[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 1st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8880 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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 873)
---------------------------------------
Vector Time (GMT): 2013/001/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5456735
81 A = 6788897
95 meter
Y = 107313
98 meter E =
0022988
Z = -4062085
10 I = 51
43308
XDOT = -2984
259542 Wp = 109
90810
YDOT = -5884
519722 meter/sec RA = 215
27498 deg
ZDOT = 3863
635769 TA = 200
30799
MA = 200
39956
Ha = 230
246 n
mi
Hp = 212
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17902676
53 X = -5437797
90
Y = 352079
97 feet Y = 46399
43 meter
Z = -13327050
85 Z = -4088547
23
XDOT = -9790
877762 XDOT = -2937
004160
YDOT = -19306
167066 feet/sec YDOT = -5917
627556 meter/sec
ZDOT = 12675
970370 ZDOT = 3849
253095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4804132
70 X = -1464299
65
Y = -17164206
41 feet Y = -5231650
12 meter
Z = -13436904
36 Z = -4095568
45
XDOT = 14965
836957 XDOT = 4561
587105
YDOT = -14039
830446 feet/sec YDOT = -4279
340320 meter/sec
ZDOT = 12616
922429 ZDOT = 3845
637956
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 13001
52012361
00016717 00000-0 10270-3 0 9002
2 25544 51
6441 216
2888 0015668 109
9671 250
3170 15
51850049 8742
Satellite: ISS
Catalog Number: 25544
Epoch time: 13001
52012361 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 216
2888 deg
Eccentricity:
0015668
Arg of perigee: 109
9671 deg
Mean anomaly: 250
3170 deg
Mean motion: 15
51850049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 288
Coasting Arc #2 (Orbit 897)
---------------------------------------
Vector Time (GMT): 2013/002/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5882846
50 A = 6790984
90 meter
Y = 352148
93 meter E =
0027396
Z = 3344347
84 I = 51
46646
XDOT = 2321
986673 Wp = 103
53675
YDOT = 5648
533634 meter/sec RA = 210
29344 deg
ZDOT = -4653
446256 TA = 37
34410
MA = 37
15398
Ha = 229
987 n
mi
Hp = 212
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19300677
51 X = 5862225
63
Y = 1155344
26 feet Y = 417819
18 meter
Z = 10972269
82 Z = 3372875
95
XDOT = 7618
066512 XDOT = 2281
256058
YDOT = 18531
934494 feet/sec YDOT = 5674
271978 meter/sec
ZDOT = -15267
212126 ZDOT = -4642
265040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4023492
05 X = 1226360
38
Y = 18842782
87 feet Y = 5743280
22 meter
Z = 11090659
27 Z = 3380432
95
XDOT = -14423
376408 XDOT = -4396
245129
YDOT = 12088
262942 feet/sec YDOT = 3684
502545 meter/sec
ZDOT = -15221
415710 ZDOT = -4639
487508
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 13002
55046624
00016717 00000-0 10270-3 0 9016
2 25544 51
6446 211
1697 0015481 113
4522 246
8259 15
51895994 8989
Satellite: ISS
Catalog Number: 25544
Epoch time: 13002
55046624 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 211
1697 deg
Eccentricity:
0015481
Arg of perigee: 113
4522 deg
Mean anomaly: 246
8259 deg
Mean motion: 15
51895994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 898
Checksum: 319
Coasting Arc #3 (Orbit 912)
---------------------------------------
Vector Time (GMT): 2013/003/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6254278
80 A = 6792982
01 meter
Y = -685166
82 meter E =
0018412
Z = -2583397
29 I = 51
49849
XDOT = -1566
420755 Wp = 103
50885
YDOT = -5351
072522 meter/sec RA = 205
31609 deg
ZDOT = 5238
792543 TA = 227
45568
MA = 227
61126
Ha = 230
135 n
mi
Hp = 212
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20519287
41 X = -6233602
88
Y = -2247922
62 feet Y = -754990
40 meter
Z = -8475712
89 Z = -2613729
73
XDOT = -5139
175707 XDOT = -1531
