[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 30th 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) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 751)
---------------------------------------
Vector Time (GMT): 2011/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1075345
12 A = 6767030
35 meter
Y = 5803342
38 meter E =
0019430
Z = 3308053
14 I = 51
37237
XDOT = -5881
181878 Wp = 55
76530
YDOT = 1589
469868 meter/sec RA = 307
10491 deg
ZDOT = -4669
803047 TA = 85
49021
MA = 85
26828
Ha = 214
844 n
mi
Hp = 202
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3528035
15 X = -1156228
82
Y = 19039837
22 feet Y = 5790864
62 meter
Z = 10853192
71 Z = 3302633
41
XDOT = -19295
216135 XDOT = -5875
834037
YDOT = 5214
796155 feet/sec YDOT = 1523
733318 meter/sec
ZDOT = -15320
876138 ZDOT = -4698
359968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17515617
02 X = 5338760
07
Y = -8285558
46 feet Y = -2525438
22 meter
Z = 10830831
30 Z = 3301237
38
XDOT = 14901
766998 XDOT = 4542
058581
YDOT = 11192
469521 feet/sec YDOT = 3411
464710 meter/sec
ZDOT = -15436
962234 ZDOT = -4705
186089
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 11210
53893437
00016717 00000-0 10270-3 0 9004
2 25544 51
6415 307
5560 0011767 17
1982 342
9571 15
60220143 7529
Satellite: ISS
Catalog Number: 25544
Epoch time: 11210
53893437 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 307
5560 deg
Eccentricity:
0011767
Arg of perigee: 17
1982 deg
Mean anomaly: 342
9571 deg
Mean motion: 15
60220143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 287
Coasting Arc #2 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2011/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3685504
05 A = 6771646
74 meter
Y = -5662754
28 meter E =
0023774
Z = 144103
57 I = 51
37103
XDOT = 3948
152087 Wp = 33
64130
YDOT = 2733
913503 meter/sec RA = 302
08080 deg
ZDOT = 6003
233477 TA = 327
92282
MA = 328
06728
Ha = 214
932 n
mi
Hp = 202
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12091548
73 X = 3747852
15
Y = -18578590
15 feet Y = -5621192
13 meter
Z = 472780
76 Z = 162158
23
XDOT = 12953
254878 XDOT = 3888
125669
YDOT = 8969
532490 feet/sec YDOT = 2777
728013 meter/sec
ZDOT = 19695
647892 ZDOT = 6022
267513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22112833
67 X = -6739991
70
Y = 1522192
26 feet Y = 463964
20 meter
Z = 546445
18 Z = 166556
49
XDOT = -445
738236 XDOT = -135
861014
YDOT = -14036
282448 feet/sec YDOT = -4278
258890 meter/sec
ZDOT = 19772
802817 ZDOT = 6026
750299
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 11211
56373360
00016717 00000-0 10270-3 0 9017
2 25544 51
6419 302
4001 0011972 20
3975 339
7657 15
60231473 7687
Satellite: ISS
Catalog Number: 25544
Epoch time: 11211
56373360 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 302
4001 deg
Eccentricity:
0011972
Arg of perigee: 20
3975 deg
Mean anomaly: 339
7657 deg
Mean motion: 15
60231473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 288
Coasting Arc #3 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2011/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4818777
70 A = 6766044
56 meter
Y = 3154514
08 meter E =
0015377
Z = -3570522
82 I = 51
33647
XDOT = -794
543897 Wp = 40
97674
YDOT = -6212
771568 meter/sec RA = 297
05322 deg
ZDOT = -4416
021259 TA = 181
46180
MA = 181
46630
Ha = 214
972 n
mi
Hp = 202
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15809638
14 X = -4836349
47
Y = 10349455
66 feet Y = 3100529
53 meter
Z = -11714313
73 Z = -3593974
31
XDOT = -2606
771317 XDOT = -703
560781
YDOT = -20383
108818 feet/sec YDOT = -6221
147674 meter/sec
