[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 19th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 3628)
---------------------------------------
Vector Time (GMT): 2011/138/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5076780
32 A = 6728011
15 meter
Y = -4185867
01 meter E =
0011839
Z = 1371454
01 I = 51
40661
XDOT = 2184
595424 Wp = 47
94873
YDOT = 4561
770480 meter/sec RA = 310
91842 deg
ZDOT = 5812
124693 TA = 327
18446
MA = 327
25793
Ha = 187
116 n
mi
Hp = 183
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16656103
40 X = 5116547
82
Y = -13733159
47 feet Y = -4128873
20 meter
Z = 4499521
02 Z = 1396213
30
XDOT = 7167
307820 XDOT = 2105
187924
YDOT = 14966
438582 feet/sec YDOT = 4585
755175 meter/sec
ZDOT = 19068
650566 ZDOT = 5822
545302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18937773
78 X = -5772233
45
Y = 10318558
20 feet Y = 3145096
54 meter
Z = 4599915
19 Z = 1402054
15
XDOT = -3324
147850 XDOT = -1013
200265
YDOT = -14654
786349 feet/sec YDOT = -4466
778879 meter/sec
ZDOT = 19110
576754 ZDOT = 5824
903795
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 11138
87651251
00016717 00000-0 10270-3 0 9006
2 25544 51
6474 311
1990 0003533 286
6214 73
4561 15
75165424 36292
Satellite: ISS
Catalog Number: 25544
Epoch time: 11138
87651251 = yrday
fracday
Element set: 900
Inclination: 51
6474 deg
RA of node: 311
1990 deg
Eccentricity:
0003533
Arg of perigee: 286
6214 deg
Mean anomaly: 73
4561 deg
Mean motion: 15
75165424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3629
Checksum: 302
Coasting Arc #2 (Orbit 3643)
---------------------------------------
Vector Time (GMT): 2011/139/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1876404
74 A = 6718011
25 meter
Y = -4157136
39 meter E =
0009195
Z = -4940790
53 I = 51
35417
XDOT = 5550
291393 Wp = 102
82100
YDOT = -4926
025413 meter/sec RA = 305
72510 deg
ZDOT = 2038
006744 TA = 186
99286
MA = 187
00570
Ha = 187
074 n
mi
Hp = 183
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6156183
54 X = -1805777
80
Y = -13638898
93 feet Y = -4177723
90 meter
Z = -16209942
67 Z = -4949735
18
XDOT = 18209
617430 XDOT = 5595
062324
YDOT = -16161
500700 feet/sec YDOT = -4863
708645 meter/sec
ZDOT = 6686
373832 ZDOT = 2065
078260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3603014
90 X = 1098198
94
Y = 14483394
03 feet Y = 4414538
50 meter
Z = -16245922
02 Z = -4951757
03
XDOT = -19639
280935 XDOT = -5986
052829
YDOT = 12504
539596 feet/sec YDOT = 3811
383669 meter/sec
ZDOT = 6796
164678 ZDOT = 2071
470994
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 11139
82811664
00016717 00000-0 10270-3 0 9019
2 25544 51
6474 306
3037 0003655 291
0084 69
0689 15
75230191 36443
Satellite: ISS
Catalog Number: 25544
Epoch time: 11139
82811664 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 306
3037 deg
Eccentricity:
0003655
Arg of perigee: 291
0084 deg
Mean anomaly: 69
0689 deg
Mean motion: 15
75230191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3644
Checksum: 306
Coasting Arc #3 (Orbit 3659)
---------------------------------------
Vector Time (GMT): 2011/140/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4620203
84 A = 6726308
79 meter
Y = 4365237
41 meter E =
0002970
Z = -2195891
27 I = 51
36666
XDOT = -2121
856414 Wp = 161
87712
YDOT = -4992
262752 meter/sec RA = 300
59688 deg
ZDOT = -5464
503711 TA = 42
83210
MA = 42
80897
Ha = 187
092 n
mi
Hp = 182
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15158149
09 X = -4658006
13
Y = 14321645
05 feet Y = 4313360
42 meter
Z = -7204367
68 Z = -2218427
47
XDOT = -6961
471176 XDOT = -2039
328690
YDOT = -16378
814803 feet/sec YDOT = -5015
528470 meter/sec
ZDOT = -17928
