[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 6th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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 184)
---------------------------------------
Vector Time (GMT): 2012/065/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3534575
68 A = 6771641
45 meter
Y = 4856441
53 meter E =
0021399
Z = -3131136
15 I = 51
30617
XDOT = -2900
809723 Wp = 118
24905
YDOT = -5203
334872 meter/sec RA = 281
36821 deg
ZDOT = -4831
046939 TA = 98
06806
MA = 97
82522
Ha = 219
735 n
mi
Hp = 201
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11596376
91 X = -3573408
67
Y = 15933207
13 feet Y = 4816698
33 meter
Z = -10272756
39 Z = -3148401
33
XDOT = -9517
092266 XDOT = -2818
941763
YDOT = -17071
308635 feet/sec YDOT = -5235
316191 meter/sec
ZDOT = -15849
891533 ZDOT = -4844
939327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16667177
76 X = -5080155
78
Y = 10444227
71 feet Y = 3183400
61 meter
Z = -10343880
51 Z = -3152814
78
XDOT = -1568
854797 XDOT = -478
186942
YDOT = -18143
774546 feet/sec YDOT = -5530
222482 meter/sec
ZDOT = -15906
457745 ZDOT = -4848
288321
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 12065
51219432
00016717 00000-0 10270-3 0 9008
2 25544 51
6408 281
9545 0017077 122
6062 237
6745 15
58764394 1851
Satellite: ISS
Catalog Number: 25544
Epoch time: 12065
51219432 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 281
9545 deg
Eccentricity:
0017077
Arg of perigee: 122
6062 deg
Mean anomaly: 237
6745 deg
Mean motion: 15
58764394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 185
Checksum: 313
Coasting Arc #2 (Orbit 200)
---------------------------------------
Vector Time (GMT): 2012/066/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4217032
40 A = 6765015
44 meter
Y = -1711200
44 meter E =
0022813
Z = 4993071
56 I = 51
27877
XDOT = 721
525051 Wp = 125
26505
YDOT = 7409
947233 meter/sec RA = 276
31445 deg
ZDOT = 1910
959859 TA = 306
04752
MA = 306
25866
Ha = 219
603 n
mi
Hp = 201
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13835408
14 X = 4211599
26
Y = -5614174
68 feet Y = -1664072
80 meter
Z = 16381468
37 Z = 5013544
27
XDOT = 2367
208171 XDOT = 629
329085
YDOT = 24310
850501 feet/sec YDOT = 7417
500488 meter/sec
ZDOT = 6269
553343 ZDOT = 1914
240159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14835175
59 X = 4521761
52
Y = -307501
95 feet Y = -93726
60 meter
Z = 16465509
08 Z = 5018687
17
XDOT = -6577
067227 XDOT = -2004
690091
YDOT = 22444
688588 feet/sec YDOT = 6841
141082 meter/sec
ZDOT = 6282
475207 ZDOT = 1914
898443
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 12066
53794008
00016717 00000-0 10270-3 0 9019
2 25544 51
6403 276
8044 0017106 125
8877 234
3869 15
58794131 2017
Satellite: ISS
Catalog Number: 25544
Epoch time: 12066
53794008 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 276
8044 deg
Eccentricity:
0017106
Arg of perigee: 125
8877 deg
Mean anomaly: 234
3869 deg
Mean motion: 15
58794131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 201
Checksum: 310
Coasting Arc #3 (Orbit 215)
---------------------------------------
Vector Time (GMT): 2012/067/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4011255
16 A = 6764665
39 meter
Y = -2087777
41 meter E =
0029457
Z = -5057342
66 I = 51
27441
XDOT = 1567
126089 Wp = 118
14439
YDOT = -7282
767457 meter/sec RA = 271
23739 deg
ZDOT = 1757
722096 TA = 169
00716
MA = 168
94265
Ha = 219
498 n
mi
Hp = 201
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13160285
97 X = -3963044
10
Y = -6849663
42 feet Y = -2132364
85 meter
Z = -16592331
57 Z = -5076711
43
XDOT = 5141
489792 XDOT = 1639
908524
YDOT = -23893
594020 feet/sec YDOT = -7264
