[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 15th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 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
There are no maneuvers
Coasting Arc #1 (Orbit 3071)
---------------------------------------
Vector Time (GMT): 2011/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4566506
04 A = 6723829
28 meter
Y = 674410
58 meter E =
0014562
Z = -4902219
12 I = 51
88329
XDOT = -3419
071506 Wp = 77
91039
YDOT = 6492
901051 meter/sec RA = 131
97093 deg
ZDOT = -2294
405984 TA = 169
81354
MA = 169
78400
Ha = 192
077 n
mi
Hp = 184
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14981975
19 X = 4582439
22
Y = 2212633
14 feet Y = 725564
81 meter
Z = -16083396
07 Z = -4879996
50
XDOT = -11217
426202 XDOT = -3480
276502
YDOT = 21302
168803 feet/sec YDOT = 6454
324564 meter/sec
ZDOT = -7527
578688 ZDOT = -2311
164800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14895385
91 X = 4540113
63
Y = -3219583
85 feet Y = -981329
16 meter
Z = -15993520
98 Z = -4874825
19
XDOT = -3221
646047 XDOT = -981
957715
YDOT = 22781
467533 feet/sec YDOT = 6943
791304 meter/sec
ZDOT = -7595
464400 ZDOT = -2315
097549
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 11103
51989527
00016717 00000-0 10270-3 0 9009
2 25544 51
6446 132
8181 0002539 99
7231 260
4218 15
73314736 30727
Satellite: ISS
Catalog Number: 25544
Epoch time: 11103
51989527 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 132
8181 deg
Eccentricity:
0002539
Arg of perigee: 99
7231 deg
Mean anomaly: 260
4218 deg
Mean motion: 15
73314736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3072
Checksum: 300
Coasting Arc #2 (Orbit 3087)
---------------------------------------
Vector Time (GMT): 2011/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2304446
71 A = 6731801
35 meter
Y = -5928581
82 meter E =
0016653
Z = 2181115
25 I = 51
92932
XDOT = 5370
350980 Wp = 107
79730
YDOT = 44
846999 meter/sec RA = 126
82145 deg
ZDOT = -5522
818557 TA = 47
87078
MA = 47
72937
Ha = 191
973 n
mi
Hp = 183
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7560520
71 X = 2359974
54
Y = -19450727
74 feet Y = -5902501
45 meter
Z = 7155889
94 Z = 2192445
57
XDOT = 17619
261747 XDOT = 5396
279137
YDOT = 147
135822 feet/sec YDOT = 105
046060 meter/sec
ZDOT = -18119
483456 ZDOT = -5496
666492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -144391
83 X = -44010
63
Y = -20852147
01 feet Y = -6355734
41 meter
Z = 7201816
44 Z = 2195113
65
XDOT = 15023
854687 XDOT = 4579
270909
YDOT = -6358
507741 feet/sec YDOT = -1938
073160 meter/sec
ZDOT = -18013
698676 ZDOT = -5490
575356
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 11104
53614418
00016717 00000-0 10270-3 0 9017
2 25544 51
6432 127
6044 0002639 100
6418 259
5043 15
73397660 30881
Satellite: ISS
Catalog Number: 25544
Epoch time: 11104
53614418 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 127
6044 deg
Eccentricity:
0002639
Arg of perigee: 100
6418 deg
Mean anomaly: 259
5043 deg
Mean motion: 15
73397660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3088
Checksum: 292
Coasting Arc #3 (Orbit 3103)
---------------------------------------
Vector Time (GMT): 2011/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4729774
43 A = 6724101
80 meter
Y = 590475
98 meter E =
0010333
Z = 4736601
00 I = 51
92045
XDOT = 1836
263301 Wp = 114
65936
YDOT = -6980
088331 meter/sec RA = 121
75033 deg
ZDOT = 2694
988892 TA = 308
91039
MA = 309
00248
Ha = 192
042 n
mi
Hp = 183
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15517632
66 X = -4759035
32
Y = 1937257
16 feet Y = 537421
59 meter
Z = 15540029
54 Z = 4713552
59
XDOT = 6024