161782 ZDOT = -5474
611904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17168109
10 X = 5232839
65
Y = -11781746
52 feet Y = -3591076
34 meter
Z = -7295779
13 Z = -2223753
48
XDOT = 3349
224833 XDOT = 1020
843729
YDOT = 15997
953506 feet/sec YDOT = 4876
176228 meter/sec
ZDOT = -17968
813018 ZDOT = -5476
894208
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 11140
84313077
00016717 00000-0 10270-3 0 9029
2 25544 51
6481 301
0821 0003599 296
7624 63
3171 15
75305166 36609
Satellite: ISS
Catalog Number: 25544
Epoch time: 11140
84313077 = yrday
fracday
Element set: 902
Inclination: 51
6481 deg
RA of node: 301
0821 deg
Eccentricity:
0003599
Arg of perigee: 296
7624 deg
Mean anomaly: 63
3171 deg
Mean motion: 15
75305166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3660
Checksum: 292
Coasting Arc #4 (Orbit 3675)
---------------------------------------
Vector Time (GMT): 2011/141/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1863967
60 A = 6719192
67 meter
Y = 4573958
79 meter E =
0007116
Z = 4554283
45 I = 51
32774
XDOT = -5023
411843 Wp = 39
17810
YDOT = 5022
159136 meter/sec RA = 295
38849 deg
ZDOT = -2979
907935 TA = 80
56449
MA = 80
48405
Ha = 187
030 n
mi
Hp = 182
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6115379
27 X = 1790558
35
Y = 15006426
47 feet Y = 4594391
81 meter
Z = 14941874
85 Z = 4563160
82
XDOT = -16481
009985 XDOT = -5064
721419
YDOT = 16476
900051 feet/sec YDOT = 4965
753675 meter/sec
ZDOT = -9776
600836 ZDOT = -3004
411360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3875626
13 X = -1181290
84
Y = -15700385
96 feet Y = -4785477
64 meter
Z = 14977574
09 Z = 4565164
58
XDOT = 17412
994164 XDOT = 5307
480621
YDOT = -13744
620302 feet/sec YDOT = -4189
360268 meter/sec
ZDOT = -9876
003382 ZDOT = -3010
205831
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 11141
85811106
00016717 00000-0 10270-3 0 9038
2 25544 51
6474 295
8606 0003768 301
3038 58
7757 15
75371746 36764
Satellite: ISS
Catalog Number: 25544
Epoch time: 11141
85811106 = yrday
fracday
Element set: 903
Inclination: 51
6474 deg
RA of node: 295
8606 deg
Eccentricity:
0003768
Arg of perigee: 301
3038 deg
Mean anomaly: 58
7757 deg
Mean motion: 15
75371746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3676
Checksum: 326
Coasting Arc #5 (Orbit 3691)
---------------------------------------
Vector Time (GMT): 2011/142/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4159086
49 A = 6724296
66 meter
Y = -4343282
32 meter E =
0010963
Z = 2995503
07 I = 51
33255
XDOT = 2180
371085 Wp = 70
01078
YDOT = 5500
469942 meter/sec RA = 290
26742 deg
ZDOT = 4937
089044 TA = 324
81330
MA = 324
88564
Ha = 187
172 n
mi
Hp = 182
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13645296
90 X = 4192793
24
Y = -14249613
91 feet Y = -4296584
72 meter
Z = 9827765
98 Z = 3015789
29
XDOT = 7153
448441 XDOT = 2094
718322
YDOT = 18046
161226 feet/sec YDOT = 5524
372774 meter/sec
ZDOT = 16197
798700 ZDOT = 4947
473747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15226776
05 X = -4641121
34
Y = 12480644
51 feet Y = 3804100
45 meter
Z = 9910066
19 Z = 3020588
17
XDOT = -3886
037957 XDOT = -1184
464369
YDOT = -17664
046567 feet/sec YDOT = -5384
001394 meter/sec
ZDOT = 16239
561456 ZDOT = 4949
818332
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 11142
87306154
00016717 00000-0 10270-3 0 9044
2 25544 51
6471 290
6381 0003656 309
2057 50
8782 15
75373551 36923
Satellite: ISS
Catalog Number: 25544
Epoch time: 11142
87306154 = yrday
fracday
Element set: 904
Inclination: 51
6471 deg
RA of node: 290
6381 deg
Eccentricity:
0003656
Arg of perigee: 309
2057 deg
Mean anomaly: 50
8782 deg
Mean motion: 15
