[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 15th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
077/06:07:32
851 -1
4 6
5 6
6
N/A -6
4 -1
0 193
6
000/00:15:01
703 0
3 0
5 187
2
Coasting Arc #1 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2011/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4128245
16 A = 6729788
61 meter
Y = 3902840
32 meter E =
0010932
Z = -3620045
73 I = 51
31654
XDOT = -1901
105256 Wp = 69
20824
YDOT = -6044
140774 meter/sec RA = 285
93045 deg
ZDOT = -4355
102054 TA = 154
29656
MA = 154
24219
Ha = 193
784 n
mi
Hp = 183
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13544111
43 X = -4153995
42
Y = 12804594
22 feet Y = 3856531
63 meter
Z = -11876790
44 Z = -3640163
12
XDOT = -6237
221969 XDOT = -1812
221300
YDOT = -19829
858184 feet/sec YDOT = -6064
903317 meter/sec
ZDOT = -14288
392567 ZDOT = -4364
121277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15314728
84 X = -4667929
35
Y = 10531960
89 feet Y = 3210141
68 meter
Z = -11958077
57 Z = -3644822
04
XDOT = -2196
502356 XDOT = -669
493918
YDOT = -19433
183398 feet/sec YDOT = -5923
234300 meter/sec
ZDOT = -14324
649970 ZDOT = -4366
153311
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 11073
52411238
00016717 00000-0 10270-3 0 9005
2 25544 51
6445 286
4886 0005516 58
6833 301
4869 15
72815969 26001
Satellite: ISS
Catalog Number: 25544
Epoch time: 11073
52411238 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 286
4886 deg
Eccentricity:
0005516
Arg of perigee: 58
6833 deg
Mean anomaly: 301
4869 deg
Mean motion: 15
72815969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 320
Coasting Arc #2 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2011/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2379040
42 A = 6728132
00 meter
Y = 4819283
22 meter E =
0015976
Z = 4038094
88 I = 51
30479
XDOT = -4121
183529 Wp = 71
41920
YDOT = 5260
329738 meter/sec RA = 280
72822 deg
ZDOT = -3832
563484 TA = 58
25969
MA = 58
10410
Ha = 193
581 n
mi
Hp = 183
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7805250
73 X = 2305357
53
Y = 15811296
65 feet Y = 4845475
36 meter
Z = 13248342
79 Z = 4049472
76
XDOT = -13520
943337 XDOT = -4161
081718
YDOT = 17258
299664 feet/sec YDOT = 5214
020849 meter/sec
ZDOT = -12574
027178 ZDOT = -3852
681016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5438368
93 X = 1657614
85
Y = 16736997
93 feet Y = 5101436
97 meter
Z = 13294159
29 Z = 4052059
75
XDOT = -14506
673272 XDOT = -4421
634013
YDOT = 14810
988940 feet/sec YDOT = 4514
389429 meter/sec
ZDOT = -12655
341772 ZDOT = -3857
348172
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 11074
54068633
00016717 00000-0 10270-3 0 9016
2 25544 51
6448 281
2767 0005432 60
7467 299
4238 15
72913418 26160
Satellite: ISS
Catalog Number: 25544
Epoch time: 11074
54068633 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 281
2767 deg
Eccentricity:
0005432
Arg of perigee: 60
7467 deg
Mean anomaly: 299
4238 deg
Mean motion: 15
72913418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 320
Coasting Arc #3 (Orbit 2631)
---------------------------------------
Vector Time (GMT): 2011/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2977740
78 A = 6731032
07 meter
Y = -5189094
91 meter E =
0018236
Z = 3064793
81 I = 51
30877
XDOT = 3445
265019 Wp = 79
10884
YDOT = 4870
146163 meter/sec RA = 275
62699 deg
ZDOT = 4877
251415 TA = 316
63266
MA = 316
77600
Ha = 193
512 n
mi
Hp = 183
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9769490
74 X = 3020657
02
Y = -17024589
59 feet Y = -5155555
79 meter
Z = 10055097
81 Z = 3079364
04
XDOT = 11303
362922 XDOT = 3366
857767
YDOT = 15978
169826 feet/sec YDOT = 4908
235213 meter/sec
ZDOT = 16001
481020 ZDOT = 4893
797292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11726507
92 X = 3574239
61
Y = -15702876
99 feet Y = -4786236
91 meter
Z = 10114012
97 Z = 3082751
15
XDOT = 8015
107371 XDOT = 2443