485896 XDOT = 1901
087709
YDOT = -22900
552268 feet/sec YDOT = -6959
191429 meter/sec
ZDOT = 8841
827074 ZDOT = 2704
067554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13678641
72 X = -4169250
00
Y = 7767497
24 feet Y = 2367533
16 meter
Z = 15446784
59 Z = 4708179
94
XDOT = -2685
837836 XDOT = -818
643372
YDOT = -22443
947242 feet/sec YDOT = -6840
915119 meter/sec
ZDOT = 8878
671153 ZDOT = 2706
218968
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 11105
55235063
00016717 00000-0 10270-3 0 9026
2 25544 51
6424 122
3900 0002672 103
9675 256
1786 15
73446276 31047
Satellite: ISS
Catalog Number: 25544
Epoch time: 11105
55235063 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 122
3900 deg
Eccentricity:
0002672
Arg of perigee: 103
9675 deg
Mean anomaly: 256
1786 deg
Mean motion: 15
73446276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 287
Coasting Arc #4 (Orbit 3118)
---------------------------------------
Vector Time (GMT): 2011/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -910018
64 A = 6730743
85 meter
Y = 6183783
56 meter E =
0007084
Z = -2498628
93 I = 51
95962
XDOT = -5362
487667 Wp = 68
67246
YDOT = 1365
463388 meter/sec RA = 116
59838 deg
ZDOT = 5346
986197 TA = 263
20796
MA = 263
28858
Ha = 191
749 n
mi
Hp = 183
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2985625
46 X = -966961
27
Y = 20288003
82 feet Y = 6173288
59 meter
Z = -8197601
47 Z = -2503188
67
XDOT = -17593
463476 XDOT = -5403
332884
YDOT = 4479
866757 feet/sec YDOT = 1305
268873 meter/sec
ZDOT = 17542
605632 ZDOT = 5320
835700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5396524
62 X = 1644860
70
Y = 19775993
71 feet Y = 6027722
88 meter
Z = -8216162
30 Z = -2504286
27
XDOT = -13001
676847 XDOT = -3962
911103
YDOT = 10772
412002 feet/sec YDOT = 3283
431178 meter/sec
ZDOT = 17436
793593 ZDOT = 5314
734687
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 11106
50500380
00016717 00000-0 10270-3 0 9030
2 25544 51
6430 117
5023 0002695 108
0748 252
0709 15
73544006 31194
Satellite: ISS
Catalog Number: 25544
Epoch time: 11106
50500380 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 117
5023 deg
Eccentricity:
0002695
Arg of perigee: 108
0748 deg
Mean anomaly: 252
0709 deg
Mean motion: 15
73544006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 268
Coasting Arc #5 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2011/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4575646
27 A = 6724224
39 meter
Y = -1745645
82 meter E =
0012480
Z = -4619428
96 I = 51
94926
XDOT = -294
006003 Wp = 78
00674
YDOT = 7085
991066 meter/sec RA = 111
53114 deg
ZDOT = -2973
144724 TA = 162
61037
MA = 162
56759
Ha = 191
656 n
mi
Hp = 183
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15011962
81 X = 4617266
98
Y = -5727184
44 feet Y = -1694245
76 meter
Z = -15155606
81 Z = -4597098
97
XDOT = -964
586625 XDOT = -358
777869
YDOT = 23248
002186 feet/sec YDOT = 7082
340955 meter/sec
ZDOT = -9754
411825 ZDOT = -2974
730830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11370334
67 X = 3465678
01
Y = -11471975
74 feet Y = -3496658
20 meter
Z = -15065236
44 Z = -4591884
07
XDOT = 7973
843215 XDOT = 2430
427412
YDOT = 20703
370722 feet/sec YDOT = 6310
387396 meter/sec
ZDOT = -9760
974984 ZDOT = -2975
145175
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 11107
52112512
00016717 00000-0 10270-3 0 9040
2 25544 51
6417 112
2867 0002577 111
5163 248
6275 15
73580858 31358
Satellite: ISS
Catalog Number: 25544
Epoch time: 11107
52112512 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 112
2867 deg
Eccentricity:
0002577
Arg of perigee: 111
5163 deg
Mean anomaly: 248
