[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 22nd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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 610)
---------------------------------------
Vector Time (GMT): 2011/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4597882
82 A = 6766719
96 meter
Y = -3452658
03 meter E =
0010505
Z = -3559251
60 I = 51
59823
XDOT = 5571
898902 Wp = 10
12248
YDOT = 2832
289777 meter/sec RA = 352
47977 deg
ZDOT = 4462
499107 TA = 307
68523
MA = 307
78045
Ha = 213
845 n
mi
Hp = 204
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15084917
40 X = 4653439
31
Y = -11327618
22 feet Y = -3400930
85 meter
Z = -11677334
65 Z = -3536780
72
XDOT = 18280
508208 XDOT = 5518
135908
YDOT = 9292
289295 feet/sec YDOT = 2894
297255 meter/sec
ZDOT = 14640
745103 ZDOT = 4489
436550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16992950
89 X = -5179451
43
Y = -8320919
48 feet Y = -2536216
26 meter
Z = -11585841
84 Z = -3531364
59
XDOT = -632
947123 XDOT = -192
922283
YDOT = -19189
083868 feet/sec YDOT = -5848
832763 meter/sec
ZDOT = 14749
976125 ZDOT = 4495
792723
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 11201
50742287
00016717 00000-0 10270-3 0 9007
2 25544 51
6391 352
9856 0011300 343
3233 16
7550 15
60089199 6111
Satellite: ISS
Catalog Number: 25544
Epoch time: 11201
50742287 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 352
9856 deg
Eccentricity:
0011300
Arg of perigee: 343
3233 deg
Mean anomaly: 16
7550 deg
Mean motion: 15
60089199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 611
Checksum: 282
Coasting Arc #2 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2011/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6578573
05 A = 6771918
57 meter
Y = 1604331
73 meter E =
0006964
Z = 175025
65 I = 51
58563
XDOT = -1285
198041 Wp = 66
72394
YDOT = -4593
680884 meter/sec RA = 347
46916 deg
ZDOT = -6006
441306 TA = 111
38623
MA = 111
31191
Ha = 213
919 n
mi
Hp = 204
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21583244
90 X = -6596874
29
Y = 5263555
56 feet Y = 1530663
78 meter
Z = 574231
14 Z = 143023
00
XDOT = -4216
529006 XDOT = -1204
557261
YDOT = -15071
131510 feet/sec YDOT = -4607
601466 meter/sec
ZDOT = -19706
172263 ZDOT = -6012
489149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14815798
84 X = 4515855
49
Y = 16557960
52 feet Y = 5046866
37 meter
Z = 444147
53 Z = 135376
17
XDOT = -10154
505743 XDOT = -3095
093350
YDOT = 9637
242674 feet/sec YDOT = 2937
431567 meter/sec
ZDOT = -19730
441433 ZDOT = -6013
838549
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 11202
53231528
00016717 00000-0 10270-3 0 9013
2 25544 51
6384 347
8295 0011509 346
9718 13
1139 15
60131852 6276
Satellite: ISS
Catalog Number: 25544
Epoch time: 11202
53231528 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 347
8295 deg
Eccentricity:
0011509
Arg of perigee: 346
9718 deg
Mean anomaly: 13
1139 deg
Mean motion: 15
60131852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 293
Coasting Arc #3 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2011/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5844945
68 A = 6767202
75 meter
Y = 879138
73 meter E =
0015761
Z = 3273365
83 I = 51
54210
XDOT = -3403
417819 Wp = 42
52414
YDOT = 5014
471144 meter/sec RA = 342
45932 deg
ZDOT = 4728
540562 TA = 355
69613
MA = 355
70966
Ha = 213
864 n
mi
Hp = 204
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19176330
96 X = 5818779
31
Y = 2884313
43 feet Y = 944353
93 meter
Z = 10739389
21 Z = 3301696
