[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 10th 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
077/06:07:53
974 -1
6 7
4 7
5
N/A -7
4 -1
1 193
7
000/00:17:47
948 0
4 0
6 188
0
Coasting Arc #1 (Orbit 2520)
---------------------------------------
Vector Time (GMT): 2011/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2808799
19 A = 6734416
03 meter
Y = -5731283
56 meter E =
0012176
Z = -2137697
38 I = 51
40574
XDOT = 5353
695919 Wp = 41
67010
YDOT = 582
446140 meter/sec RA = 311
61319 deg
ZDOT = 5499
719046 TA = 294
35475
MA = 294
48182
Ha = 194
174 n
mi
Hp = 184
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9215220
44 X = 2883063
21
Y = -18803423
77 feet Y = -5699458
82 meter
Z = -7013442
85 Z = -2123871
45
XDOT = 17564
619157 XDOT = 5320
068531
YDOT = 1910
912533 feet/sec YDOT = 642
126864 meter/sec
ZDOT = 18043
697656 ZDOT = 5525
645392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13518153
12 X = 4120333
07
Y = -16016563
42 feet Y = -4881848
53 meter
Z = -6957488
48 Z = -2120642
49
XDOT = 15312
378268 XDOT = 4667
212896
YDOT = 5078
912678 feet/sec YDOT = 1548
052584 meter/sec
ZDOT = 18148
308894 ZDOT = 5531
604551
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 11068
50418374
00016717 00000-0 10270-3 0 9005
2 25544 51
6470 312
2129 0005797 42
6697 317
4915 15
72526027 25214
Satellite: ISS
Catalog Number: 25544
Epoch time: 11068
50418374 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 312
2129 deg
Eccentricity:
0005797
Arg of perigee: 42
6697 deg
Mean anomaly: 317
4915 deg
Mean motion: 15
72526027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2521
Checksum: 303
Coasting Arc #2 (Orbit 2536)
---------------------------------------
Vector Time (GMT): 2011/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4894431
26 A = 6726900
27 meter
Y = 415463
19 meter E =
0016047
Z = -4611774
93 I = 51
36114
XDOT = 2148
800646 Wp = 61
29217
YDOT = -6788
471679 meter/sec RA = 306
51128 deg
ZDOT = -2892
086618 TA = 179
90677
MA = 179
90647
Ha = 194
076 n
mi
Hp = 184
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16057845
35 X = -4876310
25
Y = 1363068
20 feet Y = 360831
69 meter
Z = -15130495
18 Z = -4635507
94
XDOT = 7049
870885 XDOT = 2238
600067
YDOT = -22271
888710 feet/sec YDOT = -6763
940598 meter/sec
ZDOT = -9488
473157 ZDOT = -2881
429210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15865603
52 X = -4835835
95
Y = -2255482
53 feet Y = -687471
07 meter
Z = -15226281
88 Z = -4640970
72
XDOT = 11758
897866 XDOT = 3584
112069
YDOT = -18952
482107 feet/sec YDOT = -5776
716546 meter/sec
ZDOT = -9445
278758 ZDOT = -2878
920966
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 11069
52095644
00016717 00000-0 10270-3 0 9010
2 25544 51
6466 307
0027 0005703 44
9957 315
1666 15
72580338 25379
Satellite: ISS
Catalog Number: 25544
Epoch time: 11069
52095644 = yrday
fracday
Element set: 901
Inclination: 51
6466 deg
RA of node: 307
0027 deg
Eccentricity:
0005703
Arg of perigee: 44
9957 deg
Mean anomaly: 315
1666 deg
Mean motion: 15
72580338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2537
Checksum: 313
Coasting Arc #3 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2011/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -939411
52 A = 6732413
19 meter
Y = 5998171
64 meter E =
0017713
Z = 2896773
50 I = 51
36299
XDOT = -5635
549397 Wp = 83