916080
YDOT = -17556
012212 feet/sec YDOT = -5368
396451 meter/sec
ZDOT = 17187
639578 ZDOT = 5231
266682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3649514
78 X = -1112372
11
Y = -20263911
15 feet Y = -6176440
12 meter
Z = -8601567
74 Z = -2621757
85
XDOT = 13868
268876 XDOT = 4227
048353
YDOT = -9742
869282 feet/sec YDOT = -2969
626557 meter/sec
ZDOT = 17156
977373 ZDOT = 5229
446703
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 13003
51640659
00016717 00000-0 10270-3 0 9022
2 25544 51
6433 206
3699 0015657 117
4466 242
8279 15
51873500 9134
Satellite: ISS
Catalog Number: 25544
Epoch time: 13003
51640659 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 206
3699 deg
Eccentricity:
0015657
Arg of perigee: 117
4466 deg
Mean anomaly: 242
8279 deg
Mean motion: 15
51873500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 913
Checksum: 310
Coasting Arc #4 (Orbit 928)
---------------------------------------
Vector Time (GMT): 2013/004/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6497276
25 A = 6794533
62 meter
Y = 1006386
88 meter E =
0029350
Z = 1655435
45 I = 51
53260
XDOT = 681
836623 Wp = 118
66101
YDOT = 5088
193523 meter/sec RA = 200
34445 deg
ZDOT = -5706
352596 TA = 43
16830
MA = 42
93857
Ha = 229
912 n
mi
Hp = 212
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21316523
12 X = 6477498
06
Y = 3301794
24 feet Y = 1078932
86 meter
Z = 5431218
67 Z = 1686950
64
XDOT = 2236
996795 XDOT = 652
608625
YDOT = 16693
548305 feet/sec YDOT = 5095
655002 meter/sec
ZDOT = -18721
629251 ZDOT = -5703
111128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3237336
98 X = 986740
31
Y = 21292683
69 feet Y = 6490009
99 meter
Z = 5561960
99 Z = 1695285
71
XDOT = -13664
142815 XDOT = -4164
830730
YDOT = 7017
199525 feet/sec YDOT = 2138
842415 meter/sec
ZDOT = -18708
721970 ZDOT = -5702
418457
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 13004
54673122
00016717 00000-0 10270-3 0 9038
2 25544 51
6439 201
2506 0015451 120
6583 239
6094 15
51926092 9290
Satellite: ISS
Catalog Number: 25544
Epoch time: 13004
54673122 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 201
2506 deg
Eccentricity:
0015451
Arg of perigee: 120
6583 deg
Mean anomaly: 239
6094 deg
Mean motion: 15
51926092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 929
Checksum: 292
Coasting Arc #5 (Orbit 943)
---------------------------------------
Vector Time (GMT): 2013/005/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6647335
77 A = 6795553
59 meter
Y = -1210713
99 meter E =
0019491
Z = -749911
15 I = 51
56359
XDOT = 224
051841 Wp = 93
45607
YDOT = -4826
355768 meter/sec RA = 195
37575 deg
ZDOT = 5938
589286 TA = 258
44816
MA = 258
66705
Ha = 230
032 n
mi
Hp = 212
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21808844
39 X = -6629660
39
Y = -3972158
75 feet Y = -1284949
80 meter
Z = -2460338
42 Z = -782160
53
XDOT = 735
078219 XDOT = 249
156365
YDOT = -15834
500550 feet/sec YDOT = -4823
710155 meter/sec
ZDOT = 19483
560649 ZDOT = 5939
738494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3129005
18 X = -953720
78
Y = -21930272
97 feet Y = -6684347
20 meter
Z = -2594119
88 Z = -790687
74
XDOT = 13614
788587 XDOT = 4149
787561
YDOT = -4199
079572 feet/sec YDOT = -1279
879454 meter/sec
ZDOT = 19488
855158 ZDOT = 5940
203052
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 13005
51265475
00016717 00000-0 10270-3 0 9045
2 25544 51
6427 196
4509 0015681 124
7942 235
4688 15
51894810 9446
Satellite: ISS
Catalog Number: 25544
Epoch time: 13005
51265475 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 196
4509 deg
Eccentricity:
0015681
Arg of perigee: 124
7942 deg
Mean anomaly: 235
4688 deg
Mean motion: 15