80
XDOT = -11166
068960 XDOT = -3482
207818
YDOT = 16451
676981 feet/sec YDOT = 4975
971161 meter/sec
ZDOT = 15513
584520 ZDOT = 4711
815920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6775039
01 X = -2065031
89
Y = -18101556
20 feet Y = -5517354
33 meter
Z = 10854396
50 Z = 3308420
05
XDOT = 18531
549453 XDOT = 5648
416273
YDOT = 2329
295174 feet/sec YDOT = 709
969169 meter/sec
ZDOT = 15445
337658 ZDOT = 4707
738918
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 11203
55719681
00016717 00000-0 10270-3 0 9028
2 25544 51
6396 342
6739 0011350 350
5849 9
5092 15
60147682 6438
Satellite: ISS
Catalog Number: 25544
Epoch time: 11203
55719681 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 342
6739 deg
Eccentricity:
0011350
Arg of perigee: 350
5849 deg
Mean anomaly: 9
5092 deg
Mean motion: 15
60147682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 310
Coasting Arc #4 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2011/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2849689
33 A = 6760325
28 meter
Y = -3286084
92 meter E =
0018841
Z = -5188781
89 I = 51
49080
XDOT = 6565
205221 Wp = 43
03395
YDOT = -3771
466570 meter/sec RA = 337
40694 deg
ZDOT = -1206
222390 TA = 215
30476
MA = 215
42968
Ha = 214
134 n
mi
Hp = 204
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9349374
46 X = -2787525
95
Y = -10781118
51 feet Y = -3317603
86 meter
Z = -17023562
64 Z = -5202474
86
XDOT = 21539
387208 XDOT = 6612
750109
YDOT = -12373
577986 feet/sec YDOT = -3697
784504 meter/sec
ZDOT = -3957
422539 ZDOT = -1174
213734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4693134
93 X = -1430467
53
Y = 13406285
85 feet Y = 4086235
93 meter
Z = -17078963
32 Z = -5205668
02
XDOT = -20539
248190 XDOT = -6260
362848
YDOT = -12111
270841 feet/sec YDOT = -3691
515352 meter/sec
ZDOT = -3827
184305 ZDOT = -1166
525776
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 11204
51801340
00016717 00000-0 10270-3 0 9030
2 25544 51
6399 337
8417 0011511 354
6760 5
4271 15
60154437 6582
Satellite: ISS
Catalog Number: 25544
Epoch time: 11204
51801340 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 337
8417 deg
Eccentricity:
0011511
Arg of perigee: 354
6760 deg
Mean anomaly: 5
4271 deg
Mean motion: 15
60154437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 286
Coasting Arc #5 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2011/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1186149
84 A = 6762818
02 meter
Y = 4784945
16 meter E =
0016655
Z = 4630551
95 I = 51
47133
XDOT = -7026
527161 Wp = 25
47003
YDOT = 1079
491353 meter/sec RA = 332
33334 deg
ZDOT = -2896
738998 TA = 93
46517
MA = 93
27466
Ha = 214
354 n
mi
Hp = 203
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3891567
73 X = -1262062
07
Y = 15698638
96 feet Y = 4771255
99 meter
Z = 15192099
58 Z = 4624605
78
XDOT = -23052
910633 XDOT = -7024
004296
YDOT = 3541
638296 feet/sec YDOT = 1000
930845 meter/sec
ZDOT = -9503
736870 ZDOT = -2930
867352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15502206
71 X = 4725072
61
Y = -4692078
89 feet Y = -1430145
65 meter
Z = 15167644
42 Z = 4623098
02
XDOT = 14560
086599 XDOT = 4437
914395
YDOT = 16737
077473 feet/sec YDOT = 5101
461214 meter/sec
ZDOT = -9642
409416 ZDOT = -2939
006390
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 11205
54287355
00016717 00000-0 10270-3 0 9049
2 25544 51
6400 332
6849 0011459 358
8393 1
2734 15
60127801 6747
Satellite: ISS
Catalog Number: 25544
Epoch time: 11205
54287355 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 332
