[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 27th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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
091/21:57:19
525 -1
5 3
1 3
1
N/A -1
3 0
0 214
2
000/00:06:39
051 2
4 -0
0 207
8
Coasting Arc #1 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2012/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3413985
31 A = 6766313
59 meter
Y = 4039139
80 meter E =
0014119
Z = -4215784
12 I = 51
56880
XDOT = -6531
073558 Wp = 160
77423
YDOT = 1728
301054 meter/sec RA = 190
55914 deg
ZDOT = -3649
576529 TA = 71
94876
MA = 71
79497
Ha = 216
689 n
mi
Hp = 204
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11200739
20 X = 3389044
43
Y = 13251771
00 feet Y = 4077177
09 meter
Z = -13831312
74 Z = -4199260
25
XDOT = -21427
406687 XDOT = -6532
185537
YDOT = 5670
279050 feet/sec YDOT = 1655
259852 meter/sec
ZDOT = -11973
676276 ZDOT = -3681
307122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11417854
67 X = 3480162
10
Y = 13136341
21 feet Y = 4003956
80 meter
Z = -13763732
78 Z = -4195185
75
XDOT = -20337
977253 XDOT = -6199
015467
YDOT = 5052
424685 feet/sec YDOT = 1539
979044 meter/sec
ZDOT = -12103
969423 ZDOT = -3689
289880
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 12083
52277957
00016717 00000-0 10270-3 0 9005
2 25544 51
6417 191
4878 0016249 189
8301 170
2539 15
59471904 4664
Satellite: ISS
Catalog Number: 25544
Epoch time: 12083
52277957 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 191
4878 deg
Eccentricity:
0016249
Arg of perigee: 189
8301 deg
Mean anomaly: 170
2539 deg
Mean motion: 15
59471904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 333
Coasting Arc #2 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2012/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 440863
77 A = 6761603
05 meter
Y = -4178894
09 meter E =
0015697
Z = 5298516
85 I = 51
58432
XDOT = 7637
989016 Wp = 185
41533
YDOT = 770
541659 meter/sec RA = 185
50544 deg
ZDOT = -43
121533 TA = 264
90583
MA = 265
08501
Ha = 216
309 n
mi
Hp = 204
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1446403
45 X = 461821
16
Y = -13710282
44 feet Y = -4173846
26 meter
Z = 17383585
46 Z = 5300709
96
XDOT = 25059
019082 XDOT = 7629
014464
YDOT = 2528
023815 feet/sec YDOT = 855
904189 meter/sec
ZDOT = -141
474846 ZDOT = -6
038300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 965977
97 X = 294430
08
Y = -13740808
42 feet Y = -4188198
41 meter
Z = 17392815
80 Z = 5301330
26
XDOT = 24117
096366 XDOT = 7350
890972
YDOT = 1772
509466 feet/sec YDOT = 540
260885 meter/sec
ZDOT = 10
654997 ZDOT = 3
247643
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 12084
54806115
00016717 00000-0 10270-3 0 9013
2 25544 51
6419 186
3353 0016064 193
7106 166
3615 15
59551284 4828
Satellite: ISS
Catalog Number: 25544
Epoch time: 12084
54806115 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 186
3353 deg
Eccentricity:
0016064
Arg of perigee: 193
7106 deg
Mean anomaly: 166
3615 deg
Mean motion: 15
59551284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 482
Checksum: 305
Coasting Arc #3 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2012/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4260431
86 A = 6766163
96 meter
Y = 3249242
24 meter E =
0018123
Z = -4146424
53 I = 51
62998
XDOT = -5965
798881 Wp = 171
97793
YDOT = -3016
632375 meter/sec RA = 180
45381 deg
ZDOT = 3750
335566 TA = 136
70576
MA = 136
56320
Ha = 216
081 n
mi
Hp = 204
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13977794
80 X = -4276306
39
Y = 10660243
56 feet Y = 3201510
26 meter
Z = -13603755
02 Z = -4167160
52
XDOT = -19572
830975 XDOT = -5949
841277
YDOT = -9897
087843 feet/sec YDOT = -3083
256008 meter/sec
ZDOT = 12304
250546 ZDOT = 3721
392912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13406860
86 X = -4086411
19
Y = 11267125
24 feet Y = 3434219
77 meter
Z = -13689034
36 Z = -4172417
67
XDOT = -19246
