[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 19th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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 1142)
---------------------------------------
Vector Time (GMT): 2013/018/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1194989
53 A = 6790096
31 meter
Y = -5592794
40 meter E =
0018411
Z = 3637124
17 I = 51
90473
XDOT = 6075
804712 Wp = 134
02297
YDOT = -1575
954438 meter/sec RA = 131
96677 deg
ZDOT = -4418
197426 TA = 2
98550
MA = 2
97453
Ha = 228
209 n
mi
Hp = 215
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3920569
33 X = 1239772
51
Y = -18349062
99 feet Y = -5579180
93 meter
Z = 11932822
07 Z = 3643037
98
XDOT = 19933
742494 XDOT = 6114
438027
YDOT = -5170
454193 feet/sec YDOT = -1507
794916 meter/sec
ZDOT = -14495
398378 ZDOT = -4388
588143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8876368
20 X = 2705517
03
Y = 16512618
14 feet Y = 5033046
01 meter
Z = 11958041
19 Z = 3644810
96
XDOT = -10779
926386 XDOT = -3285
721563
YDOT = 16205
919071 feet/sec YDOT = 4939
564133 meter/sec
ZDOT = -14372
082785 ZDOT = -4380
610833
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 13018
32625294
00016717 00000-0 10270-3 0 9003
2 25544 51
6444 132
7899 0013686 173
9513 186
1806 15
51928532 11438
Satellite: ISS
Catalog Number: 25544
Epoch time: 13018
32625294 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 132
7899 deg
Eccentricity:
0013686
Arg of perigee: 173
9513 deg
Mean anomaly: 186
1806 deg
Mean motion: 15
51928532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1143
Checksum: 315
Coasting Arc #2 (Orbit 1157)
---------------------------------------
Vector Time (GMT): 2013/019/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1667747
59 A = 6792156
30 meter
Y = 5938209
76 meter E =
0012679
Z = -2864450
94 I = 51
93064
XDOT = -5647
345319 Wp = 157
27138
YDOT = 870
196556 meter/sec RA = 127
01757 deg
ZDOT = 5088
137944 TA = 170
38333
MA = 170
35904
Ha = 228
097 n
mi
Hp = 215
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5471612
84 X = -1720111
33
Y = 19482315
49 feet Y = 5919267
25 meter
Z = -9397804
92 Z = -2872679
69
XDOT = -18528
035824 XDOT = -5681
372933
YDOT = 2854
975579 feet/sec YDOT = 806
854017 meter/sec
ZDOT = 16693
365959 ZDOT = 5060
621220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8723233
53 X = -2658841
58
Y = -18241360
79 feet Y = -5559966
77 meter
Z = -9432701
35 Z = -2875087
37
XDOT = 10834
575141 XDOT = 3302
378503
YDOT = -13760
726527 feet/sec YDOT = -4194
269445 meter/sec
ZDOT = 16578
821436 ZDOT = 5053
224774
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 13019
29214799
00016717 00000-0 10270-3 0 9015
2 25544 51
6434 127
9895 0013785 176
5869 183
5379 15
51957623 11587
Satellite: ISS
Catalog Number: 25544
Epoch time: 13019
29214799 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 127
9895 deg
Eccentricity:
0013785
Arg of perigee: 176
5869 deg
Mean anomaly: 183
5379 deg
Mean motion: 15
51957623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1158
Checksum: 356
Coasting Arc #3 (Orbit 1173)
---------------------------------------
Vector Time (GMT): 2013/020/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2049274
76 A = 6793810
86 meter
Y = -6157414
41 meter E =
0022658
Z = 1959200
41 I = 51
95467
XDOT = 5226
323080 Wp = 146
12716
YDOT = -53
734095 meter/sec RA = 122
07399 deg
ZDOT = -5622
644709 TA = 12
34221
MA = 12
28680
Ha = 227
763 n
mi
Hp = 216
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6723342
39 X = 2108458
77
Y = -20201490
85 feet Y = -6134167
29 meter
Z = 6427822