ZDOT = -14488
258723 ZDOT = -4419
660413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17842126
68 X = 5438280
21
Y = 6038988
26 feet Y = 1840683
62 meter
Z = -11809749
06 Z = -3599611
51
XDOT = -14077
638957 XDOT = -4290
864354
YDOT = 13227
363862 feet/sec YDOT = 4031
700505 meter/sec
ZDOT = -14502
692666 ZDOT = -4420
420725
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 11212
52447153
00016717 00000-0 10270-3 0 9027
2 25544 51
6409 297
5669 0011862 23
9708 336
1998 15
60259807 7838
Satellite: ISS
Catalog Number: 25544
Epoch time: 11212
52447153 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 297
5669 deg
Eccentricity:
0011862
Arg of perigee: 23
9708 deg
Mean anomaly: 336
1998 deg
Mean motion: 15
60259807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 329
Coasting Arc #4 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2011/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4183508
49 A = 6759539
68 meter
Y = 838939
72 meter E =
0012313
Z = 5234724
31 I = 51
30247
XDOT = -2333
320822 Wp = 41
17113
YDOT = 7289
409683 meter/sec RA = 291
97959 deg
ZDOT = 704
703463 TA = 42
12969
MA = 42
03510
Ha = 214
859 n
mi
Hp = 202
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13725421
56 X = 4148387
67
Y = 2752426
92 feet Y = 885525
72 meter
Z = 17174292
35 Z = 5254962
00
XDOT = -7655
252040 XDOT = -2418
082236
YDOT = 23915
386098 feet/sec YDOT = 7262
843116 meter/sec
ZDOT = 2312
019237 ZDOT = 693
162842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6424173
11 X = -1958087
96
Y = -12323320
91 feet Y = -3756148
21 meter
Z = 17256451
84 Z = 5259766
52
XDOT = 22519
833420 XDOT = 6864
045226
YDOT = -8605
706448 feet/sec YDOT = -2623
019325 meter/sec
ZDOT = 2264
747799 ZDOT = 690
295129
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 11213
54924658
00016717 00000-0 10270-3 0 9031
2 25544 51
6410 292
4102 0011916 27
3158 332
8622 15
60314918 7992
Satellite: ISS
Catalog Number: 25544
Epoch time: 11213
54924658 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 292
4102 deg
Eccentricity:
0011916
Arg of perigee: 27
3158 deg
Mean anomaly: 332
8622 deg
Mean motion: 15
60314918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 297
Coasting Arc #5 (Orbit 813)
---------------------------------------
Vector Time (GMT): 2011/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2266302
13 A = 6763106
28 meter
Y = -4629848
01 meter E =
0016437
Z = -4386766
55 I = 51
30296
XDOT = 4411
652679 Wp = 64
17091
YDOT = -5310
737698 meter/sec RA = 286
89628 deg
ZDOT = 3342
668379 TA = 239
68932
MA = 239
85202
Ha = 215
074 n
mi
Hp = 201
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7435374
44 X = -2193052
16
Y = -15189790
06 feet Y = -4654781
54 meter
Z = -14392278
72 Z = -4397598
18
XDOT = 14473
926111 XDOT = 4454
472760
YDOT = -17423
680113 feet/sec YDOT = -5261
164549 meter/sec
ZDOT = 10966
759772 ZDOT = 3364
203646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6927623
53 X = -2111539
65
Y = 15387044
93 feet Y = 4689971
30 meter
Z = -14436034
16 Z = -4400103
21
XDOT = -21486
074014 XDOT = -6548
955359
YDOT = 646
141459 feet/sec YDOT = 196
943917 meter/sec
ZDOT = 11054
512506 ZDOT = 3369
415412
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 11214
50996511
00016717 00000-0 10270-3 0 9046
2 25544 51
6398 287
5771 0012101 31
4635 328
7242 15
60326151 8149
Satellite: ISS
Catalog Number: 25544
Epoch time: 11214
50996511 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 287
5771 deg
Eccentricity:
0012101
Arg of perigee: 31
4635 deg
Mean anomaly: 328
7242 deg
Mean motion: 15
60326151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 814
