[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 21st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
235/09:48:11
950 0
4 2
9 2
9
N/A 2
1 -0
5 223
0
000/00:06:23
900 -1
9 -0
1 217
2
235/13:34:24
070 -3
6 9
2 9
3
N/A -3
1 -1
4 231
1
000/00:34:48
140 8
0 -0
8 219
4
Coasting Arc #1 (Orbit 2757)
---------------------------------------
Vector Time (GMT): 2012/230/15:17:36
814
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4583257
19 A = 6785516
75 meter
Y = -3380797
49 meter E =
0010909
Z = 3688335
31 I = 51
67376
XDOT = 5626
690058 Wp = 48
00633
YDOT = 2886
314036 meter/sec RA = 174
37893 deg
ZDOT = -4330
903195 TA = 88
13304
MA = 88
00810
Ha = 222
483 n
mi
Hp = 216
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15036933
04 X = 4602804
59
Y = -11091855
27 feet Y = -3329435
23 meter
Z = 12100837
62 Z = 3710647
71
XDOT = 18460
269220 XDOT = 5615
034641
YDOT = 9469
534240 feet/sec YDOT = 2949
169871 meter/sec
ZDOT = -14208
999983 ZDOT = -4303
597944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11581600
30 X = -3530071
77
Y = 14586271
83 feet Y = 4445895
65 meter
Z = 12193280
45 Z = 3716511
88
XDOT = -19302
059582 XDOT = -5883
267761
YDOT = -3500
322910 feet/sec YDOT = -1066
898423 meter/sec
ZDOT = -14096
432138 ZDOT = -4296
592516
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 12230
67734618
00016717 00000-0 10270-3 0 9007
2 25544 51
6434 175
2833 0007199 330
1456 29
9284 15
53429032 27582
Satellite: ISS
Catalog Number: 25544
Epoch time: 12230
67734618 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 175
2833 deg
Eccentricity:
0007199
Arg of perigee: 330
1456 deg
Mean anomaly: 29
9284 deg
Mean motion: 15
53429032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2758
Checksum: 313
Coasting Arc #2 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2012/231/15:17:36
814
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5526830
65 A = 6788572
08 meter
Y = 3038233
56 meter E =
0009874
Z = -2496268
15 I = 51
71538
XDOT = -4302
624903 Wp = 4
67656
YDOT = -3466
118959 meter/sec RA = 169
40600 deg
ZDOT = 5318
610782 TA = 327
36360
MA = 327
42459
Ha = 222
538 n
mi
Hp = 216
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18132646
47 X = -5548267
93
Y = 9967957
87 feet Y = 2976309
11 meter
Z = -8189856
14 Z = -2523169
01
XDOT = -14116
223436 XDOT = -4289
382435
YDOT = -11371
781363 feet/sec YDOT = -3514
159273 meter/sec
ZDOT = 17449
510439 ZDOT = 5297
741526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14637384
24 X = 4461474
72
Y = -14562392
90 feet Y = -4438617
36 meter
Z = -8301234
34 Z = -2530216
23
XDOT = 15742
535555 XDOT = 4798
324837
YDOT = 5946
030355 feet/sec YDOT = 1812
350052 meter/sec
ZDOT = 17363
567179 ZDOT = 5292
415276
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 12231
64230619
00016717 00000-0 10270-3 0 9018
2 25544 51
6444 170
4774 0007287 333
0515 27
0258 15
53454693 27738
Satellite: ISS
Catalog Number: 25544
Epoch time: 12231
64230619 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 170
4774 deg
Eccentricity:
0007287
Arg of perigee: 333
0515 deg
Mean anomaly: 27
0258 deg
Mean motion: 15
53454693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 300
Coasting Arc #3 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2012/232/15:17:36
814
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6177400
82 A = 6790829
72 meter
Y = -2601753
07 meter E =
0008655
Z = 1077814
50 I = 51
75230
XDOT = 2744
293290 Wp = 96
00388
YDOT = 4058
033002 meter/sec RA = 164
44244 deg