87 Z = 1969299
05
XDOT = 17146
729264 XDOT = 5253
848594
YDOT = -176
292963 feet/sec YDOT = 4
864040 meter/sec
ZDOT = -18446
997076 ZDOT = -5597
189036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8575070
69 X = 2613681
55
Y = 19473592
88 feet Y = 5935551
11 meter
Z = 6470534
40 Z = 1972218
89
XDOT = -11272
821287 XDOT = -3435
955928
YDOT = 11072
055100 feet/sec YDOT = 3374
762395 meter/sec
ZDOT = -18341
108128 ZDOT = -5590
369757
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 13020
32240672
00016717 00000-0 10270-3 0 9021
2 25544 51
6437 122
8702 0013529 180
9682 179
1446 15
52024816 11743
Satellite: ISS
Catalog Number: 25544
Epoch time: 13020
32240672 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 122
8702 deg
Eccentricity:
0013529
Arg of perigee: 180
9682 deg
Mean anomaly: 179
1446 deg
Mean motion: 15
52024816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1174
Checksum: 288
Coasting Arc #4 (Orbit 1188)
---------------------------------------
Vector Time (GMT): 2013/021/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2354430
26 A = 6794962
70 meter
Y = 6300985
64 meter E =
0008062
Z = -995199
24 I = 51
97409
XDOT = -4770
366366 Wp = 139
57627
YDOT = -850
059730 meter/sec RA = 117
13277 deg
ZDOT = 5924
536091 TA = 209
71609
MA = 209
76191
Ha = 227
710 n
mi
Hp = 216
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7724508
73 X = -2419879
86
Y = 20672525
07 feet Y = 6274291
02 meter
Z = -3265089
38 Z = -1006795
42
XDOT = -15650
808286 XDOT = -4789
285809
YDOT = -2788
909876 feet/sec YDOT = -903
511025 meter/sec
ZDOT = 19437
454367 ZDOT = 5901
316291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8484813
32 X = -2586171
10
Y = -20364358
12 feet Y = -6207056
36 meter
Z = -3314060
60 Z = -1010125
67
XDOT = 11940
692612 XDOT = 3639
523108
YDOT = -8111
605415 feet/sec YDOT = -2472
417330 meter/sec
ZDOT = 19340
961930 ZDOT = 5895
125196
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 13021
28825218
00016717 00000-0 10270-3 0 9033
2 25544 51
6437 118
0700 0013724 183
4015 176
7045 15
52040336 11892
Satellite: ISS
Catalog Number: 25544
Epoch time: 13021
28825218 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 118
0700 deg
Eccentricity:
0013724
Arg of perigee: 183
4015 deg
Mean anomaly: 176
7045 deg
Mean motion: 15
52040336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1189
Checksum: 279
Coasting Arc #5 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2013/022/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2594346
24 A = 6795211
00 meter
Y = -6264323
33 meter E =
0022814
Z = -45729
06 I = 51
98881
XDOT = 4353
577889 Wp = 162
68709
YDOT = 1841
380597 meter/sec RA = 112
19468 deg
ZDOT = -6047
327615 TA = 17
80337
MA = 17
72356
Ha = 227
372 n
mi
Hp = 216
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8511634
66 X = 2664424
55
Y = -20552241
89 feet Y = -6234919
89 meter
Z = -150029
74 Z = -32956
23
XDOT = 14283
392025 XDOT = 4362
039564
YDOT = 6041
274925 feet/sec YDOT = 1890
112675 meter/sec
ZDOT = -19840
313698 ZDOT = -6026
157909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8169515
31 X = 2490068
27
Y = 20690936
52 feet Y = 6306597
45 meter
Z = -96153
80 Z = -29307
68
XDOT = -13044
696418 XDOT = -3976
023468
YDOT = 5077
560459 feet/sec YDOT = 1547
640428 meter/sec
ZDOT = -19752
459313 ZDOT = -6020
549598
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 13022
31845804
00016717 00000-0 10270-3 0 9042
2 25544 51
6439 112
9503 0013404 187
4289 172
6666 15
52110773 12056
Satellite: ISS
Catalog Number: 25544
Epoch time: 13022
