[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 10th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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
There are no maneuvers
Coasting Arc #1 (Orbit 730)
---------------------------------------
Vector Time (GMT): 2012/100/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1029610
52 A = 6773098
49 meter
Y = -5841561
21 meter E =
0005625
Z = 3262676
40 I = 51
97952
XDOT = 4856
618647 Wp = 115
01418
YDOT = -3529
183771 meter/sec RA = 105
47546 deg
ZDOT = -4782
004466 TA = 27
26773
MA = 27
23821
Ha = 213
132 n
mi
Hp = 211
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3377987
28 X = -980062
04
Y = -19165227
06 feet Y = -5852797
80 meter
Z = 10704318
91 Z = 3257795
09
XDOT = 15933
788213 XDOT = 4918
951947
YDOT = -11578
686914 feet/sec YDOT = -3474
525701 meter/sec
ZDOT = -15688
991029 ZDOT = -4758
259386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5411428
17 X = -1649403
30
Y = -18704361
69 feet Y = -5701089
44 meter
Z = 10684683
85 Z = 3256691
64
XDOT = 13377
973083 XDOT = 4077
606196
YDOT = -12784
438466 feet/sec YDOT = -3896
696844 meter/sec
ZDOT = -15591
172991 ZDOT = -4752
189528
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 12100
50728225
00016717 00000-0 10270-3 0 9002
2 25544 51
6397 106
1792 0007832 256
8916 103
1365 15
58165399 7318
Satellite: ISS
Catalog Number: 25544
Epoch time: 12100
50728225 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 106
1792 deg
Eccentricity:
0007832
Arg of perigee: 256
8916 deg
Mean anomaly: 103
1365 deg
Mean motion: 15
58165399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 731
Checksum: 304
Coasting Arc #2 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2012/101/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -896759
22 A = 6777411
69 meter
Y = 6699036
82 meter E =
0006886
Z = -434583
22 I = 52
00236
XDOT = -4743
781571 Wp = 357
79175
YDOT = -244
230376 meter/sec RA = 100
50378 deg
ZDOT = 6027
517592 TA = 357
53772
MA = 357
54111
Ha = 212
826 n
mi
Hp = 211
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2942123
42 X = -969491
43
Y = 21978467
26 feet Y = 6688602
03 meter
Z = -1425797
98 Z = -439116
46
XDOT = -15563
587832 XDOT = -4769
978560
YDOT = -801
280762 feet/sec YDOT = -297
424650 meter/sec
ZDOT = 19775
320185 ZDOT = 6004
408673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -257529
65 X = -78495
04
Y = 22171781
35 feet Y = 6757958
96 meter
Z = -1444923
29 Z = -440412
62
XDOT = -14048
568889 XDOT = -4282
003797
YDOT = 1118
637195 feet/sec YDOT = 340
960617 meter/sec
ZDOT = 19680
380888 ZDOT = 5998
580095
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 12101
46931737
00016717 00000-0 10270-3 0 9013
2 25544 51
6406 101
3542 0007888 259
3633 100
6634 15
58208027 7467
Satellite: ISS
Catalog Number: 25544
Epoch time: 12101
46931737 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 101
3542 deg
Eccentricity:
0007888
Arg of perigee: 259
3633 deg
Mean anomaly: 100
6634 deg
Mean motion: 15
58208027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 746
Checksum: 294
Coasting Arc #3 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2012/102/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2553731
71 A = 6774847
45 meter
Y = -5731306
03 meter E =
0005647
Z = -2545355
18 I = 51
99720
XDOT = 3779
893243 Wp = 222
38726
YDOT = 4045
725260 meter/sec RA = 95
53663 deg
ZDOT = -5314
548503 TA = 346
10620
MA = 346
12173
Ha = 212
573 n
mi
Hp = 211
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8378384
86 X = 2629995
35
Y = -18803497
47 feet Y = -5702322
24 meter
Z = -8350902
81 Z = -2532763
90
XDOT = 12401