ZDOT = -5893
135191 TA = 72
33332
MA = 72
23884
Ha = 222
734 n
mi
Hp = 216
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20267063
07 X = 6200799
33
Y = -8535935
28 feet Y = -2532542
64 meter
Z = 3536136
80 Z = 1107880
63
XDOT = 9003
586911 XDOT = 2727
338715
YDOT = 13313
756568 feet/sec YDOT = 4088
626239 meter/sec
ZDOT = -19334
433042 ZDOT = -5879
845143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16871317
26 X = -5142377
50
Y = 14074061
60 feet Y = 4289773
98 meter
Z = 3660566
06 Z = 1115740
54
XDOT = -11584
382282 XDOT = -3530
919720
YDOT = -8839
448590 feet/sec YDOT = -2694
263930 meter/sec
ZDOT = -19279
844787 ZDOT = -5876
496691
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 12232
67158847
00016717 00000-0 10270-3 0 9025
2 25544 51
6443 165
3517 0007151 336
6383 23
4443 15
53430432 27895
Satellite: ISS
Catalog Number: 25544
Epoch time: 12232
67158847 = yrday
fracday
Element set: 902
Inclination: 51
6443 deg
RA of node: 165
3517 deg
Eccentricity:
0007151
Arg of perigee: 336
6383 deg
Mean anomaly: 23
4443 deg
Mean motion: 15
53430432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 304
Coasting Arc #4 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2012/233/15:17:36
814
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6443978
36 A = 6791140
63 meter
Y = 2069945
49 meter E =
0016838
Z = 406230
92 I = 51
78289
XDOT = -1106
527082 Wp = 25
25236
YDOT = -4639
448034 meter/sec RA = 159
48305 deg
ZDOT = 6010
852490 TA = 339
12102
MA = 339
18971
Ha = 222
826 n
mi
Hp = 216
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21141661
28 X = -6468619
35
Y = 6791159
73 feet Y = 1997747
16 meter
Z = 1332778
62 Z = 374866
66
XDOT = -3630
338197 XDOT = -1083
764693
YDOT = -15221
286202 feet/sec YDOT = -4651
694266 meter/sec
ZDOT = 19720
644652 ZDOT = 6005
532653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18024916
21 X = 5493994
46
Y = -12981568
99 feet Y = -3956782
23 meter
Z = 1203018
38 Z = 366680
00
XDOT = 7314
457522 XDOT = 2229
446653
YDOT = 12007
511150 feet/sec YDOT = 3659
889399 meter/sec
ZDOT = 19699
032913 ZDOT = 6004
265232
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 12233
70085755
00016717 00000-0 10270-3 0 9038
2 25544 51
6444 160
2253 0007382 339
9678 20
1183 15
53488498 28055
Satellite: ISS
Catalog Number: 25544
Epoch time: 12233
70085755 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 160
2253 deg
Eccentricity:
0007382
Arg of perigee: 339
9678 deg
Mean anomaly: 20
1183 deg
Mean motion: 15
53488498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 317
Coasting Arc #5 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2012/234/15:17:36
814
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6373463
20 A = 6789808
82 meter
Y = -1391462
38 meter E =
0002666
Z = -1887664
69 I = 51
80591
XDOT = -539
016538 Wp = 60
17525
YDOT = 5164
764439 meter/sec RA = 154
52528 deg
ZDOT = -5631
717132 TA = 140
53675
MA = 140
51733
Ha = 222
922 n
mi
Hp = 216
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20910312
34 X = 6397718
94
Y = -4565165
30 feet Y = -1320054
83 meter
Z = -6193125
62 Z = -1856643
85
XDOT = -1768
426962 XDOT = -569
372456
YDOT = 16944
765220 feet/sec YDOT = 5158
566793 meter/sec
ZDOT = -18476
762245 ZDOT = -5634
409645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18330841
23 X = -5587240
41
Y = 11119119
66 feet Y = 3389107
67 meter
Z = -6064828
02 Z = -1848559
58
XDOT = -3124
348108 XDOT = -952
301303
YDOT = -15226
512825 feet/sec YDOT = -4641
041109 meter/sec
ZDOT = -18488