51894810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 944
Checksum: 325
Coasting Arc #6 (Orbit 959)
---------------------------------------
Vector Time (GMT): 2013/006/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6624546
77 A = 6795656
76 meter
Y = 1436843
37 meter E =
0027096
Z = -272562
76 I = 51
59419
XDOT = -1231
196817 Wp = 131
86508
YDOT = 4613
605264 meter/sec RA = 190
41104 deg
ZDOT = -6004
547425 TA = 51
07377
MA = 50
83253
Ha = 229
887 n
mi
Hp = 213
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21734077
34 X = 6609311
38
Y = 4714053
06 feet Y = 1510838
03 meter
Z = -894234
78 Z = -240418
08
XDOT = -4039
359635 XDOT = -1253
527021
YDOT = 15136
500210 feet/sec YDOT = 4599
712744 meter/sec
ZDOT = -19699
958742 ZDOT = -6010
582466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2788369
44 X = 849895
01
Y = 22068939
70 feet Y = 6726612
82 meter
Z = -760898
39 Z = -231921
83
XDOT = -13967
066684 XDOT = -4257
161925
YDOT = 1138
030317 feet/sec YDOT = 346
871641 meter/sec
ZDOT = -19725
522136 ZDOT = -6012
339147
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 13006
54296143
00016717 00000-0 10270-3 0 9056
2 25544 51
6429 191
3315 0015545 127
8422 232
4139 15
51948552 9602
Satellite: ISS
Catalog Number: 25544
Epoch time: 13006
54296143 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 191
3315 deg
Eccentricity:
0015545
Arg of perigee: 127
8422 deg
Mean anomaly: 232
4139 deg
Mean motion: 15
51948552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 960
Checksum: 302
Coasting Arc #7 (Orbit 975)
---------------------------------------
Vector Time (GMT): 2013/007/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6498181
06 A = 6795170
17 meter
Y = -1576179
31 meter E =
0023489
Z = 1202325
01 I = 51
62172
XDOT = 2178
504717 Wp = 98
40643
YDOT = -4443
956883 meter/sec RA = 185
44712 deg
ZDOT = 5847
025892 TA = 274
64062
MA = 274
90886
Ha = 229
936 n
mi
Hp = 213
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21319491
67 X = -6485913
52
Y = -5171191
97 feet Y = -1648777
55 meter
Z = 3944635
85 Z = 1170786
98
XDOT = 7147
325186 XDOT = 2199
632692
YDOT = -14579
911033 feet/sec YDOT = -4419
477813 meter/sec
ZDOT = 19183
155815 ZDOT = 5857
659878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2601261
49 X = -792864
50
Y = -21806199
44 feet Y = -6646529
59 meter
Z = 3813818
03 Z = 1162451
73
XDOT = 14524
797979 XDOT = 4427
158424
YDOT = 1690
336618 feet/sec YDOT = 515
214601 meter/sec
ZDOT = 19227
807331 ZDOT = 5860
635674
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 13007
57326055
00016717 00000-0 10270-3 0 9067
2 25544 51
6421 186
2119 0015757 132
2778 227
9712 15
51925579 9765
Satellite: ISS
Catalog Number: 25544
Epoch time: 13007
57326055 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 186
2119 deg
Eccentricity:
0015757
Arg of perigee: 132
2778 deg
Mean anomaly: 227
9712 deg
Mean motion: 15
51925579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 976
Checksum: 326
Coasting Arc #8 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2013/008/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6175880
81 A = 6793681
41 meter
Y = 1779919
71 meter E =
0021988
Z = -2183502
86 I = 51
64781
XDOT = -3166
876537 Wp = 136
34446
YDOT = 4315
571240 meter/sec RA = 180
48426 deg
ZDOT = -5487
873479 TA = 67
87183
MA = 67
63857
Ha = 229
853 n
mi
Hp = 213
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20262076
14 X = 6166125
24
Y = 5839631
58 feet Y = 1848927
94 meter
Z = -7163723
29 Z = -2153524
48
XDOT = -10390
014886 XDOT = -3188
240175
YDOT = 14158
698295 feet/sec YDOT = 4280
038342 meter/sec
ZDOT = -18004
834248 ZDOT = -5503
309353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1975153