75373551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3692
Checksum: 311
Coasting Arc #6 (Orbit 3706)
---------------------------------------
Vector Time (GMT): 2011/143/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1973153
76 A = 6721023
61 meter
Y = -5023687
75 meter E =
0004074
Z = -4008465
30 I = 51
31361
XDOT = 4526
816095 Wp = 86
05820
YDOT = -4870
924909 meter/sec RA = 285
04853 deg
ZDOT = 3879
936303 TA = 224
13844
MA = 224
17096
Ha = 187
189 n
mi
Hp = 182
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6473601
57 X = -1897358
92
Y = -16481915
18 feet Y = -5045328
64 meter
Z = -13151132
86 Z = -4017867
15
XDOT = 14851
758843 XDOT = 4562
099291
YDOT = -15980
724768 feet/sec YDOT = -4820
106337 meter/sec
ZDOT = 12729
449812 ZDOT = 3902
012828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4625061
68 X = 1409718
80
Y = 17063814
37 feet Y = 5201050
62 meter
Z = -13188949
33 Z = -4019991
76
XDOT = -15130
077546 XDOT = -4611
647636
YDOT = 13999
728889 feet/sec YDOT = 4267
117365 meter/sec
ZDOT = 12819
014905 ZDOT = 3907
235743
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 11143
82454488
00016717 00000-0 10270-3 0 9055
2 25544 51
6481 285
7426 0003818 312
5914 47
4928 15
75446373 37072
Satellite: ISS
Catalog Number: 25544
Epoch time: 11143
82454488 = yrday
fracday
Element set: 905
Inclination: 51
6481 deg
RA of node: 285
7426 deg
Eccentricity:
0003818
Arg of perigee: 312
5914 deg
Mean anomaly: 47
4928 deg
Mean motion: 15
75446373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3707
Checksum: 331
Coasting Arc #7 (Orbit 3722)
---------------------------------------
Vector Time (GMT): 2011/144/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3778242
86 A = 6721661
54 meter
Y = 4096461
22 meter E =
0005476
Z = -3764780
39 I = 51
30890
XDOT = -2350
317755 Wp = 37
29812
YDOT = -6015
829209 meter/sec RA = 279
93037 deg
ZDOT = -4185
990552 TA = 188
52558
MA = 188
53488
Ha = 187
251 n
mi
Hp = 182
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12395809
92 X = -3805480
86
Y = 13439833
41 feet Y = 4054058
58 meter
Z = -12351641
68 Z = -3783200
97
XDOT = -7711
016255 XDOT = -2262
538140
YDOT = -19736
972472 feet/sec YDOT = -6041
620806 meter/sec
ZDOT = -13733
564803 ZDOT = -4197
195579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13457433
72 X = 4101825
80
Y = -12301668
35 feet Y = -3749548
51 meter
Z = -12426371
62 Z = -3787558
07
XDOT = 4963
220664 XDOT = 1512
789658
YDOT = 19351
521052 feet/sec YDOT = 5898
343617 meter/sec
ZDOT = -13778
641705 ZDOT = -4199
729992
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 11144
83942937
00016717 00000-0 10270-3 0 9069
2 25544 51
6475 280
5199 0003884 316
7223 43
3635 15
75502126 37234
Satellite: ISS
Catalog Number: 25544
Epoch time: 11144
83942937 = yrday
fracday
Element set: 906
Inclination: 51
6475 deg
RA of node: 280
5199 deg
Eccentricity:
0003884
Arg of perigee: 316
7223 deg
Mean anomaly: 43
3635 deg
Mean motion: 15
75502126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3723
Checksum: 317
Coasting Arc #8 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2011/145/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2165658
24 A = 6723063
34 meter
Y = 5465865
02 meter E =
0010687
Z = 3255037
69 I = 51
30874
XDOT = -4153
229079 Wp = 75
11106
YDOT = 4460
415992 meter/sec RA = 274
70784 deg
ZDOT = -4711
106664 TA = 66
53157
MA = 66
41927
Ha = 187
281 n
mi
Hp = 182
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7105177
97 X = 2088564
51
Y = 17932628
03 feet Y = 5489651
47 meter
Z = 10679257
53 Z = 3265371
57
XDOT = -13626
079655 XDOT = -4179
911860
YDOT = 14633
910734 feet/sec YDOT = 4413
823162 meter/sec
ZDOT = -15456
386694 ZDOT = -4731