72152
YDOT = 1552
145821 meter/sec RA = 301
32095 deg
ZDOT = -5013
362369 TA = 62
82292
MA = 62
64247
Ha = 194
058 n
mi
Hp = 184
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3082058
80 X = -1020486
29
Y = 19679040
80 feet Y = 5987213
42 meter
Z = 9503850
07 Z = 2892012
60
XDOT = -18489
335292 XDOT = -5628
133113
YDOT = 5092
341931 feet/sec YDOT = 1489
166873 meter/sec
ZDOT = -16448
039268 ZDOT = -5040
721733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7156188
39 X = -2181206
22
Y = 18598940
60 feet Y = 5668957
09 meter
Z = 9484475
52 Z = 2890868
14
XDOT = -17690
798479 XDOT = -5392
155376
YDOT = 1684
388738 feet/sec YDOT = 513
401687 meter/sec
ZDOT = -16558
491648 ZDOT = -5047
028254
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 11070
53769455
00016717 00000-0 10270-3 0 9022
2 25544 51
6467 301
7925 0005783 48
9074 311
2587 15
72644146 25535
Satellite: ISS
Catalog Number: 25544
Epoch time: 11070
53769455 = yrday
fracday
Element set: 902
Inclination: 51
6467 deg
RA of node: 301
7925 deg
Eccentricity:
0005783
Arg of perigee: 48
9074 deg
Mean anomaly: 311
2587 deg
Mean motion: 15
72644146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 321
Coasting Arc #4 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2011/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4796439
96 A = 6728518
08 meter
Y = -2278767
83 meter E =
0014522
Z = 4118991
47 I = 51
33459
XDOT = -1
566118 Wp = 86
30828
YDOT = 6746
496177 meter/sec RA = 296
22344 deg
ZDOT = 3723
863963 TA = 325
40864
MA = 325
50303
Ha = 193
934 n
mi
Hp = 184
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15736351
56 X = 4801555
98
Y = -7476272
40 feet Y = -2225102
33 meter
Z = 13513751
54 Z = 4142304
87
XDOT = -5
138184 XDOT = -95
096277
YDOT = 22134
173810 feet/sec YDOT = 6745
955887 meter/sec
ZDOT = 12217
401455 ZDOT = 3723
628850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16793850
93 X = 5118765
76
Y = -4352081
12 feet Y = -1326514
33 meter
Z = 13607896
64 Z = 4147686
89
XDOT = -4616
484828 XDOT = -1407
104575
YDOT = 20488
657071 feet/sec YDOT = 6244
942675 meter/sec
ZDOT = 12216
275504 ZDOT = 3723
520774
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 11071
55439762
00016717 00000-0 10270-3 0 9031
2 25544 51
6460 296
5815 0005752 51
8111 308
3569 15
72656263 25695
Satellite: ISS
Catalog Number: 25544
Epoch time: 11071
55439762 = yrday
fracday
Element set: 903
Inclination: 51
6460 deg
RA of node: 296
5815 deg
Eccentricity:
0005752
Arg of perigee: 51
8111 deg
Mean anomaly: 308
3569 deg
Mean motion: 15
72656263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 320
Coasting Arc #5 (Orbit 2583)
---------------------------------------
Vector Time (GMT): 2011/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -890740
20 A = 6730225
06 meter
Y = -5640880
01 meter E =
0010123
Z = -3567393
41 I = 51
32785
XDOT = 5169
016850 Wp = 75
49392
YDOT = -3600
007212 meter/sec RA = 291
02418 deg
ZDOT = 4414
756744 TA = 241
77213
MA = 241
87436
Ha = 193
855 n
mi
Hp = 183
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2922375
97 X = -810267
09
Y = -18506824
18 feet Y = -5650391
01 meter
Z = -11704046
63 Z = -3571524
85
XDOT = 16958
716701 XDOT = 5187
442845
YDOT = -11811
047285 feet/sec YDOT = -3542
100916 meter/sec
ZDOT = 14484
110053 ZDOT = 4439
912395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 408489