835705 meter/sec
ZDOT = 5766
804776 ZDOT = 1765
512730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9918185
41 X = -3023062
91
Y = -10913496
41 feet Y = -3326433
70 meter
Z = -16671582
92 Z = -5081498
47
XDOT = 12194
443441 XDOT = 3716
866361
YDOT = -19970
147892 feet/sec YDOT = -6086
901077 meter/sec
ZDOT = 5799
240701 ZDOT = 1767
608566
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 12067
49955230
00016717 00000-0 10270-3 0 9022
2 25544 51
6389 271
9745 0016972 129
7609 230
5044 15
58860830 2169
Satellite: ISS
Catalog Number: 25544
Epoch time: 12067
49955230 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 271
9745 deg
Eccentricity:
0016972
Arg of perigee: 129
7609 deg
Mean anomaly: 230
5044 deg
Mean motion: 15
58860830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 216
Checksum: 325
Coasting Arc #4 (Orbit 231)
---------------------------------------
Vector Time (GMT): 2012/068/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2898334
02 A = 6771042
94 meter
Y = 5208589
30 meter E =
0027829
Z = 3176400
48 I = 51
29726
XDOT = -3516
749851 Wp = 116
21012
YDOT = 4887
876959 meter/sec RA = 266
18147 deg
ZDOT = -4785
718060 TA = 26
73210
MA = 26
58893
Ha = 219
166 n
mi
Hp = 201
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9508969
87 X = 2824445
07
Y = 17088547
59 feet Y = 5240587
58 meter
Z = 10421261
41 Z = 3190300
05
XDOT = -11537
893213 XDOT = -3547
898063
YDOT = 16036
341729 feet/sec YDOT = 4848
375647 meter/sec
ZDOT = -15701
174737 ZDOT = -4802
878403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3343923
55 X = 1019227
90
Y = 19237299
71 feet Y = 5863528
95 meter
Z = 10477887
73 Z = 3193660
18
XDOT = -14650
592219 XDOT = -4465
500508
YDOT = 11173
311880 feet/sec YDOT = 3405
625461 meter/sec
ZDOT = -15771
845425 ZDOT = -4807
258486
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 12068
52524806
00016717 00000-0 10270-3 0 9039
2 25544 51
6393 266
8241 0016723 133
5333 226
7214 15
58931250 2328
Satellite: ISS
Catalog Number: 25544
Epoch time: 12068
52524806 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 266
8241 deg
Eccentricity:
0016723
Arg of perigee: 133
5333 deg
Mean anomaly: 226
7214 deg
Mean motion: 15
58931250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 232
Checksum: 291
Coasting Arc #5 (Orbit 246)
---------------------------------------
Vector Time (GMT): 2012/069/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1154909
81 A = 6775411
14 meter
Y = -6677741
16 meter E =
0020074
Z = -143286
88 I = 51
31337
XDOT = 4704
118122 Wp = 101
21322
YDOT = -926
701383 meter/sec RA = 261
15793 deg
ZDOT = 5982
579487 TA = 257
23496
MA = 257
45938
Ha = 219
240 n
mi
Hp = 201
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3789074
18 X = -1079456
08
Y = -21908599
59 feet Y = -6690234
21 meter
Z = -470101
32 Z = -148713
13
XDOT = 15433
458405 XDOT = 4685
069253
YDOT = -3040
358869 feet/sec YDOT = -874
202694 meter/sec
ZDOT = 19627
885456 ZDOT = 6005
385568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3201469
79 X = 975807
99
Y = -22001668
94 feet Y = -6706108
69 meter
Z = -491903
92 Z = -149932
32
XDOT = 13896
528699 XDOT = 4235
661947
YDOT = 1630
961530 feet/sec YDOT = 497
117074 meter/sec
ZDOT = 19721
431764 ZDOT = 6011
092402
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 12069
48681732
00016717 00000-0 10270-3 0 9048
2 25544 51
6377 261
9945 0016844 137
2689 222
9779 15
58921524 2479
Satellite: ISS
Catalog Number: 25544
Epoch time: 12069
48681732 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 261
9945 deg
Eccentricity:
0016844
Arg of perigee: 137
2689 deg
Mean anomaly: 222
9779 deg
Mean motion: 15
58921524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 247