31845804 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 112
9503 deg
Eccentricity:
0013404
Arg of perigee: 187
4289 deg
Mean anomaly: 172
6666 deg
Mean motion: 15
52110773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 292
Coasting Arc #6 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2013/023/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2773283
00 A = 6794674
11 meter
Y = 6113270
04 meter E =
0010669
Z = 1068585
16 I = 51
99850
XDOT = -3954
863694 Wp = 123
90096
YDOT = -2835
667522 meter/sec RA = 107
25677 deg
ZDOT = 5910
514064 TA = 247
60671
MA = 247
71979
Ha = 227
290 n
mi
Hp = 216
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9098697
51 X = -2846627
59
Y = 20056660
24 feet Y = 6081847
30 meter
Z = 3505856
81 Z = 1054935
19
XDOT = -12975
274586 XDOT = -3951
571996
YDOT = -9303
371135 feet/sec YDOT = -2879
875217 meter/sec
ZDOT = 19391
450342 ZDOT = 5891
309798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7744287
27 X = -2360458
76
Y = -20627213
61 feet Y = -6287174
71 meter
Z = 3448336
09 Z = 1051052
84
XDOT = 14331
057762 XDOT = 4368
106406
YDOT = -2125
209327 feet/sec YDOT = -647
763803 meter/sec
ZDOT = 19311
886291 ZDOT = 5886
262942
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 13023
34863869
00016717 00000-0 10270-3 0 9058
2 25544 51
6445 107
8303 0013659 190
5310 169
5558 15
52129343 12212
Satellite: ISS
Catalog Number: 25544
Epoch time: 13023
34863869 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 107
8303 deg
Eccentricity:
0013659
Arg of perigee: 190
5310 deg
Mean anomaly: 169
5558 deg
Mean motion: 15
52129343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 304
Coasting Arc #7 (Orbit 1235)
---------------------------------------
Vector Time (GMT): 2013/024/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2929430
02 A = 6793205
68 meter
Y = -5747447
04 meter E =
0017947
Z = -2093929
13 I = 52
00247
XDOT = 3607
049353 Wp = 176
73719
YDOT = 3858
633314 meter/sec RA = 102
31831 deg
ZDOT = -5564
679122 TA = 26
32797
MA = 26
23687
Ha = 227
057 n
mi
Hp = 216
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9610990
88 X = 3003653
03
Y = -18856453
54 feet Y = -5714273
20 meter
Z = -6869846
23 Z = -2079518
50
XDOT = 11834
151422 XDOT = 3590
664449
YDOT = 12659
558116 feet/sec YDOT = 3898
878286 meter/sec
ZDOT = -18256
821267 ZDOT = -5547
196296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6864404
04 X = 2092270
35
Y = 20041123
48 feet Y = 6108534
44 meter
Z = -6809192
30 Z = -2075441
81
XDOT = -15942
818768 XDOT = -4859
371161
YDOT = -695
518389 feet/sec YDOT = -211
994005 meter/sec
ZDOT = -18184
539474 ZDOT = -5542
647632
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 13024
31440805
00016717 00000-0 10270-3 0 9068
2 25544 51
6449 103
0305 0013399 193
9890 166
0892 15
52169724 12363
Satellite: ISS
Catalog Number: 25544
Epoch time: 13024
31440805 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 103
0305 deg
Eccentricity:
0013399
Arg of perigee: 193
9890 deg
Mean anomaly: 166
0892 deg
Mean motion: 15
52169724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 305
Coasting Arc #8 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2013/025/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3058378
88 A = 6791107
80 meter
Y = 5263099
94 meter E =
0014433
Z = 3017410
73 I = 52
00202
XDOT = -3303
275510 Wp = 141
65079
YDOT = -4788
435522 meter/sec RA = 97
37707 deg
ZDOT = 4980
309329 TA = 252
65368
MA = 252
81160
Ha = 226
833 n
mi
Hp = 216
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10034051
44 X = -3131662
14
Y = 17267388
27 feet Y = 5228489
35 meter
Z = 9899641