Checksum: 289
Coasting Arc #6 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2011/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -283058
68 A = 6770569
79 meter
Y = 6626506
38 meter E =
0019232
Z = 1353885
56 I = 51
31999
XDOT = -4941
681733 Wp = 80
54607
YDOT = 986
484807 meter/sec RA = 281
85143 deg
ZDOT = -5787
994466 TA = 84
60915
MA = 84
38977
Ha = 215
224 n
mi
Hp = 201
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -928670
22 X = -363713
35
Y = 21740506
50 feet Y = 6622890
06 meter
Z = 4441881
76 Z = 1352314
67
XDOT = -16212
866577 XDOT = -4924
228948
YDOT = 3236
498711 feet/sec YDOT = 931
321572 meter/sec
ZDOT = -18989
483157 ZDOT = -5811
958358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17050988
58 X = 5197141
32
Y = -13521666
95 feet Y = -4121404
09 meter
Z = 4435163
56 Z = 1351837
85
XDOT = 12005
267263 XDOT = 3659
205462
YDOT = 8799
047034 feet/sec YDOT = 2681
949536 meter/sec
ZDOT = -19086
872811 ZDOT = -5817
678833
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 11215
53471924
00016717 00000-0 10270-3 0 9057
2 25544 51
6395 282
4198 0012245 34
8070 325
3885 15
60334270 8307
Satellite: ISS
Catalog Number: 25544
Epoch time: 11215
53471924 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 282
4198 deg
Eccentricity:
0012245
Arg of perigee: 34
8070 deg
Mean anomaly: 325
3885 deg
Mean motion: 15
60334270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 298
Coasting Arc #7 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2011/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2546880
61 A = 6769103
50 meter
Y = -5820414
99 meter E =
0025025
Z = 2293490
21 I = 51
30953
XDOT = 3896
376918 Wp = 56
63241
YDOT = 3844
770107 meter/sec RA = 276
82825 deg
ZDOT = 5401
393817 TA = 329
15411
MA = 329
30091
Ha = 215
264 n
mi
Hp = 201
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8355907
53 X = 2600635
11
Y = -19095849
70 feet Y = -5791633
71 meter
Z = 7524574
17 Z = 2305993
25
XDOT = 12783
388838 XDOT = 3826
855685
YDOT = 12614
075155 feet/sec YDOT = 3887
952940 meter/sec
ZDOT = 17721
108325 ZDOT = 5420
153405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19761072
18 X = -6023174
80
Y = 6572778
49 feet Y = 2003382
88 meter
Z = 7575651
29 Z = 2309058
51
XDOT = 1397
741382 XDOT = 426
031573
YDOT = -16419
198591 feet/sec YDOT = -5004
571730 meter/sec
ZDOT = 17797
116602 ZDOT = 5424
561140
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 11216
55946221
00016717 00000-0 10270-3 0 9068
2 25544 51
6392 277
2629 0012296 38
7847 321
4189 15
60324969 8461
Satellite: ISS
Catalog Number: 25544
Epoch time: 11216
55946221 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 277
2629 deg
Eccentricity:
0012296
Arg of perigee: 38
7847 deg
Mean anomaly: 321
4189 deg
Mean motion: 15
60324969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 846
Checksum: 333
Coasting Arc #8 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2011/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3979663
66 A = 6761194
42 meter
Y = 2535767
32 meter E =
0023433
Z = -4863888
40 I = 51
28030
XDOT = -1658
738561 Wp = 57
35429
YDOT = -7102
667879 meter/sec RA = 271
76969 deg
ZDOT = -2341
592647 TA = 189
55802
MA = 189
60269
Ha = 215
367 n
mi
Hp = 201
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13056639
32 X = -3984095
66
Y = 8319446
58 feet Y = 2491239
70 meter
Z = -15957639
10 Z = -4883232
09
XDOT = -5442
055645 XDOT = -1567
816940
YDOT = -23302
716138 feet/sec YDOT = -7120
708444 meter/sec
ZDOT = -7682
390573 ZDOT = -2349
430150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14916324