Checksum: 351
Coasting Arc #6 (Orbit 262)
---------------------------------------
Vector Time (GMT): 2012/070/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1021863
15 A = 6771365
50 meter
Y = 5969129
52 meter E =
0020775
Z = -3024164
00 I = 51
30575
XDOT = -4874
707433 Wp = 134
20139
YDOT = -3308
727972 meter/sec RA = 256
13694 deg
ZDOT = -4918
854589 TA = 80
71708
MA = 80
48219
Ha = 219
049 n
mi
Hp = 202
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3352569
40 X = -1073844
55
Y = 19583758
26 feet Y = 5957411
39 meter
Z = -9921797
92 Z = -3029255
17
XDOT = -15993
134624 XDOT = -4813
451651
YDOT = -10855
406733 feet/sec YDOT = -3362
898085 meter/sec
ZDOT = -16137
974374 ZDOT = -4942
386418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8904387
75 X = -2714057
39
Y = 17749729
32 feet Y = 5410117
50 meter
Z = -9943056
42 Z = -3030643
60
XDOT = -10706
118031 XDOT = -3263
224776
YDOT = -14400
390991 feet/sec YDOT = -4389
239174 meter/sec
ZDOT = -16234
220357 ZDOT = -4948
190365
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 12070
51246532
00016717 00000-0 10270-3 0 9050
2 25544 51
6375 256
8430 0016803 140
8272 219
4103 15
58969749 2633
Satellite: ISS
Catalog Number: 25544
Epoch time: 12070
51246532 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 256
8430 deg
Eccentricity:
0016803
Arg of perigee: 140
8272 deg
Mean anomaly: 219
4103 deg
Mean motion: 15
58969749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 263
Checksum: 307
Coasting Arc #7 (Orbit 278)
---------------------------------------
Vector Time (GMT): 2012/071/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3041430
35 A = 6764631
56 meter
Y = -3420020
83 meter E =
0022423
Z = 4973737
08 I = 51
29143
XDOT = 3853
947521 Wp = 139
13532
YDOT = 6343
138646 meter/sec RA = 251
08269 deg
ZDOT = 1983
187397 TA = 291
42731
MA = 291
66636
Ha = 218
937 n
mi
Hp = 202
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9978446
03 X = 3055286
38
Y = -11220540
77 feet Y = -3385931
69 meter
Z = 16318035
05 Z = 4988546
22
XDOT = 12644
184781 XDOT = 3773
096959
YDOT = 20810
822330 feet/sec YDOT = 6385
784013 meter/sec
ZDOT = 6506
520331 ZDOT = 2001
712643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12604807
22 X = 3841945
24
Y = -8037199
11 feet Y = -2449738
29 meter
Z = 16378963
76 Z = 4992308
15
XDOT = 5747
599543 XDOT = 1751
868341
YDOT = 22572
578104 feet/sec YDOT = 6880
121806 meter/sec
ZDOT = 6582
051449 ZDOT = 2006
209282
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 12071
53808883
00016717 00000-0 10270-3 0 9067
2 25544 51
6374 251
6914 0016767 144
5681 215
6591 15
58970590 2798
Satellite: ISS
Catalog Number: 25544
Epoch time: 12071
53808883 = yrday
fracday
Element set: 906
Inclination: 51
6374 deg
RA of node: 251
6914 deg
Eccentricity:
0016767
Arg of perigee: 144
5681 deg
Mean anomaly: 215
6591 deg
Mean motion: 15
58970590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 279
Checksum: 339
Coasting Arc #8 (Orbit 293)
---------------------------------------
Vector Time (GMT): 2012/072/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4514776
74 A = 6764118
49 meter
Y = -180047
25 meter E =
0027918
Z = -5057229
94 I = 51
30130
XDOT = -1690
191866 Wp = 128
65782
YDOT = -7258
132817 meter/sec RA = 246
00557 deg
ZDOT = 1756
766816 TA = 158
49810
MA = 158
38061
Ha = 218
835 n
mi
Hp = 202
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14812259
66 X = -4487861
01
Y = -590706
21 feet Y = -230384
18 meter
Z = -16591961
73 Z = -5079097
10
XDOT = -5545
248903 XDOT = -1617
438312
YDOT = -23812
771709 feet/sec YDOT = -7276
626659 meter/sec
ZDOT = 5763
670657 ZDOT = 1748
733240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14047068