30 X = 124507
54
Y = -18721343
85 feet Y = -5706265
60 meter
Z = -11720578
10 Z = -3572432
21
XDOT = 17302
905892 XDOT = 5273
925716
YDOT = -8727
343781 feet/sec YDOT = -2660
094384 meter/sec
ZDOT = 14585
724712 ZDOT = 4445
728892
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 11072
50752204
00016717 00000-0 10270-3 0 9047
2 25544 51
6453 291
6961 0005521 54
2753 305
8922 15
72739482 25845
Satellite: ISS
Catalog Number: 25544
Epoch time: 11072
50752204 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 291
6961 deg
Eccentricity:
0005521
Arg of perigee: 54
2753 deg
Mean anomaly: 305
8922 deg
Mean motion: 15
72739482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2584
Checksum: 306
Coasting Arc #6 (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 = -4121113
62 A = 6729931
17 meter
Y = 3925133
62 meter E =
0010798
Z = -3604150
14 I = 51
31648
XDOT = -1921
012271 Wp = 68
94925
YDOT = -6025
449347 meter/sec RA = 285
92747 deg
ZDOT = -4372
250432 TA = 154
31678
MA = 154
26312
Ha = 193
807 n
mi
Hp = 183
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13520713
98 X = -4147190
91
Y = 12877734
99 feet Y = 3878902
86 meter
Z = -11824639
55 Z = -3624233
68
XDOT = -6302
533697 XDOT = -1832
252544
YDOT = -19768
534603 feet/sec YDOT = -6046
435197 meter/sec
ZDOT = -14344
653648 ZDOT = -4381
366664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15303404
14 X = -4664477
58
Y = 10607819
64 feet Y = 3233263
43 meter
Z = -11905790
60 Z = -3628884
97
XDOT = -2264
760316 XDOT = -690
298944
YDOT = -19383
640287 feet/sec YDOT = -5908
133560 meter/sec
ZDOT = -14381
303031 ZDOT = -4383
421164
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
52415470
00016717 00000-0 10270-3 0 9052
2 25544 51
6443 286
4852 0005465 57
6380 302
5311 15
72783605 26006
Satellite: ISS
Catalog Number: 25544
Epoch time: 11073
52415470 = yrday
fracday
Element set: 905
Inclination: 51
6443 deg
RA of node: 286
4852 deg
Eccentricity:
0005465
Arg of perigee: 57
6380 deg
Mean anomaly: 302
5311 deg
Mean motion: 15
72783605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 292
Coasting Arc #7 (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 = 2401632
44 A = 6728152
26 meter
Y = 4790715
04 meter E =
0015845
Z = 4058847
44 I = 51
30431
XDOT = -4103
890049 Wp = 70
78302
YDOT = 5294
526379 meter/sec RA = 280
72553 deg
ZDOT = -3803
689850 TA = 58
54029
MA = 58
38551
Ha = 193
606 n
mi
Hp = 183
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7879371
54 X = 2328166
52
Y = 15717569
02 feet Y = 4817161
03 meter
Z = 13316428
62 Z = 4070335
60
XDOT = -13464
206198 XDOT = -4144
312177
YDOT = 17370
493370 feet/sec YDOT = 5248
407949 meter/sec
ZDOT = -12479
297409 ZDOT = -3823
724647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5524465
79 X = 1683857
17
Y = 16654504
31 feet Y = 5076292
91 meter
Z = 13362690
86 Z = 4072948
17
XDOT = -14472
764171 XDOT = -4411
298519
YDOT = 14923
661569 feet/sec YDOT = 4548
732046 meter/sec
ZDOT = -12560
278822 ZDOT = -3828
372985
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
54074963
00016717 00000-0 10270-3 0 9064
2 25544 51
6445 281
2735 0005384 59
6943 300
4752 15
72880493 26164
Satellite: ISS
Catalog Number: 25544
Epoch time: 11074
54074963 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 281
2735 deg
Eccentricity:
0005384
Arg of perigee: 59
6943 deg
Mean anomaly: 300
4752 deg