09 X = 602026
66
Y = 21036105
66 feet Y = 6411805
01 meter
Z = -7039388
24 Z = -2145605
54
XDOT = -15398
480130 XDOT = -4693
456744
YDOT = -4546
630535 feet/sec YDOT = -1385
812987 meter/sec
ZDOT = -18069
427477 ZDOT = -5507
561495
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 13008
53915550
00016717 00000-0 10270-3 0 9079
2 25544 51
6423 181
4121 0015694 135
1369 225
1054 15
51961796 9912
Satellite: ISS
Catalog Number: 25544
Epoch time: 13008
53915550 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 181
4121 deg
Eccentricity:
0015694
Arg of perigee: 135
1369 deg
Mean anomaly: 225
1054 deg
Mean motion: 15
51961796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 305
Coasting Arc #9 (Orbit 1006)
---------------------------------------
Vector Time (GMT): 2013/009/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5769805
18 A = 6791894
36 meter
Y = -1934246
87 meter E =
0025536
Z = 3009274
75 I = 51
67197
XDOT = 4027
591924 Wp = 114
24611
YDOT = -4242
326814 meter/sec RA = 175
52051 deg
ZDOT = 4952
019958 TA = 280
16005
MA = 280
44799
Ha = 229
812 n
mi
Hp = 213
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18929807
03 X = -5762365
38
Y = -6345954
28 feet Y = -1998727
18 meter
Z = 9872948
64 Z = 2981263
53
XDOT = 13213
884265 XDOT = 4050
675716
YDOT = -13918
395060 feet/sec YDOT = -4197
159246 meter/sec
ZDOT = 16246
784638 ZDOT = 4971
641145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1367578
26 X = -416837
85
Y = -19975453
44 feet Y = -6088518
21 meter
Z = 9756784
03 Z = 2973867
77
XDOT = 16406
837861 XDOT = 5000
804180
YDOT = 6922
784561 feet/sec YDOT = 2110
064734 meter/sec
ZDOT = 16328
770296 ZDOT = 4977
009186
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 13009
56943422
00016717 00000-0 10270-3 0 9083
2 25544 51
6419 176
2924 0015813 139
5749 220
6570 15
51965084 10079
Satellite: ISS
Catalog Number: 25544
Epoch time: 13009
56943422 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 176
2924 deg
Eccentricity:
0015813
Arg of perigee: 139
5749 deg
Mean anomaly: 220
6570 deg
Mean motion: 15
51965084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1007
Checksum: 316
Coasting Arc #10 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2013/010/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5175801
21 A = 6789543
02 meter
Y = 2191681
79 meter E =
0019039
Z = -3812318
50 I = 51
69563
XDOT = -4849
474630 Wp = 126
29605
YDOT = 4176
524029 meter/sec RA = 170
55577 deg
ZDOT = -4208
477651 TA = 99
37276
MA = 99
15745
Ha = 229
725 n
mi
Hp = 213
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16980975
10 X = 5169427
70
Y = 7190557
04 feet Y = 2249525
62 meter
Z = -12507606
62 Z = -3787190
43
XDOT = -15910
349835 XDOT = -4875
373556
YDOT = 13702
506656 feet/sec YDOT = 4122
149829 meter/sec
ZDOT = -13807
341375 ZDOT = -4232
098152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 169042
50 X = 51524
15
Y = 18510109
68 feet Y = 5641881
43 meter
Z = -12403431
53 Z = -3780565
93
XDOT = -17506
301669 XDOT = -5335
920749
YDOT = -9101
514050 feet/sec YDOT = -2774
141482 meter/sec
ZDOT = -13905
952368 ZDOT = -4238
534282
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 13010
53531200
00016717 00000-0 10270-3 0 9090
2 25544 51
6429 171
4927 0015765 142
5229 217
7024 15
51977126 10221
Satellite: ISS
Catalog Number: 25544
Epoch time: 13010
53531200 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 171
4927 deg
Eccentricity:
0015765
Arg of perigee: 142
5229 deg
Mean anomaly: 217
7024 deg
Mean motion: 15
51977126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 285
Coasting Arc #11 (Orbit 1037)
---------------------------------------