224551 XDOT = 3760
189193
YDOT = 13273
376838 feet/sec YDOT = 4087
884133 meter/sec
ZDOT = -17436
182754 ZDOT = -5296
233770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5756789
68 X = 1754669
50
Y = -19786282
97 feet Y = -6030859
05 meter
Z = -8298723
20 Z = -2529450
83
XDOT = 12774
140051 XDOT = 3893
557887
YDOT = 11002
059553 feet/sec YDOT = 3353
427752 meter/sec
ZDOT = -17361
227063 ZDOT = -5291
702009
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 12102
49547137
00016717 00000-0 10270-3 0 9025
2 25544 51
6398 96
2066 0007874 264
1156 95
9102 15
58180893 7623
Satellite: ISS
Catalog Number: 25544
Epoch time: 12102
49547137 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 96
2066 deg
Eccentricity:
0007874
Arg of perigee: 264
1156 deg
Mean anomaly: 95
9102 deg
Mean motion: 15
58180893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 322
Coasting Arc #4 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2012/103/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3702665
68 A = 6768174
11 meter
Y = 3172246
72 meter E =
0003798
Z = 4696481
62 I = 51
97666
XDOT = -2173
517610 Wp = 190
19242
YDOT = -6778
736709 meter/sec RA = 90
54409 deg
ZDOT = 2861
837734 TA = 231
52877
MA = 231
56285
Ha = 211
819 n
mi
Hp = 211
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12147853
28 X = -3760677
66
Y = 10407633
58 feet Y = 3130516
94 meter
Z = 15408404
25 Z = 4678353
25
XDOT = -7130
963287 XDOT = -2111
457036
YDOT = -22239
949833 feet/sec YDOT = -6802
695278 meter/sec
ZDOT = 9389
231412 ZDOT = 2851
429733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10481934
54 X = -3194893
65
Y = 12178512
65 feet Y = 3712010
66 meter
Z = 15333655
00 Z = 4673698
04
XDOT = -9656
869078 XDOT = -2943
413695
YDOT = -20093
780735 feet/sec YDOT = -6124
584368 meter/sec
ZDOT = 9346
983065 ZDOT = 2848
960438
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 12103
52160770
00016717 00000-0 10270-3 0 9035
2 25544 51
6394 91
0591 0007907 268
9419 91
0830 15
58213075 7787
Satellite: ISS
Catalog Number: 25544
Epoch time: 12103
52160770 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 91
0591 deg
Eccentricity:
0007907
Arg of perigee: 268
9419 deg
Mean anomaly: 91
0830 deg
Mean motion: 15
58213075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 306
Coasting Arc #5 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2012/104/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4188898
41 A = 6765535
78 meter
Y = 273057
59 meter E =
0006865
Z = -5311676
14 I = 51
96720
XDOT = 179
201789 Wp = 96
09641
YDOT = 7649
690686 meter/sec RA = 85
52615 deg
ZDOT = 534
450640 TA = 178
97935
MA = 178
97795
Ha = 212
021 n
mi
Hp = 211
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13743105
02 X = 4211336
58
Y = 895858
24 feet Y = 320025
74 meter
Z = -17426759
00 Z = -5291272
21
XDOT = 587
932378 XDOT = 91
051843
YDOT = 25097
410387 feet/sec YDOT = 7651
201774 meter/sec
ZDOT = 1753
446982 ZDOT = 535
106841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13796620
10 X = 4205209
81
Y = -1497932
52 feet Y = -456569
83 meter
Z = -17342920
72 Z = -5286122
23
XDOT = 4771
658738 XDOT = 1454
401583
YDOT = 23619
028276 feet/sec YDOT = 7199
079818 meter/sec
ZDOT = 1755
541211 ZDOT = 535
088961
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 12104
48359420
00016717 00000-0 10270-3 0 9044
2 25544 51
6394 86
2338 0007909 272
4790 87
5459 15
58227782 7930
Satellite: ISS
Catalog Number: 25544
Epoch time: 12104
48359420 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 86
2338 deg
Eccentricity:
0007909
Arg of perigee: 272
4790 deg
Mean anomaly: 87
5459 deg
Mean motion: 15