52 Z = 3002375
94
XDOT = -10837
518076 XDOT = -3273
677203
YDOT = -15710
090296 feet/sec YDOT = -4825
209545 meter/sec
ZDOT = 16339
597537 ZDOT = 4964
334323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5744852
64 X = -1751031
08
Y = -19159564
97 feet Y = -5839835
40 meter
Z = 9836438
70 Z = 2998146
52
XDOT = 17551
327652 XDOT = 5349
644668
YDOT = 3132
499505 feet/sec YDOT = 954
785849 meter/sec
ZDOT = 16273
700958 ZDOT = 4960
224052
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 13025
34453568
00016717 00000-0 10270-3 0 9073
2 25544 51
6454 97
9105 0013546 197
7352 162
3329 15
52213580 12529
Satellite: ISS
Catalog Number: 25544
Epoch time: 13025
34453568 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 97
9105 deg
Eccentricity:
0013546
Arg of perigee: 197
7352 deg
Mean anomaly: 162
3329 deg
Mean motion: 15
52213580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 306
Coasting Arc #9 (Orbit 1266)
---------------------------------------
Vector Time (GMT): 2013/026/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3210835
86 A = 6788610
36 meter
Y = -4564283
17 meter E =
0010977
Z = -3857647
15 I = 51
99724
XDOT = 3033
627455 Wp = 173
68786
YDOT = 5662
551878 meter/sec RA = 92
43250 deg
ZDOT = -4186
563353 TA = 52
50162
MA = 52
40187
Ha = 226
669 n
mi
Hp = 217
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10534238
38 X = 3280374
98
Y = -14974682
33 feet Y = -4527988
67 meter
Z = -12656322
67 Z = -3841880
78
XDOT = 9952
845982 XDOT = 2990
418865
YDOT = 18577
926110 feet/sec YDOT = 5696
234327 meter/sec
ZDOT = -13735
444073 ZDOT = -4171
931391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4024127
43 X = 1226554
04
Y = 17907770
84 feet Y = 5458288
55 meter
Z = -12590152
30 Z = -3837478
42
XDOT = -19214
572759 XDOT = -5856
601777
YDOT = -5269
454087 feet/sec YDOT = -1606
129606 meter/sec
ZDOT = -13675
242694 ZDOT = -4168
213973
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 13026
31025717
00016717 00000-0 10270-3 0 9083
2 25544 51
6458 93
1107 0013361 201
1825 158
8775 15
52230762 12675
Satellite: ISS
Catalog Number: 25544
Epoch time: 13026
31025717 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 93
1107 deg
Eccentricity:
0013361
Arg of perigee: 201
1825 deg
Mean anomaly: 158
8775 deg
Mean motion: 15
52230762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 292
Coasting Arc #10 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2013/027/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3370907
40 A = 6786109
40 meter
Y = 3781618
49 meter E =
0015710
Z = 4521358
74 I = 51
99014
XDOT = -2797
787236 Wp = 170
12711
YDOT = -6362
338656 meter/sec RA = 87
48304 deg
ZDOT = 3218
787965 TA = 247
55696
MA = 247
72342
Ha = 226
346 n
mi
Hp = 217
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11059407
49 X = -3434906
74
Y = 12406884
81 feet Y = 3743565
02 meter
Z = 14833854
14 Z = 4504828
15
XDOT = -9179
091981 XDOT = -2742
069909
YDOT = -20873
814487 feet/sec YDOT = -6393
313758 meter/sec
ZDOT = 10560
327968 ZDOT = 3205
332176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2041025
07 X = -622104
44
Y = -16556736
58 feet Y = -5046493
31 meter
Z = 14764592
91 Z = 4500247
92
XDOT = 20607
098391 XDOT = 6281
043589
YDOT = 6876
800172 feet/sec YDOT = 2096
048692 meter/sec
ZDOT = 10505
108127 ZDOT = 3201
956957
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 13027
34033296
00016717 00000-0 10270-3 0 9099
2 25544 51
6461 87
9901 0013397 205
1299 154
9202 15
52295996 12830
Satellite: ISS
Catalog Number: 25544
Epoch time: 13027
34033296 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 87
