[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 18th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 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
116/12:16:22
004 4
0 6
6 6
6
N/A -2
3 -0
1 214
2
000/00:14:44
008 -4
7 -0
1 213
1
Coasting Arc #1 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2012/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1335968
26 A = 6776402
43 meter
Y = 6528971
26 meter E =
0009949
Z = 1190519
78 I = 51
98723
XDOT = -4916
577345 Wp = 22
60985
YDOT = -70
349377 meter/sec RA = 70
40896 deg
ZDOT = 5895
732548 TA = 350
28759
MA = 350
30681
Ha = 212
875 n
mi
Hp = 211
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4383097
98 X = 1257077
41
Y = 21420509
39 feet Y = 6543469
88 meter
Z = 3905904
79 Z = 1196817
72
XDOT = -16130
503099 XDOT = -4944
065450
YDOT = -230
805044 feet/sec YDOT = -125
482815 meter/sec
ZDOT = 19342
954553 ZDOT = 5871
781245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12767394
68 X = 3891501
90
Y = 17743864
68 feet Y = 5408329
95 meter
Z = 3931254
53 Z = 1198246
38
XDOT = -13616
459994 XDOT = -4150
297006
YDOT = 5528
549104 feet/sec YDOT = 1685
101767 meter/sec
ZDOT = 19244
516673 ZDOT = 5865
728682
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 12107
56180640
00016717 00000-0 10270-3 0 9008
2 25544 51
6398 70
7960 0008059 283
9497 76
0761 15
58375620 8419
Satellite: ISS
Catalog Number: 25544
Epoch time: 12107
56180640 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 70
7960 deg
Eccentricity:
0008059
Arg of perigee: 283
9497 deg
Mean anomaly: 76
0761 deg
Mean motion: 15
58375620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 841
Checksum: 321
Coasting Arc #2 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2012/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 830215
41 A = 6770582
35 meter
Y = -5487011
95 meter E =
0004610
Z = -3880903
33 I = 51
95754
XDOT = 5269
916081 Wp = 340
70170
YDOT = 3731
062820 meter/sec RA = 65
42802 deg
ZDOT = -4142
164126 TA = 245
99118
MA = 246
03944
Ha = 213
139 n
mi
Hp = 211
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2723803
83 X = 910363
23
Y = -18002007
72 feet Y = -5477280
17 meter
Z = -12732622
48 Z = -3876675
02
XDOT = 17289
750922 XDOT = 5247
924708
YDOT = 12241
019752 feet/sec YDOT = 3789
870973 meter/sec
ZDOT = -13589
777315 ZDOT = -4116
616715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5136430
26 X = -1565583
94
Y = -17480342
05 feet Y = -5328008
26 meter
Z = -12714786
29 Z = -3875466
86
XDOT = 19656
902933 XDOT = 5991
424014
YDOT = 4046
215045 feet/sec YDOT = 1233
286346 meter/sec
ZDOT = -13485
086719 ZDOT = -4110
254432
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 12108
52371381
00016717 00000-0 10270-3 0 9010
2 25544 51
6407 65
9696 0008130 289
0457 70
9817 15
58386130 8564
Satellite: ISS
Catalog Number: 25544
Epoch time: 12108
52371381 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 65
9696 deg
Eccentricity:
0008130
Arg of perigee: 289
0457 deg
Mean anomaly: 70
9817 deg
Mean motion: 15
58386130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 318
Coasting Arc #3 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2012/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3039570
31 A = 6765166
54 meter
Y = 2987890
03 meter E =
0004827
Z = 5257495
27 I = 51
92673
XDOT = -4405
861561 Wp = 285
03138
YDOT = -6204
373071 meter/sec RA = 60
41521 deg
ZDOT = 980
771890 TA = 155
63499
MA = 155
61217
Ha = 213
343 n
mi
Hp = 210
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9972343
55 X = -3098295
56
Y = 9802788
80 feet Y = 2953571
75 meter
Z = 17249000
21 Z = 5242586
15
XDOT = -14454
926381 XDOT = -4340
919960
YDOT = -20355
554696 feet/sec YDOT = -6253
278952 meter/sec
ZDOT = 3217
755546 ZDOT = 959
526473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4712209
96 X = -1436281
60
Y = 13245989
49 feet Y = 4037377
