[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 13th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 105)
---------------------------------------
Vector Time (GMT): 2012/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3772114
37 A = 6786008
80 meter
Y = -1988355
68 meter E =
0012936
Z = 5290196
10 I = 51
96535
XDOT = 2502
673175 Wp = 284
20341
YDOT = -7175
899248 meter/sec RA = 103
84391 deg
ZDOT = -911
386321 TA = 174
49859
MA = 174
48437
Ha = 224
964 n
mi
Hp = 219
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12375703
32 X = -3775299
18
Y = -6523476
63 feet Y = -2030555
59 meter
Z = 17356286
40 Z = 5271863
05
XDOT = 8210
869997 XDOT = 2587
157021
YDOT = -23542
976535 feet/sec YDOT = -7147
440423 meter/sec
ZDOT = -2990
112602 ZDOT = -899
022811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12903093
82 X = 3932863
00
Y = -5643440
27 feet Y = -1720120
59 meter
Z = 17280515
31 Z = 5267101
07
XDOT = 12784
663816 XDOT = 3896
765531
YDOT = 20221
772310 feet/sec YDOT = 6163
596200 meter/sec
ZDOT = -2938
097401 ZDOT = -895
532088
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 12317
54676918
00016717 00000-0 10270-3 0 9007
2 25544 51
6441 104
4941 0015548 275
3864 84
5513 15
51252857 1068
Satellite: ISS
Catalog Number: 25544
Epoch time: 12317
54676918 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 104
4941 deg
Eccentricity:
0015548
Arg of perigee: 275
3864 deg
Mean anomaly: 84
5513 deg
Mean motion: 15
51252857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 106
Checksum: 309
Coasting Arc #2 (Orbit 120)
---------------------------------------
Vector Time (GMT): 2012/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3639162
14 A = 6786526
50 meter
Y = 2586056
70 meter E =
0002602
Z = -5109316
86 I = 51
97556
XDOT = -2502
490036 Wp = 256
49736
YDOT = 7025
487623 meter/sec RA = 98
89744 deg
ZDOT = 1772
146967 TA = 30
57629
MA = 30
56112
Ha = 225
132 n
mi
Hp = 219
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11939508
35 X = 3634794
51
Y = 8484437
99 feet Y = 2626727
79 meter
Z = -16762850
58 Z = -5091647
97
XDOT = -8210
269146 XDOT = -2589
473470
YDOT = 23049
500077 feet/sec YDOT = 6997
016821 meter/sec
ZDOT = 5814
130469 ZDOT = 1759
778497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14083968
21 X = -4292793
51
Y = 4315068
59 feet Y = 1315232
91 meter
Z = -16689899
03 Z = -5087081
23
XDOT = -12843
600241 XDOT = -3914
729353
YDOT = -19616
396468 feet/sec YDOT = -5979
077643 meter/sec
ZDOT = 5762
089053 ZDOT = 1756
284743
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 12318
51305217
00016717 00000-0 10270-3 0 9017
2 25544 51
6454 99
6983 0015627 278
9224 81
0158 15
51329758 1219
Satellite: ISS
Catalog Number: 25544
Epoch time: 12318
51305217 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 99
6983 deg
Eccentricity:
0015627
Arg of perigee: 278
9224 deg
Mean anomaly: 81
0158 deg
Mean motion: 15
51329758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 121
Checksum: 310
Coasting Arc #3 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2012/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3565144
32 A = 6787797
19 meter
Y = -3183261
33 meter E =
0011180
Z = 4830230
55 I = 51
98368
XDOT = 2502
872427 Wp = 308
75927
YDOT = -6751
014688 meter/sec RA = 93
95094 deg
ZDOT = -2599
013185 TA = 166
78415
MA = 166
75484
Ha = 225
210 n
mi
Hp = 219
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11696667
73 X = -3552748
28
Y = -10443770
78 feet Y = -3223059
95 meter
Z = 15847213
10 Z = 4812940
70
XDOT = 8211
523712 XDOT = 2590
803434
YDOT = -22148
998319 feet/sec YDOT = -6722
534217 meter/sec
ZDOT = -8526
946144 ZDOT = -2586