6275 deg
Mean motion: 15
73580858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3135
Checksum: 292
Coasting Arc #6 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2011/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -384353
76 A = 6729954
99 meter
Y = -6149178
44 meter E =
0016110
Z = 2689042
32 I = 51
97926
XDOT = 5024
937545 Wp = 103
36615
YDOT = -2608
895772 meter/sec RA = 106
37619 deg
ZDOT = -5225
331154 TA = 46
11884
MA = 45
98588
Ha = 191
475 n
mi
Hp = 183
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1261003
16 X = -328627
00
Y = -20174469
94 feet Y = -6153164
83 meter
Z = 8822317
31 Z = 2687310
69
XDOT = 16486
015568 XDOT = 5079
121360
YDOT = -8559
369330 feet/sec YDOT = -2552
401113 meter/sec
ZDOT = -17143
474915 ZDOT = -5200
787914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9861930
36 X = -3005916
37
Y = -17648307
21 feet Y = -5379204
04 meter
Z = 8815454
11 Z = 2686950
41
XDOT = 10007
876072 XDOT = 3050
400627
YDOT = -14142
733341 feet/sec YDOT = -4310
705122 meter/sec
ZDOT = -17044
122520 ZDOT = -5195
048544
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 11108
53720143
00016717 00000-0 10270-3 0 9058
2 25544 51
6412 107
0711 0002487 112
7487 247
3939 15
73678563 31517
Satellite: ISS
Catalog Number: 25544
Epoch time: 11108
53720143 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 107
0711 deg
Eccentricity:
0002487
Arg of perigee: 112
7487 deg
Mean anomaly: 247
3939 deg
Mean motion: 15
73678563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 299
Coasting Arc #7 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2011/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4147587
91 A = 6724216
81 meter
Y = 2766507
74 meter E =
0011355
Z = 4505681
83 I = 51
96754
XDOT = -1151
537933 Wp = 114
08532
YDOT = -6922
336727 meter/sec RA = 101
31238 deg
ZDOT = 3179
549368 TA = 304
26256
MA = 304
37005
Ha = 191
442 n
mi
Hp = 183
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13607571
88 X = -4200103
38
Y = 9076468
98 feet Y = 2719833
30 meter
Z = 14782420
70 Z = 4485404
96
XDOT = -3778
011590 XDOT = -1089
491364
YDOT = -22711
078500 feet/sec YDOT = -6934
866978 meter/sec
ZDOT = 10431
592415 ZDOT = 3174
105877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8217559
20 X = -2504712
04
Y = 14228168
67 feet Y = 4336745
81 meter
Z = 14700312
93 Z = 4480655
38
XDOT = -12518
575271 XDOT = -3815
661743
YDOT = -18022
088403 feet/sec YDOT = -5493
132545 meter/sec
ZDOT = 10409
746606 ZDOT = 3172
890765
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 11109
55323370
00016717 00000-0 10270-3 0 9063
2 25544 51
6408 101
8559 0002433 119
3189 240
8218 15
73725868 31673
Satellite: ISS
Catalog Number: 25544
Epoch time: 11109
55323370 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 101
8559 deg
Eccentricity:
0002433
Arg of perigee: 119
3189 deg
Mean anomaly: 240
8218 deg
Mean motion: 15
73725868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 310
Coasting Arc #8 (Orbit 3181)
---------------------------------------
Vector Time (GMT): 2011/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1594474
61 A = 6729324
34 meter
Y = 5892133
75 meter E =
0006365
Z = -2836883
78 I = 51
99051
XDOT = -4422
617524 Wp = 81
95890
YDOT = 3658
791672 meter/sec RA = 96
15645 deg
ZDOT = 5124
070695 TA = 245
70331
MA = 245
76980
Ha = 191
285 n
mi
Hp = 183
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5231215
91 X = 1542250
37
Y = 19331147
49 feet Y = 5909672
19 meter
Z = -9307361
48 Z = -2829264
48
XDOT = -14509
900012 XDOT = -4488
094232
YDOT = 12003
909686 feet/sec YDOT = 3608
969089 meter/sec
ZDOT = 16811
255561 ZDOT = 5102