58227782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 338
Coasting Arc #6 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2012/105/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3912505
69 A = 6769951
89 meter
Y = -3623013
58 meter E =
0004098
Z = 4171729
72 I = 51
97862
XDOT = 1913
382745 Wp = 30
85555
YDOT = -6406
360286 meter/sec RA = 80
51279 deg
ZDOT = -3764
172414 TA = 97
68473
MA = 97
63819
Ha = 212
352 n
mi
Hp = 211
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12836304
77 X = -3891966
91
Y = -11886527
51 feet Y = -3666650
60 meter
Z = 13686777
30 Z = 4152773
06
XDOT = 6277
502445 XDOT = 2003
163210
YDOT = -21018
242407 feet/sec YDOT = -6384
461851 meter/sec
ZDOT = -12349
647027 ZDOT = -3754
658923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14930400
22 X = -4550785
99
Y = -9233756
06 feet Y = -2814448
85 meter
Z = 13609152
35 Z = 4148069
64
XDOT = 1597
891033 XDOT = 487
037187
YDOT = -20751
402860 feet/sec YDOT = -6325
027592 meter/sec
ZDOT = -12310
033845 ZDOT = -3752
098316
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 12105
50969550
00016717 00000-0 10270-3 0 9050
2 25544 51
6389 81
0860 0008006 276
9483 83
0761 15
58281392 8096
Satellite: ISS
Catalog Number: 25544
Epoch time: 12105
50969550 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 81
0860 deg
Eccentricity:
0008006
Arg of perigee: 276
9483 deg
Mean anomaly: 83
0761 deg
Mean motion: 15
58281392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 320
Coasting Arc #7 (Orbit 823)
---------------------------------------
Vector Time (GMT): 2012/106/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2853960
12 A = 6776076
47 meter
Y = 5915253
67 meter E =
0008159
Z = -1644714
29 I = 51
99313
XDOT = -3762
190299 Wp = 339
44755
YDOT = 3415
226420 meter/sec RA = 75
52950 deg
ZDOT = 5753
504451 TA = 2
59558
MA = 2
59135
Ha = 212
712 n
mi
Hp = 211
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9363386
21 X = 2795592
08
Y = 19407000
22 feet Y = 5946841
95 meter
Z = -5396044
24 Z = -1630992
06
XDOT = -12343
144025 XDOT = -3828
049624
YDOT = 11204
811089 feet/sec YDOT = 3372
787422 meter/sec
ZDOT = 18876
326940 ZDOT = 5735
067733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13185356
05 X = 4018896
52
Y = 17060229
67 feet Y = 5199958
00 meter
Z = -5340121
89 Z = -1627669
15
XDOT = -8643
538448 XDOT = -2634
550519
YDOT = 12566
333143 feet/sec YDOT = 3830
218342 meter/sec
ZDOT = 18800
272405 ZDOT = 5730
323029
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 12106
47164987
00016717 00000-0 10270-3 0 9069
2 25544 51
6387 76
2602 0007813 280
3028 79
7254 15
58308125 8243
Satellite: ISS
Catalog Number: 25544
Epoch time: 12106
47164987 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 76
2602 deg
Eccentricity:
0007813
Arg of perigee: 280
3028 deg
Mean anomaly: 79
7254 deg
Mean motion: 15
58308125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 824
Checksum: 316
Coasting Arc #8 (Orbit 839)
---------------------------------------
Vector Time (GMT): 2012/107/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1106651
32 A = 6776241
82 meter
Y = -6524186
95 meter E =
0005293
Z = -1442354
22 I = 51
98586
XDOT = 4980
984204 Wp = 208
55129
YDOT = 442
824363 meter/sec RA = 70
56309 deg
ZDOT = -5820
455417 TA = 347
13130
MA = 347
14480
Ha = 212
954 n
mi
Hp = 211
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3630745
82 X = -1026607
65
Y = -21404812
83 feet Y = -6536114
77 meter
Z = -4732133
27 Z = -1447535
35
XDOT = 16341
811692 XDOT = 5003
936748
YDOT = 1452
835838 feet/sec YDOT = 498
652687 meter/sec
ZDOT = -19095
982340 ZDOT = -5796