472984 XDOT = -5866
324965
YDOT = -8034
833378 feet/sec YDOT = -2449
017214 meter/sec
ZDOT = 12185
642095 ZDOT = 3714
183711
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 12085
50924555
00016717 00000-0 10270-3 0 9020
2 25544 51
6415 181
5051 0015998 197
0823 162
9796 15
59565022 4977
Satellite: ISS
Catalog Number: 25544
Epoch time: 12085
50924555 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 181
5051 deg
Eccentricity:
0015998
Arg of perigee: 197
0823 deg
Mean anomaly: 162
9796 deg
Mean motion: 15
59565022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 497
Checksum: 331
Coasting Arc #4 (Orbit 512)
---------------------------------------
Vector Time (GMT): 2012/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6479817
56 A = 6772918
90 meter
Y = -1481164
39 meter E =
0022928
Z = 1216787
19 I = 51
68217
XDOT = 2128
447301 Wp = 164
68807
YDOT = 4485
132175 meter/sec RA = 175
44231 deg
ZDOT = -5871
604493 TA = 2
04388
MA = 2
03452
Ha = 215
868 n
mi
Hp = 204
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21259243
96 X = 6489987
73
Y = -4859463
23 feet Y = -1408646
09 meter
Z = 3992083
96 Z = 1248290
87
XDOT = 6983
094818 XDOT = 2106
658557
YDOT = 14715
000573 feet/sec YDOT = 4508
811439 meter/sec
ZDOT = -19263
794267 ZDOT = -5861
317854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20894512
26 X = 6368647
34
Y = -6159499
91 feet Y = -1877415
57 meter
Z = 4121466
85 Z = 1256223
09
XDOT = 7544
746191 XDOT = 2299
638639
YDOT = 12724
414769 feet/sec YDOT = 3878
401622 meter/sec
ZDOT = -19221
829247 ZDOT = -5858
813555
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 12086
53448840
00016717 00000-0 10270-3 0 9033
2 25544 51
6407 176
3526 0015930 200
6453 159
4061 15
59561084 5132
Satellite: ISS
Catalog Number: 25544
Epoch time: 12086
53448840 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 176
3526 deg
Eccentricity:
0015930
Arg of perigee: 200
6453 deg
Mean anomaly: 159
4061 deg
Mean motion: 15
59561084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 513
Checksum: 299
Coasting Arc #5 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2012/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6353274
53 A = 6771348
08 meter
Y = -724685
49 meter E =
0011850
Z = 2240286
61 I = 51
70784
XDOT = 2477
682148 Wp = 146
59621
YDOT = -4784
609461 meter/sec RA = 170
44933 deg
ZDOT = 5455
389199 TA = 238
31891
MA = 238
43452
Ha = 215
596 n
mi
Hp = 205
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20844076
54 X = -6355581
62
Y = -2377577
05 feet Y = -795744
46 meter
Z = 7350021
69 Z = 2209416
98
XDOT = 8128
878439 XDOT = 2504
499275
YDOT = -15697
537602 feet/sec YDOT = -4756
752138 meter/sec
ZDOT = 17898
258527 ZDOT = 5467
491227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21010744
82 X = -6404075
02
Y = -723176
39 feet Y = -220424
16 meter
Z = 7223353
53 Z = 2201678
16
XDOT = 6704
938637 XDOT = 2043
665296
YDOT = -14747
758013 feet/sec YDOT = -4495
116642 meter/sec
ZDOT = 17948
208259 ZDOT = 5470
613877
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 12087
55970846
00016717 00000-0 10270-3 0 9043
2 25544 51
6409 171
1989 0015791 204
8369 155
2028 15
59619237 5295
Satellite: ISS
Catalog Number: 25544
Epoch time: 12087
55970846 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 171
1989 deg
Eccentricity:
0015791
Arg of perigee: 204
8369 deg
Mean anomaly: 155
2028 deg
Mean motion: 15
59619237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 529
Checksum: 342
Coasting Arc #6 (Orbit 543)
---------------------------------------
Vector Time (GMT): 2012/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3860321
35 A = 6763841
86 meter
Y = 2872323
36 meter E =
0010621
Z = -4751728
02 I = 51
71164
XDOT = -6114
638909 Wp = 164
34147
YDOT = 3784
583256 meter/sec RA = 165
42893 deg
ZDOT = -2691
248720 TA = 79
19515
MA = 79
07562
Ha = 215
421 n
mi
Hp = 205
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12665096