9901 deg
Eccentricity:
0013397
Arg of perigee: 205
1299 deg
Mean anomaly: 154
9202 deg
Mean motion: 15
52295996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 323
Coasting Arc #11 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2013/028/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3586976
54 A = 6784053
78 meter
Y = -2826654
07 meter E =
0010181
Z = -5019141
80 I = 51
98129
XDOT = 2550
571277 Wp = 144
47852
YDOT = 6919
180747 meter/sec RA = 82
52988 deg
ZDOT = -2084
091067 TA = 105
38290
MA = 105
27039
Ha = 226
161 n
mi
Hp = 217
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11768295
74 X = 3642699
26
Y = -9273799
45 feet Y = -2786230
76 meter
Z = -16467000
66 Z = -5001581
62
XDOT = 8368
016001 XDOT = 2483
133683
YDOT = 22700
724235 feet/sec YDOT = 6947
325741 meter/sec
ZDOT = -6837
569117 ZDOT = -2071
864809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -535524
91 X = -163227
99
Y = 15053983
18 feet Y = 4588454
07 meter
Z = -16393567
49 Z = -4996759
37
XDOT = -21691
483011 XDOT = -6611
564022
YDOT = -8126
666662 feet/sec YDOT = -2477
007999 meter/sec
ZDOT = -6787
537381 ZDOT = -2068
841394
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 13028
30600671
00016717 00000-0 10270-3 0 9105
2 25544 51
6463 83
1902 0013221 208
5602 151
4827 15
52310070 12984
Satellite: ISS
Catalog Number: 25544
Epoch time: 13028
30600671 = yrday
fracday
Element set: 910
Inclination: 51
6463 deg
RA of node: 83
1902 deg
Eccentricity:
0013221
Arg of perigee: 208
5602 deg
Mean anomaly: 151
4827 deg
Mean motion: 15
52310070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1298
Checksum: 263
Coasting Arc #12 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2013/029/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3827285
83 A = 6782716
35 meter
Y = 1853481
32 meter E =
0013478
Z = 5289286
09 I = 51
97282
XDOT = -2295
934304 Wp = 197
93614
YDOT = -7257
345568 meter/sec RA = 77
57248 deg
ZDOT = 869
926253 TA = 243
70675
MA = 243
84528
Ha = 225
837 n
mi
Hp = 217
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12556712
05 X = -3873420
77
Y = 6080975
44 feet Y = 1810424
42 meter
Z = 17353300
82 Z = 5270581
76
XDOT = -7532
592860 XDOT = -2218
836265
YDOT = -23810
188872 feet/sec YDOT = -7282
589039 meter/sec
ZDOT = 2854
088757 ZDOT = 858
960552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3255963
97 X = 992417
82
Y = -13665711
99 feet Y = -4165309
02 meter
Z = 17275223
40 Z = 5265488
09
XDOT = 22249
726315 XDOT = 6781
716581
YDOT = 8902
072699 feet/sec YDOT = 2713
351759 meter/sec
ZDOT = 2809
349541 ZDOT = 856
289740
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 13029
33603186
00016717 00000-0 10270-3 0 9114
2 25544 51
6467 78
0689 0013193 212
5638 147
4701 15
52372439 13147
Satellite: ISS
Catalog Number: 25544
Epoch time: 13029
33603186 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 78
0689 deg
Eccentricity:
0013193
Arg of perigee: 212
5638 deg
Mean anomaly: 147
4701 deg
Mean motion: 15
52372439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 305
Coasting Arc #13 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2013/030/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4125382
52 A = 6782435
99 meter
Y = -785804
96 meter E =
0013527
Z = -5332768
26 I = 51
96470
XDOT = 1967
841447 Wp = 147
97648
YDOT = 7390
880186 meter/sec RA = 72
61363 deg
ZDOT = 422
564081 TA = 126
10241
MA = 125
97710
Ha = 225
587 n
mi
Hp = 217
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13534719
55 X = 4159767
62
Y = -2578100
27 feet Y = -739480
33 meter
Z = -17495958
86 Z = -5312644
34