347645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5751130
33 X = -1752944
52
Y = -18387422
83 feet Y = -5604486
48 meter
Z = 10720840
69 Z = 3267712
24
XDOT = 13196
276691 XDOT = 4022
225135
YDOT = -13216
929222 feet/sec YDOT = -4028
520027 meter/sec
ZDOT = -15538
495622 ZDOT = -4736
133466
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 11145
85428074
00016717 00000-0 10270-3 0 9074
2 25544 51
6462 275
2968 0004021 322
4395 37
6488 15
75569459 37394
Satellite: ISS
Catalog Number: 25544
Epoch time: 11145
85428074 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 275
2968 deg
Eccentricity:
0004021
Arg of perigee: 322
4395 deg
Mean anomaly: 37
6488 deg
Mean motion: 15
75569459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3739
Checksum: 342
Coasting Arc #9 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2011/146/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3513879
48 A = 6719070
97 meter
Y = -3637891
17 meter E =
0006225
Z = 4417778
06 I = 51
29350
XDOT = 2637
803359 Wp = 89
67629
YDOT = 6478
831200 meter/sec RA = 269
58509 deg
ZDOT = 3233
116992 TA = 327
78225
MA = 327
82027
Ha = 187
274 n
mi
Hp = 182
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11528475
98 X = 3532837
01
Y = -11935338
50 feet Y = -3598491
13 meter
Z = 14494022
50 Z = 4434894
41
XDOT = 8654
210497 XDOT = 2549
453778
YDOT = 21256
007875 feet/sec YDOT = 6507
834522 meter/sec
ZDOT = 10607
339213 ZDOT = 3245
717339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12066525
24 X = -3677876
89
Y = 11302199
06 feet Y = 3444910
27 meter
Z = 14563447
97 Z = 4438938
94
XDOT = -6610
894268 XDOT = -2015
000573
YDOT = -20807
753142 feet/sec YDOT = -6342
203158 meter/sec
ZDOT = 10658
057609 ZDOT = 3248
575959
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 11146
86910039
00016717 00000-0 10270-3 0 9084
2 25544 51
6457 270
0733 0004091 326
7521 33
3386 15
75585490 37557
Satellite: ISS
Catalog Number: 25544
Epoch time: 11146
86910039 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 270
0733 deg
Eccentricity:
0004091
Arg of perigee: 326
7521 deg
Mean anomaly: 33
3386 deg
Mean motion: 15
75585490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 315
Coasting Arc #10 (Orbit 3769)
---------------------------------------
Vector Time (GMT): 2011/147/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2455262
42 A = 6725025
29 meter
Y = -5802233
09 meter E =
0007854
Z = -2340668
03 I = 51
31628
XDOT = 3952
498179 Wp = 15
24852
YDOT = -3839
436331 meter/sec RA = 264
36944 deg
ZDOT = 5383
054541 TA = 318
25542
MA = 318
31532
Ha = 187
337 n
mi
Hp = 181
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8055322
88 X = -2378827
60
Y = -19036197
81 feet Y = -5829261
78 meter
Z = -7679357
04 Z = -2352410
57
XDOT = 12967
513710 XDOT = 3968
987575
YDOT = -12596
575889 feet/sec YDOT = -3795
145295 meter/sec
ZDOT = 17660
940095 ZDOT = 5402
295735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7307306
82 X = 2227267
12
Y = 19316829
75 feet Y = 5887769
71 meter
Z = -7726637
93 Z = -2355079
24
XDOT = -11904
975678 XDOT = -3628
636587
YDOT = 11583
922699 feet/sec YDOT = 3530
779639 meter/sec
ZDOT = 17738
972413 ZDOT = 5406
838791
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 11147
82046268
00016717 00000-0 10270-3 0 9096
2 25544 51
6462 265
1772 0004124 330
9581 29
1354 15
75663309 37702
Satellite: ISS
Catalog Number: 25544
Epoch time: 11147
82046268 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 265
1772 deg
Eccentricity:
0004124
Arg of perigee: 330
9581 deg
Mean anomaly: 29
1354 deg
Mean motion: 15
75663309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3770
Checksum: 312
Coasting Arc #11 (Orbit 3785)