29 X = 3850998
45
Y = 9423633
07 feet Y = 2915439
42 meter
Z = -15589658
86 Z = -4732997
51
XDOT = -20061
151275 XDOT = -6143
430898
YDOT = 12416
611731 feet/sec YDOT = 3716
044426 meter/sec
ZDOT = -8829
556167 ZDOT = -2721
023648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13604965
02 X = 4146793
34
Y = 8154799
91 feet Y = 2485583
01 meter
Z = -15512935
01 Z = -4728342
59
XDOT = -18128
620355 XDOT = -5525
603484
YDOT = 13286
689881 feet/sec YDOT = 4049
783076 meter/sec
ZDOT = -8952
006637 ZDOT = -2728
571623
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 12088
52083529
00016717 00000-0 10270-3 0 9055
2 25544 51
6398 166
3680 0015726 208
7147 151
3144 15
59623665 5444
Satellite: ISS
Catalog Number: 25544
Epoch time: 12088
52083529 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 166
3680 deg
Eccentricity:
0015726
Arg of perigee: 208
7147 deg
Mean anomaly: 151
3144 deg
Mean motion: 15
59623665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 544
Checksum: 323
Coasting Arc #7 (Orbit 559)
---------------------------------------
Vector Time (GMT): 2012/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -79860
97 A = 6761632
42 meter
Y = -4325284
23 meter E =
0012068
Z = 5199201
49 I = 51
73495
XDOT = 7403
636037 Wp = 205
70111
YDOT = -1606
063079 meter/sec RA = 160
37835 deg
ZDOT = -1234
081463 TA = 256
04794
MA = 256
18218
Ha = 215
009 n
mi
Hp = 205
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -262011
07 X = -56745
42
Y = -14190565
05 feet Y = -4326047
73 meter
Z = 17057747
66 Z = 5198869
93
XDOT = 24290
144479 XDOT = 7427
039999
YDOT = -5269
235823 feet/sec YDOT = -1523
140260 meter/sec
ZDOT = -4048
823699 ZDOT = -1198
057948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1967779
69 X = -599779
25
Y = -14057253
15 feet Y = -4284650
76 meter
Z = 17056641
48 Z = 5198864
32
XDOT = 22537
467724 XDOT = 6869
420162
YDOT = -7841
444614 feet/sec YDOT = -2390
072318 meter/sec
ZDOT = -3900
830461 ZDOT = -1188
973124
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 12089
54601560
00016717 00000-0 10270-3 0 9060
2 25544 51
6404 161
2144 0015636 212
9147 147
1036 15
59700886 5600
Satellite: ISS
Catalog Number: 25544
Epoch time: 12089
54601560 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 161
2144 deg
Eccentricity:
0015636
Arg of perigee: 212
9147 deg
Mean anomaly: 147
1036 deg
Mean motion: 15
59700886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 560
Checksum: 294
Coasting Arc #8 (Orbit 574)
---------------------------------------
Vector Time (GMT): 2012/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3646696
72 A = 6768199
56 meter
Y = 4600285
61 meter E =
0013194
Z = -3377963
26 I = 51
78466
XDOT = -5958
160803 Wp = 199
05734
YDOT = -1294
886420 meter/sec RA = 155
34485 deg
ZDOT = 4651
414935 TA = 121
53818
MA = 121
40925
Ha = 214
718 n
mi
Hp = 205
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11964228
09 X = -3681457
65
Y = 15092800
57 feet Y = 4559311
44 meter
Z = -11082556
63 Z = -3395763
43
XDOT = -19547
771662 XDOT = -5965
833787
YDOT = -4248
315026 feet/sec YDOT = -1361
556882 meter/sec
ZDOT = 15260
547686 ZDOT = 4622
451944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9831271
24 X = -2996571
47
Y = 16512116
96 feet Y = 5032893
25 meter
Z = -11155919
68 Z = -3400324
32
XDOT = -18821
825498 XDOT = -5736
892412
YDOT = -938
325353 feet/sec YDOT = -286
001568 meter/sec
ZDOT = 15141
700122 ZDOT = 4615
190197
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 12090
50710630
00016717 00000-0 10270-3 0 9078
2 25544 51
6394 156
3827 0015468 215
9554 144
0562 15
59719066 5755
Satellite: ISS
Catalog Number: 25544
Epoch time: 12090
50710630 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 156
3827 deg
Eccentricity:
0015468
Arg of perigee: 215
9554 deg
Mean anomaly: 144
0562 deg
Mean motion: 15
59719066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 575
Checksum: 317
Coasting Arc #9 (Orbit 590)