Mean motion: 15
72880493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 322
Coasting Arc #8 (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 = 2952687
78 A = 6731217
59 meter
Y = -5224101
01 meter E =
0018234
Z = 3029708
75 I = 51
30887
XDOT = 3473
481697 Wp = 78
44558
YDOT = 4820
828016 meter/sec RA = 275
62431 deg
ZDOT = 4906
031257 TA = 316
82426
MA = 316
96709
Ha = 193
537 n
mi
Hp = 183
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9687295
86 X = 2996167
76
Y = -17139439
00 feet Y = -5190838
90 meter
Z = 9939989
34 Z = 3044158
64
XDOT = 11395
937326 XDOT = 3395
484029
YDOT = 15816
364882 feet/sec YDOT = 4859
234894 meter/sec
ZDOT = 16095
903073 ZDOT = 4922
715207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11659725
75 X = 3553884
41
Y = -15826871
49 feet Y = -4824030
43 meter
Z = 9998419
49 Z = 3047518
26
XDOT = 8117
248709 XDOT = 2474
137407
YDOT = 16234
763966 feet/sec YDOT = 4948
356057 meter/sec
ZDOT = 16163
147546 ZDOT = 4926
527372
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
55730939
00016717 00000-0 10270-3 0 9079
2 25544 51
6429 276
0614 0005295 64
2396 295
9313 15
72920414 26326
Satellite: ISS
Catalog Number: 25544
Epoch time: 11075
55730939 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 276
0614 deg
Eccentricity:
0005295
Arg of perigee: 64
2396 deg
Mean anomaly: 295
9313 deg
Mean motion: 15
72920414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2632
Checksum: 319
Coasting Arc #9 (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 = -3556989
99 A = 6726390
40 meter
Y = -3566245
72 meter E =
0014267
Z = -4471038
08 I = 51
28999
XDOT = 2577
854363 Wp = 95
77327
YDOT = -6519
186223 meter/sec RA = 270
42362 deg
ZDOT = 3156
306897 TA = 205
93462
MA = 206
00619
Ha = 193
575 n
mi
Hp = 183
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11669914
67 X = -3495128
14
Y = -11700281
24 feet Y = -3605676
74 meter
Z = -14668760
11 Z = -4488166
93
XDOT = 8457
527437 XDOT = 2635
229096
YDOT = -21388
406243 feet/sec YDOT = -6490
037948 meter/sec
ZDOT = 10355
337590 ZDOT = 3168
969927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10279980
04 X = -3133337
92
Y = -12859792
43 feet Y = -3919664
73 meter
Z = -14737834
36 Z = -4492091
91
XDOT = 9671
905058 XDOT = 2947
996662
YDOT = -19630
882638 feet/sec YDOT = -5983
493028 meter/sec
ZDOT = 10406
569872 ZDOT = 3171
922497
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
51030058
00016717 00000-0 10270-3 0 9082
2 25544 51
6417 271
1741 0005394 68
2695 291
9041 15
72960922 26474
Satellite: ISS
Catalog Number: 25544
Epoch time: 11076
51030058 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 271
1741 deg
Eccentricity:
0005394
Arg of perigee: 68
2695 deg
Mean anomaly: 291
9041 deg
Mean motion: 15
72960922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 310
Coasting Arc #10 (Orbit 2658)
---------------------------------------
Vector Time (GMT): 2011/077/06:16:47
948
Vector Time (MET): N/A
Weight (LBS) : 919527
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3912232
10 A = 6730035
84 meter
Y = -2904718
45 meter E =
0009551
Z = -4651285
03 I = 51
29050
XDOT = 1821
561053 Wp = 103
85426
YDOT = -6926
800606 meter/sec RA = 266
50077 deg
ZDOT = 2796
203657 TA = 193
91091
MA = 193
93724
Ha = 193
734 n
mi
Hp = 187
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12835407
16 X = -3856865
52