60 meter
Z = 17187470
79 Z = 5238741
10
XDOT = -21009
199566 XDOT = -6403
604028
YDOT = -11528
151357 feet/sec YDOT = -3513
780534 meter/sec
ZDOT = 3130
964838 ZDOT = 954
318083
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 12109
54972788
00016717 00000-0 10270-3 0 9022
2 25544 51
6413 60
8222 0008259 292
3507 67
6772 15
58425777 8727
Satellite: ISS
Catalog Number: 25544
Epoch time: 12109
54972788 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 60
8222 deg
Eccentricity:
0008259
Arg of perigee: 292
3507 deg
Mean anomaly: 67
6772 deg
Mean motion: 15
58425777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 333
Coasting Arc #4 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2012/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4725994
92 A = 6766967
97 meter
Y = 165886
16 meter E =
0003632
Z = -4843479
84 I = 51
91700
XDOT = 2337
491270 Wp = 88
96342
YDOT = 6860
316597 meter/sec RA = 55
39009 deg
ZDOT = 2517
441367 TA = 205
66403
MA = 205
68207
Ha = 213
573 n
mi
Hp = 210
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15505232
68 X = 4747317
53
Y = 544245
94 feet Y = 218854
03 meter
Z = -15890681
89 Z = -4820469
10
XDOT = 7668
934614 XDOT = 2248
374771
YDOT = 22507
600383 feet/sec YDOT = 6885
957775 meter/sec
ZDOT = 8259
322070 ZDOT = 2528
579975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14125783
40 X = 4305538
78
Y = -6645814
29 feet Y = -2025644
20 meter
Z = -15796126
45 Z = -4814659
34
XDOT = 16577
056632 XDOT = 5052
686861
YDOT = 15509
441994 feet/sec YDOT = 4727
277920 meter/sec
ZDOT = 8304
505178 ZDOT = 2531
213178
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 12110
51159931
00016717 00000-0 10270-3 0 9039
2 25544 51
6415 55
9955 0008234 296
1967 63
8341 15
58431107 8872
Satellite: ISS
Catalog Number: 25544
Epoch time: 12110
51159931 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 55
9955 deg
Eccentricity:
0008234
Arg of perigee: 296
1967 deg
Mean anomaly: 63
8341 deg
Mean motion: 15
58431107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 315
Coasting Arc #5 (Orbit 902)
---------------------------------------
Vector Time (GMT): 2012/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5359782
37 A = 6773569
32 meter
Y = -3086997
05 meter E =
0006318
Z = 2758147
76 I = 51
92225
XDOT = 584
983821 Wp = 75
90780
YDOT = -5642
037448 meter/sec RA = 50
38891 deg
ZDOT = -5166
579498 TA = 72
93553
MA = 72
86633
Ha = 213
588 n
mi
Hp = 210
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17584587
84 X = -5338263
26
Y = -10127943
07 feet Y = -3146812
97 meter
Z = 9049041
22 Z = 2732162
23
XDOT = 1919
238257 XDOT = 673
129224
YDOT = -18510
621548 feet/sec YDOT = -5635
003252 meter/sec
ZDOT = -16950
720137 ZDOT = -5163
523191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20331042
84 X = -6196901
86
Y = -598414
85 feet Y = -182396
85 meter
Z = 8942522
22 Z = 2725680
77
XDOT = -7001
803788 XDOT = -2134
149795
YDOT = -15790
337156 feet/sec YDOT = -4812
894765 meter/sec
ZDOT = -16937
660210 ZDOT = -5162
598832
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
53757599
00016717 00000-0 10270-3 0 9047
2 25544 51
6425 50
8478 0008241 300
2504 59
7834 15
58471258 9030
Satellite: ISS
Catalog Number: 25544
Epoch time: 12111
53757599 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 50
8478 deg
Eccentricity:
0008241
Arg of perigee: 300
2504 deg
Mean anomaly: 59
7834 deg
Mean motion: 15
58471258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 903
Checksum: 311
Coasting Arc #6 (Orbit 918)
---------------------------------------
Vector Time (GMT): 2012/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4587797
72 A = 6776646
48 meter
Y = 4967483
34 meter E =
0013272
Z = 280205
61 I = 51
91259
XDOT = -3653
700829 Wp = 10
97827
YDOT = 3032
040685 meter/sec RA = 45
41435 deg
ZDOT = 6035
874230 TA = 352
03711
MA = 352
05816
Ha = 213