Vector Time (GMT): 2013/011/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4542129
86 A = 6787363
04 meter
Y = -2429774
90 meter E =
0023966
Z = 4414127
60 I = 51
71875
XDOT = 5506
507709 Wp = 133
29184
YDOT = -4148
738663 meter/sec RA = 165
58939 deg
ZDOT = 3354
961089 TA = 282
69696
MA = 282
96477
Ha = 229
616 n
mi
Hp = 213
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14902000
85 X = -4536064
30
Y = -7971702
44 feet Y = -2480534
36 meter
Z = 14482045
94 Z = 4392077
20
XDOT = 18065
970175 XDOT = 5536
193303
YDOT = -13611
347319 feet/sec YDOT = -4086
995795 meter/sec
ZDOT = 11007
090187 ZDOT = 3381
782465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1076644
44 X = 328161
22
Y = -16943929
92 feet Y = -5164509
84 meter
Z = 14390670
56 Z = 4386276
39
XDOT = 18587
557668 XDOT = 5665
487577
YDOT = 10701
802665 feet/sec YDOT = 3261
909452 meter/sec
ZDOT = 11119
016086 ZDOT = 3389
076103
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 13011
56557065
00016717 00000-0 10270-3 0 9103
2 25544 51
6431 166
3729 0015762 146
9431 213
2709 15
52007529 10387
Satellite: ISS
Catalog Number: 25544
Epoch time: 13011
56557065 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 166
3729 deg
Eccentricity:
0015762
Arg of perigee: 146
9431 deg
Mean anomaly: 213
2709 deg
Mean motion: 15
52007529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1038
Checksum: 294
Coasting Arc #12 (Orbit 1052)
---------------------------------------
Vector Time (GMT): 2013/012/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3761289
51 A = 6785386
24 meter
Y = 2791559
57 meter E =
0021818
Z = -4922267
88 I = 51
74283
XDOT = -6047
117245 Wp = 117
89834
YDOT = 4073
325308 meter/sec RA = 160
62217 deg
ZDOT = -2328
566445 TA = 129
40305
MA = 129
20966
Ha = 229
487 n
mi
Hp = 213
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12340188
67 X = 3753704
72
Y = 9158660
01 feet Y = 2833578
63 meter
Z = -16149172
82 Z = -4904014
45
XDOT = -19839
623507 XDOT = -6080
905277
YDOT = 13363
928177 feet/sec YDOT = 4005
513913 meter/sec
ZDOT = -7639
653692 ZDOT = -2358
023969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2949985
59 X = -899155
61
Y = 15162252
04 feet Y = 4621454
42 meter
Z = -16073605
40 Z = -4899234
93
XDOT = -19444
833083 XDOT = -5926
785124
YDOT = -11950
004081 feet/sec YDOT = -3642
361244 meter/sec
ZDOT = -7762
543522 ZDOT = -2366
023265
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 13012
53143056
00016717 00000-0 10270-3 0 9113
2 25544 51
6444 161
5740 0015716 149
8467 210
3593 15
52003598 10539
Satellite: ISS
Catalog Number: 25544
Epoch time: 13012
53143056 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 161
5740 deg
Eccentricity:
0015716
Arg of perigee: 149
8467 deg
Mean anomaly: 210
3593 deg
Mean motion: 15
52003598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1053
Checksum: 286
Coasting Arc #13 (Orbit 1068)
---------------------------------------
Vector Time (GMT): 2013/013/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2996341
34 A = 6784018
31 meter
Y = -3145165
04 meter E =
0019451
Z = 5205013
45 I = 51
76762
XDOT = 6422
710343 Wp = 148
10361
YDOT = -3998
362986 meter/sec RA = 155
65385 deg
ZDOT = 1263
003843 TA = 289
69116
MA = 289
90092
Ha = 229
369 n
mi
Hp = 213
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9830516
20 X = -2986232
76
Y = -10318782
93 feet Y = -3178615
74 meter
Z = 17076815
79 Z = 5190482
20
XDOT = 21071
884326 XDOT = 6460
808331
YDOT = -13117
988800 feet/sec YDOT = -3926
327260 meter/sec
ZDOT = 4143
713395 ZDOT = 1294
296479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4839187
28 X = 1474984
28
Y = -13481337
03 feet Y = -4109111
53 meter
Z = 17016750
15 Z = 5186705