Y = -9529916
18 feet Y = -2948158
42 meter
Z = -15260121
48 Z = -4670155
46
XDOT = 5976
250174 XDOT = 1885
299259
YDOT = -22725
723774 feet/sec YDOT = -6906
074073 meter/sec
ZDOT = 9173
896513 ZDOT = 2805
208335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9777462
40 X = 2980170
54
Y = -12555444
75 feet Y = -3826899
56 meter
Z = -15336242
15 Z = -4674486
61
XDOT = 21689
892437 XDOT = 6611
079215
YDOT = 5650
769676 feet/sec YDOT = 1722
354597 meter/sec
ZDOT = 9210
360450 ZDOT = 2807
317865
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
27267447
00016717 00000-0 10270-3 0 9091
2 25544 51
6442 267
2645 0001687 322
4291 37
6753 15
71432196 26593
Satellite: ISS
Catalog Number: 25544
Epoch time: 11077
27267447 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 267
2645 deg
Eccentricity:
0001687
Arg of perigee: 322
4291 deg
Mean anomaly: 37
6753 deg
Mean motion: 15
71432196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2659
Checksum: 328
Coasting Arc #11 (Orbit 2674)
---------------------------------------
Vector Time (GMT): 2011/078/06:16:47
948
Vector Time (MET): N/A
Weight (LBS) : 919527
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -400685
41 A = 6738116
15 meter
Y = 6502963
62 meter E =
0005924
Z = -1709920
34 I = 51
32141
XDOT = -4870
213995 Wp = 141
95044
YDOT = -1789
863964 meter/sec RA = 261
39773 deg
ZDOT = -5680
817585 TA = 57
02557
MA = 56
96863
Ha = 193
701 n
mi
Hp = 188
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1314584
69 X = -465066
62
Y = 21335182
47 feet Y = 6498122
70 meter
Z = -5609974
85 Z = -1712024
12
XDOT = -15978
392373 XDOT = -4822
241375
YDOT = -5872
257101 feet/sec YDOT = -1844
058206 meter/sec
ZDOT = -18637
852968 ZDOT = -5704
360022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21331935
31 X = -6501973
88
Y = -1330488
45 feet Y = -405532
88 meter
Z = -5618567
28 Z = -1712539
31
XDOT = 5812
749567 XDOT = 1771
726068
YDOT = -14297
425187 feet/sec YDOT = -4357
855197 meter/sec
ZDOT = -18732
853619 ZDOT = -5709
773783
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
29015200
00016717 00000-0 10270-3 0 9104
2 25544 51
6445 262
0589 0001741 323
4383 36
6660 15
71468363 26759
Satellite: ISS
Catalog Number: 25544
Epoch time: 11078
29015200 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 262
0589 deg
Eccentricity:
0001741
Arg of perigee: 323
4383 deg
Mean anomaly: 36
6660 deg
Mean motion: 15
71468363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2675
Checksum: 297
Coasting Arc #12 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2011/079/06:16:47
948
Vector Time (MET): N/A
Weight (LBS) : 919527
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4304896
50 A = 6727385
88 meter
Y = 174960
37 meter E =
0004217
Z = 5165523
83 I = 51
29185
XDOT = 974
664160 Wp = 29
06989
YDOT = 7561
988967 meter/sec RA = 256
23221 deg
ZDOT = -1064
406044 TA = 71
15859
MA = 71
11286
Ha = 193
424 n
mi
Hp = 187
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14123676
19 X = 4277527
07
Y = 574016
97 feet Y = 222948
00 meter
Z = 16947256
66 Z = 5186370
39
XDOT = 3197
717061 XDOT = 895
202784
YDOT = 24809
675087 feet/sec YDOT = 7572
443817 meter/sec
ZDOT = -3492
145815 ZDOT = -1059
865176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -365937
05 X = -111537
61
Y = 14029066
17 feet Y = 4276059
37 meter
Z = 17031401
15 Z = 5191171
07
XDOT = -23735