202277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8272312
46 X = -2521400
84
Y = -20067891
36 feet Y = -6116693
29 meter
Z = -4752893
39 Z = -1448681
91
XDOT = 14904
943098 XDOT = 4543
026656
YDOT = -1641
671436 feet/sec YDOT = -500
381454 meter/sec
ZDOT = -18996
334373 ZDOT = -5790
082717
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
49771623
00016717 00000-0 10270-3 0 9074
2 25544 51
6392 71
1117 0007959 285
1240 74
9034 15
58332062 8402
Satellite: ISS
Catalog Number: 25544
Epoch time: 12107
49771623 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 71
1117 deg
Eccentricity:
0007959
Arg of perigee: 285
1240 deg
Mean anomaly: 74
9034 deg
Mean motion: 15
58332062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 840
Checksum: 300
Coasting Arc #9 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2012/108/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1064543
25 A = 6770010
22 meter
Y = 5318772
94 meter E =
0002773
Z = 4048467
37 I = 51
95463
XDOT = -5211
193859 Wp = 86
23520
YDOT = -4036
705415 meter/sec RA = 65
58043 deg
ZDOT = 3930
906703 TA = 323
18598
MA = 323
20501
Ha = 213
108 n
mi
Hp = 211
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3492595
95 X = -1143606
36
Y = 17450042
44 feet Y = 5306426
83 meter
Z = 13282373
27 Z = 4043103
35
XDOT = -17097
092713 XDOT = -5184
762845
YDOT = -13243
784170 feet/sec YDOT = -4094
832094 meter/sec
ZDOT = 12896
675535 ZDOT = 3905
655377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 703629
13 X = 214466
16
Y = 17798989
96 feet Y = 5425132
14 meter
Z = 13259883
48 Z = 4041612
49
XDOT = -18545
921965 XDOT = -5652
797015
YDOT = -8802
755150 feet/sec YDOT = -2683
079770 meter/sec
ZDOT = 12793
227099 ZDOT = 3899
375620
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
52376282
00016717 00000-0 10270-3 0 9082
2 25544 51
6394 65
9642 0008109 287
6612 72
3657 15
58387937 8567
Satellite: ISS
Catalog Number: 25544
Epoch time: 12108
52376282 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 65
9642 deg
Eccentricity:
0008109
Arg of perigee: 287
6612 deg
Mean anomaly: 72
3657 deg
Mean motion: 15
58387937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 343
Coasting Arc #10 (Orbit 870)
---------------------------------------
Vector Time (GMT): 2012/109/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3217848
51 A = 6765174
80 meter
Y = -2733857
51 meter E =
0008417
Z = -5292339
77 I = 51
92503
XDOT = 4228
213949 Wp = 58
14195
YDOT = 6359
760159 meter/sec RA = 60
56447 deg
ZDOT = -710
912068 TA = 205
07582
MA = 205
11672
Ha = 213
366 n
mi
Hp = 211
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10557245
77 X = 3273889
12
Y = -8969348
79 feet Y = -2697560
63 meter
Z = -17363319
45 Z = -5276571
12
XDOT = 13872
093010 XDOT = 4160
237051
YDOT = 20865
354852 feet/sec YDOT = 6406
662525 meter/sec
ZDOT = -2332
388673 ZDOT = -690
537051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8013153
46 X = 2442409
17
Y = -11399492
61 feet Y = -3474565
35 meter
Z = -17298279
05 Z = -5272515
45
XDOT = 17930
272147 XDOT = 5465
146950
YDOT = 16034
454495 feet/sec YDOT = 4887
301730 meter/sec
ZDOT = -2249
188069 ZDOT = -685
552523
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
48566722
00016717 00000-0 10270-3 0 9099
2 25544 51
6397 61
1373 0008045 292
3921 67
6381 15
58373920 8719
Satellite: ISS
Catalog Number: 25544
Epoch time: 12109
48566722 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 61
1373 deg
Eccentricity:
0008045
Arg of perigee: 292
3921 deg
Mean anomaly: 67
6381 deg
Mean motion: 15
58373920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 871
Checksum: 322