752 n
mi
Hp = 210
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15051829
80 X = 4530548
14
Y = 16297517
51 feet Y = 5018466
84 meter
Z = 919309
75 Z = 302354
05
XDOT = -11987
207445 XDOT = -3716
655604
YDOT = 9947
640044 feet/sec YDOT = 2990
830995 meter/sec
ZDOT = 19802
736974 ZDOT = 6017
971357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21080253
77 X = 6425261
35
Y = 6900349
93 feet Y = 2103226
66 meter
Z = 1009881
02 Z = 307811
74
XDOT = -5221
830834 XDOT = -1591
614038
YDOT = 13050
203186 feet/sec YDOT = 3977
701931 meter/sec
ZDOT = 19728
889593 ZDOT = 6013
365548
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
56353317
00016717 00000-0 10270-3 0 9052
2 25544 51
6425 45
6995 0008283 303
8739 56
1627 15
58489806 9197
Satellite: ISS
Catalog Number: 25544
Epoch time: 12112
56353317 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 45
6995 deg
Eccentricity:
0008283
Arg of perigee: 303
8739 deg
Mean anomaly: 56
1627 deg
Mean motion: 15
58489806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 919
Checksum: 333
Coasting Arc #7 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2012/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2452772
57 A = 6772055
70 meter
Y = -5423394
40 meter E =
0004860
Z = -3233034
29 I = 51
87674
XDOT = 5984
674677 Wp = 335
58723
YDOT = 155
912792 meter/sec RA = 40
43500 deg
ZDOT = -4794
991815 TA = 241
76560
MA = 241
81467
Ha = 213
840 n
mi
Hp = 209
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8047154
10 X = -2376239
14
Y = -17793288
71 feet Y = -5450394
97 meter
Z = -10607067
89 Z = -3244763
94
XDOT = 19634
759438 XDOT = 6005
779846
YDOT = 511
524907 feet/sec YDOT = 222
955016 meter/sec
ZDOT = -15731
600442 ZDOT = -4765
866741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15839274
44 X = -4827810
85
Y = -11378091
37 feet Y = -3468042
25 meter
Z = -10654769
99 Z = -3247573
89
XDOT = 16488
087894 XDOT = 5025
569190
YDOT = -8312
323867 feet/sec YDOT = -2533
596315 meter/sec
ZDOT = -15611
925707 ZDOT = -4758
514955
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
52534965
00016717 00000-0 10270-3 0 9060
2 25544 51
6436 40
8734 0008274 307
7057 52
3347 15
58535543 9347
Satellite: ISS
Catalog Number: 25544
Epoch time: 12113
52534965 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 40
8734 deg
Eccentricity:
0008274
Arg of perigee: 307
7057 deg
Mean anomaly: 52
3347 deg
Mean motion: 15
58535543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 934
Checksum: 311
Coasting Arc #8 (Orbit 949)
---------------------------------------
Vector Time (GMT): 2012/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -588410
45 A = 6765533
54 meter
Y = 4458166
72 meter E =
0002882
Z = 5055747
53 I = 51
83130
XDOT = -6799
266942 Wp = 320
49116
YDOT = -3024
268329 meter/sec RA = 35
42232 deg
ZDOT = 1878
232867 TA = 111
38801
MA = 111
35726
Ha = 213
945 n
mi
Hp = 209
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1930480
49 X = -662778
96
Y = 14626531
25 feet Y = 4451170
97 meter
Z = 16587098
21 Z = 5052708
34
XDOT = -22307
306241 XDOT = -6774
067812
YDOT = -9922
140188 feet/sec YDOT = -3100
161028 meter/sec
ZDOT = 6162
181322 ZDOT = 1845
262981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5823996
64 X = 1775154
18
Y = 13570972
92 feet Y = 4136432
54 meter
Z = 16574189
44 Z = 5051812
94
XDOT = -23266
326614 XDOT = -7091
576352
YDOT = 2635
091929 feet/sec YDOT = 803
176020 meter/sec
ZDOT = 6026
978276 ZDOT = 1837
022978
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
55126755
00016717 00000-0 10270-3 0 9079
2 25544 51
6435 35
7253 0008309 310
3786 49
6644 15
58578975 9506
Satellite: ISS
Catalog Number: 25544
Epoch time: 12114
55126755 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 35
7253 deg
Eccentricity:
0008309
Arg of perigee: 310
3786 deg
Mean anomaly: 49
6644 deg
Mean motion: 15