876907 XDOT = -7234
695281
YDOT = 3614
096901 feet/sec YDOT = 1101
576736 meter/sec
ZDOT = -3473
926633 ZDOT = -1058
852838
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
30759308
00016717 00000-0 10270-3 0 9112
2 25544 51
6443 256
8531 0001958 327
1581 32
9459 15
71575252 26915
Satellite: ISS
Catalog Number: 25544
Epoch time: 11079
30759308 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 256
8531 deg
Eccentricity:
0001958
Arg of perigee: 327
1581 deg
Mean anomaly: 32
9459 deg
Mean motion: 15
71575252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 321
Coasting Arc #13 (Orbit 2706)
---------------------------------------
Vector Time (GMT): 2011/080/06:16:47
948
Vector Time (MET): N/A
Weight (LBS) : 919527
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2069851
71 A = 6739045
81 meter
Y = -6404144
55 meter E =
0013227
Z = 144911
92 I = 51
34027
XDOT = 4619
109059 Wp = 38
23333
YDOT = -1350
555043 meter/sec RA = 251
10194 deg
ZDOT = 6009
450828 TA = 323
34633
MA = 323
43674
Ha = 193
592 n
mi
Hp = 187
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6790852
05 X = -1998789
46
Y = -21010972
92 feet Y = -6426893
54 meter
Z = 475432
80 Z = 135029
93
XDOT = 15154
557280 XDOT = 4604
675121
YDOT = -4430
954865 feet/sec YDOT = -1298
981382 meter/sec
ZDOT = 19716
046022 ZDOT = 6031
855525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20782207
21 X = 6334416
76
Y = -7464099
26 feet Y = -2275057
46 meter
Z = 435633
82 Z = 132781
19
XDOT = 4365
966919 XDOT = 1330
746717
YDOT = 13371
049476 feet/sec YDOT = 4075
495880 meter/sec
ZDOT = 19806
503222 ZDOT = 6037
022182
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
32500160
00016717 00000-0 10270-3 0 9127
2 25544 51
6450 251
6468 0002039 333
4289 26
6768 15
71588263 27078
Satellite: ISS
Catalog Number: 25544
Epoch time: 11080
32500160 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 251
6468 deg
Eccentricity:
0002039
Arg of perigee: 333
4289 deg
Mean anomaly: 26
6768 deg
Mean motion: 15
71588263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2707
Checksum: 299
Coasting Arc #14 (Orbit 2721)
---------------------------------------
Vector Time (GMT): 2011/081/06:16:47
948
Vector Time (MET): N/A
Weight (LBS) : 919527
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3501018
90 A = 6726928
95 meter
Y = 2418097
09 meter E =
0014265
Z = -5222593
71 I = 51
31178
XDOT = -3618
512968 Wp = 76
35854
YDOT = -6746
022240 meter/sec RA = 245
96674 deg
ZDOT = -696
029246 TA = 186
96994
MA = 186
98979
Ha = 193
538 n
mi
Hp = 187
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11486282
48 X = -3502427
88
Y = 7933389
39 feet Y = 2378938
24 meter
Z = -17134493
79 Z = -5239605
30
XDOT = -11871
761706 XDOT = -3539
427539
YDOT = -22132
618896 feet/sec YDOT = -6786
044515 meter/sec
ZDOT = -2283
560520 ZDOT = -713
415307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8483915
37 X = -2585897
41
Y = -10978950
37 feet Y = -3346384
07 meter
Z = -17203199
08 Z = -5243535
08
XDOT = 20721
030968 XDOT = 6315
770239
YDOT = -12315
253125 feet/sec YDOT = -3753
689152 meter/sec
ZDOT = -2353
649350 ZDOT = -717
392322
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
27878759
00016717 00000-0 10270-3 0 9135
2 25544 51
6455 246
7661 0002148 336
8744 23
2321 15
71667831 27221
Satellite: ISS
Catalog Number: 25544
Epoch time: 11081