640777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15427379
75 X = 4702265
35
Y = -3183620
14 feet Y = -970367
42 meter
Z = 15775901
37 Z = 4808494
74
XDOT = 12547
779782 XDOT = 3824
563277
YDOT = 18763
845944 feet/sec YDOT = 5719
220244 meter/sec
ZDOT = -8474
897156 ZDOT = -2583
148653
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 12319
54374171
00016717 00000-0 10270-3 0 9027
2 25544 51
6458 94
5812 0015561 282
8832 77
0581 15
51306776 1371
Satellite: ISS
Catalog Number: 25544
Epoch time: 12319
54374171 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 94
5812 deg
Eccentricity:
0015561
Arg of perigee: 282
8832 deg
Mean anomaly: 77
0581 deg
Mean motion: 15
51306776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 312
Coasting Arc #4 (Orbit 151)
---------------------------------------
Vector Time (GMT): 2012/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3525663
97 A = 6789167
07 meter
Y = 3741816
95 meter E =
0006753
Z = -4427606
41 I = 51
99116
XDOT = -2534
437940 Wp = 281
78796
YDOT = 6395
995307 meter/sec RA = 89
00756 deg
ZDOT = 3384
164095 TA = 22
29601
MA = 22
26667
Ha = 225
547 n
mi
Hp = 219
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11567139
01 X = 3505068
95
Y = 12276302
32 feet Y = 3781128
28 meter
Z = -14526267
75 Z = -4410528
27
XDOT = -8315
085106 XDOT = -2622
210804
YDOT = 20984
236570 feet/sec YDOT = 6367
162635 meter/sec
ZDOT = 11102
900573 ZDOT = 3371
638880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16775560
56 X = -5113190
86
Y = 2264133
95 feet Y = 690108
03 meter
Z = -14455899
27 Z = -4406158
10
XDOT = -11940
998857 XDOT = -3639
616452
YDOT = -17857
790053 feet/sec YDOT = -5443
054408 meter/sec
ZDOT = 11050
238899 ZDOT = 3368
112817
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 12320
50999622
00016717 00000-0 10270-3 0 9030
2 25544 51
6470 89
7853 0015731 286
8199 73
1227 15
51361582 1522
Satellite: ISS
Catalog Number: 25544
Epoch time: 12320
50999622 = yrday
fracday
Element set: 903
Inclination: 51
6470 deg
RA of node: 89
7853 deg
Eccentricity:
0015731
Arg of perigee: 286
8199 deg
Mean anomaly: 73
1227 deg
Mean motion: 15
51361582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 152
Checksum: 316
Coasting Arc #5 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2012/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3534665
76 A = 6790905
33 meter
Y = -4267469
58 meter E =
0008113
Z = 3934621
17 I = 51
99599
XDOT = 2597
620704 Wp = 333
43236
YDOT = -5926
701197 meter/sec RA = 84
06554 deg
ZDOT = -4090
699375 TA = 159
28185
MA = 159
24894
Ha = 225
638 n
mi
Hp = 219
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11596672
46 X = -3505797
14
Y = -14000884
44 feet Y = -4306835
29 meter
Z = 12908862
11 Z = 3917519
45
XDOT = 8522
377639 XDOT = 2683
573276
YDOT = -19444
557734 feet/sec YDOT = -5897
172094 meter/sec
ZDOT = -13420
929707 ZDOT = -4077
871694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18160789
89 X = 5535408
76
Y = -1583032
98 feet Y = -482508
45 meter
Z = 12838458
45 Z = 3913162
14
XDOT = 10927
055047 XDOT = 3330
566378
YDOT = 16847
881581 feet/sec YDOT = 5135
234306 meter/sec
ZDOT = -13367
052324 ZDOT = -4074
277548
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 12321
54065457
00016717 00000-0 10270-3 0 9046
2 25544 51
6475 84
6690 0015631 290
6498 69
2977 15
51368727 1687
Satellite: ISS
Catalog Number: 25544
Epoch time: 12321
54065457 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 84
6690 deg
Eccentricity:
0015631
Arg of perigee: 290
6498 deg
Mean anomaly: 69
2977 deg
Mean motion: 15
51368727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 168
Checksum: 337