48 X = 4546495
70
Y = 3830715
58 feet Y = 1167602
11 meter
Z = -16036338
40 Z = -4887875
94
XDOT = -13117
384663 XDOT = -3998
178845
YDOT = 18728
326845 feet/sec YDOT = 5708
394022 meter/sec
ZDOT = -7713
877150 ZDOT = -2351
189755
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 11217
52014819
00016717 00000-0 10270-3 0 9076
2 25544 51
6389 272
4280 0012275 42
1849 318
0249 15
60333412 8614
Satellite: ISS
Catalog Number: 25544
Epoch time: 11217
52014819 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 272
4280 deg
Eccentricity:
0012275
Arg of perigee: 42
1849 deg
Mean anomaly: 318
0249 deg
Mean motion: 15
60333412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 861
Checksum: 294
Coasting Arc #9 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2011/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4129180
57 A = 6760314
77 meter
Y = 1873010
65 meter E =
0017868
Z = 5006090
11 I = 51
27829
XDOT = -1068
522853 Wp = 48
51116
YDOT = 7379
283596 meter/sec RA = 266
67919 deg
ZDOT = -1863
601509 TA = 59
68422
MA = 59
50759
Ha = 215
234 n
mi
Hp = 201
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13547180
33 X = 4083610
85
Y = 6145048
06 feet Y = 1918930
57 meter
Z = 16424180
15 Z = 5026038
91
XDOT = -3505
652404 XDOT = -1141
907064
YDOT = 24210
248017 feet/sec YDOT = 7366
924520 meter/sec
ZDOT = -6114
178178 ZDOT = -1868
970152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4893588
38 X = -1491565
74
Y = -13952599
81 feet Y = -4252752
42 meter
Z = 16505125
13 Z = 5030762
14
XDOT = 18835
333246 XDOT = 5741
009573
YDOT = -13926
765385 feet/sec YDOT = -4244
878089 meter/sec
ZDOT = -6136
345342 ZDOT = -1870
358060
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 11218
54486712
00016717 00000-0 10270-3 0 9085
2 25544 51
6390 267
2711 0012330 45
4458 314
7703 15
60398924 8775
Satellite: ISS
Catalog Number: 25544
Epoch time: 11218
54486712 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 267
2711 deg
Eccentricity:
0012330
Arg of perigee: 45
4458 deg
Mean anomaly: 314
7703 deg
Mean motion: 15
60398924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 877
Checksum: 314
Coasting Arc #10 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2011/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3003113
14 A = 6767921
59 meter
Y = -5417759
08 meter E =
0017268
Z = -2722968
04 I = 51
30681
XDOT = 3496
407362 Wp = 52
01425
YDOT = -4504
375397 meter/sec RA = 261
61505 deg
ZDOT = 5138
703491 TA = 276
94891
MA = 277
14531
Ha = 215
400 n
mi
Hp = 200
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9852733
40 X = -2929079
97
Y = -17774800
12 feet Y = -5450927
56 meter
Z = -8933622
17 Z = -2737377
60
XDOT = 11471
152763 XDOT = 3521
553685
YDOT = -14778
134503 feet/sec YDOT = -4465
136241 meter/sec
ZDOT = 16859
263422 ZDOT = 5155
749578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5683219
70 X = -1732245
36
Y = 19485281
93 feet Y = 5939113
93 meter
Z = -8991900
92 Z = -2740731
40
XDOT = -17072
942211 XDOT = -5203
832786
YDOT = 2783
334356 feet/sec YDOT = 848
360312 meter/sec
ZDOT = 16928
728415 ZDOT = 5159
876421
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 11219
50553370
00016717 00000-0 10270-3 0 9098
2 25544 51
6390 262
4366 0012493 49
7333 310
4914 15
60407025 8924
Satellite: ISS
Catalog Number: 25544
Epoch time: 11219
50553370 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 262
4366 deg
Eccentricity:
0012493
Arg of perigee: 49
7333 deg
Mean anomaly: 310
4914 deg
Mean motion: 15
60407025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 296
Coasting Arc #11 (Orbit 907)
---------------------------------------