58578975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 950
Checksum: 329
Coasting Arc #9 (Orbit 964)
---------------------------------------
Vector Time (GMT): 2012/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3673853
95 A = 6765397
01 meter
Y = -2502193
80 meter E =
0007647
Z = -5105596
53 I = 51
80577
XDOT = 5673
704443 Wp = 67
72009
YDOT = 4875
785946 meter/sec RA = 30
38814 deg
ZDOT = 1697
939740 TA = 218
61016
MA = 218
66487
Ha = 214
164 n
mi
Hp = 209
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12053326
59 X = 3726363
16
Y = -8209297
26 feet Y = -2460816
87 meter
Z = -16750644
78 Z = -5087621
30
XDOT = 18614
515888 XDOT = 5610
512389
YDOT = 15996
673050 feet/sec YDOT = 4938
879479 meter/sec
ZDOT = 5570
668438 ZDOT = 1725
349319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5929520
66 X = 1807317
90
Y = -13416154
73 feet Y = -4089243
96 meter
Z = -16676538
04 Z = -5083008
79
XDOT = 23263
414698 XDOT = 7090
688800
YDOT = 3237
716371 feet/sec YDOT = 986
855950 meter/sec
ZDOT = 5682
839387 ZDOT = 1732
129445
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
51304968
00016717 00000-0 10270-3 0 9081
2 25544 51
6440 30
8986 0008335 314
7291 45
3185 15
58583511 9650
Satellite: ISS
Catalog Number: 25544
Epoch time: 12115
51304968 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 30
8986 deg
Eccentricity:
0008335
Arg of perigee: 314
7291 deg
Mean anomaly: 45
3185 deg
Mean motion: 15
58583511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 965
Checksum: 315
Coasting Arc #10 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5890724
72 A = 6771713
82 meter
Y = 113889
49 meter E =
0009186
Z = 3338162
65 I = 51
79988
XDOT = -2771
387096 Wp = 50
53277
YDOT = -5400
554242 meter/sec RA = 25
37031 deg
ZDOT = -4692
009733 TA = 90
61741
MA = 90
51216
Ha = 214
239 n
mi
Hp = 209
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19326524
69 X = -5907776
70
Y = 373653
17 feet Y = 47920
37 meter
Z = 10951977
19 Z = 3309503
97
XDOT = -9092
477348 XDOT = -2687
997996
YDOT = -17718
353813 feet/sec YDOT = -5431
079279 meter/sec
ZDOT = -15393
732719 ZDOT = -4705
270717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16040536
24 X = -4889155
45
Y = 10905107
34 feet Y = 3323876
72 meter
Z = 10834196
26 Z = 3302263
02
XDOT = -16420
363595 XDOT = -5004
926824
YDOT = -8758
677385 feet/sec YDOT = -2669
644867 meter/sec
ZDOT = -15447
704376 ZDOT = -4708
460294
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
53893107
00016717 00000-0 10270-3 0 9093
2 25544 51
6437 25
7503 0008294 318
4019 41
6504 15
58601147 9815
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53893107 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 25
7503 deg
Eccentricity:
0008294
Arg of perigee: 318
4019 deg
Mean anomaly: 41
6504 deg
Mean motion: 15
58601147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 302
Coasting Arc #11 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:23:44
008
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2193639
87 A = 6772364
87 meter
Y = -4768474
77 meter E =
0004187
Z = -4282233
85 I = 51
78978
XDOT = 6783
679157 Wp =
38125
YDOT = 95
841006 meter/sec RA = 25
33708 deg
ZDOT = -3577
699268 TA = 233
18300
MA = 233
22141
Ha = 214
187 n
mi
Hp = 213
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7196981
19 X = -2119352
37
Y = -15644602
25 feet Y = -4792589
97 meter
Z = -14049323
67 Z = -4292710
23
XDOT = 22256
165214 XDOT = 6799
483148
YDOT = 314
438995 feet/sec YDOT = 171
788721 meter/sec
ZDOT = -11737
858490 ZDOT = -3544
705631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15379762
26 X = -4687751
54
Y = -7669061
30 feet Y = -2337529
88 meter
Z = -14091913
46 Z = -4295215
22
XDOT = 16976
744932 XDOT = 5174
511855
YDOT = -12702
000482 feet/sec YDOT = -3871
569747 meter/sec
ZDOT = -11602
283737 ZDOT = -3536
376083
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