426386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13600498
05 X = 4145431
80
Y = 14719211
40 feet Y = 4486415
63 meter
Z = -9276698
21 Z = -2827537
61
XDOT = -6360
678810 XDOT = -1938
734901
YDOT = 16395
204126 feet/sec YDOT = 4997
258218 meter/sec
ZDOT = 16723
577270 ZDOT = 5097
346352
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 11110
50572232
00016717 00000-0 10270-3 0 9074
2 25544 51
6411 96
9666 0002546 120
8487 239
2927 15
73779817 31822
Satellite: ISS
Catalog Number: 25544
Epoch time: 11110
50572232 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 96
9666 deg
Eccentricity:
0002546
Arg of perigee: 120
8487 deg
Mean anomaly: 239
2927 deg
Mean motion: 15
73779817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3182
Checksum: 320
Coasting Arc #9 (Orbit 3197)
---------------------------------------
Vector Time (GMT): 2011/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3560869
47 A = 6724027
13 meter
Y = -3560837
11 meter E =
0011112
Z = -4466074
02 I = 51
97572
XDOT = 2431
589895 Wp = 80
23359
YDOT = 6524
240831 meter/sec RA = 91
09252 deg
ZDOT = -3268
093576 TA = 157
14957
MA = 157
10008
Ha = 191
141 n
mi
Hp = 183
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11682642
63 X = 3622118
32
Y = -11682536
46 feet Y = -3520674
70 meter
Z = -14652473
80 Z = -4448626
53
XDOT = 7977
657136 XDOT = 2374
329787
YDOT = 21404
989602 feet/sec YDOT = 6551
112291 meter/sec
ZDOT = -10722
091786 ZDOT = -3256
419701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4789207
31 X = 1459750
39
Y = -15877542
99 feet Y = -4839475
10 meter
Z = -14581766
27 Z = -4444522
36
XDOT = 16103
766916 XDOT = 4908
428156
YDOT = 14646
136247 feet/sec YDOT = 4464
142328 meter/sec
ZDOT = -10675
050726 ZDOT = -3253
755461
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 11111
52166570
00016717 00000-0 10270-3 0 9082
2 25544 51
6414 91
7499 0002505 126
2964 233
8431 15
73850851 31982
Satellite: ISS
Catalog Number: 25544
Epoch time: 11111
52166570 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 91
7499 deg
Eccentricity:
0002505
Arg of perigee: 126
2964 deg
Mean anomaly: 233
8431 deg
Mean motion: 15
73850851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 308
Coasting Arc #10 (Orbit 3213)
---------------------------------------
Vector Time (GMT): 2011/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2634696
32 A = 6728806
35 meter
Y = -5479083
76 meter E =
0015508
Z = 2865917
13 I = 51
99228
XDOT = 3681
037786 Wp = 103
41850
YDOT = -4448
813700 meter/sec RA = 85
93556 deg
ZDOT = -5101
843819 TA = 43
81885
MA = 43
69591
Ha = 190
949 n
mi
Hp = 183
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8644016
80 X = -2587154
48
Y = -17975996
60 feet Y = -5508280
82 meter
Z = 9402615
26 Z = 2853233
03
XDOT = 12076
895623 XDOT = 3755
295586
YDOT = -14595
845471 feet/sec YDOT = -4407
234727 meter/sec
ZDOT = -16738
332741 ZDOT = -5083
781073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16406581
87 X = -5000726
15
Y = -11385908
60 feet Y = -3470424
94 meter
Z = 9351460
35 Z = 2850325
12
XDOT = 2608
646266 XDOT = 795
115382
YDOT = -17498
807967 feet/sec YDOT = -5333
636668 meter/sec
ZDOT = -16665
095779 ZDOT = -5079
521193
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 11112
53756144
00016717 00000-0 10270-3 0 9097
2 25544 51
6415 86
5341 0002333 130
4212 229
7155 15
73943094 32141
Satellite: ISS
Catalog Number: 25544
Epoch time: 11112
53756144 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 86
5341 deg
Eccentricity:
0002333
Arg of perigee: 130
4212 deg
Mean anomaly: 229
7155 deg
Mean motion: 15
73943094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 282