---------------------------------------
Vector Time (GMT): 2011/148/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3445556
68 A = 6716737
98 meter
Y = 3014151
36 meter E =
0012750
Z = -4926355
85 I = 51
29170
XDOT = -2976
774003 Wp = 55
22692
YDOT = -6787
018062 meter/sec RA = 259
23449 deg
ZDOT = -2067
205284 TA = 194
61513
MA = 194
65203
Ha = 187
465 n
mi
Hp = 181
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11304319
80 X = -3455073
77
Y = 9888948
04 feet Y = 2975568
27 meter
Z = -16162584
82 Z = -4943117
43
XDOT = -9766
318909 XDOT = -2890
616789
YDOT = -22267
119626 feet/sec YDOT = -6819
824244 meter/sec
ZDOT = -6782
169568 ZDOT = -2081
457947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11396816
36 X = 3473749
63
Y = -9669021
15 feet Y = -2947117
65 meter
Z = -16230548
18 Z = -4947071
09
XDOT = 8586
799327 XDOT = 2617
256435
YDOT = 21620
761972 feet/sec YDOT = 6590
008249 meter/sec
ZDOT = -6839
573290 ZDOT = -2084
701939
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 11148
83521836
00016717 00000-0 10270-3 0 9109
2 25544 51
6452 259
9529 0004308 334
4085 25
6866 15
75686990 37861
Satellite: ISS
Catalog Number: 25544
Epoch time: 11148
83521836 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 259
9529 deg
Eccentricity:
0004308
Arg of perigee: 334
4085 deg
Mean anomaly: 25
6866 deg
Mean motion: 15
75686990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3786
Checksum: 344
Coasting Arc #12 (Orbit 3801)
---------------------------------------
Vector Time (GMT): 2011/149/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2745762
07 A = 6726489
95 meter
Y = 6011593
06 meter E =
0010717
Z = 1232366
91 I = 51
33206
XDOT = -3996
995260 Wp = 106
36960
YDOT = 3031
656536 meter/sec RA = 254
03335 deg
ZDOT = -5844
225570 TA = 60
05192
MA = 59
94555
Ha = 187
518 n
mi
Hp = 181
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9008405
73 X = 2672348
51
Y = 19723074
35 feet Y = 6041887
23 meter
Z = 4043198
53 Z = 1245528
32
XDOT = -13113
501509 XDOT = -4002
208180
YDOT = 9946
379710 feet/sec YDOT = 2986
931177 meter/sec
ZDOT = -19173
968406 ZDOT = -5863
655583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8940798
28 X = -2725155
32
Y = -19742886
79 feet Y = -6017631
89 meter
Z = 4096222
31 Z = 1248528
56
XDOT = 11580
343075 XDOT = 3529
688569
YDOT = -9265
021921 feet/sec YDOT = -2823
978681 meter/sec
ZDOT = -19252
735277 ZDOT = -5868
233713
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 11149
84994118
00016717 00000-0 10270-3 0 9119
2 25544 51
6451 254
7288 0004546 339
1971 20
9008 15
75761433 38026
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
84994118 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 254
7288 deg
Eccentricity:
0004546
Arg of perigee: 339
1971 deg
Mean anomaly: 20
9008 deg
Mean motion: 15
75761433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3802
Checksum: 319
Coasting Arc #13 (Orbit 3817)
---------------------------------------
Vector Time (GMT): 2011/150/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3591698
82 A = 6715204
38 meter
Y = -2264416
62 meter E =
0003166
Z = 5201073
86 I = 51
30328
XDOT = 3304
567142 Wp = 24
48295
YDOT = 6922
283038 meter/sec RA = 248
87994 deg
ZDOT = 734
442539 TA = 58
51796
MA = 58
48702
Ha = 187
450 n
mi
Hp = 181
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11783788
78 X = 3591486
80
Y = -7429188
37 feet Y = -2224253
90 meter
Z = 17063890
62 Z = 5218521
78
XDOT = 10841
755715 XDOT = 3223
347400
YDOT = 22710
902355 feet/sec YDOT = 6958
782498 meter/sec
ZDOT = 2409
588383 ZDOT = 750
299931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11568402
27 X = -3526049
01
Y = 7602904