53894968
00016717 00000-0 10270-3 0 9101
2 25544 51
6445 25
7505 0007976 279
0166 81
0086 15
57269186 9812
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53894968 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 25
7505 deg
Eccentricity:
0007976
Arg of perigee: 279
0166 deg
Mean anomaly: 81
0086 deg
Mean motion: 15
57269186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 337
Coasting Arc #12 (Orbit 996)
---------------------------------------
Vector Time (GMT): 2012/117/12:23:44
008
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -724316
77 A = 6768262
57 meter
Y = 4173522
86 meter E =
0005227
Z = 5283324
09 I = 51
74798
XDOT = -7333
859123 Wp = 274
17316
YDOT = -2139
341611 meter/sec RA = 20
31890 deg
ZDOT = 685
477127 TA = 169
29783
MA = 169
28670
Ha = 214
463 n
mi
Hp = 213
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2376367
37 X = -796597
58
Y = 13692660
30 feet Y = 4165018
86 meter
Z = 17333740
44 Z = 5279629
86
XDOT = -24061
217594 XDOT = -7312
721425
YDOT = -7018
837306 feet/sec YDOT = -2221
235183 meter/sec
ZDOT = 2248
940704 ZDOT = 649
900506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6909260
02 X = 2105942
45
Y = 12080495
78 feet Y = 3682135
11 meter
Z = 17318151
56 Z = 5278572
60
XDOT = -22065
802618 XDOT = -6725
656638
YDOT = 9609
988636 feet/sec YDOT = 2929
124536 meter/sec
ZDOT = 2102
951488 ZDOT = 640
979614
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
56570691
00016717 00000-0 10270-3 0 9110
2 25544 51
6442 20
6074 0008059 282
2786 77
7466 15
57301290 9975
Satellite: ISS
Catalog Number: 25544
Epoch time: 12117
56570691 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 20
6074 deg
Eccentricity:
0008059
Arg of perigee: 282
2786 deg
Mean anomaly: 77
7466 deg
Mean motion: 15
57301290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 997
Checksum: 319
Coasting Arc #13 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2012/118/12:23:44
008
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3610763
64 A = 6770044
22 meter
Y = -3003875
61 meter E =
0003722
Z = -4879207
28 I = 51
72532
XDOT = 6291
785602 Wp = 109
54535
YDOT = 3677
399188 meter/sec RA = 15
29303 deg
ZDOT = 2392
397665 TA = 183
86302
MA = 183
86590
Ha = 214
757 n
mi
Hp = 212
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11846337
41 X = 3667787
49
Y = -9855234
93 feet Y = -2963178
91 meter
Z = -16007897
90 Z = -4861527
75
XDOT = 20642
341213 XDOT = 6238
574740
YDOT = 12064
957966 feet/sec YDOT = 3747
460274 meter/sec
ZDOT = 7849
073703 ZDOT = 2422
833908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2541019
43 X = 774502
72
Y = -15275297
60 feet Y = -4655910
71 meter
Z = -15934951
02 Z = -4856973
07
XDOT = 22342
480558 XDOT = 6809
988074
YDOT = -4600
577349 feet/sec YDOT = -1402
255976 meter/sec
ZDOT = 7973
786165 ZDOT = 2430
410023
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
52827662
00016717 00000-0 10270-3 0 9121
2 25544 51
6444 15
7858 0008123 286
3313 73
6948 15
57313666 10124
Satellite: ISS
Catalog Number: 25544
Epoch time: 12118
52827662 = yrday
fracday
Element set: 912
Inclination: 51
6444 deg
RA of node: 15
7858 deg
Eccentricity:
0008123
Arg of perigee: 286
3313 deg
Mean anomaly: 73
6948 deg
Mean motion: 15
57313666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 309
Coasting Arc #14 (Orbit 1027)
---------------------------------------
Vector Time (GMT): 2012/119/12:23:44
008
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5806202
92 A = 6775882
25 meter
Y = 1481841
84 meter E =
0005624
Z = 3160449
36 I = 51
71520
XDOT = -3807
035785 Wp = 71
89634
YDOT = -4574
006085 meter/sec RA = 10
28409 deg
ZDOT = -4840
682795 TA = 71
63921
MA = 71
57805
Ha = 214
848 n
mi
Hp = 212
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19049222
16 X = -5837694
47
Y = 4861685
83 feet Y = 1416737
19 meter
Z = 10368928
35 Z = 3132166
45
XDOT = -12490