004727
YDOT = 16379
170456 feet/sec YDOT = 4992
371155 meter/sec
ZDOT = 16068
167187 ZDOT = 4897
577359
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 11075
55722508
00016717 00000-0 10270-3 0 9027
2 25544 51
6432 276
0645 0005345 65
2904 294
8814 15
72952438 26321
Satellite: ISS
Catalog Number: 25544
Epoch time: 11075
55722508 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 276
0645 deg
Eccentricity:
0005345
Arg of perigee: 65
2904 deg
Mean anomaly: 294
8814 deg
Mean motion: 15
72952438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2632
Checksum: 312
Coasting Arc #4 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2011/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3533402
83 A = 6726408
36 meter
Y = -3624872
50 meter E =
0014186
Z = -4442406
76 I = 51
29058
XDOT = 2619
689925 Wp = 95
92520
YDOT = -6476
907743 meter/sec RA = 270
42571 deg
ZDOT = 3208
669265 TA = 206
37159
MA = 206
44386
Ha = 193
548 n
mi
Hp = 183
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11592528
96 X = -3471026
24
Y = -11892626
31 feet Y = -3664036
87 meter
Z = -14574825
33 Z = -4459419
77
XDOT = 8594
783218 XDOT = 2676
334421
YDOT = -21249
697319 feet/sec YDOT = -6447
295715 meter/sec
ZDOT = 10527
130133 ZDOT = 3221
533749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10183252
62 X = -3103855
40
Y = -13042933
66 feet Y = -3975486
18 meter
Z = -14643430
93 Z = -4463317
75
XDOT = 9779
346739 XDOT = 2980
744886
YDOT = -19485
595298 feet/sec YDOT = -5939
209447 meter/sec
ZDOT = 10579
174803 ZDOT = 3224
532480
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 11076
51019644
00016717 00000-0 10270-3 0 9035
2 25544 51
6420 271
1771 0005442 69
3235 290
8510 15
72993596 26479
Satellite: ISS
Catalog Number: 25544
Epoch time: 11076
51019644 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 271
1771 deg
Eccentricity:
0005442
Arg of perigee: 69
3235 deg
Mean anomaly: 290
8510 deg
Mean motion: 15
72993596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 308
Coasting Arc #5 (Orbit 2658)
---------------------------------------
Vector Time (GMT): 2011/077/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4060258
62 A = 6728269
42 meter
Y = -2239167
94 meter E =
0012092
Z = -4886464
76 I = 51
28742
XDOT = 1334
650615 Wp = 100
55085
YDOT = -7240
864351 meter/sec RA = 266
51319 deg
ZDOT = 2211
521456 TA = 191
06912
MA = 191
09574
Ha = 193
645 n
mi
Hp = 187
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13321058
46 X = -4011180
91
Y = -7346351
52 feet Y = -2284298
43 meter
Z = -16031708
52 Z = -4906069
65
XDOT = 4378
774982 XDOT = 1404
777160
YDOT = -23756
116637 feet/sec YDOT = -7225
547100 meter/sec
ZDOT = 7255
647821 ZDOT = 2218
176321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7702935
31 X = 2347854
68
Y = -13020825
86 feet Y = -3968747
72 meter
Z = -16110805
04 Z = -4910573
37
XDOT = 22680
028867 XDOT = 6912
872799
YDOT = 4416
255446 feet/sec YDOT = 1346
074660 meter/sec
ZDOT = 7282
632171 ZDOT = 2219
746286
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 11077
27255376
00016717 00000-0 10270-3 0 9044
2 25544 51
6444 267
2679 0001280 356
6991 3
4162 15
71708683 26599
Satellite: ISS
Catalog Number: 25544
Epoch time: 11077
27255376 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 267
2679 deg
Eccentricity:
0001280
Arg of perigee: 356
6991 deg
Mean anomaly: 3
4162 deg
Mean motion: 15
71708683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2659
Checksum: 327
Coasting Arc #6 (Orbit 2674)
---------------------------------------
Vector Time (GMT): 2011/078/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -18445
62 A = 6737911
90 meter
Y = 6616205
21 meter E =
0008062
Z = -1258676
27 I = 51
32355
XDOT = -4891
832959 Wp = 137
57811
YDOT = -1118
175579 meter/sec RA = 261
40047 deg
ZDOT = -5833
573933 TA = 56
27244
MA = 56
19562
Ha = 193
600 n
mi
Hp = 187
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -60517