304022 ZDOT = -5635
235066
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 12234
66578992
00016717 00000-0 10270-3 0 9045
2 25544 51
6440 155
4200 0007304 342
4301 17
6598 15
53464314 28204
Satellite: ISS
Catalog Number: 25544
Epoch time: 12234
66578992 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 155
4200 deg
Eccentricity:
0007304
Arg of perigee: 342
4301 deg
Mean anomaly: 17
6598 deg
Mean motion: 15
53464314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 293
Coasting Arc #6 (Orbit 2831)
---------------------------------------
Vector Time (GMT): 2012/235/09:51:23
900
Vector Time (MET): N/A
Weight (LBS) : 955845
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6171901
27 A = 6789901
18 meter
Y = -1116227
21 meter E =
0002491
Z = -2605092
72 I = 51
81901
XDOT = -1235
151935 Wp = 45
23688
YDOT = 5433
819302 meter/sec RA = 150
68440 deg
ZDOT = -5255
932746 TA = 163
97079
MA = 163
96291
Ha = 223
019 n
mi
Hp = 217
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20249019
91 X = 6196579
36
Y = -3662162
77 feet Y = -1047071
29 meter
Z = -8546892
11 Z = -2575049
99
XDOT = -4052
335744 XDOT = -1270
290158
YDOT = 17827
491149 feet/sec YDOT = 5419
810383 meter/sec
ZDOT = -17243
873839 ZDOT = -5262
018612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12808015
54 X = -3903883
14
Y = -16170878
70 feet Y = -4928883
83 meter
Z = -8422649
72 Z = -2567223
63
XDOT = 16400
340872 XDOT = 4998
823898
YDOT = -3997
289700 feet/sec YDOT = -1218
373900 meter/sec
ZDOT = -17269
465864 ZDOT = -5263
733195
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 12235
43773818
00016717 00000-0 10270-3 0 9056
2 25544 51
6405 151
5734 0005486 335
6375 24
4517 15
52972304 28320
Satellite: ISS
Catalog Number: 25544
Epoch time: 12235
43773818 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 151
5734 deg
Eccentricity:
0005486
Arg of perigee: 335
6375 deg
Mean anomaly: 24
4517 deg
Mean motion: 15
52972304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2832
Checksum: 310
Coasting Arc #7 (Orbit 2834)
---------------------------------------
Vector Time (GMT): 2012/235/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4531754
91 A = 6791760
30 meter
Y = -1696615
70 meter E =
0011884
Z = 4757587
99 I = 51
80673
XDOT = 4834
414063 Wp = 18
50367
YDOT = -5289
184952 meter/sec RA = 149
85529 deg
ZDOT = 2727
866824 TA = 44
62818
MA = 44
53257
Ha = 231
113 n
mi
Hp = 219
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14867962
31 X = -4535557
43
Y = -5566324
48 feet Y = -1747313
69 meter
Z = 15608884
49 Z = 4735563
81
XDOT = 15860
938528 XDOT = 4879
948187
YDOT = -17352
969003 feet/sec YDOT = -5234
868828 meter/sec
ZDOT = 8949
694304 ZDOT = 2751
462930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14803904
93 X = 4512230
22
Y = 5976070
06 feet Y = 1821506
15 meter
Z = 15518006
70 Z = 4729888
44
XDOT = -15842
871538 XDOT = -4828
907245
YDOT = 15830
172247 feet/sec YDOT = 4825
036501 meter/sec
ZDOT = 9047
638199 ZDOT = 2757
720123
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 12235
63091006
00016717 00000-0 10270-3 0 9061
2 25544 51
6461 150
6140 0015207 347
9348 12
1436 15
50045477 28358
Satellite: ISS
Catalog Number: 25544
Epoch time: 12235
63091006 = yrday
fracday
Element set: 906
Inclination: 51
6461 deg
RA of node: 150
6140 deg
Eccentricity:
0015207
Arg of perigee: 347
9348 deg
Mean anomaly: 12
1436 deg
Mean motion: 15
50045477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2835
Checksum: 283
Coasting Arc #8 (Orbit 2849)