Coasting Arc #11 (Orbit 3229)
---------------------------------------
Vector Time (GMT): 2011/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2854054
88 A = 6723525
64 meter
Y = 4152748
90 meter E =
0011317
Z = 4445590
32 I = 51
97276
XDOT = -3566
682536 Wp = 116
90562
YDOT = -5984
415415 meter/sec RA = 80
87240 deg
ZDOT = 3289
028080 TA = 300
22025
MA = 300
33226
Ha = 190
762 n
mi
Hp = 183
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9363697
12 X = -2921875
45
Y = 13624504
28 feet Y = 4120453
81 meter
Z = 14585270
08 Z = 4431560
71
XDOT = -11701
714358 XDOT = -3515
476061
YDOT = -19633
908843 feet/sec YDOT = -6024
014001 meter/sec
ZDOT = 10790
774542 ZDOT = 3271
825373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1257111
53 X = -383167
59
Y = 16534286
45 feet Y = 5039650
51 meter
Z = 14528354
56 Z = 4428242
47
XDOT = -18877
671824 XDOT = -5753
914372
YDOT = -10888
862478 feet/sec YDOT = -3318
925283 meter/sec
ZDOT = 10721
353678 ZDOT = 3267
868601
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 11113
55340930
00016717 00000-0 10270-3 0 9104
2 25544 51
6421 81
3185 0002354 139
5154 220
6185 15
74039735 32305
Satellite: ISS
Catalog Number: 25544
Epoch time: 11113
55340930 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 81
3185 deg
Eccentricity:
0002354
Arg of perigee: 139
5154 deg
Mean anomaly: 220
6185 deg
Mean motion: 15
74039735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3230
Checksum: 273
Coasting Arc #12 (Orbit 3244)
---------------------------------------
Vector Time (GMT): 2011/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3559571
74 A = 6728506
13 meter
Y = 4950240
04 meter E =
0005692
Z = -2849883
66 I = 51
98363
XDOT = -2854
222143 Wp = 85
85898
YDOT = 4991
157879 meter/sec RA = 75
71320 deg
ZDOT = 5113
740119 TA = 241
62930
MA = 241
68670
Ha = 190
667 n
mi
Hp = 183
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11678384
96 X = 3517796
82
Y = 16240945
02 feet Y = 4989811
79 meter
Z = -9350012
02 Z = -2832692
73
XDOT = -9364
245876 XDOT = -2934
663635
YDOT = 16375
189892 feet/sec YDOT = 4958
790401 meter/sec
ZDOT = 16777
362596 ZDOT = 5099
679022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18475061
49 X = 5631198
74
Y = 7753588
53 feet Y = 2363293
78 meter
Z = -9280606
82 Z = -2828728
96
XDOT = 1013
745905 XDOT = 308
989752
YDOT = 17561
688894 feet/sec YDOT = 5352
802775 meter/sec
ZDOT = 16720
283704 ZDOT = 5096
342473
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 11114
50572497
00016717 00000-0 10270-3 0 9116
2 25544 51
6420 76
4276 0002378 139
0012 221
1331 15
74065937 32452
Satellite: ISS
Catalog Number: 25544
Epoch time: 11114
50572497 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 76
4276 deg
Eccentricity:
0002378
Arg of perigee: 139
0012 deg
Mean anomaly: 221
1331 deg
Mean motion: 15
74065937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3245
Checksum: 282
Coasting Arc #13 (Orbit 3260)
---------------------------------------
Vector Time (GMT): 2011/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2153575
52 A = 6722956
49 meter
Y = -4509762
48 meter E =
0010683
Z = -4506767
53 I = 51
95795
XDOT = 4522
319090 Wp = 81
65047
YDOT = 5342
739365 meter/sec RA = 70
64640 deg
ZDOT = -3190
161330 TA = 156
59902
MA = 156
55036
Ha = 190
468 n
mi
Hp = 183
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7065536
47 X = 2225737
46
Y = -14795808
66 feet Y = -4485276
44 meter
Z = -14785982
71 Z = -4496130
19
XDOT = 14837
004888 XDOT = 4477
736615
YDOT = 17528
672457 feet/sec YDOT = 5393
061388 meter/sec
ZDOT = -10466
408564 ZDOT = -3168
300310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1879463