64 X = -4281546
52
Y = -4410144
32 feet Y = -1344211
99 meter
Z = -16681596
26 Z = -5084550
54
XDOT = 505
663026 XDOT = 154
126090
YDOT = -23419
213523 feet/sec YDOT = -7138
176282 meter/sec
ZDOT = 5731
202874 ZDOT = 1746
870636
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 12072
49958489
00016717 00000-0 10270-3 0 9072
2 25544 51
6374 246
8610 0016875 148
2250 211
9927 15
59041976 2947
Satellite: ISS
Catalog Number: 25544
Epoch time: 12072
49958489 = yrday
fracday
Element set: 907
Inclination: 51
6374 deg
RA of node: 246
8610 deg
Eccentricity:
0016875
Arg of perigee: 148
2250 deg
Mean anomaly: 211
9927 deg
Mean motion: 15
59041976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 294
Checksum: 343
Coasting Arc #9 (Orbit 309)
---------------------------------------
Vector Time (GMT): 2012/073/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4829887
72 A = 6770691
65 meter
Y = 3529092
35 meter E =
0025932
Z = 3135556
02 I = 51
33711
XDOT = -1153
113509 Wp = 127
46523
YDOT = 5877
059281 meter/sec RA = 240
95087 deg
ZDOT = -4826
613736 TA = 16
05249
MA = 15
97048
Ha = 218
526 n
mi
Hp = 202
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15846088
31 X = 4774833
95
Y = 11578386
99 feet Y = 3582795
50 meter
Z = 10287257
27 Z = 3158885
38
XDOT = -3783
180805 XDOT = -1195
299745
YDOT = 19281
690554 feet/sec YDOT = 5863
928291 meter/sec
ZDOT = -15835
346902 ZDOT = -4832
318307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12476099
71 X = 3802715
19
Y = 15084167
45 feet Y = 4597654
24 meter
Z = 10382680
31 Z = 3164640
96
XDOT = -7185
816084 XDOT = -2190
236742
YDOT = 16885
983192 feet/sec YDOT = 5146
847677 meter/sec
ZDOT = -15859
110060 ZDOT = -4833
856746
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 12073
52515529
00016717 00000-0 10270-3 0 9082
2 25544 51
6373 241
7099 0016713 152
4104 207
7942 15
59079170 3103
Satellite: ISS
Catalog Number: 25544
Epoch time: 12073
52515529 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 241
7099 deg
Eccentricity:
0016713
Arg of perigee: 152
4104 deg
Mean anomaly: 207
7942 deg
Mean motion: 15
59079170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 310
Checksum: 299
Coasting Arc #10 (Orbit 324)
---------------------------------------
Vector Time (GMT): 2012/074/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3808639
69 A = 6774808
26 meter
Y = -5608529
98 meter E =
0016946
Z = -16397
64 I = 51
36727
XDOT = 3957
515394 Wp = 114
02965
YDOT = -2690
644623 meter/sec RA = 235
93112 deg
ZDOT = 5987
719560 TA = 245
79294
MA = 245
97015
Ha = 218
519 n
mi
Hp = 202
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12495537
04 X = -3745561
25
Y = -18400688
90 feet Y = -5650767
85 meter
Z = -53798
04 Z = -34746
22
XDOT = 12983
974389 XDOT = 3958
221811
YDOT = -8827
574223 feet/sec YDOT = -2646
384999 meter/sec
ZDOT = 19644
749211 ZDOT = 6006
946698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7979083
27 X = -2432024
58
Y = -20761607
94 feet Y = -6328138
10 meter
Z = -128678
85 Z = -39221
31
XDOT = 13021
699894 XDOT = 3969
014128
YDOT = -5085
064875 feet/sec YDOT = -1549
927774 meter/sec
ZDOT = 19723
756101 ZDOT = 6011
800860
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 12074
48660422
00016717 00000-0 10270-3 0 9092
2 25544 51
6375 236
8803 0016843 155
6551 204
5403 15
59132516 3255
Satellite: ISS
Catalog Number: 25544
Epoch time: 12074
48660422 = yrday
fracday
Element set: 909
Inclination: 51
6375 deg
RA of node: 236
8803 deg
Eccentricity:
0016843
Arg of perigee: 155
6551 deg
Mean anomaly: 204
5403 deg
Mean motion: 15
59132516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 325
Checksum: 301
Coasting Arc #11 (Orbit 340)