11 X = -86313
56
Y = 21706710
00 feet Y = 6615619
29 meter
Z = -4129515
33 Z = -1258931
64
XDOT = -16049
320731 XDOT = -4850
627625
YDOT = -3668
555049 feet/sec YDOT = -1172
649436 meter/sec
ZDOT = -19139
022089 ZDOT = -5857
237924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21705125
63 X = -6615722
29
Y = -251163
45 feet Y = -76554
62 meter
Z = -4130648
45 Z = -1259021
65
XDOT = 3808
892107 XDOT = 1160
950314
YDOT = -14314
618751 feet/sec YDOT = -4363
095795 meter/sec
ZDOT = -19234
523770 ZDOT = -5862
682845
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 11078
28985054
00016717 00000-0 10270-3 0 9050
2 25544 51
6447 262
0610 0001258 356
7463 3
3691 15
71744634 26750
Satellite: ISS
Catalog Number: 25544
Epoch time: 11078
28985054 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 262
0610 deg
Eccentricity:
0001258
Arg of perigee: 356
7463 deg
Mean anomaly: 3
3691 deg
Mean motion: 15
71744634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2675
Checksum: 314
Coasting Arc #7 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2011/079/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4231368
19 A = 6726341
13 meter
Y = -301937
66 meter E =
0003680
Z = 5218044
56 I = 51
29124
XDOT = 1326
494775 Wp = 43
05720
YDOT = 7557
946575 meter/sec RA = 256
24036 deg
ZDOT = -635
417626 TA = 53
03034
MA = 52
99665
Ha = 193
291 n
mi
Hp = 187
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13882441
58 X = 4209081
86
Y = -990609
11 feet Y = -254743
84 meter
Z = 17119568
75 Z = 5238546
33
XDOT = 4352
016979 XDOT = 1244
968517
YDOT = 24796
412647 feet/sec YDOT = 7572
324321 meter/sec
ZDOT = -2084
703496 ZDOT = -629
172590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1090244
31 X = 332306
47
Y = 13772232
51 feet Y = 4197776
47 meter
Z = 17202328
45 Z = 5243269
71
XDOT = -23759
610127 XDOT = -7241
929167
YDOT = 4465
335056 feet/sec YDOT = 1361
034125 meter/sec
ZDOT = -2059
605401 ZDOT = -627
767726
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 11079
30710994
00016717 00000-0 10270-3 0 9064
2 25544 51
6445 256
8540 0001442 355
1412 4
9736 15
71855930 26910
Satellite: ISS
Catalog Number: 25544
Epoch time: 11079
30710994 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 256
8540 deg
Eccentricity:
0001442
Arg of perigee: 355
1412 deg
Mean anomaly: 4
9736 deg
Mean motion: 15
71855930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 308
Coasting Arc #8 (Orbit 2705)
---------------------------------------
Vector Time (GMT): 2011/080/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2287066
06 A = 6738231
03 meter
Y = -6329532
38 meter E =
0013103
Z = -142125
03 I = 51
34049
XDOT = 4483
308465 Wp = 39
38910
YDOT = -1747
887071 meter/sec RA = 251
10157 deg
ZDOT = 6009
761497 TA = 319
06155
MA = 319
15986
Ha = 193
442 n
mi
Hp = 187
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7503497
57 X = -2215427
63
Y = -20766182
35 feet Y = -6354707
20 meter
Z = -466289
48 Z = -153060
85
XDOT = 14709
017272 XDOT = 4473
326153
YDOT = -5734
537636 feet/sec YDOT = -1697
807125 meter/sec
ZDOT = 19717
065280 ZDOT = 6031
517334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20576357
63 X = 6271673
81
Y = -8006702
63 feet Y = -2440442
96 meter
Z = -510343
40 Z = -155552
67
XDOT = 5505
381582 XDOT = 1678
040306
YDOT = 12945
638397 feet/sec YDOT = 3945
830583 meter/sec
ZDOT = 19804
908913 ZDOT = 6036
536237
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 11080
26076057
00016717 00000-0 10270-3 0 9077
2 25544 51
6452 251
9720 0001562
1689 359
9474 15
71870847 27063
Satellite: ISS
Catalog Number: 25544
Epoch time: 11080
26076057 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 251
9720 deg
Eccentricity:
0001562
Arg of perigee:
1689 deg
Mean anomaly: 359
9474 deg
Mean motion: 15
71870847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2706
Checksum: 314
Coasting Arc #9 (Orbit 2721)
---------------------------------------