Coasting Arc #6 (Orbit 182)
---------------------------------------
Vector Time (GMT): 2012/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3558314
42 A = 6792642
99 meter
Y = 4718247
76 meter E =
0011968
Z = -3333189
48 I = 51
99868
XDOT = -2722
203181 Wp = 305
96230
YDOT = 5393
651115 meter/sec RA = 79
12568 deg
ZDOT = 4723
864966 TA = 15
46956
MA = 15
43301
Ha = 226
065 n
mi
Hp = 219
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11674259
92 X = 3521481
60
Y = 15479815
47 feet Y = 4757833
32 meter
Z = -10935661
03 Z = -3315992
31
XDOT = -8931
112798 XDOT = -2805
261534
YDOT = 17695
705759 feet/sec YDOT = 5362
745036 meter/sec
ZDOT = 15498
244640 ZDOT = 4710
439060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19395581
72 X = -5911773
31
Y = 1125486
94 feet Y = 343048
42 meter
Z = -10864916
14 Z = -3311626
44
XDOT = -9584
409011 XDOT = -2921
327866
YDOT = -15940
884100 feet/sec YDOT = -4858
781474 meter/sec
ZDOT = 15441
937287 ZDOT = 4706
702485
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 12322
50688071
00016717 00000-0 10270-3 0 9057
2 25544 51
6482 79
8726 0015821 294
9048 65
0458 15
51395833 1833
Satellite: ISS
Catalog Number: 25544
Epoch time: 12322
50688071 = yrday
fracday
Element set: 905
Inclination: 51
6482 deg
RA of node: 79
8726 deg
Eccentricity:
0015821
Arg of perigee: 294
9048 deg
Mean anomaly: 65
0458 deg
Mean motion: 15
51395833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 183
Checksum: 324
Coasting Arc #7 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2012/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3607570
89 A = 6794254
77 meter
Y = -5109567
78 meter E =
0004536
Z = 2660507
75 I = 51
99775
XDOT = 2899
403839 Wp = 352
85214
YDOT = -4774
992590 meter/sec RA = 74
18786 deg
ZDOT = -5235
562681 TA = 157
36384
MA = 157
34383
Ha = 226
136 n
mi
Hp = 219
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11835862
50 X = -3563090
77
Y = -16763673
82 feet Y = -5149661
31 meter
Z = 8728699
98 Z = 2643089
98
XDOT = 9512
479786 XDOT = 2978
016725
YDOT = -15665
986188 feet/sec YDOT = -4742
129855 meter/sec
ZDOT = -17177
042918 ZDOT = -5221
286649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20532116
45 X = 6258189
09
Y = -886346
21 feet Y = -270158
33 meter
Z = 8657088
93 Z = 2638680
70
XDOT = 7873
207448 XDOT = 2399
753630
YDOT = 15084
414028 feet/sec YDOT = 4597
729396 meter/sec
ZDOT = -17117
275172 ZDOT = -5217
345472
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 12323
53750790
00016717 00000-0 10270-3 0 9060
2 25544 51
6483 74
7565 0015684 298
5820 61
3753 15
51426226 1999
Satellite: ISS
Catalog Number: 25544
Epoch time: 12323
53750790 = yrday
fracday
Element set: 906
Inclination: 51
6483 deg
RA of node: 74
7565 deg
Eccentricity:
0015684
Arg of perigee: 298
5820 deg
Mean anomaly: 61
3753 deg
Mean motion: 15
51426226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 199
Checksum: 323
Coasting Arc #8 (Orbit 213)
---------------------------------------
Vector Time (GMT): 2012/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3638027
16 A = 6795664
95 meter
Y = 5400502
67 meter E =
0016672
Z = -1905121
07 I = 51
99388
XDOT = -3157
250196 Wp = 327
85751
YDOT = 4122
052289 meter/sec RA = 69
25067 deg
ZDOT = 5646
921973 TA = 11
26485
MA = 11
22757
Ha = 226
562 n
mi
Hp = 219
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11935784
66 X = 3586621
95
Y = 17718184
62 feet Y = 5440897
99 meter
Z = -6250397
22 Z = -1887572
26
XDOT = -10358
432401 XDOT = -3230
540893
YDOT = 13523
793599 feet/sec YDOT = 4086
335995 meter/sec
ZDOT = 18526
646892 ZDOT = 5631
406158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21369185