6849 deg
Eccentricity:
0011459
Arg of perigee: 358
8393 deg
Mean anomaly: 1
2734 deg
Mean motion: 15
60127801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 300
Coasting Arc #6 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2011/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4495787
11 A = 6770348
91 meter
Y = -4679965
53 meter E =
0017902
Z = -1895075
78 I = 51
47144
XDOT = 4725
839106 Wp = 15
38786
YDOT = 2278
190288 meter/sec RA = 327
29563 deg
ZDOT = 5614
341952 TA = 323
61512
MA = 323
73669
Ha = 214
464 n
mi
Hp = 203
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14749957
71 X = 4556991
10
Y = -15354217
62 feet Y = -4629348
47 meter
Z = -6217440
24 Z = -1873087
33
XDOT = 15504
721477 XDOT = 4672
739507
YDOT = 7474
377586 feet/sec YDOT = 2330
739957 meter/sec
ZDOT = 18419
757062 ZDOT = 5637
171149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20861982
67 X = -6358732
32
Y = -4381444
97 feet Y = -1335464
43 meter
Z = -6127840
87 Z = -1867765
90
XDOT = -2155
476587 XDOT = -656
989264
YDOT = -15492
629564 feet/sec YDOT = -4722
153491 meter/sec
ZDOT = 18512
326619 ZDOT = 5642
557153
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 11206
50366682
00016717 00000-0 10270-3 0 9058
2 25544 51
6408 327
8515 0011665 1
8357 358
2840 15
60163965 6895
Satellite: ISS
Catalog Number: 25544
Epoch time: 11206
50366682 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 327
8515 deg
Eccentricity:
0011665
Arg of perigee: 1
8357 deg
Mean anomaly: 358
2840 deg
Mean motion: 15
60163965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 317
Coasting Arc #7 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2011/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5916015
01 A = 6770307
81 meter
Y = 2781636
70 meter E =
0008188
Z = -1780103
71 I = 51
44703
XDOT = -717
895917 Wp = 43
90709
YDOT = -5135
103881 meter/sec RA = 322
28437 deg
ZDOT = -5648
216177 TA = 155
72387
MA = 155
68527
Ha = 214
495 n
mi
Hp = 203
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19409498
06 X = -5938032
80
Y = 9126104
66 feet Y = 2715357
33 meter
Z = -5840235
26 Z = -1808896
49
XDOT = -2355
301564 XDOT = -632
983158
YDOT = -16847
453678 feet/sec YDOT = -5142
656344 meter/sec
ZDOT = -18530
892970 ZDOT = -5651
498071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18214483
86 X = 5551774
68
Y = 11263450
94 feet Y = 3433099
85 meter
Z = -5957348
37 Z = -1815799
78
XDOT = -12077
914409 XDOT = -3681
348312
YDOT = 9740
256230 feet/sec YDOT = 2968
830099 meter/sec
ZDOT = -18543
896065 ZDOT = -5652
179521
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 11207
52850307
00016717 00000-0 10270-3 0 9064
2 25544 51
6408 322
6954 0011654 5
7939 354
3349 15
60205142 7056
Satellite: ISS
Catalog Number: 25544
Epoch time: 11207
52850307 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 322
6954 deg
Eccentricity:
0011654
Arg of perigee: 5
7939 deg
Mean anomaly: 354
3349 deg
Mean motion: 15
60205142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 294
Coasting Arc #8 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2011/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4950725
89 A = 6762512
72 meter
Y = 399286
22 meter E =
0012370
Z = 4577264
70 I = 51
39885
XDOT = -3271
341059 Wp = 49
42467
YDOT = 6278
988569 meter/sec RA = 317
24366 deg
ZDOT = 2993
122417 TA = 10
70412
MA = 10
67782
Ha = 214
418 n
mi
Hp = 203
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16242539
02 X = 4923657
88
Y = 1309994
16 feet Y = 454496
31 meter