Coasting Arc #11 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2012/110/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4814441
39 A = 6767466
29 meter
Y = -454604
32 meter E =
0007156
Z = 4737672
77 I = 51
91771
XDOT = -2076
773524 Wp = 357
53459
YDOT = -6849
982732 meter/sec RA = 55
54119 deg
ZDOT = -2760
900357 TA = 119
70750
MA = 119
63626
Ha = 213
494 n
mi
Hp = 210
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15795411
38 X = -4832014
93
Y = -1491484
00 feet Y = -508540
30 meter
Z = 15543545
84 Z = 4714241
49
XDOT = -6813
561432 XDOT = -1986
609275
YDOT = -22473
696628 feet/sec YDOT = -6872
702564 meter/sec
ZDOT = -9058
072037 ZDOT = -2770
769846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15694795
60 X = -4783773
70
Y = 2894145
78 feet Y = 882135
63 meter
Z = 15447286
95 Z = 4708333
06
XDOT = -12413
747336 XDOT = -3783
710188
YDOT = -18638
859363 feet/sec YDOT = -5681
124334 meter/sec
ZDOT = -9098
040622 ZDOT = -2773
082781
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
51167911
00016717 00000-0 10270-3 0 9104
2 25544 51
6404 55
9897 0008117 296
2541 63
7779 15
58410043 8874
Satellite: ISS
Catalog Number: 25544
Epoch time: 12110
51167911 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 55
9897 deg
Eccentricity:
0008117
Arg of perigee: 296
2541 deg
Mean anomaly: 63
7779 deg
Mean motion: 15
58410043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 312
Coasting Arc #12 (Orbit 901)
---------------------------------------
Vector Time (GMT): 2012/111/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5322257
35 A = 6774130
31 meter
Y = 3301547
75 meter E =
0008019
Z = -2566922
73 I = 51
92233
XDOT = -853
481639 Wp = 337
57804
YDOT = 5491
916444 meter/sec RA = 50
54219 deg
ZDOT = 5295
835665 TA = 353
62131
MA = 353
63151
Ha = 213
747 n
mi
Hp = 210
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17461474
23 X = 5297412
93
Y = 10831849
58 feet Y = 3360925
46 meter
Z = -8421662
50 Z = -2541127
58
XDOT = -2800
136611 XDOT = -940
556309
YDOT = 18018
098571 feet/sec YDOT = 5481
885737 meter/sec
ZDOT = 17374
788928 ZDOT = 5291
477595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19894877
41 X = 6063958
63
Y = 5309930
74 feet Y = 1618466
89 meter
Z = -8315944
65 Z = -2534699
93
XDOT = 2811
313408 XDOT = 856
888327
YDOT = 16639
440698 feet/sec YDOT = 5071
701525 meter/sec
ZDOT = 17356
392768 ZDOT = 5290
228516
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
47354820
00016717 00000-0 10270-3 0 9118
2 25544 51
6406 51
1634 0008155 300
1619 59
8733 15
58423783 9025
Satellite: ISS
Catalog Number: 25544
Epoch time: 12111
47354820 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 51
1634 deg
Eccentricity:
0008155
Arg of perigee: 300
1619 deg
Mean anomaly: 59
8733 deg
Mean motion: 15
58423783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 902
Checksum: 287
Coasting Arc #13 (Orbit 917)
---------------------------------------
Vector Time (GMT): 2012/112/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4441470
39 A = 6776634
49 meter
Y = -5090411
45 meter E =
0003767
Z = -500047
53 I = 51
91227
XDOT = 3868
051016 Wp = 172
94748
YDOT = -2785
190682 meter/sec RA = 45
56900 deg
ZDOT = -6011
991074 TA = 12
43406
MA = 12
42476
Ha = 213
748 n
mi
Hp = 210
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14571753
25 X = -4381789
11
Y = -16700824
96 feet Y = -5139745
04 meter
Z = -1640575
87 Z = -521479
19
XDOT = 12690
456089 XDOT = 3928
113511
YDOT = -9137
764705 feet/sec YDOT = -2741
600170 meter/sec
ZDOT = -19724
380164 ZDOT = -5993
053915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18965527
32 X = -5780692
73
Y = -11457188
43 feet Y = -3492151