44 X = -6513327
72
Y = 806996
43 feet Y = 245972
51 meter
Z = -6178281
09 Z = -1883140
08
XDOT = -5892
978741 XDOT = -1796
179920
YDOT = -14478
071049 feet/sec YDOT = -4412
916056 meter/sec
ZDOT = 18461
810199 ZDOT = 5627
159749
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 12324
50370540
00016717 00000-0 10270-3 0 9070
2 25544 51
6489 69
9594 0015866 303
0023 56
9603 15
51437924 2141
Satellite: ISS
Catalog Number: 25544
Epoch time: 12324
50370540 = yrday
fracday
Element set: 907
Inclination: 51
6489 deg
RA of node: 69
9594 deg
Eccentricity:
0015866
Arg of perigee: 303
0023 deg
Mean anomaly: 56
9603 deg
Mean motion: 15
51437924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 214
Checksum: 305
Coasting Arc #9 (Orbit 229)
---------------------------------------
Vector Time (GMT): 2012/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3663781
30 A = 6796538
89 meter
Y = -5617768
87 meter E =
0002289
Z = 1109016
56 I = 51
98519
XDOT = 3470
580135 Wp = 325
99502
YDOT = -3427
683756 meter/sec RA = 64
31523 deg
ZDOT = -5901
590996 TA = 202
05438
MA = 202
06422
Ha = 226
636 n
mi
Hp = 219
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12020279
87 X = -3606077
34
Y = -18431000
23 feet Y = -5658416
94 meter
Z = 3638505
77 Z = 1091357
99
XDOT = 11386
417765 XDOT = 3537
320134
YDOT = -11245
681613 feet/sec YDOT = -3388
500317 meter/sec
ZDOT = -19362
175183 ZDOT = -5884
568850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21999085
98 X = 6705321
41
Y = -867019
62 feet Y = -264267
58 meter
Z = 3565966
22 Z = 1086906
50
XDOT = 3678
325552 XDOT = 1121
153628
YDOT = 14043
842412 feet/sec YDOT = 4280
563167 meter/sec
ZDOT = -19291
171781 ZDOT = -5879
949159
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 12325
53430170
00016717 00000-0 10270-3 0 9081
2 25544 51
6485 64
8433 0015731 306
5615 53
4088 15
51477959 2308
Satellite: ISS
Catalog Number: 25544
Epoch time: 12325
53430170 = yrday
fracday
Element set: 908
Inclination: 51
6485 deg
RA of node: 64
8433 deg
Eccentricity:
0015731
Arg of perigee: 306
5615 deg
Mean anomaly: 53
4088 deg
Mean motion: 15
51477959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 230
Checksum: 303
Coasting Arc #10 (Orbit 244)
---------------------------------------
Vector Time (GMT): 2012/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3629682
73 A = 6796998
30 meter
Y = 5725304
35 meter E =
0019239
Z = -265059
24 I = 51
97347
XDOT = -3867
219787 Wp = 347
76283
YDOT = 2734
014022 meter/sec RA = 59
37870 deg
ZDOT = 6036
262325 TA = 9
39417
MA = 9
35824
Ha = 226
994 n
mi
Hp = 218
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11908407
92 X = 3566679
03
Y = 18783806
94 feet Y = 5765541
46 meter
Z = -869616
92 Z = -247579
21
XDOT = -12687
728961 XDOT = -3926
827823
YDOT = 8969
862276 feet/sec YDOT = 2690
435041 meter/sec
ZDOT = 19804
010252 ZDOT = 6017
330550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22222608
97 X = -6773451
21
Y = 957559
51 feet Y = 291864
14 meter
Z = -797838
45 Z = -243181
16
XDOT = -1317
435566 XDOT = -401
554361
YDOT = -13956
051053 feet/sec YDOT = -4253
804361 meter/sec
ZDOT = 19725
170067 ZDOT = 6012
231837
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 12326
50047072
00016717 00000-0 10270-3 0 9095
2 25544 51
6493 60
0457 0015876 310
9753 49
0024 15
51487844 2454
Satellite: ISS
Catalog Number: 25544
Epoch time: 12326
50047072 = yrday
fracday
Element set: 909
Inclination: 51
6493 deg
RA of node: 60
0457 deg
Eccentricity:
0015876
Arg of perigee: 310
9753 deg
Mean anomaly: 49
0024 deg
Mean motion: 15
51487844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 245
Checksum: 303
Coasting Arc #11 (Orbit 260)