---------------------------------------
Vector Time (GMT): 2012/236/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4416422
68 A = 6791080
72 meter
Y = 1617481
78 meter E =
0020650
Z = -4913407
55 I = 51
83026
XDOT = -4685
637857 Wp = 25
82195
YDOT = 5564
243462 meter/sec RA = 144
91148 deg
ZDOT = -2365
606442 TA = 220
93636
MA = 221
09159
Ha = 231
152 n
mi
Hp = 219
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14489575
73 X = 4421875
60
Y = 5306698
77 feet Y = 1666899
38 meter
Z = -16120103
53 Z = -4891939
60
XDOT = -15372
827614 XDOT = -4736
018570
YDOT = 18255
391937 feet/sec YDOT = 5511
564010 meter/sec
ZDOT = -7761
175992 ZDOT = -2388
491478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14531980
63 X = -4429347
70
Y = -5456992
48 feet Y = -1663291
31 meter
Z = -16031511
68 Z = -4886404
76
XDOT = 15116
016282 XDOT = 4607
361763
YDOT = -17034
959169 feet/sec YDOT = -5192
255555 meter/sec
ZDOT = -7856
220342 ZDOT = -2394
575960
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 12236
59797696
00016717 00000-0 10270-3 0 9076
2 25544 51
6459 145
8227 0015323 350
9412 9
1460 15
50082376 28501
Satellite: ISS
Catalog Number: 25544
Epoch time: 12236
59797696 = yrday
fracday
Element set: 907
Inclination: 51
6459 deg
RA of node: 145
8227 deg
Eccentricity:
0015323
Arg of perigee: 350
9412 deg
Mean anomaly: 9
1460 deg
Mean motion: 15
50082376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2850
Checksum: 321
Coasting Arc #9 (Orbit 2865)
---------------------------------------
Vector Time (GMT): 2012/237/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4244011
90 A = 6790494
85 meter
Y = -1609032
31 meter E =
0012463
Z = 5044103
76 I = 51
85256
XDOT = 4550
107479 Wp = 16
69910
YDOT = -5846
931156 meter/sec RA = 139
96788 deg
ZDOT = 1973
669385 TA = 54
25215
MA = 54
13631
Ha = 231
383 n
mi
Hp = 218
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13923923
56 X = -4250206
96
Y = -5278977
38 feet Y = -1656526
14 meter
Z = 16548896
86 Z = 5023471
57
XDOT = 14928
174144 XDOT = 4605
563295
YDOT = -19182
845001 feet/sec YDOT = -5795
738957 meter/sec
ZDOT = 6475
293259 ZDOT = 1995
908200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14060508
52 X = 4285643
00
Y = 5182299
19 feet Y = 1579564
79 meter
Z = 16463751
45 Z = 5018151
44
XDOT = -14379
411651 XDOT = -4382
844671
YDOT = 18258
060868 feet/sec YDOT = 5565
056952 meter/sec
ZDOT = 6567
708203 ZDOT = 2001
837460
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 12237
62950767
00016717 00000-0 10270-3 0 9082
2 25544 51
6459 140
7112 0015286 354
9886 5
1109 15
50071540 28669
Satellite: ISS
Catalog Number: 25544
Epoch time: 12237
62950767 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 140
7112 deg
Eccentricity:
0015286
Arg of perigee: 354
9886 deg
Mean anomaly: 5
1109 deg
Mean motion: 15
50071540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2866
Checksum: 315
Coasting Arc #10 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2012/238/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4136396
72 A = 6789961
88 meter
Y = 1591369
24 meter E =
0022151
Z = -5159309
07 I = 51
87314
XDOT = -4340
322286 Wp = 34
95125
YDOT = 6095
317037 meter/sec RA = 135
02609 deg
ZDOT = -1585
420304 TA = 219
69012
MA = 219
85244
Ha = 231
404 n
mi
Hp = 218
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13570855
37 X = 4143356
83
Y = 5221027
70 feet Y = 1637663
98 meter
Z = -16926867
02 Z = -5139197
87
XDOT = -14239
902513 XDOT = -4400
457244
YDOT = 19997
759309 feet/sec YDOT = 6046