---------------------------------------
Vector Time (GMT): 2012/075/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1440950
52 A = 6770402
20 meter
Y = 5798033
41 meter E =
0019484
Z = -3175016
00 I = 51
37103
XDOT = -5879
641123 Wp = 147
85080
YDOT = -1152
048258 meter/sec RA = 230
91296 deg
ZDOT = -4801
979185 TA = 69
07051
MA = 68
86207
Ha = 218
285 n
mi
Hp = 202
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4727527
97 X = 1391431
99
Y = 19022419
33 feet Y = 5813869
98 meter
Z = -10416719
16 Z = -3168136
58
XDOT = -19290
161164 XDOT = -5842
995034
YDOT = -3779
685885 feet/sec YDOT = -1217
593378 meter/sec
ZDOT = -15754
524886 ZDOT = -4830
452816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 672974
74 X = 205122
70
Y = 19604298
24 feet Y = 5975390
10 meter
Z = -10388868
63 Z = -3166527
16
XDOT = -16536
156153 XDOT = -5040
220395
YDOT = -7791
079676 feet/sec YDOT = -2374
721085 meter/sec
ZDOT = -15871
216168 ZDOT = -4837
546688
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 12075
51212219
00016717 00000-0 10270-3 0 9106
2 25544 51
6377 231
7286 0016647 159
0080 201
1762 15
59177651 3411
Satellite: ISS
Catalog Number: 25544
Epoch time: 12075
51212219 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 231
7286 deg
Eccentricity:
0016647
Arg of perigee: 159
0080 deg
Mean anomaly: 201
1762 deg
Mean motion: 15
59177651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 341
Checksum: 291
Coasting Arc #12 (Orbit 356)
---------------------------------------
Vector Time (GMT): 2012/076/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1548580
76 A = 6763622
82 meter
Y = -4209985
50 meter E =
0021037
Z = 5059060
61 I = 51
36813
XDOT = 6107
397098 Wp = 154
32514
YDOT = 4329
165657 meter/sec RA = 225
86035 deg
ZDOT = 1711
794574 TA = 278
97597
MA = 279
21402
Ha = 218
094 n
mi
Hp = 202
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5080645
53 X = 1570967
16
Y = -13812288
38 feet Y = -4192542
82 meter
Z = 16597967
89 Z = 5066638
07
XDOT = 20037
392053 XDOT = 6050
218192
YDOT = 14203
299400 feet/sec YDOT = 4397
142745 meter/sec
ZDOT = 5616
123932 ZDOT = 1741
324429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7564105
41 X = 2305539
33
Y = -12583142
63 feet Y = -3835341
87 meter
Z = 16629300
59 Z = 5068610
82
XDOT = 15950
363394 XDOT = 4861
670763
YDOT = 17262
215503 feet/sec YDOT = 5261
523285 meter/sec
ZDOT = 5736
967289 ZDOT = 1748
627630
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 12076
53761283
00016717 00000-0 10270-3 0 9110
2 25544 51
6372 226
5765 0016601 163
1960 196
9748 15
59208970 3574
Satellite: ISS
Catalog Number: 25544
Epoch time: 12076
53761283 = yrday
fracday
Element set: 911
Inclination: 51
6372 deg
RA of node: 226
5765 deg
Eccentricity:
0016601
Arg of perigee: 163
1960 deg
Mean anomaly: 196
9748 deg
Mean motion: 15
59208970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 357
Checksum: 328
Coasting Arc #13 (Orbit 371)
---------------------------------------
Vector Time (GMT): 2012/077/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4395174
47 A = 6763949
13 meter
Y = 1435658
86 meter E =
0025306
Z = -4957071
76 I = 51
39269
XDOT = -4332
639085 Wp = 140
82674
YDOT = -5956
369890 meter/sec RA = 220
78874 deg
ZDOT = 2103
092793 TA = 149
81637
MA = 149
67034
Ha = 217
948 n
mi
Hp = 202
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14419863
76 X = -4386821
72
Y = 4710166
88 feet Y = 1386555
61 meter
Z = -16263358
79 Z = -4978402
78
XDOT = -14214
695160 XDOT = -4275
927920
YDOT = -19541
895965 feet/sec YDOT = -6004
502876 meter/sec
ZDOT = 6899
910739 ZDOT = 2082
183621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14928347
82 X = -4550160
41
Y = 2099129
61 feet Y = 639814