25 X = -572860
40
Y = -16327319
13 feet Y = -4976566
87 meter
Z = -14742771
52 Z = -4493596
76
XDOT = 20777
896686 XDOT = 6333
102910
YDOT = 6964
663999 feet/sec YDOT = 2122
829587 meter/sec
ZDOT = -10378
118951 ZDOT = -3163
250656
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 11115
52148007
00016717 00000-0 10270-3 0 9126
2 25544 51
6428 71
2101 0002353 144
9771 215
1548 15
74158596 32615
Satellite: ISS
Catalog Number: 25544
Epoch time: 11115
52148007 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 71
2101 deg
Eccentricity:
0002353
Arg of perigee: 144
9771 deg
Mean anomaly: 215
1548 deg
Mean motion: 15
74158596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3261
Checksum: 285
Coasting Arc #14 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2011/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4325516
47 A = 6728371
90 meter
Y = -4369604
79 meter E =
0015304
Z = 2713546
07 I = 51
96579
XDOT = 2065
111443 Wp = 107
85091
YDOT = -5290
489530 meter/sec RA = 65
48667 deg
ZDOT = -5208
098127 TA = 41
31041
MA = 41
19473
Ha = 190
350 n
mi
Hp = 182
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14191326
99 X = -4289515
11
Y = -14335973
72 feet Y = -4417773
99 meter
Z = 8902710
21 Z = 2692620
31
XDOT = 6775
300011 XDOT = 2149
417163
YDOT = -17357
249114 feet/sec YDOT = -5266
924935 meter/sec
ZDOT = -17086
936112 ZDOT = -5197
860947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19780156
25 X = -6028991
63
Y = -4142143
98 feet Y = -1262525
48 meter
Z = 8818175
28 Z = 2687779
83
XDOT = -4101
413577 XDOT = -1250
110858
YDOT = -16837
771262 feet/sec YDOT = -5132
152681 meter/sec
ZDOT = -17045
311613 ZDOT = -5195
410980
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 11116
53718628
00016717 00000-0 10270-3 0 9131
2 25544 51
6431 65
9931 0002321 150
0617 210
0679 15
74233149 32776
Satellite: ISS
Catalog Number: 25544
Epoch time: 11116
53718628 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 65
9931 deg
Eccentricity:
0002321
Arg of perigee: 150
0617 deg
Mean anomaly: 210
0679 deg
Mean motion: 15
74233149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 291
Coasting Arc #15 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2011/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1472847
76 A = 6722080
14 meter
Y = 4683088
93 meter E =
0010304
Z = 4587477
75 I = 51
93251
XDOT = -5353
645603 Wp = 124
19512
YDOT = -4647
456028 meter/sec RA = 60
41657 deg
ZDOT = 3015
034637 TA = 295
94324
MA = 296
04939
Ha = 190
082 n
mi
Hp = 182
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4832177
69 X = -1547390
64
Y = 15364465
01 feet Y = 4666202
01 meter
Z = 15050780
02 Z = 4580141
44
XDOT = -17564
454079 XDOT = -5315
925463
YDOT = -15247
559148 feet/sec YDOT = -4707
112741 meter/sec
ZDOT = 9891
845922 ZDOT = 2989
118392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4603491
08 X = 1403144
08
Y = 15463593
52 feet Y = 4713303
30 meter
Z = 15020913
78 Z = 4578374
52
XDOT = -22025
088168 XDOT = -6713
246874
YDOT = -2983
481984 feet/sec YDOT = -909
365309 meter/sec
ZDOT = 9787
128986 ZDOT = 2983
116915
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 11117
55284148
00016717 00000-0 10270-3 0 9140
2 25544 51
6436 60
7759 0002412 159
6974 200
4286 15
74339745 32938
Satellite: ISS
Catalog Number: 25544
Epoch time: 11117
55284148 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 60
7759 deg
Eccentricity:
0002412
Arg of perigee: 159
6974 deg
Mean anomaly: 200
4286 deg
Mean motion: 15
74339745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 322
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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