45
XDOT = 20109
623773 XDOT = 6129
413326
YDOT = 12689
561882 feet/sec YDOT = 3867
778462 meter/sec
ZDOT = 4274
237641 ZDOT = 1302
787633
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 13013
56166984
00016717 00000-0 10270-3 0 9123
2 25544 51
6449 156
4541 0015616 154
0346 206
1592 15
52034675 10698
Satellite: ISS
Catalog Number: 25544
Epoch time: 13013
56166984 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 156
4541 deg
Eccentricity:
0015616
Arg of perigee: 154
0346 deg
Mean anomaly: 206
1592 deg
Mean motion: 15
52034675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1069
Checksum: 305
Coasting Arc #14 (Orbit 1083)
---------------------------------------
Vector Time (GMT): 2013/014/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2149119
76 A = 6783443
47 meter
Y = 3614260
39 meter E =
0025267
Z = -5340743
74 I = 51
79403
XDOT = -6630
333646 Wp = 124
31254
YDOT = 3814
097385 meter/sec RA = 150
68660 deg
ZDOT = -101
131807 TA = 144
80708
MA = 144
63995
Ha = 229
195 n
mi
Hp = 214
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7050917
85 X = 2134488
00
Y = 11857809
69 feet Y = 3638211
53 meter
Z = -17522125
14 Z = -5330339
16
XDOT = -21753
063144 XDOT = -6671
999648
YDOT = 12513
442864 feet/sec YDOT = 3739
719874 meter/sec
ZDOT = -331
797266 ZDOT = -133
441853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7248370
37 X = -2209303
29
Y = 11801886
65 feet Y = 3597215
05 meter
Z = -17479260
89 Z = -5327678
72
XDOT = -20239
853468 XDOT = -6169
107337
YDOT = -13052
493299 feet/sec YDOT = -3978
399957 meter/sec
ZDOT = -466
544240 ZDOT = -142
202684
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 13014
52751107
00016717 00000-0 10270-3 0 9138
2 25544 51
6457 151
6557 0015624 156
9973 203
1881 15
52043762 10849
Satellite: ISS
Catalog Number: 25544
Epoch time: 13014
52751107 = yrday
fracday
Element set: 913
Inclination: 51
6457 deg
RA of node: 151
6557 deg
Eccentricity:
0015624
Arg of perigee: 156
9973 deg
Mean anomaly: 203
1881 deg
Mean motion: 15
52043762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1084
Checksum: 301
Coasting Arc #15 (Orbit 1099)
---------------------------------------
Vector Time (GMT): 2013/015/12:16:01
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1369635
66 A = 6783751
37 meter
Y = -4061521
79 meter E =
0015149
Z = 5249157
46 I = 51
82178
XDOT = 6704
803513 Wp = 147
59758
YDOT = -3584
897402 meter/sec RA = 145
72021 deg
ZDOT = -1035
457183 TA = 312
22286
MA = 312
35131
Ha = 229
136 n
mi
Hp = 214
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4493555
32 X = -1349615
64
Y = -13325202
73 feet Y = -4076726
03 meter
Z = 17221645
22 Z = 5242552
59
XDOT = 21997
386855 XDOT = 6749
422167
YDOT = -11761
474415 feet/sec YDOT = -3509
670599 meter/sec
ZDOT = -3397
169237 ZDOT = -1002
778044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9549757
04 X = 2910765
95
Y = -10367502
93 feet Y = -3160014
89 meter
Z = 17194625
75 Z = 5240921
93
XDOT = 20039
858339 XDOT = 6108
148822
YDOT = 13111
460798 feet/sec YDOT = 3996
373251 meter/sec
ZDOT = -3260
900132 ZDOT = -993
922360
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 13015
55773167
00016717 00000-0 10270-3 0 9143
2 25544 51
6462 146
5359 0015522 160
7271 199
4471 15
52038249 11004
Satellite: ISS
Catalog Number: 25544
Epoch time: 13015
55773167 = yrday
fracday
Element set: 914
Inclination: 51
6462 deg
RA of node: 146
5359 deg
Eccentricity:
0015522
Arg of perigee: 160
7271 deg
Mean anomaly: 199
4471 deg
Mean motion: 15
52038249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1100
Checksum: 301
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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