71 meter
Z = -16350934
79 Z = -4983764
92
XDOT = -10417
893956 XDOT = -3175
374078
YDOT = -20668
458356 feet/sec YDOT = -6299
746107 meter/sec
ZDOT = 6814
504517 ZDOT = 2077
060977
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 12077
49898477
00016717 00000-0 10270-3 0 9123
2 25544 51
6382 221
7470 0016634 166
4711 193
6894 15
59245125 3727
Satellite: ISS
Catalog Number: 25544
Epoch time: 12077
49898477 = yrday
fracday
Element set: 912
Inclination: 51
6382 deg
RA of node: 221
7470 deg
Eccentricity:
0016634
Arg of perigee: 166
4711 deg
Mean anomaly: 193
6894 deg
Mean motion: 15
59245125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 372
Checksum: 334
Coasting Arc #14 (Orbit 387)
---------------------------------------
Vector Time (GMT): 2012/078/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5947733
15 A = 6770931
24 meter
Y = 1505898
49 meter E =
0024411
Z = 2825071
08 I = 51
43972
XDOT = 975
168890 Wp = 139
35773
YDOT = 5691
473836 meter/sec RA = 215
74203 deg
ZDOT = -5080
420211 TA = 8
30696
MA = 8
26662
Ha = 217
683 n
mi
Hp = 203
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19513560
19 X = 5916728
51
Y = 4940611
85 feet Y = 1572236
65 meter
Z = 9268605
91 Z = 2853888
94
XDOT = 3199
373000 XDOT = 936
132320
YDOT = 18672
814423 feet/sec YDOT = 5702
159996 meter/sec
ZDOT = -16668
045311 ZDOT = -5075
778361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18414750
38 X = 5612815
92
Y = 7992625
02 feet Y = 2436152
11 meter
Z = 9386727
11 Z = 2861074
42
XDOT = 851
291110 XDOT = 259
473530
YDOT = 17616
639600 feet/sec YDOT = 5369
551750 meter/sec
ZDOT = -16649
335108 ZDOT = -5074
717341
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 12078
52442097
00016717 00000-0 10270-3 0 9132
2 25544 51
6378 216
5940 0016579 170
3332 189
8145 15
59267663 3881
Satellite: ISS
Catalog Number: 25544
Epoch time: 12078
52442097 = yrday
fracday
Element set: 913
Inclination: 51
6378 deg
RA of node: 216
5940 deg
Eccentricity:
0016579
Arg of perigee: 170
3332 deg
Mean anomaly: 189
8145 deg
Mean motion: 15
59267663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 388
Checksum: 337
Coasting Arc #15 (Orbit 403)
---------------------------------------
Vector Time (GMT): 2012/079/11:40:35
831
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5626460
05 A = 6774128
75 meter
Y = -3755107
09 meter E =
0014060
Z = 442875
13 I = 51
47805
XDOT = 2989
056675 Wp = 125
19602
YDOT = -3757
097328 meter/sec RA = 210
73166 deg
ZDOT = 5975
604974 TA = 239
59398
MA = 239
73302
Ha = 217
532 n
mi
Hp = 203
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18459514
61 X = -5586202
87
Y = -12319905
16 feet Y = -3817800
50 meter
Z = 1453002
40 Z = 415640
69
XDOT = 9806
616387 XDOT = 3001
819440
YDOT = -12326
434804 feet/sec YDOT = -3723
599775 meter/sec
ZDOT = 19605
003197 ZDOT = 5990
156903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16514867
31 X = -5033731
56
Y = -14835919
63 feet Y = -4521988
30 meter
Z = 1341493
68 Z = 408887
27
XDOT = 10269
587803 XDOT = 3130
170362
YDOT = -9607
882398 feet/sec YDOT = -2928
482555 meter/sec
ZDOT = 19664
911728 ZDOT = 5993
865095
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 12079
54982739
00016717 00000-0 10270-3 0 9148
2 25544 51
6394 211
4419 0016489 174
0638 186
0716 15
59344533 4048
Satellite: ISS
Catalog Number: 25544
Epoch time: 12079
54982739 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 211
4419 deg
Eccentricity:
0016489
Arg of perigee: 174
0638 deg
Mean anomaly: 186
0716 deg
Mean motion: 15
59344533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 404
Checksum: 330
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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