---------------------------------------
Vector Time (GMT): 2012/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5844053
42 A = 6773081
38 meter
Y = -3395674
15 meter E =
0020242
Z = 76720
59 I = 51
82883
XDOT = 2445
330092 Wp = 182
68759
YDOT = 4073
854507 meter/sec RA = 150
35263 deg
ZDOT = -6042
604009 TA = 356
48518
MA = 356
49938
Ha = 214
416 n
mi
Hp = 205
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19173403
60 X = 5881217
50
Y = -11140663
22 feet Y = -3330114
53 meter
Z = 251707
97 Z = 105201
12
XDOT = 8022
736522 XDOT = 2428
947176
YDOT = 13365
664392 feet/sec YDOT = 4101
107702 meter/sec
ZDOT = -19824
816301 ZDOT = -6030
764813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17323022
79 X = 5280057
35
Y = -13841024
43 feet Y = -4218744
25 meter
Z = 368868
37 Z = 112431
08
XDOT = 9012
123364 XDOT = 2746
895201
YDOT = 10757
265831 feet/sec YDOT = 3278
814625 meter/sec
ZDOT = -19776
442508 ZDOT = -6027
859677
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 12091
53224948
00016717 00000-0 10270-3 0 9085
2 25544 51
6399 151
2289 0015262 219
9810 140
0223 15
59736429 5917
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
53224948 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 151
2289 deg
Eccentricity:
0015262
Arg of perigee: 219
9810 deg
Mean anomaly: 140
0223 deg
Mean motion: 15
59736429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 591
Checksum: 316
Coasting Arc #10 (Orbit 597)
---------------------------------------
Vector Time (GMT): 2012/091/22:00:39
051
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5865701
50 A = 6774732
63 meter
Y = 3379496
81 meter E =
0001272
Z = 268738
75 I = 51
84019
XDOT = -2161
349160 Wp = 259
66146
YDOT = -4228
475244 meter/sec RA = 148
26422 deg
ZDOT = 6023
413299 TA = 103
23022
MA = 103
21603
Ha = 214
239 n
mi
Hp = 207
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19244427
49 X = -5904361
23
Y = 11087587
95 feet Y = 3313686
77 meter
Z = 881688
82 Z = 240149
44
XDOT = -7091
040551 XDOT = -2143
165104
YDOT = -13872
950277 feet/sec YDOT = -4252
542694 meter/sec
ZDOT = 19761
854654 ZDOT = 6012
958076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21942078
55 X = 6687945
54
Y = -3467181
36 feet Y = -1056796
88 meter
Z = 764076
97 Z = 232890
66
XDOT = 1518
187817 XDOT = 462
743647
YDOT = 13933
478294 feet/sec YDOT = 4246
924184 meter/sec
ZDOT = 19719
172305 ZDOT = 6010
403718
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 12091
98076795
00016717 00000-0 10270-3 0 9090
2 25544 51
6404 148
9745 0013670 230
7053 129
2890 15
59153819 5987
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
98076795 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 148
9745 deg
Eccentricity:
0013670
Arg of perigee: 230
7053 deg
Mean anomaly: 129
2890 deg
Mean motion: 15
59153819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 598
Checksum: 341
Coasting Arc #11 (Orbit 612)
---------------------------------------
Vector Time (GMT): 2012/092/22:00:39
051
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5767570
08 A = 6769844
05 meter
Y = -976786
27 meter E =
0010339
Z = -3393687
00 I = 51
85030
XDOT = -1744
159057 Wp = 218
39140
YDOT = 5858
984295 meter/sec RA = 143
27727 deg
ZDOT = -4650
904719 TA = 1
26001
MA = 1
25741
Ha = 214
057 n
mi
Hp = 207
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18922474
01 X = 5794549
71
Y = -3204679
37 feet Y = -912139
17 meter
Z = -11134143
69 Z = -3365602
95
XDOT = -5722
306619 XDOT = -1786
952854
YDOT = 19222
389420 feet/sec YDOT = 5839
240366 meter/sec
ZDOT = -15258
873749 ZDOT = -4659
482153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18942257
59 X = -5773600
11
Y = -3475254
18 feet Y = -1059257
47 meter
Z = -11018740
12 Z = -3358511
99
XDOT = 11604
172050 XDOT = 3536
951641
YDOT = -14760
436856 feet/sec YDOT = -4498
981154 meter/sec
ZDOT = -15294
456909 ZDOT = -4661
750466
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 12092