444639 meter/sec
ZDOT = -5201
510185 ZDOT = -1606
651218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13795536
63 X = -4204879
56
Y = -4890135
82 feet Y = -1490513
40 meter
Z = -16843865
76 Z = -5134010
28
XDOT = 13366
992714 XDOT = 4074
259379
YDOT = -19326
797674 feet/sec YDOT = -5890
807931 meter/sec
ZDOT = -5289
797616 ZDOT = -1612
330313
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 12238
59655783
00016717 00000-0 10270-3 0 9090
2 25544 51
6454 135
9194 0015383 357
9069 2
2015 15
50108672 28812
Satellite: ISS
Catalog Number: 25544
Epoch time: 12238
59655783 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 135
9194 deg
Eccentricity:
0015383
Arg of perigee: 357
9069 deg
Mean anomaly: 2
2015 deg
Mean motion: 15
50108672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 326
Coasting Arc #11 (Orbit 2896)
---------------------------------------
Vector Time (GMT): 2012/239/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3981502
83 A = 6789568
22 meter
Y = -1651833
75 meter E =
0013642
Z = 5240167
34 I = 51
89291
XDOT = 4146
449262 Wp = 16
33628
YDOT = -6343
196749 meter/sec RA = 130
08495 deg
ZDOT = 1162
972742 TA = 62
61828
MA = 62
47954
Ha = 231
617 n
mi
Hp = 218
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13062673
32 X = -3988191
00
Y = -5419402
08 feet Y = -1696394
84 meter
Z = 17192150
07 Z = 5220809
36
XDOT = 13603
836163 XDOT = 4211
422638
YDOT = -20811
012957 feet/sec YDOT = -6296
465299 meter/sec
ZDOT = 3815
527370 ZDOT = 1183
273508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13379672
58 X = 4078124
20
Y = 4871170
70 feet Y = 1484732
83 meter
Z = 17112259
78 Z = 5215816
78
XDOT = -12356
037844 XDOT = -3766
120335
YDOT = 20376
972397 feet/sec YDOT = 6210
901187 meter/sec
ZDOT = 3900
006721 ZDOT = 1188
722049
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 12239
62807090
00016717 00000-0 10270-3 0 9107
2 25544 51
6458 130
8080 0015342 1
9163 358
2043 15
50095965 28972
Satellite: ISS
Catalog Number: 25544
Epoch time: 12239
62807090 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 130
8080 deg
Eccentricity:
0015342
Arg of perigee: 1
9163 deg
Mean anomaly: 358
2043 deg
Mean motion: 15
50095965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2897
Checksum: 303
Coasting Arc #12 (Orbit 2911)
---------------------------------------
Vector Time (GMT): 2012/240/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3900169
80 A = 6789227
05 meter
Y = 1689607
89 meter E =
0023087
Z = -5309601
49 I = 51
90989
XDOT = -3883
869105 Wp = 43
28592
YDOT = 6545
737319 meter/sec RA = 125
14502 deg
ZDOT = -755
540698 TA = 219
41978
MA = 219
58799
Ha = 231
624 n
mi
Hp = 218
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12795832
66 X = 3906778
80
Y = 5543332
97 feet Y = 1733258
95 meter
Z = -17419952
41 Z = -5290638
91
XDOT = -12742
352707 XDOT = -3953
106050
YDOT = 21475
516139 feet/sec YDOT = 6501
918349 meter/sec
ZDOT = -2478
808065 ZDOT = -774
576246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13203735
79 X = -4024498
67
Y = -4779505
57 feet Y = -1456793
30 meter
Z = -17341692
64 Z = -5285747
92
XDOT = 11102
911786 XDOT = 3384
167512
YDOT = -21218
930591 feet/sec YDOT = -6467
530044 meter/sec
ZDOT = -2558
087035 ZDOT = -779
704928
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 12240
59510475
00016717 00000-0 10270-3 0 9114
2 25544 51
6449 126
0159 0015398 4
9666 355
1634 15
50132516 29122
Satellite: ISS
Catalog Number: 25544
Epoch time: 12240