Vector Time (GMT): 2011/081/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3382755
73 A = 6726240
56 meter
Y = 2632231
17 meter E =
0014946
Z = -5196684
76 I = 51
31240
XDOT = -3761
930129 Wp = 76
61127
YDOT = -6640
592846 meter/sec RA = 245
96890 deg
ZDOT = -913
589627 TA = 184
62349
MA = 184
63731
Ha = 193
376 n
mi
Hp = 186
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11098279
95 X = -3386693
85
Y = 8635929
02 feet Y = 2594380
67 meter
Z = -17049490
68 Z = -5213127
99
XDOT = -12342
290448 XDOT = -3682
956102
YDOT = -21786
721936 feet/sec YDOT = -6682
219541 meter/sec
ZDOT = -2997
341297 ZDOT = -931
672688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9085997
59 X = -2769412
07
Y = -10626696
42 feet Y = -3239017
07 meter
Z = -17115904
63 Z = -5216927
73
XDOT = 20479
415698 XDOT = 6242
125905
YDOT = -12558
808968 feet/sec YDOT = -3827
924973 meter/sec
ZDOT = -3070
245217 ZDOT = -935
810742
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 11081
27795088
00016717 00000-0 10270-3 0 9082
2 25544 51
6458 246
7647 0001672 2
2542 357
8627 15
71950782 27224
Satellite: ISS
Catalog Number: 25544
Epoch time: 11081
27795088 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 246
7647 deg
Eccentricity:
0001672
Arg of perigee: 2
2542 deg
Mean anomaly: 357
8627 deg
Mean motion: 15
71950782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2722
Checksum: 330
Coasting Arc #10 (Orbit 2737)
---------------------------------------
Vector Time (GMT): 2011/082/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4156441
60 A = 6737091
99 meter
Y = 5098732
15 meter E =
0013500
Z = 1427976
01 I = 51
36254
XDOT = -3013
661057 Wp = 112
65631
YDOT = 4087
778731 meter/sec RA = 240
80605 deg
ZDOT = -5785
540252 TA = 51
58531
MA = 51
46417
Ha = 193
391 n
mi
Hp = 186
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13636619
41 X = 4092180
84
Y = 16728123
85 feet Y = 5144852
78 meter
Z = 4684960
65 Z = 1448011
59
XDOT = -9887
339425 XDOT = -3031
042288
YDOT = 13411
347543 feet/sec YDOT = 4053
980610 meter/sec
ZDOT = -18981
431272 ZDOT = -5800
223080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15898414
82 X = -4845836
84
Y = 14569288
88 feet Y = 4440719
25 meter
Z = 4765773
88 Z = 1452607
88
XDOT = -12900
149515 XDOT = -3931
965572
YDOT = -7808
096844 feet/sec YDOT = -2379
907918 meter/sec
ZDOT = -19040
762870 ZDOT = -5803
624523
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 11082
29510583
00016717 00000-0 10270-3 0 9091
2 25544 51
6457 241
5575 0001608 6
8163 353
3020 15
71954346 27389
Satellite: ISS
Catalog Number: 25544
Epoch time: 11082
29510583 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 241
5575 deg
Eccentricity:
0001608
Arg of perigee: 6
8163 deg
Mean anomaly: 353
3020 deg
Mean motion: 15
71954346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2738
Checksum: 304
Coasting Arc #11 (Orbit 2753)
---------------------------------------
Vector Time (GMT): 2011/083/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1730006
34 A = 6727543
18 meter
Y = -4334426
64 meter E =
0006288
Z = 4841004
64 I = 51
34721
XDOT = 5539
899301 Wp = 106
04990
YDOT = 4816
215105 meter/sec RA = 235
69751 deg
ZDOT = 2328
246863 TA = 321
15158
MA = 321
19677
Ha = 193
254 n
mi
Hp = 186
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5675873
82 X = 1754829
49
Y = -14220559
85 feet Y = -4314941
66 meter
Z = 15882561
17 Z = 4849469
47
XDOT = 18175
522640 XDOT = 5474
321561
YDOT = 15801
230658 feet/sec YDOT = 4877
799049 meter/sec
ZDOT = 7638
605195 ZDOT = 2355
000115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14603009
19 X = 4450997
20
Y = 4483674
75 feet Y = 1366624
06 meter
Z = 15916796
12 Z = 4851439
46
XDOT = -14050
723138 XDOT = -4282
660412
YDOT = 18213
360613 feet/sec YDOT = 5551
432315 meter/sec
ZDOT = 7746
552410 ZDOT = 2361
149174
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 11083
31222099
00016717 00000-0 10270-3 0 9109