94217180
00016717 00000-0 10270-3 0 9104
2 25544 51
6412 144
1454 0013716 234
5206 125
4670 15
59186823 6137
Satellite: ISS
Catalog Number: 25544
Epoch time: 12092
94217180 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 144
1454 deg
Eccentricity:
0013716
Arg of perigee: 234
5206 deg
Mean anomaly: 125
4670 deg
Mean motion: 15
59186823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 613
Checksum: 285
Coasting Arc #12 (Orbit 628)
---------------------------------------
Vector Time (GMT): 2012/093/22:00:39
051
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3893996
85 A = 6763248
01 meter
Y = -1972639
81 meter E =
0012584
Z = 5174764
01 I = 51
85230
XDOT = 4823
479341 Wp = 218
78125
YDOT = -5792
602644 meter/sec RA = 138
25537 deg
ZDOT = 1413
779157 TA = 217
61812
MA = 217
70621
Ha = 213
663 n
mi
Hp = 208
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12775580
23 X = -3896786
70
Y = -6471915
40 feet Y = -2016199
96 meter
Z = 16977572
20 Z = 5155840
66
XDOT = 15825
063455 XDOT = 4881
027115
YDOT = -19004
601849 feet/sec YDOT = -5738
341603 meter/sec
ZDOT = 4638
383061 ZDOT = 1437
351660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10071732
52 X = 3069864
07
Y = 10309725
99 feet Y = 3142404
48 meter
Z = 16899966
01 Z = 5151109
64
XDOT = -20369
410797 XDOT = -6208
596411
YDOT = 12094
867207 feet/sec YDOT = 3686
515525 meter/sec
ZDOT = 4735
558713 ZDOT = 1443
398296
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 12093
96765134
00016717 00000-0 10270-3 0 9115
2 25544 51
6411 138
9936 0013639 238
2500 121
7327 15
59226017 6299
Satellite: ISS
Catalog Number: 25544
Epoch time: 12093
96765134 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 138
9936 deg
Eccentricity:
0013639
Arg of perigee: 238
2500 deg
Mean anomaly: 121
7327 deg
Mean motion: 15
59226017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 629
Checksum: 308
Coasting Arc #13 (Orbit 643)
---------------------------------------
Vector Time (GMT): 2012/094/22:00:39
051
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 942329
71 A = 6764319
99 meter
Y = 4590582
28 meter E =
0009892
Z = -4881083
08 I = 51
87847
XDOT = -6194
945321 Wp = 183
86124
YDOT = 3838
208221 meter/sec RA = 133
21745 deg
ZDOT = 2403
880509 TA = 109
65717
MA = 109
55039
Ha = 213
264 n
mi
Hp = 208
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3091632
89 X = 914638
01
Y = 15060965
50 feet Y = 4600964
58 meter
Z = -16014052
09 Z = -4876573
10
XDOT = -20324
623757 XDOT = -6249
082006
YDOT = 12592
546658 feet/sec YDOT = 3768
630103 meter/sec
ZDOT = 7886
747076 ZDOT = 2373
653853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1622485
62 X = 494533
62
Y = -15308245
12 feet Y = -4665953
11 meter
Z = -15995809
19 Z = -4875522
64
XDOT = 22150
814033 XDOT = 6751
568117
YDOT = -5797
302992 feet/sec YDOT = -1767
017952 meter/sec
ZDOT = 7762
349124 ZDOT = 2365
964013
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 12094
92902103
00016717 00000-0 10270-3 0 9122
2 25544 51
6412 134
1636 0013647 242
3387 117
6383 15
59256993 6442
Satellite: ISS
Catalog Number: 25544
Epoch time: 12094
92902103 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 134
1636 deg
Eccentricity:
0013647
Arg of perigee: 242
3387 deg
Mean anomaly: 117
6383 deg
Mean motion: 15
59256993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 644
Checksum: 308
Coasting Arc #14 (Orbit 659)
---------------------------------------
Vector Time (GMT): 2012/095/22:00:39
051
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2020824
97 A = 6771464
61 meter
Y = -5897772
22 meter E =
0008535
Z = 2629356
70 I = 51
92221
XDOT = 5579
719397 Wp = 173
90764
YDOT = -428
999730 meter/sec RA = 128
20858 deg
ZDOT = -5257
346315 TA = 336
51031
MA = 336
54927
Ha = 212
963 n
mi
Hp = 208
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6630003
17 X = 2073852
00
Y = -19349646
38 feet Y = -5874877
28 meter
Z = 8626498
35 Z = 2639303
36
XDOT = 18306