Z = 15017272
64 Z = 4601249
25
XDOT = -10732
746258 XDOT = -3355
850606
YDOT = 20600
356196 feet/sec YDOT = 6241
933531 meter/sec
ZDOT = 9819
955436 ZDOT = 2977
026046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7953216
87 X = -2424140
50
Y = -14119066
80 feet Y = -4303491
56 meter
Z = 15114659
44 Z = 4606948
20
XDOT = 22082
461652 XDOT = 6730
734312
YDOT = -2006
055313 feet/sec YDOT = -611
445659 meter/sec
ZDOT = 9754
187508 ZDOT = 2973
076352
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 11208
55332660
00016717 00000-0 10270-3 0 9076
2 25544 51
6416 317
5394 0011669 9
3477 350
7894 15
60242924 7211
Satellite: ISS
Catalog Number: 25544
Epoch time: 11208
55332660 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 317
5394 deg
Eccentricity:
0011669
Arg of perigee: 9
3477 deg
Mean anomaly: 350
7894 deg
Mean motion: 15
60242924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 311
Coasting Arc #9 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2011/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2251948
22 A = 6760010
04 meter
Y = -3704221
90 meter E =
0019236
Z = -5199986
06 I = 51
36896
XDOT = 5710
634848 Wp = 60
51064
YDOT = -4997
192877 meter/sec RA = 312
16527 deg
ZDOT = 1099
026456 TA = 219
99122
MA = 220
13303
Ha = 214
666 n
mi
Hp = 202
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7388281
57 X = -2185099
46
Y = -12152959
00 feet Y = -3729030
14 meter
Z = -17060321
71 Z = -5210763
89
XDOT = 18735
678636 XDOT = 5760
751240
YDOT = -16394
989755 feet/sec YDOT = -4933
053002 meter/sec
ZDOT = 3605
729842 ZDOT = 1126
889259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5773082
92 X = -1759635
67
Y = 12940821
89 feet Y = 3944362
51 meter
Z = -17103869
04 Z = -5213259
28
XDOT = -23221
687798 XDOT = -7077
970441
YDOT = -5497
308104 feet/sec YDOT = -1675
579510 meter/sec
ZDOT = 3719
204471 ZDOT = 1133
613523
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 11209
51409032
00016717 00000-0 10270-3 0 9082
2 25544 51
6417 312
7069 0011841 13
1551 346
9912 15
60249462 7364
Satellite: ISS
Catalog Number: 25544
Epoch time: 11209
51409032 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 312
7069 deg
Eccentricity:
0011841
Arg of perigee: 13
1551 deg
Mean anomaly: 346
9912 deg
Mean motion: 15
60249462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 290
Coasting Arc #10 (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 = -1095511
16 A = 6767040
83 meter
Y = 5808955
44 meter E =
0019498
Z = 3291604
89 I = 51
37258
XDOT = -5876
150279 Wp = 55
89239
YDOT = 1563
772540 meter/sec RA = 307
09987 deg
ZDOT = -4684
743136 TA = 85
59168
MA = 85
36894
Ha = 214
855 n
mi
Hp = 202
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3594196
71 X = -1176376
23
Y = 19058252
76 feet Y = 5796252
27 meter
Z = 10799228
64 Z = 3286087
24
XDOT = -19278
708263 XDOT = -5870
442885
YDOT = 5130
487337 feet/sec YDOT = 1498
094268 meter/sec
ZDOT = -15369
892180 ZDOT = -4713
274744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17569212
83 X = 5355096
07
Y = -8243122
00 feet Y = -2512503
58 meter
Z = 10776469
18 Z = 3284667
81
XDOT = 14826
777947 XDOT = 4519
201918
YDOT = 11224
528783 feet/sec YDOT = 3421
236373 meter/sec
ZDOT = -15485
873913 ZDOT = -4720
094369
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
53889366
00016717 00000-0 10270-3 0 9099
2 25544 51
6415 307
5508 0011846 17
3391 342
8167 15
60232657 7528
Satellite: ISS
Catalog Number: 25544
Epoch time: 11210
53889366 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 307