2 25544 51
6459 236
3497 0001865 7
1290 352
9899 15
72035965 27541
Satellite: ISS
Catalog Number: 25544
Epoch time: 11083
31222099 = yrday
fracday
Element set: 910
Inclination: 51
6459 deg
RA of node: 236
3497 deg
Eccentricity:
0001865
Arg of perigee: 7
1290 deg
Mean anomaly: 352
9899 deg
Mean motion: 15
72035965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2754
Checksum: 324
Coasting Arc #12 (Orbit 2768)
---------------------------------------
Vector Time (GMT): 2011/084/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5323754
89 A = 6734599
04 meter
Y = -3202689
29 meter E =
0006503
Z = -2595121
48 I = 51
38944
XDOT = 814
156774 Wp = 40
05566
YDOT = -5583
278975 meter/sec RA = 230
51626 deg
ZDOT = 5232
399487 TA = 290
38984
MA = 290
45968
Ha = 193
161 n
mi
Hp = 186
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17466387
44 X = -5274939
59
Y = -10507510
80 feet Y = -3261949
89 meter
Z = -8514178
07 Z = -2620865
41
XDOT = 2671
118026 XDOT = 851
111680
YDOT = -18317
844407 feet/sec YDOT = -5573
967776 meter/sec
ZDOT = 17166
664984 ZDOT = 5236
444586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8839823
34 X = 2694378
16
Y = -18318292
54 feet Y = -5583415
57 meter
Z = -8618084
66 Z = -2626792
20
XDOT = 17140
972549 XDOT = 5224
568433
YDOT = 206
235354 feet/sec YDOT = 62
860536 meter/sec
ZDOT = 17183
071706 ZDOT = 5237
400256
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 11084
26573175
00016717 00000-0 10270-3 0 9119
2 25544 51
6454 231
4672 0002028 3
5893 356
5284 15
72097114 27696
Satellite: ISS
Catalog Number: 25544
Epoch time: 11084
26573175 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 231
4672 deg
Eccentricity:
0002028
Arg of perigee: 3
5893 deg
Mean anomaly: 356
5284 deg
Mean motion: 15
72097114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2769
Checksum: 309
Coasting Arc #13 (Orbit 2784)
---------------------------------------
Vector Time (GMT): 2011/085/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 349082
47 A = 6729575
98 meter
Y = 5203954
10 meter E =
0009499
Z = -4262630
45 I = 51
39235
XDOT = -6375
130248 Wp = 58
45136
YDOT = -2459
337629 meter/sec RA = 225
42424 deg
ZDOT = -3525
400982 TA = 175
62632
MA = 175
61801
Ha = 193
138 n
mi
Hp = 186
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1145283
70 X = 311571
78
Y = 17073340
23 feet Y = 5207647
86 meter
Z = -13985008
04 Z = -4261025
93
XDOT = -20915
781655 XDOT = -6330
030079
YDOT = -8068
693009 feet/sec YDOT = -2530
376159 meter/sec
ZDOT = -11566
276188 ZDOT = -3556
261384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16833150
50 X = -5130744
27
Y = 3104037
97 feet Y = 946110
77 meter
Z = -13978593
06 Z = -4260675
16
XDOT = 5947
601775 XDOT = 1812
829021
YDOT = -20381
379966 feet/sec YDOT = -6212
244614 meter/sec
ZDOT = -11690
867108 ZDOT = -3563
376294
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 11085
28277315
00016717 00000-0 10270-3 0 9120
2 25544 51
6446 226
2589 0002056 3
9869 356
1309 15
72152996 27856
Satellite: ISS
Catalog Number: 25544
Epoch time: 11085
28277315 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 226
2589 deg
Eccentricity:
0002056
Arg of perigee: 3
9869 deg
Mean anomaly: 356
1309 deg
Mean motion: 15
72152996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2785
Checksum: 330
Coasting Arc #14 (Orbit 2800)
---------------------------------------
Vector Time (GMT): 2011/086/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5626591
92 A = 6731618
92 meter
Y = 1074979
73 meter E =
0012755
Z = 3527644
61 I = 51
42309
XDOT = 1649
563246 Wp = 76
96759
YDOT = 6055
848869 meter/sec RA = 220
23551 deg
ZDOT = -4460
096622 TA = 60
90808
MA = 60
78042
Ha = 192
971 n
mi
Hp = 186
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18459947
23 X = 5597016
69
Y = 3526836
37 feet Y = 1137734
49 meter
Z = 11573637
17 Z = 3554906
31
XDOT = 5411
952907 XDOT = 1603
389029
YDOT = 19868