166002 XDOT = 5609
640937
YDOT = -1407
479430 feet/sec YDOT = -366
437231 meter/sec
ZDOT = -17248
511531 ZDOT = -5230
167484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11952986
48 X = -3643270
28
Y = 16576454
85 feet Y = 5052503
44 meter
Z = 8667726
91 Z = 2641923
16
XDOT = -16807
817519 XDOT = -5123
022780
YDOT = -3170
537743 feet/sec YDOT = -966
379904 meter/sec
ZDOT = -17136
837567 ZDOT = -5223
308090
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 12095
95446466
00016717 00000-0 10270-3 0 9132
2 25544 51
6408 129
0122 0013532 245
9345 114
0395 15
59262698 6607
Satellite: ISS
Catalog Number: 25544
Epoch time: 12095
95446466 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 129
0122 deg
Eccentricity:
0013532
Arg of perigee: 245
9345 deg
Mean anomaly: 114
0395 deg
Mean motion: 15
59262698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 660
Checksum: 313
Coasting Arc #15 (Orbit 675)
---------------------------------------
Vector Time (GMT): 2012/096/22:00:39
051
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4143814
12 A = 6774078
26 meter
Y = 5308674
53 meter E =
0004190
Z = 711517
24 I = 51
94914
XDOT = -3360
936033 Wp = 325
83676
YDOT = -3423
373354 meter/sec RA = 123
23112 deg
ZDOT = 5988
609048 TA = 41
83084
MA = 41
79883
Ha = 212
570 n
mi
Hp = 208
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13595190
68 X = -4206325
23
Y = 17416911
18 feet Y = 5261986
40 meter
Z = 2334374
16 Z = 691234
12
XDOT = -11026
693021 XDOT = -3351
496944
YDOT = -11231
539875 feet/sec YDOT = -3460
903896 meter/sec
ZDOT = 19647
667479 ZDOT = 5972
304992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17890524
33 X = 5453031
81
Y = -12980398
59 feet Y = -3956425
49 meter
Z = 2250710
81 Z = 686016
65
XDOT = 6663
737643 XDOT = 2031
107234
YDOT = 12567
599858 feet/sec YDOT = 3830
604437 meter/sec
ZDOT = 19580
909321 ZDOT = 5968
261161
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 12096
97988645
00016717 00000-0 10270-3 0 9146
2 25544 51
6405 123
8589 0013663 250
3667 109
6014 15
59319652 6763
Satellite: ISS
Catalog Number: 25544
Epoch time: 12096
97988645 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 123
8589 deg
Eccentricity:
0013663
Arg of perigee: 250
3667 deg
Mean anomaly: 109
6014 deg
Mean motion: 15
59319652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 676
Checksum: 343
Coasting Arc #16 (Orbit 690)
---------------------------------------
Vector Time (GMT): 2012/097/22:00:39
051
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4859570
89 A = 6768354
03 meter
Y = -2831068
21 meter E =
0007971
Z = -3756982
02 I = 51
94500
XDOT = 389
844906 Wp = 251
40555
YDOT = 6361
400300 meter/sec RA = 118
24597 deg
ZDOT = -4284
447430 TA = 333
45951
MA = 333
50031
Ha = 212
440 n
mi
Hp = 207
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15943474
05 X = 4909118
10
Y = -9288281
53 feet Y = -2776448
85 meter
Z = -12326056
50 Z = -3733253
48
XDOT = 1279
018719 XDOT = 339
494621
YDOT = 20870
735893 feet/sec YDOT = 6365
477804 meter/sec
ZDOT = -14056
586057 ZDOT = -4282
676539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17880570
75 X = -5449997
96
Y = 4811434
59 feet Y = 1466525
26 meter
Z = -12228388
87 Z = -3727212
93
XDOT = 4451
920874 XDOT = 1356
945482
YDOT = -19204
600687 feet/sec YDOT = -5853
562289 meter/sec
ZDOT = -14049
730769 ZDOT = -4282
357938
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 12097
94120391
00016717 00000-0 10270-3 0 9151
2 25544 51
6397 119
0288 0013785 254
1547 105
8089 15
59316597 6912
Satellite: ISS
Catalog Number: 25544
Epoch time: 12097
94120391 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 119
0288 deg
Eccentricity:
0013785
Arg of perigee: 254
1547 deg
Mean anomaly: 105
8089 deg
Mean motion: 15
59316597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 691
Checksum: 337
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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