59510475 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 126
0159 deg
Eccentricity:
0015398
Arg of perigee: 4
9666 deg
Mean anomaly: 355
1634 deg
Mean motion: 15
50132516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2912
Checksum: 300
Coasting Arc #13 (Orbit 2927)
---------------------------------------
Vector Time (GMT): 2012/241/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3782025
89 A = 6789074
26 meter
Y = -1809919
40 meter E =
0015296
Z = 5334842
60 I = 51
92629
XDOT = 3642
383271 Wp = 18
46758
YDOT = -6739
047919 meter/sec RA = 120
20599 deg
ZDOT = 309
762280 TA = 68
67203
MA = 68
50882
Ha = 231
813 n
mi
Hp = 218
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12408221
41 X = -3787420
87
Y = -5938055
76 feet Y = -1852242
39 meter
Z = 17502764
43 Z = 5316456
98
XDOT = 11950
076347 XDOT = 3715
965262
YDOT = -22109
737267 feet/sec YDOT = -6697
905094 meter/sec
ZDOT = 1016
280447 ZDOT = 327
635376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12927830
44 X = 3940402
72
Y = 4974512
56 feet Y = 1516231
43 meter
Z = 17426894
51 Z = 5311717
45
XDOT = -9876
445739 XDOT = -3010
340661
YDOT = 22006
073315 feet/sec YDOT = 6707
451146 meter/sec
ZDOT = 1090
779812 ZDOT = 332
469687
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 12241
62660024
00016717 00000-0 10270-3 0 9126
2 25544 51
6452 120
9047 0015356 8
8309 351
3109 15
50119419 29285
Satellite: ISS
Catalog Number: 25544
Epoch time: 12241
62660024 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 120
9047 deg
Eccentricity:
0015356
Arg of perigee: 8
8309 deg
Mean anomaly: 351
3109 deg
Mean motion: 15
50119419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2928
Checksum: 285
Coasting Arc #14 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2012/242/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3742970
97 A = 6788958
57 meter
Y = 1891585
42 meter E =
0023396
Z = -5354129
15 I = 51
93911
XDOT = -3341
571152 Wp = 50
75479
YDOT = 6879
379734 meter/sec RA = 115
26749 deg
ZDOT = 109
116105 TA = 220
19671
MA = 220
36998
Ha = 231
813 n
mi
Hp = 217
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12280088
47 X = 3747549
33
Y = 6205988
90 feet Y = 1933466
98 meter
Z = -17566040
53 Z = -5335935
29
XDOT = -10963
159948 XDOT = -3418
779498
YDOT = 22570
143485 feet/sec YDOT = 6841
580514 meter/sec
ZDOT = 357
992472 ZDOT = 92
695345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12909130
72 X = -3934703
04
Y = -5030019
93 feet Y = -1533150
08 meter
Z = -17490966
08 Z = -5331246
46
XDOT = 8459
174150 XDOT = 2578
356281
YDOT = -22547
986881 feet/sec YDOT = -6872
626401 meter/sec
ZDOT = 289
478751 ZDOT = 88
233123
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 12242
59361792
00016717 00000-0 10270-3 0 9134
2 25544 51
6438 116
1121 0015372 12
1924 347
9595 15
50154117 29439
Satellite: ISS
Catalog Number: 25544
Epoch time: 12242
59361792 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 116
1121 deg
Eccentricity:
0015372
Arg of perigee: 12
1924 deg
Mean anomaly: 347
9595 deg
Mean motion: 15
50154117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 297
Coasting Arc #15 (Orbit 2958)
---------------------------------------
Vector Time (GMT): 2012/243/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3677201
03 A = 6789077
91 meter
Y = -2056952
97 meter E =
0017241
Z = 5318836
42 I = 51
95156
XDOT = 3069
646037 Wp = 23
25983
YDOT = -7001
925651 meter/sec RA = 110
32989 deg
ZDOT = -569
589168 TA = 72
24788
MA = 72
05979
Ha = 231
977 n
mi
Hp = 217