270569 feet/sec YDOT = 6074
036900 meter/sec
ZDOT = -14632
862934 ZDOT = -4452
195601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1156577
22 X = -352524
74
Y = 18689841
87 feet Y = 5696663
80 meter
Z = 11683725
59 Z = 3561199
56
XDOT = -17642
687428 XDOT = -5377
491128
YDOT = 8069
103299 feet/sec YDOT = 2459
462686 meter/sec
ZDOT = -14601
022229 ZDOT = -4450
391575
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 11086
29977495
00016717 00000-0 10270-3 0 9139
2 25544 51
6448 221
0503 0002283 7
4395 352
6801 15
72263602 28016
Satellite: ISS
Catalog Number: 25544
Epoch time: 11086
29977495 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 221
0503 deg
Eccentricity:
0002283
Arg of perigee: 7
4395 deg
Mean anomaly: 352
6801 deg
Mean motion: 15
72263602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2801
Checksum: 299
Coasting Arc #15 (Orbit 2816)
---------------------------------------
Vector Time (GMT): 2011/087/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2506790
16 A = 6731852
08 meter
Y = -5170695
30 meter E =
0012877
Z = 3494079
43 I = 51
44659
XDOT = 6252
109661 Wp = 81
83916
YDOT = 17
257192 meter/sec RA = 215
14956 deg
ZDOT = 4498
736137 TA = 319
79413
MA = 319
88931
Ha = 193
109 n
mi
Hp = 186
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8224377
18 X = -2465757
49
Y = -16964223
41 feet Y = -5198498
09 meter
Z = 11463515
20 Z = 3482001
64
XDOT = 20512
170803 XDOT = 6229
598317
YDOT = 56
618083 feet/sec YDOT = 87
046492 meter/sec
ZDOT = 14759
632994 ZDOT = 4529
053717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15588577
70 X = 4751398
48
Y = -10655344
10 feet Y = -3247748
88 meter
Z = 11414785
34 Z = 3479226
57
XDOT = 2115
377367 XDOT = 644
767022
YDOT = 19080
996836 feet/sec YDOT = 5815
887836 meter/sec
ZDOT = 14882
086994 ZDOT = 4536
060116
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 11087
31673984
00016717 00000-0 10270-3 0 9140
2 25544 51
6436 215
8407 0002319 10
3888 349
7322 15
72268713 28177
Satellite: ISS
Catalog Number: 25544
Epoch time: 11087
31673984 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 215
8407 deg
Eccentricity:
0002319
Arg of perigee: 10
3888 deg
Mean anomaly: 349
7322 deg
Mean motion: 15
72268713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2817
Checksum: 321
Coasting Arc #16 (Orbit 2831)
---------------------------------------
Vector Time (GMT): 2011/088/06:15:03
703
Vector Time (MET): N/A
Weight (LBS) : 919647
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5111142
98 A = 6728857
58 meter
Y = 981985
06 meter E =
0008734
Z = -4272944
00 I = 51
46243
XDOT = -4003
222806 Wp = 95
92550
YDOT = -5543
774085 meter/sec RA = 209
96266 deg
ZDOT = 3519
746271 TA = 209
85906
MA = 209
90892
Ha = 192
961 n
mi
Hp = 185
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16768841
79 X = -5100986
99
Y = 3221735
76 feet Y = 924885
59 meter
Z = -14018845
15 Z = -4297748
95
XDOT = -13133
933091 XDOT = -3958
031761
YDOT = -18188
235188 feet/sec YDOT = -5588
287584 meter/sec
ZDOT = 11547
723986 ZDOT = 3500
409150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5871711
93 X = -1789697
80
Y = -15946066
76 feet Y = -4860361
15 meter
Z = -14119051
29 Z = -4303486
83
XDOT = 14655
714480 XDOT = 4467
061773
YDOT = -15536
891683 feet/sec YDOT = -4735
644585 meter/sec
ZDOT = 11469
664023 ZDOT = 3495
953594
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 11088
27010667
00016717 00000-0 10270-3 0 9150
2 25544 51
6428 210
9563 0002287 13
6932 346
4292 15
72346483 28325
Satellite: ISS
Catalog Number: 25544
Epoch time: 11088
27010667 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 210
9563 deg
Eccentricity:
0002287
Arg of perigee: 13
6932 deg
Mean anomaly: 346
4292 deg
Mean motion: 15
72346483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2832
Checksum: 309
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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