27878759 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 246
7661 deg
Eccentricity:
0002148
Arg of perigee: 336
8744 deg
Mean anomaly: 23
2321 deg
Mean motion: 15
71667831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2722
Checksum: 320
Coasting Arc #15 (Orbit 2737)
---------------------------------------
Vector Time (GMT): 2011/082/06:16:47
948
Vector Time (MET): N/A
Weight (LBS) : 919527
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4106941
90 A = 6738018
81 meter
Y = 5165775
81 meter E =
0012461
Z = 1333395
43 I = 51
36272
XDOT = -3102
221516 Wp = 113
97500
YDOT = 3976
971166 meter/sec RA = 240
80871 deg
ZDOT = -5814
564181 TA = 51
33776
MA = 51
22633
Ha = 193
573 n
mi
Hp = 187
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13474218
84 X = 4042394
58
Y = 16948083
35 feet Y = 5211341
30 meter
Z = 4374656
92 Z = 1353189
85
XDOT = -10177
892113 XDOT = -3118
216101
YDOT = 13047
805663 feet/sec YDOT = 3942
190460 meter/sec
ZDOT = -19076
654136 ZDOT = -5829
673861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16017333
28 X = -4882083
19
Y = 14544147
59 feet Y = 4433056
19 meter
Z = 4454495
61 Z = 1357730
26
XDOT = -12626
269954 XDOT = -3848
487082
YDOT = -8006
519763 feet/sec YDOT = -2440
387224 meter/sec
ZDOT = -19137
707412 ZDOT = -5833
173219
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
29612607
00016717 00000-0 10270-3 0 9147
2 25544 51
6455 241
5601 0002079 340
4126 19
6956 15
71669850 27389
Satellite: ISS
Catalog Number: 25544
Epoch time: 11082
29612607 = yrday
fracday
Element set: 914
Inclination: 51
6455 deg
RA of node: 241
5601 deg
Eccentricity:
0002079
Arg of perigee: 340
4126 deg
Mean anomaly: 19
6956 deg
Mean motion: 15
71669850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2738
Checksum: 310
Coasting Arc #16 (Orbit 2753)
---------------------------------------
Vector Time (GMT): 2011/083/06:16:47
948
Vector Time (MET): N/A
Weight (LBS) : 919527
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1735988
42 A = 6728348
81 meter
Y = -4330460
70 meter E =
0005336
Z = 4844121
82 I = 51
34695
XDOT = 5536
847090 Wp = 104
20172
YDOT = 4821
113136 meter/sec RA = 235
70140 deg
ZDOT = 2322
224886 TA = 323
06316
MA = 323
09989
Ha = 193
459 n
mi
Hp = 187
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5695500
07 X = 1760751
64
Y = -14207548
21 feet Y = -4310909
16 meter
Z = 15892788
11 Z = 4852615
55
XDOT = 18165
508827 XDOT = 5471
244060
YDOT = 15817
300315 feet/sec YDOT = 4882
662807 meter/sec
ZDOT = 7618
848052 ZDOT = 2348
963248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14625339
32 X = 4457803
42
Y = 4393123
07 feet Y = 1339023
91 meter
Z = 15927139
76 Z = 4854592
20
XDOT = -13927
205482 XDOT = -4245
012231
YDOT = 18311
950934 feet/sec YDOT = 5581
482645 meter/sec
ZDOT = 7726
735084 ZDOT = 2355
108854
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
31342549
00016717 00000-0 10270-3 0 9157
2 25544 51
6457 236
3536 0002360 344
6981 15
4109 15
71750629 27545
Satellite: ISS
Catalog Number: 25544
Epoch time: 11083
31342549 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 236
3536 deg
Eccentricity:
0002360
Arg of perigee: 344
6981 deg
Mean anomaly: 15
4109 deg
Mean motion: 15
71750629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2754
Checksum: 306
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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