83 feet Y = 2317365
39 meter
Z = 17134607
91 Z = 5222628
49
XDOT = -10612
426067 XDOT = -3234
667465
YDOT = -21702
336766 feet/sec YDOT = -6614
872246 meter/sec
ZDOT = 2473
492698 ZDOT = 753
920574
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 11150
86463268
00016717 00000-0 10270-3 0 9121
2 25544 51
6446 249
5047 0004613 342
0605 18
0396 15
75781444 38186
Satellite: ISS
Catalog Number: 25544
Epoch time: 11150
86463268 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 249
5047 deg
Eccentricity:
0004613
Arg of perigee: 342
0605 deg
Mean anomaly: 18
0396 deg
Mean motion: 15
75781444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3818
Checksum: 311
Coasting Arc #14 (Orbit 3832)
---------------------------------------
Vector Time (GMT): 2011/151/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2996570
82 A = 6726841
17 meter
Y = -6012747
05 meter E =
0015036
Z = -28280
13 I = 51
35549
XDOT = 4299
373250 Wp = 30
35342
YDOT = -2164
396117 meter/sec RA = 243
70257 deg
ZDOT = 6019
931335 TA = 329
33777
MA = 329
42556
Ha = 187
481 n
mi
Hp = 181
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9831269
09 X = -2928975
03
Y = -19726860
41 feet Y = -6045878
58 meter
Z = -92782
58 Z = -42674
33
XDOT = 14105
555282 XDOT = 4294
012316
YDOT = -7101
037128 feet/sec YDOT = -2116
348763 meter/sec
ZDOT = 19750
430890 ZDOT = 6040
804608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10460831
16 X = 3188461
34
Y = 19399993
57 feet Y = 5913118
04 meter
Z = -150807
90 Z = -45966
25
XDOT = -12336
223558 XDOT = -3760
080941
YDOT = 6784
104910 feet/sec YDOT = 2067
795176 meter/sec
ZDOT = 19835
015890 ZDOT = 6045
712843
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 11151
81587596
00016717 00000-0 10270-3 0 9139
2 25544 51
6444 244
6078 0004489 346
5144 13
5900 15
75876845 38330
Satellite: ISS
Catalog Number: 25544
Epoch time: 11151
81587596 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 244
6078 deg
Eccentricity:
0004489
Arg of perigee: 346
5144 deg
Mean anomaly: 13
5900 deg
Mean motion: 15
75876845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3833
Checksum: 333
Coasting Arc #15 (Orbit 3848)
---------------------------------------
Vector Time (GMT): 2011/152/19:34:43
830
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3968644
09 A = 6714915
42 meter
Y = 1508981
26 meter E =
0014345
Z = -5213878
88 I = 51
33002
XDOT = -3508
767553 Wp = 76
67734
YDOT = -6811
251328 meter/sec RA = 238
52594 deg
ZDOT = 704
360627 TA = 200
02793
MA = 200
08428
Ha = 187
653 n
mi
Hp = 180
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13020485
87 X = -3959894
55
Y = 4950725
92 feet Y = 1464651
23 meter
Z = -17105901
85 Z = -5233137
24
XDOT = -11511
704569 XDOT = -3435
763736
YDOT = -22346
625091 feet/sec YDOT = -6850
080423 meter/sec
ZDOT = 2310
894447 ZDOT = 687
491112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12657364
76 X = 3857964
78
Y = -5581958
60 feet Y = -1701380
98 meter
Z = -17183930
67 Z = -5237662
07
XDOT = 12208
103973 XDOT = 3721
030091
YDOT = 20826
925926 feet/sec YDOT = 6348
047022 meter/sec
ZDOT = 2242
871576 ZDOT = 683
627256
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 11152
83050526
00016717 00000-0 10270-3 0 9141
2 25544 51
6445 239
3830 0004796 350
1618 9
9451 15
75874230 38499
Satellite: ISS
Catalog Number: 25544
Epoch time: 11152
83050526 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 239
3830 deg
Eccentricity:
0004796
Arg of perigee: 350
1618 deg
Mean anomaly: 9
9451 deg
Mean motion: 15
75874230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3849
Checksum: 314
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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