Vector Time (GMT): 2011/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 787988
46 A = 6770709
78 meter
Y = 6656180
89 meter E =
0016252
Z = -970837
06 I = 51
32204
XDOT = -4908
928344 Wp = 90
56525
YDOT = -265
182053 meter/sec RA = 256
59007 deg
ZDOT = -5888
162234 TA = 100
01550
MA = 99
83206
Ha = 215
526 n
mi
Hp = 200
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2585263
97 X = 718215
26
Y = 21837863
80 feet Y = 6664602
62 meter
Z = -3185160
97 Z = -967177
96
XDOT = -16105
407954 XDOT = -4876
994981
YDOT = -870
019858 feet/sec YDOT = -319
897609 meter/sec
ZDOT = -19318
117567 ZDOT = -5911
931917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13339320
03 X = 4065824
74
Y = -17485162
97 feet Y = -5329477
67 meter
Z = -3170607
63 Z = -966401
20
XDOT = 9592
463075 XDOT = 2923
782745
YDOT = 10787
320041 feet/sec YDOT = 3287
975148 meter/sec
ZDOT = -19414
676759 ZDOT = -5917
593476
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 11220
53023185
00016717 00000-0 10270-3 0 9101
2 25544 51
6394 257
2789 0012609 53
2010 307
0301 15
60414516 9083
Satellite: ISS
Catalog Number: 25544
Epoch time: 11220
53023185 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 257
2789 deg
Eccentricity:
0012609
Arg of perigee: 53
2010 deg
Mean anomaly: 307
0301 deg
Mean motion: 15
60414516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 908
Checksum: 268
Coasting Arc #12 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2011/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1808551
79 A = 6763768
25 meter
Y = -5026499
84 meter E =
0021189
Z = 4127824
84 I = 51
30549
XDOT = 4739
736870 Wp = 78
30890
YDOT = 4775
368370 meter/sec RA = 251
55002 deg
ZDOT = 3726
400505 TA = 333
26478
MA = 333
37386
Ha = 215
554 n
mi
Hp = 200
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5933568
85 X = 1844572
83
Y = -16491141
19 feet Y = -5006074
47 meter
Z = 13542732
42 Z = 4136697
67
XDOT = 15550
317815 XDOT = 4667
883676
YDOT = 15667
219063 feet/sec YDOT = 4827
968916 meter/sec
ZDOT = 12225
723443 ZDOT = 3749
251596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15548111
73 X = -4739064
45
Y = 8027276
15 feet Y = 2446713
77 meter
Z = 13579014
62 Z = 4138883
65
XDOT = 11
674269 XDOT = 3
558317
YDOT = -20881
470052 feet/sec YDOT = -6364
672072 meter/sec
ZDOT = 12318
353357 ZDOT = 3754
634103
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 11221
55491902
00016717 00000-0 10270-3 0 9111
2 25544 51
6381 252
1220 0012734 57
2751 302
9631 15
60414849 9245
Satellite: ISS
Catalog Number: 25544
Epoch time: 11221
55491902 = yrday
fracday
Element set: 911
Inclination: 51
6381 deg
RA of node: 252
1220 deg
Eccentricity:
0012734
Arg of perigee: 57
2751 deg
Mean anomaly: 302
9631 deg
Mean motion: 15
60414849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 280
Coasting Arc #13 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2011/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4016745
77 A = 6759138
46 meter
Y = 1373950
85 meter E =
0026409
Z = -5281775
50 I = 51
30158
XDOT = -2828
321368 Wp = 77
77917
YDOT = -7111
833182 meter/sec RA = 246
46700 deg
ZDOT = 307
701800 TA = 195
13166
MA = 195
21080
Ha = 215
581 n
mi
Hp = 200
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13178299
78 X = -4006153
72
Y = 4507712
78 feet Y = 1329092
78 meter
Z = -17328659
77 Z = -5301262
56
XDOT = -9279
269579 XDOT = -2750
079983
YDOT = -23332
786030 feet/sec YDOT = -7143
023748 meter/sec
ZDOT = 1009
520342 ZDOT = 294
151635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12715319
11 X = 3875629
27
Y = 5436441
82 feet Y = 1657027
47 meter
Z = -17407908
