -324
107683
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 12123
53311792
00016717 00000-0 10270-3 0 9131
2 25544 51
6412 350
7081 0008601 305
5654 54
4699 15
57487328 10905
Satellite: ISS
Catalog Number: 25544
Epoch time: 12123
53311792 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 350
7081 deg
Eccentricity:
0008601
Arg of perigee: 305
5654 deg
Mean anomaly: 54
4699 deg
Mean motion: 15
57487328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1090
Checksum: 300
Coasting Arc #15 (Orbit 1105)
---------------------------------------
Vector Time (GMT): 2012/124/12:23:47
747
Vector Time (MET): N/A
Weight (LBS) : 907501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2043176
15 A = 6770066
67 meter
Y = 4411536
64 meter E =
0009040
Z = 4715297
63 I = 51
54370
XDOT = -7152
484734 Wp = 1
10360
YDOT = -368
867346 meter/sec RA = 345
22942 deg
ZDOT = -2745
180316 TA = 116
13981
MA = 116
04679
Ha = 215
611 n
mi
Hp = 211
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6703333
82 X = -2115261
26
Y = 14473545
39 feet Y = 4388285
67 meter
Z = 15470136
58 Z = 4705196
56
XDOT = -23466
157264 XDOT = -7134
492682
YDOT = -1210
194705 feet/sec YDOT = -448
750344 meter/sec
ZDOT = -9006
497099 ZDOT = -2779
883676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5938292
53 X = 1809991
56
Y = 14847577
59 feet Y = 4525541
65 meter
Z = 15428203
00 Z = 4702516
28
XDOT = -15782
032371 XDOT = -4810
363467
YDOT = 15849
416378 feet/sec YDOT = 4830
902112 meter/sec
ZDOT = -9149
035503 ZDOT = -2788
626021
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 12124
55973387
00016717 00000-0 10270-3 0 9149
2 25544 51
6415 345
5643 0008737 308
8512 51
1862 15
57524098 11063
Satellite: ISS
Catalog Number: 25544
Epoch time: 12124
55973387 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 345
5643 deg
Eccentricity:
0008737
Arg of perigee: 308
8512 deg
Mean anomaly: 51
1862 deg
Mean motion: 15
57524098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1106
Checksum: 316
Coasting Arc #16 (Orbit 1120)
---------------------------------------
Vector Time (GMT): 2012/125/12:23:47
747
Vector Time (MET): N/A
Weight (LBS) : 907501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4638384
29 A = 6776173
06 meter
Y = -4048147
43 meter E =
0008586
Z = -2817533
38 I = 51
53338
XDOT = 5207
070460 Wp = 343
47598
YDOT = 2425
417057 meter/sec RA = 340
20860 deg
ZDOT = 5091
660828 TA = 344
41756
MA = 344
44397
Ha = 215
804 n
mi
Hp = 211
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15217796
23 X = 4696994
01
Y = -13281323
59 feet Y = -3995950
48 meter
Z = -9243875
90 Z = -2794857
40
XDOT = 17083
564501 XDOT = 5154
827258
YDOT = 7957
405044 feet/sec YDOT = 2483
353693 meter/sec
ZDOT = 16704
923976 ZDOT = 5116
830175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 371074
41 X = 113103
48
Y = -20237542
04 feet Y = -6168402
81 meter
Z = -9150317
82 Z = -2789016
87
XDOT = 15809
083322 XDOT = 4818
608597
YDOT = -7303
458616 feet/sec YDOT = -2226
094186 meter/sec
ZDOT = 16808
083820 ZDOT = 5123
103948
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 12125
52217143
00016717 00000-0 10270-3 0 9159
2 25544 51
6400 340
7407 0008734 312
2250 47
8163 15
57519552 11219
Satellite: ISS
Catalog Number: 25544
Epoch time: 12125
52217143 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 340
7407 deg
Eccentricity:
0008734
Arg of perigee: 312
2250 deg
Mean anomaly: 47
8163 deg
Mean motion: 15
57519552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1121
Checksum: 272
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list