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12064307
86 X = -3679763
72
Y = -6748533
38 feet Y = -2098087
68 meter
Z = 17450250
72 Z = 5300966
98
XDOT = 10071
017183 XDOT = 3150
481764
YDOT = -22972
197018 feet/sec YDOT = -6967
147019 meter/sec
ZDOT = -1868
730866 ZDOT = -554
480391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12838143
52 X = 3913066
15
Y = 5370266
24 feet Y = 1636857
15 meter
Z = 17376529
81 Z = 5296366
29
XDOT = -7107
309111 XDOT = -2166
307817
YDOT = 23004
282410 feet/sec YDOT = 7011
705279 meter/sec
ZDOT = -1805
625334 ZDOT = -550
354602
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 12243
62509563
00016717 00000-0 10270-3 0 9140
2 25544 51
6438 111
0006 0015330 15
8834 344
2794 15
50142650 29596
Satellite: ISS
Catalog Number: 25544
Epoch time: 12243
62509563 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 111
0006 deg
Eccentricity:
0015330
Arg of perigee: 15
8834 deg
Mean anomaly: 344
2794 deg
Mean motion: 15
50142650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2959
Checksum: 290
Coasting Arc #16 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2012/244/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3692071
90 A = 6789201
63 meter
Y = 2166311
23 meter E =
0023092
Z = -5284545
16 I = 51
96029
XDOT = -2750
438992 Wp = 57
12092
YDOT = 7068
473426 meter/sec RA = 105
39246 deg
ZDOT = 991
309221 TA = 222
26095
MA = 222
43914
Ha = 231
978 n
mi
Hp = 217
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12113096
79 X = 3693244
13
Y = 7107320
30 feet Y = 2207604
37 meter
Z = -17337746
60 Z = -5266606
84
XDOT = -9023
749973 XDOT = -2834
091195
YDOT = 23190
529613 feet/sec YDOT = 7037
248664 meter/sec
ZDOT = 3252
326841 ZDOT = 977
744103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13021856
91 X = -3969061
99
Y = -5498432
20 feet Y = -1675922
14 meter
Z = -17263749
84 Z = -5261990
95
XDOT = 5626
946625 XDOT = 1715
093331
YDOT = -23201
186535 feet/sec YDOT = -7071
721656 meter/sec
ZDOT = 3195
592589 ZDOT = 974
016621
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 12244
59209704
00016717 00000-0 10270-3 0 9152
2 25544 51
6423 106
2075 0015325 19
6091 340
5646 15
50175115 29747
Satellite: ISS
Catalog Number: 25544
Epoch time: 12244
59209704 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 106
2075 deg
Eccentricity:
0015325
Arg of perigee: 19
6091 deg
Mean anomaly: 340
5646 deg
Mean motion: 15
50175115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 293
Coasting Arc #17 (Orbit 2989)
---------------------------------------
Vector Time (GMT): 2012/245/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3688900
88 A = 6789604
91 meter
Y = -2357405
77 meter E =
0019323
Z = 5184897
01 I = 51
96862
XDOT = 2470
373048 Wp = 30
33610
YDOT = -7109
697376 meter/sec RA = 100
45576 deg
ZDOT = -1456
352665 TA = 73
72617
MA = 73
51370
Ha = 232
119 n
mi
Hp = 217
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12102693
17 X = -3687452
52
Y = -7734270
88 feet Y = -2398648
75 meter
Z = 17010816
98 Z = 5166980
43
XDOT = 8104
898450 XDOT = 2556
766115
YDOT = -23325
778794 feet/sec YDOT = -7081
589217 meter/sec
ZDOT = -4778
059926 ZDOT = -1444
141290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13192473
90 X = 4021066
05
Y = 5895855
36 feet Y = 1797056
71 meter
Z = 16936928
42 Z = 5162375
78
XDOT = -4262
140335 XDOT = -1299
100374
YDOT = 23291
895295 feet/sec YDOT = 7099
369686 meter/sec
ZDOT = -4726
912624 ZDOT = -1440
762968
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 12245
62355675