03 meter
Z = -1728190
74 Z = -526752
54
XDOT = 8572
494650 XDOT = 2612
896369
YDOT = -11230
912078 feet/sec YDOT = -3423
182001 meter/sec
ZDOT = -19646
304749 ZDOT = -5988
193687
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
49952392
00016717 00000-0 10270-3 0 9120
2 25544 51
6419 46
0154 0008174 303
7143 56
3232 15
58463921 9182
Satellite: ISS
Catalog Number: 25544
Epoch time: 12112
49952392 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 46
0154 deg
Eccentricity:
0008174
Arg of perigee: 303
7143 deg
Mean anomaly: 56
3232 deg
Mean motion: 15
58463921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 918
Checksum: 296
Coasting Arc #14 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2012/113/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2225171
55 A = 6771696
39 meter
Y = 5414267
17 meter E =
0007682
Z = 3394249
71 I = 51
87438
XDOT = -6094
118900 Wp = 50
04947
YDOT = -413
240436 meter/sec RA = 40
58824 deg
ZDOT = 4652
171866 TA = 349
56796
MA = 349
58389
Ha = 213
840 n
mi
Hp = 209
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7300431
60 X = 2147973
94
Y = 17763343
74 feet Y = 5438718
86 meter
Z = 11135989
88 Z = 3404872
05
XDOT = -19993
828411 XDOT = -6111
644645
YDOT = -1355
775710 feet/sec YDOT = -481
486521 meter/sec
ZDOT = 15263
031056 ZDOT = 4622
523808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12562349
43 X = 3829004
11
Y = 14493346
72 feet Y = 4417572
08 meter
Z = 11179142
66 Z = 3407402
68
XDOT = -18397
679784 XDOT = -5607
612798
YDOT = 4262
257470 feet/sec YDOT = 1299
136077 meter/sec
ZDOT = 15141
230808 ZDOT = 4615
047150
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
52548050
00016717 00000-0 10270-3 0 9138
2 25544 51
6421 40
8675 0008167 307
2116 52
8293 15
58500412 9349
Satellite: ISS
Catalog Number: 25544
Epoch time: 12113
52548050 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 40
8675 deg
Eccentricity:
0008167
Arg of perigee: 307
2116 deg
Mean anomaly: 52
8293 deg
Mean motion: 15
58500412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 934
Checksum: 281
Coasting Arc #15 (Orbit 948)
---------------------------------------
Vector Time (GMT): 2012/114/11:14:35
521
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 811400
72 A = 6765446
09 meter
Y = -4362804
82 meter E =
0010879
Z = -5114826
38 I = 51
83023
XDOT = 6756
995429 Wp = 39
95956
YDOT = 3220
179969 meter/sec RA = 35
57353 deg
ZDOT = -1668
642518 TA = 213
93841
MA = 214
00805
Ha = 214
000 n
mi
Hp = 209
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2662075
86 X = 884973
30
Y = -14313664
11 feet Y = -4353319
91 meter
Z = -16780926
43 Z = -5110705
82
XDOT = 22168
620173 XDOT = 6728
590556
YDOT = 10564
894912 feet/sec YDOT = 3295
582038 meter/sec
ZDOT = -5474
548942 ZDOT = -1635
885776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2235587
42 X = -681407
05
Y = -14406649
57 feet Y = -4391146
79 meter
Z = -16763583
06 Z = -5109540
12
XDOT = 23414
910818 XDOT = 7136
864817
YDOT = 2604
025488 feet/sec YDOT = 793
706969 meter/sec
ZDOT = -5340
240039 ZDOT = -1627
705164
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
48729839
00016717 00000-0 10270-3 0 9141
2 25544 51
6425 36
0411 0008214 311
2500 48
7947 15
58530833 9499
Satellite: ISS
Catalog Number: 25544
Epoch time: 12114
48729839 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 36
0411 deg
Eccentricity:
0008214
Arg of perigee: 311
2500 deg
Mean anomaly: 48
7947 deg
Mean motion: 15
58530833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 949
Checksum: 304
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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