---------------------------------------
Vector Time (GMT): 2012/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3561341
35 A = 6796742
61 meter
Y = -5761880
77 meter E =
0005140
Z = -579374
12 I = 51
95606
XDOT = 4299
523310 Wp = 304
36272
YDOT = -2050
684023 meter/sec RA = 54
44257 deg
ZDOT = -5993
848427 TA = 241
84962
MA = 241
90156
Ha = 227
112 n
mi
Hp = 218
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11684190
78 X = -3493831
59
Y = -18903808
30 feet Y = -5801328
45 meter
Z = -1900833
74 Z = -596511
24
XDOT = 14106
047604 XDOT = 4351
252124
YDOT = -6727
965955 feet/sec YDOT = -2002
314824 meter/sec
ZDOT = -19664
857045 ZDOT = -5972
835584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22191352
14 X = 6763924
13
Y = -1070423
33 feet Y = -326265
03 meter
Z = -1971176
19 Z = -600814
50
XDOT = -1070
882043 XDOT = -326
404847
YDOT = 14088
138333 feet/sec YDOT = 4294
064564 meter/sec
ZDOT = -19577
470363 ZDOT = -5967
212967
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 12327
53103677
00016717 00000-0 10270-3 0 9105
2 25544 51
6486 54
9296 0015797 314
5633 45
4228 15
51526640 2610
Satellite: ISS
Catalog Number: 25544
Epoch time: 12327
53103677 = yrday
fracday
Element set: 910
Inclination: 51
6486 deg
RA of node: 54
9296 deg
Eccentricity:
0015797
Arg of perigee: 314
5633 deg
Mean anomaly: 45
4228 deg
Mean motion: 15
51526640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 261
Checksum: 309
Coasting Arc #12 (Orbit 276)
---------------------------------------
Vector Time (GMT): 2012/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3392587
69 A = 6795959
29 meter
Y = 5697403
09 meter E =
0018675
Z = 1430276
69 I = 51
93598
XDOT = -4798
865883 Wp = 4
76848
YDOT = 1399
495058 meter/sec RA = 49
50345 deg
ZDOT = 5820
696846 TA = 10
76505
MA = 10
72514
Ha = 227
364 n
mi
Hp = 218
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11130537
03 X = 3321677
90
Y = 18692267
34 feet Y = 5734944
63 meter
Z = 4692508
81 Z = 1446585
81
XDOT = -15744
310639 XDOT = -4842
434797
YDOT = 4591
519218 feet/sec YDOT = 1345
587497 meter/sec
ZDOT = 19096
774430 ZDOT = 5797
277937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21715466
64 X = -6618874
23
Y = 1046818
13 feet Y = 319070
17 meter
Z = 4759415
12 Z = 1450669
73
XDOT = 3452
300692 XDOT = 1052
261251
YDOT = -14580
465183 feet/sec YDOT = -4444
125788 meter/sec
ZDOT = 18999
492156 ZDOT = 5791
045209
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 12328
56158710
00016717 00000-0 10270-3 0 9118
2 25544 51
6494 49
8121 0015882 318
9415 41
0540 15
51547073 2779
Satellite: ISS
Catalog Number: 25544
Epoch time: 12328
56158710 = yrday
fracday
Element set: 911
Inclination: 51
6494 deg
RA of node: 49
8121 deg
Eccentricity:
0015882
Arg of perigee: 318
9415 deg
Mean anomaly: 41
0540 deg
Mean motion: 15
51547073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 277
Checksum: 301
Coasting Arc #13 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2012/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3170518
69 A = 6794625
13 meter
Y = -5582332
01 meter E =
0009950
Z = -2236000
04 I = 51
91047
XDOT = 5292
930452 Wp = 325
79200
YDOT = -806
561612 meter/sec RA = 44
56279 deg
ZDOT = -5471
589404 TA = 238
91068
MA = 239
00836
Ha = 227
552 n
mi
Hp = 218
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10401964
21 X = -3096998
04
Y = -18314737
58 feet Y = -5617375
62 meter
Z = -7335958
13 Z = -2251224
10
XDOT = 17365
257388 XDOT = 5328
136489
YDOT = -2646
199516 feet/sec YDOT = -747
175816 meter/sec
ZDOT = -17951
408805 ZDOT = -5445
790563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21020246
19 X = 6406971