24 Z = -5305930
43
XDOT = -8385
663197 XDOT = -2555
950142
YDOT = 22599
494639 feet/sec YDOT = 6888
325966 meter/sec
ZDOT = 954
772387 ZDOT = 291
014624
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 11222
51555187
00016717 00000-0 10270-3 0 9125
2 25544 51
6390 247
2875 0012582 60
2732 299
9674 15
60418710 9399
Satellite: ISS
Catalog Number: 25544
Epoch time: 11222
51555187 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 247
2875 deg
Eccentricity:
0012582
Arg of perigee: 60
2732 deg
Mean anomaly: 299
9674 deg
Mean motion: 15
60418710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 318
Coasting Arc #14 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2011/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4910928
65 A = 6764791
57 meter
Y = 2726134
62 meter E =
0023925
Z = 3756184
02 I = 51
33257
XDOT = -328
160268 Wp = 72
99422
YDOT = 6424
334933 meter/sec RA = 241
38832 deg
ZDOT = -4204
495798 TA = 61
61101
MA = 61
37003
Ha = 215
505 n
mi
Hp = 200
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16111970
63 X = 4861833
11
Y = 8944011
21 feet Y = 2780776
89 meter
Z = 12323438
39 Z = 3779921
59
XDOT = -1076
641300 XDOT = -379
549904
YDOT = 21077
214347 feet/sec YDOT = 6420
378156 meter/sec
ZDOT = -13794
277552 ZDOT = -4206
214404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6179947
91 X = -1883648
12
Y = -17292052
48 feet Y = -5270617
60 meter
Z = 12419791
97 Z = 3785552
59
XDOT = 13365
263349 XDOT = 4073
732269
YDOT = -14757
294909 feet/sec YDOT = -4498
023488 meter/sec
ZDOT = -13801
534529 ZDOT = -4206
707725
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 11223
54021496
00016717 00000-0 10270-3 0 9131
2 25544 51
6373 242
1296 0012745 63
8436 296
4029 15
60482504 9558
Satellite: ISS
Catalog Number: 25544
Epoch time: 11223
54021496 = yrday
fracday
Element set: 913
Inclination: 51
6373 deg
RA of node: 242
1296 deg
Eccentricity:
0012745
Arg of perigee: 63
8436 deg
Mean anomaly: 296
4029 deg
Mean motion: 15
60482504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 303
Coasting Arc #15 (Orbit 969)
---------------------------------------
Vector Time (GMT): 2011/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4005084
63 A = 6770779
46 meter
Y = -5434424
91 meter E =
0023316
Z = -404731
31 I = 51
36867
XDOT = 3663
852500 Wp = 55
98720
YDOT = -3126
507608 meter/sec RA = 236
35666 deg
ZDOT = 5983
992952 TA = 299
61912
MA = 299
85119
Ha = 215
525 n
mi
Hp = 200
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13140041
44 X = -3942052
11
Y = -17829478
04 feet Y = -5478859
76 meter
Z = -1327858
61 Z = -424034
57
XDOT = 12020
513452 XDOT = 3669
473060
YDOT = -10257
570891 feet/sec YDOT = -3085
504967 meter/sec
ZDOT = 19632
522807 ZDOT = 6001
804993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1477567
14 X = -450362
46
Y = 22094204
71 feet Y = 6734313
59 meter
Z = -1406093
42 Z = -428577
27
XDOT = -14099
834870 XDOT = -4297
629668
YDOT = 259
867018 feet/sec YDOT = 79
207467 meter/sec
ZDOT = 19705
043661 ZDOT = 6006
097308
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 11224
50082696
00016717 00000-0 10270-3 0 9148
2 25544 51
6377 237
2953 0012678 67
9486 292
3015 15
60504719 9702
Satellite: ISS
Catalog Number: 25544
Epoch time: 11224
50082696 = yrday
fracday
Element set: 914
Inclination: 51
6377 deg
RA of node: 237
2953 deg
Eccentricity:
0012678
Arg of perigee: 67
9486 deg
Mean anomaly: 292
3015 deg
Mean motion: 15
60504719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 970
Checksum: 324
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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