00016717 00000-0 10270-3 0 9167
2 25544 51
6422 101
0955 0015289 23
1901 336
9936 15
50166286 29903
Satellite: ISS
Catalog Number: 25544
Epoch time: 12245
62355675 = yrday
fracday
Element set: 916
Inclination: 51
6422 deg
RA of node: 101
0955 deg
Eccentricity:
0015289
Arg of perigee: 23
1901 deg
Mean anomaly: 336
9936 deg
Mean motion: 15
50166286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2990
Checksum: 314
Coasting Arc #18 (Orbit 3004)
---------------------------------------
Vector Time (GMT): 2012/246/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3763583
90 A = 6789957
51 meter
Y = 2474962
28 meter E =
0022281
Z = -5094711
45 I = 51
97377
XDOT = -2156
131396 Wp = 61
99086
YDOT = 7097
336489 meter/sec RA = 95
51935 deg
ZDOT = 1871
427537 TA = 226
00954
MA = 226
19344
Ha = 232
125 n
mi
Hp = 216
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12347716
21 X = 3760377
46
Y = 8119955
00 feet Y = 2517030
59 meter
Z = -16714932
58 Z = -5076436
27
XDOT = -7073
921902 XDOT = -2244
425955
YDOT = 23285
224701 feet/sec YDOT = 7072
731789 meter/sec
ZDOT = 6139
854123 ZDOT = 1860
738033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13594046
83 X = -4143465
47
Y = -6009591
94 feet Y = -1831723
62 meter
Z = -16639574
26 Z = -5071742
24
XDOT = 2833
169391 XDOT = 863
550030
YDOT = -23135
225223 feet/sec YDOT = -7051
616648 meter/sec
ZDOT = 6094
992284 ZDOT = 1857
753648
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 12246
59054168
00016717 00000-0 10270-3 0 9178
2 25544 51
6414 96
3022 0015292 27
1946 333
0002 15
50197488 30050
Satellite: ISS
Catalog Number: 25544
Epoch time: 12246
59054168 = yrday
fracday
Element set: 917
Inclination: 51
6414 deg
RA of node: 96
3022 deg
Eccentricity:
0015292
Arg of perigee: 27
1946 deg
Mean anomaly: 333
0002 deg
Mean motion: 15
50197488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3005
Checksum: 292
Coasting Arc #19 (Orbit 3020)
---------------------------------------
Vector Time (GMT): 2012/247/13:51:48
140
Vector Time (MET): N/A
Weight (LBS) : 954312
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3826481
94 A = 6790632
81 meter
Y = -2669655
33 meter E =
0021418
Z = 4928270
32 I = 51
97779
XDOT = 1893
324267 Wp = 39
10930
YDOT = -7053
991266 meter/sec RA = 90
58336 deg
ZDOT = -2329
431916 TA = 73
69688
MA = 73
46142
Ha = 232
249 n
mi
Hp = 216
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12554074
62 X = -3820285
29
Y = -8758711
71 feet Y = -2712410
32 meter
Z = 16168865
89 Z = 4909696
80
XDOT = 6211
693791 XDOT = 1983
378574
YDOT = -23143
015964 feet/sec YDOT = -7032
315635 meter/sec
ZDOT = -7642
493163 ZDOT = -2320
014839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14008812
64 X = 4269886
09
Y = 6367357
69 feet Y = 1940770
62 meter
Z = 16092295
33 Z = 4904931
62
XDOT = -1577
454260 XDOT = -480
808059
YDOT = 22866
100888 feet/sec YDOT = 6969
587551 meter/sec
ZDOT = -7602
886299 ZDOT = -2317
359744
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 12247
62198335
00016717 00000-0 10270-3 0 9189
2 25544 51
6413 91
1898 0015268 30
7626 329
4417 15
50190888 30215
Satellite: ISS
Catalog Number: 25544
Epoch time: 12247
62198335 = yrday
fracday
Element set: 918
Inclination: 51
6413 deg
RA of node: 91
1898 deg
Eccentricity:
0015268
Arg of perigee: 30
7626 deg
Mean anomaly: 329
4417 deg
Mean motion: 15
50190888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3021
Checksum: 318
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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