5508 deg
Eccentricity:
0011846
Arg of perigee: 17
3391 deg
Mean anomaly: 342
8167 deg
Mean motion: 15
60232657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 311
Coasting Arc #11 (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 = 3701379
58 A = 6771608
10 meter
Y = -5651555
57 meter E =
0023889
Z = 169107
38 I = 51
37107
XDOT = 3928
496922 Wp = 33
81732
YDOT = 2764
109414 meter/sec RA = 302
07586 deg
ZDOT = 6002
445017 TA = 328
01831
MA = 328
16307
Ha = 214
944 n
mi
Hp = 202
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12143633
80 X = 3763479
81
Y = -18541849
00 feet Y = -5609817
29 meter
Z = 554814
24 Z = 187238
56
XDOT = 12888
769429 XDOT = 3868
138139
YDOT = 9068
600438 feet/sec YDOT = 2807
702270 meter/sec
ZDOT = 19693
061081 ZDOT = 6021
382766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22114523
06 X = -6740506
63
Y = 1458876
14 feet Y = 444665
45 meter
Z = 628788
82 Z = 191654
83
XDOT = -332
436408 XDOT = -101
326617
YDOT = -14044
269422 feet/sec YDOT = -4280
693320 meter/sec
ZDOT = 19769
823148 ZDOT = 6025
842096
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
56368491
00016717 00000-0 10270-3 0 9106
2 25544 51
6419 302
3949 0012049 20
5484 339
6154 15
60243568 7689
Satellite: ISS
Catalog Number: 25544
Epoch time: 11211
56368491 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 302
3949 deg
Eccentricity:
0012049
Arg of perigee: 20
5484 deg
Mean anomaly: 339
6154 deg
Mean motion: 15
60243568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 309
Coasting Arc #12 (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 = -4822272
06 A = 6765947
61 meter
Y = 3124998
21 meter E =
0015557
Z = -3591740
35 I = 51
33632
XDOT = -765
375092 Wp = 40
96564
YDOT = -6232
008089 meter/sec RA = 297
04798 deg
ZDOT = -4393
871857 TA = 181
78493
MA = 181
79048
Ha = 214
986 n
mi
Hp = 202
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15821102
55 X = -4839410
45
Y = 10252618
78 feet Y = 3070977
00 meter
Z = -11783925
04 Z = -3615207
76
XDOT = -2511
073135 XDOT = -674
286631
YDOT = -20446
220763 feet/sec YDOT = -6240
057424 meter/sec
ZDOT = -14415
590081 ZDOT = -4397
369058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17772585
01 X = 5417083
91
Y = 6107281
67 feet Y = 1861499
45 meter
Z = -11879423
40 Z = -3620848
25
XDOT = -14181
020112 XDOT = -4322
374930
YDOT = 13196
174464 feet/sec YDOT = 4022
193976 meter/sec
ZDOT = -14429
446348 ZDOT = -4398
095247
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
52441579
00016717 00000-0 10270-3 0 9113
2 25544 51
6408 297
5616 0011940 24
1166 336
0546 15
60270853 7839
Satellite: ISS
Catalog Number: 25544
Epoch time: 11212
52441579 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 297
5616 deg
Eccentricity:
0011940
Arg of perigee: 24
1166 deg
Mean anomaly: 336
0546 deg
Mean motion: 15
60270853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 296
Coasting Arc #13 (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 = 4170803
84 A = 6759492
40 meter
Y = 878057
42 meter E =
0012428
Z = 5238390
77 I = 51
30249
XDOT = -2361
898384 Wp = 40
89597
YDOT = 7283
681797 meter/sec RA = 291
97394 deg
ZDOT = 668
006689 TA = 42
75870
MA = 42
66208
Ha = 214
874 n
mi
Hp = 202
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13683739
62 X = 4135228
73
Y = 2880765
81 feet Y = 924498
80 meter
Z = 17186321
42 Z = 5258565
64
XDOT = -7749
010447 XDOT = -2446
415362
YDOT = 23896
593823 feet/sec YDOT = 7256
797027 meter/sec
ZDOT = 2191
622995 ZDOT = 656
327834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6298124