274886 XDOT = -3732
090297
YDOT = -15006
581643 feet/sec YDOT = -4616
159646 meter/sec
ZDOT = -15881
505233 ZDOT = -4858
995287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10946449
89 X = -3336477
93
Y = 16403773
94 feet Y = 4999870
30 meter
Z = 10252558
94 Z = 3124979
96
XDOT = -18056
446116 XDOT = -5503
604776
YDOT = -2058
213116 feet/sec YDOT = -627
343358 meter/sec
ZDOT = -15956
306618 ZDOT = -4863
482257
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
55500073
00016717 00000-0 10270-3 0 9130
2 25544 51
6443 10
6429 0008065 290
4463 69
5825 15
57330396 10282
Satellite: ISS
Catalog Number: 25544
Epoch time: 12119
55500073 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 10
6429 deg
Eccentricity:
0008065
Arg of perigee: 290
4463 deg
Mean anomaly: 69
5825 deg
Mean motion: 15
57330396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1028
Checksum: 296
Coasting Arc #15 (Orbit 1042)
---------------------------------------
Vector Time (GMT): 2012/120/12:23:44
008
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6744538
20 A = 6779788
62 meter
Y = 159039
98 meter E =
0011563
Z = -587785
66 I = 51
69897
XDOT = 408
269228 Wp = 357
83702
YDOT = 4786
803652 meter/sec RA = 5
29647 deg
ZDOT = 5987
325675 TA = 355
81295
MA = 355
82261
Ha = 215
016 n
mi
Hp = 212
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22127750
00 X = 6745113
86
Y = 521784
72 feet Y = 234464
80 meter
Z = -1928430
65 Z = -555019
44
XDOT = 1339
465972 XDOT = 325
626652
YDOT = 15704
736390 feet/sec YDOT = 4790
907134 meter/sec
ZDOT = 19643
456938 ZDOT = 5989
108265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16548292
14 X = 5043919
44
Y = -14716138
20 feet Y = -4485478
92 meter
Z = -1793802
68 Z = -546751
06
XDOT = 10529
748633 XDOT = 3209
467383
YDOT = 9448
658304 feet/sec YDOT = 2879
951051 meter/sec
ZDOT = 19650
310651 ZDOT = 5989
414686
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
51753729
00016717 00000-0 10270-3 0 9147
2 25544 51
6446 5
8205 0008243 293
7481 66
2808 15
57372897 10431
Satellite: ISS
Catalog Number: 25544
Epoch time: 12120
51753729 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 5
8205 deg
Eccentricity:
0008243
Arg of perigee: 293
7481 deg
Mean anomaly: 66
2808 deg
Mean motion: 15
57372897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1043
Checksum: 312
Coasting Arc #16 (Orbit 1058)
---------------------------------------
Vector Time (GMT): 2012/121/12:23:44
008
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6185432
44 A = 6777916
26 meter
Y = -1737667
86 meter E =
0003403
Z = -2154467
29 I = 51
66213
XDOT = 3134
670563 Wp = 255
67058
YDOT = -4331
892467 meter/sec RA =
31339 deg
ZDOT = -5499
278316 TA = 308
24166
MA = 308
27228
Ha = 215
179 n
mi
Hp = 212
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20293413
53 X = -6155075
79
Y = -5701010
05 feet Y = -1806667
51 meter
Z = -7068462
25 Z = -2184442
26
XDOT = 10284
352240 XDOT = 3209
592105
YDOT = -14212
245626 feet/sec YDOT = -4296
419847 meter/sec
ZDOT = -18042
251693 ZDOT = -5483
868060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18530394
21 X = -5648064
16
Y = 9959653
17 feet Y = 3035702
29 meter
Z = -7191460
63 Z = -2191957
20
XDOT = -1664
772577 XDOT = -507
422681
YDOT = -16093
941808 feet/sec YDOT = -4905
433463 meter/sec
ZDOT = -17978
503997 ZDOT = -5479
848018
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
54422732
00016717 00000-0 10270-3 0 9159
2 25544 51
6444
6776 0008344 296
6018 63
4281 15
57356373 10597
Satellite: ISS
Catalog Number: 25544
Epoch time: 12121
54422732 = yrday
fracday
Element set: 915
Inclination: 51
6444 deg
RA of node:
6776 deg
Eccentricity:
0008344
Arg of perigee: 296
6018 deg
Mean anomaly: 63
4281 deg
Mean motion: 15
57356373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1059
Checksum: 300
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