04
Y = -927441
77 feet Y = -282684
25 meter
Z = -7398368
43 Z = -2255022
70
XDOT = -5630
724203 XDOT = -1716
244737
YDOT = 15243
333056 feet/sec YDOT = 4646
167916 meter/sec
ZDOT = -17844
334348 ZDOT = -5438
953109
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 12329
52771438
00016717 00000-0 10270-3 0 9124
2 25544 51
6486 45
0157 0015876 322
5561 37
4483 15
51570936 2929
Satellite: ISS
Catalog Number: 25544
Epoch time: 12329
52771438 = yrday
fracday
Element set: 912
Inclination: 51
6486 deg
RA of node: 45
0157 deg
Eccentricity:
0015876
Arg of perigee: 322
5561 deg
Mean anomaly: 37
4483 deg
Mean motion: 15
51570936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 292
Checksum: 317
Coasting Arc #14 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2012/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2816485
88 A = 6792809
94 meter
Y = 5390338
17 meter E =
0015351
Z = 3003316
03 I = 51
88313
XDOT = -5820
118431 Wp = 15
43941
YDOT = 265
202154 meter/sec RA = 39
61740 deg
ZDOT = 4990
639774 TA = 18
80940
MA = 18
75274
Ha = 227
721 n
mi
Hp = 218
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9240439
25 X = 2741410
91
Y = 17684836
51 feet Y = 5421414
01 meter
Z = 9853399
05 Z = 3016816
50
XDOT = -19094
876742 XDOT = -5846
895334
YDOT = 870
085806 feet/sec YDOT = 199
968075 meter/sec
ZDOT = 16373
490072 ZDOT = 4962
300254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19919590
81 X = -6071491
28
Y = 506623
73 feet Y = 154418
91 meter
Z = 9908676
36 Z = 3020164
55
XDOT = 7660
721705 XDOT = 2334
987976
YDOT = -16185
030074 feet/sec YDOT = -4933
197166 meter/sec
ZDOT = 16255
952310 ZDOT = 4954
814264
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 12330
55823464
00016717 00000-0 10270-3 0 9137
2 25544 51
6493 39
8981 0015938 326
5648 33
4496 15
51605684 3089
Satellite: ISS
Catalog Number: 25544
Epoch time: 12330
55823464 = yrday
fracday
Element set: 913
Inclination: 51
6493 deg
RA of node: 39
8981 deg
Eccentricity:
0015938
Arg of perigee: 326
5648 deg
Mean anomaly: 33
4496 deg
Mean motion: 15
51605684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 330
Coasting Arc #15 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2012/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2409049
84 A = 6790903
12 meter
Y = -5181488
65 meter E =
0015087
Z = -3680912
60 I = 51
85194
XDOT = 6288
570919 Wp = 350
75243
YDOT = 185
568234 meter/sec RA = 34
66878 deg
ZDOT = -4359
909532 TA = 232
76851
MA = 232
90625
Ha = 227
954 n
mi
Hp = 217
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7903706
83 X = -2333048
87
Y = -16999634
69 feet Y = -5208003
03 meter
Z = -12076484
90 Z = -3692431
56
XDOT = 20631
794353 XDOT = 6307
208389
YDOT = 608
819664 feet/sec YDOT = 255
995385 meter/sec
ZDOT = -14304
165130 ZDOT = -4329
313986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18716558
76 X = 5704807
11
Y = 85350
89 feet Y = 26014
95 meter
Z = -12123563
51 Z = -3695262
16
XDOT = -9297
520455 XDOT = -2833
884235
YDOT = 17157
971405 feet/sec YDOT = 5229
749684 meter/sec
ZDOT = -14177
333927 ZDOT = -4321
251381
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 12331
52433544
00016717 00000-0 10270-3 0 9142
2 25544 51
6485 35
1014 0015959 330
5079 29
5171 15
51610353 3234
Satellite: ISS
Catalog Number: 25544
Epoch time: 12331
52433544 = yrday
fracday
Element set: 914
Inclination: 51
6485 deg
RA of node: 35
1014 deg
Eccentricity:
0015959
Arg of perigee: 330
5079 deg
Mean anomaly: 29
5171 deg
Mean motion: 15
51610353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 280
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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