44 X = -1919668
33
Y = -12371550
71 feet Y = -3770848
66 meter
Z = 17268223
63 Z = 5263354
56
XDOT = 22560
195670 XDOT = 6876
347640
YDOT = -8530
737736 feet/sec YDOT = -2600
168862 meter/sec
ZDOT = 2143
790381 ZDOT = 653
427308
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
54918373
00016717 00000-0 10270-3 0 9128
2 25544 51
6409 292
4048 0011994 27
4619 332
7169 15
60325635 7991
Satellite: ISS
Catalog Number: 25544
Epoch time: 11213
54918373 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 292
4048 deg
Eccentricity:
0011994
Arg of perigee: 27
4619 deg
Mean anomaly: 332
7169 deg
Mean motion: 15
60325635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 323
Coasting Arc #14 (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 = -2240353
85 A = 6763152
72 meter
Y = -4661193
36 meter E =
0016440
Z = -4366739
22 I = 51
30330
XDOT = 4428
435530 Wp = 63
82942
YDOT = -5275
546804 meter/sec RA = 286
89074 deg
ZDOT = 3376
288569 TA = 240
41818
MA = 240
58211
Ha = 215
089 n
mi
Hp = 201
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7350242
30 X = -2166852
59
Y = -15292629
14 feet Y = -4685835
32 meter
Z = -14326572
26 Z = -4377444
19
XDOT = 14528
987958 XDOT = 4470
697534
YDOT = -17308
224421 feet/sec YDOT = -5225
789099 meter/sec
ZDOT = 11077
062234 ZDOT = 3397
904011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7060868
16 X = -2152152
62
Y = 15388108
95 feet Y = 4690295
61 meter
Z = -14369811
56 Z = -4379918
56
XDOT = -21432
403665 XDOT = -6532
596637
YDOT = 540
021289 feet/sec YDOT = 164
598489 meter/sec
ZDOT = 11165
138783 ZDOT = 3403
134301
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
50989603
00016717 00000-0 10270-3 0 9130
2 25544 51
6397 287
5717 0012177 31
6125 328
5760 15
60336110 8146
Satellite: ISS
Catalog Number: 25544
Epoch time: 11214
50989603 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 287
5717 deg
Eccentricity:
0012177
Arg of perigee: 31
6125 deg
Mean anomaly: 328
5760 deg
Mean motion: 15
60336110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 814
Checksum: 300
Coasting Arc #15 (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 = -314657
85 A = 6770587
09 meter
Y = 6632771
36 meter E =
0019222
Z = 1316139
36 I = 51
32023
XDOT = -4939
082406 Wp = 80
66560
YDOT = 931
419506 meter/sec RA = 281
84628 deg
ZDOT = -5799
208240 TA = 84
91283
MA = 84
69346
Ha = 215
241 n
mi
Hp = 201
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1032342
02 X = -395196
86
Y = 21761060
88 feet Y = 6628802
32 meter
Z = 4318042
54 Z = 1314415
25
XDOT = -16204
338604 XDOT = -4920
959591
YDOT = 3055
838275 feet/sec YDOT = 876
289085 meter/sec
ZDOT = -19026
273753 ZDOT = -5823
157878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17133944
02 X = 5222426
14
Y = -13457369
95 feet Y = -4101806
36 meter
Z = 4310701
64 Z = 1313901
86
XDOT = 11867
733903 XDOT = 3617
285294
YDOT = 8904
748861 feet/sec YDOT = 2714
167453 meter/sec
ZDOT = -19123
602702 ZDOT = -5828
874104
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
53464394
00016717 00000-0 10270-3 0 9140
2 25544 51
6394 282
4144 0012322 34
9628 325
2335 15
60343162 8302
Satellite: ISS
Catalog Number: 25544
Epoch time: 11215
53464394 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 282
4144 deg
Eccentricity:
0012322
Arg of perigee: 34
9628 deg
Mean anomaly: 325
2335 deg
Mean motion: 15
60343162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 286
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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