XDOT = 6456
172726 XDOT = 1882
996141
YDOT = 24248
294574 feet/sec YDOT = 7412
411446 meter/sec
ZDOT = 1386
365095 ZDOT = 431
917088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6381651
31 X = -1945127
32
Y = 12330326
01 feet Y = 3758283
37 meter
Z = -17412104
93 Z = -5307209
58
XDOT = -22166
167826 XDOT = -6756
247953
YDOT = -9411
212846 feet/sec YDOT = -2868
537675 meter/sec
ZDOT = 1424
369188 ZDOT = 434
147729
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 13030
30165796
00016717 00000-0 10270-3 0 9124
2 25544 51
6467 73
2687 0013047 215
6496 144
3786 15
52405791 13299
Satellite: ISS
Catalog Number: 25544
Epoch time: 13030
30165796 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 73
2687 deg
Eccentricity:
0013047
Arg of perigee: 215
6496 deg
Mean anomaly: 144
3786 deg
Mean motion: 15
52405791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1329
Checksum: 317
Coasting Arc #14 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2013/031/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4432325
60 A = 6783259
75 meter
Y = -221072
04 meter E =
0008118
Z = 5131766
73 I = 51
95806
XDOT = -1577
998057 Wp = 209
21250
YDOT = -7308
150786 meter/sec RA = 67
65400 deg
ZDOT = -1685
766143 TA = 256
95955
MA = 257
05018
Ha = 225
367 n
mi
Hp = 217
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14541750
67 X = -4454452
47
Y = -725301
97 feet Y = -270760
55 meter
Z = 16836505
01 Z = 5110181
48
XDOT = -5177
158980 XDOT = -1487
970613
YDOT = -23976
872656 feet/sec YDOT = -7325
293661 meter/sec
ZDOT = -5530
728817 ZDOT = -1693
212775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9408687
53 X = 2867767
96
Y = -11246388
12 feet Y = -3427899
10 meter
Z = 16746696
08 Z = 5104392
96
XDOT = 21408
777637 XDOT = 6525
395424
YDOT = 9669
431605 feet/sec YDOT = 2947
242753 meter/sec
ZDOT = -5560
800379 ZDOT = -1694
931955
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 13031
33163375
00016717 00000-0 10270-3 0 9130
2 25544 51
6472 68
1472 0012952 219
4588 140
5621 15
52423554 13459
Satellite: ISS
Catalog Number: 25544
Epoch time: 13031
33163375 = yrday
fracday
Element set: 913
Inclination: 51
6472 deg
RA of node: 68
1472 deg
Eccentricity:
0012952
Arg of perigee: 219
4588 deg
Mean anomaly: 140
5621 deg
Mean motion: 15
52423554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 293
Coasting Arc #15 (Orbit 1359)
---------------------------------------
Vector Time (GMT): 2013/032/06:52:15
477
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4759659
03 A = 6784966
34 meter
Y = 1228785
24 meter E =
0013072
Z = -4683791
00 I = 51
95198
XDOT = 1060
126818 Wp = 175
30916
YDOT = 7007
704388 meter/sec RA = 62
69599 deg
ZDOT = 2903
651651 TA = 123
53083
MA = 123
40590
Ha = 225
025 n
mi
Hp = 218
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15615679
22 X = 4768317
07
Y = 4031447
65 feet Y = 1282058
94 meter
Z = -15366768
37 Z = -4660648
29
XDOT = 3478
106358 XDOT = 967
581398
YDOT = 22991
156130 feet/sec YDOT = 7019
042070 meter/sec
ZDOT = 9526
416178 ZDOT = 2908
576496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12512680
55 X = -3813865
03
Y = 10318960
51 feet Y = 3145219
16 meter
Z = -15270607
62 Z = -4654481
20
XDOT = -19839
479941 XDOT = -6047
073486
YDOT = -9871
260082 feet/sec YDOT = -3008
760073 meter/sec
ZDOT = 9546
020087 ZDOT = 2909
626922
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 13032
29721147
00016717 00000-0 10270-3 0 9144
2 25544 51
6474 63
3464 0012975 222
9075 137
1065 15
52482415 13606
Satellite: ISS
Catalog Number: 25544
Epoch time: 13032
29721147 = yrday
fracday
Element set: 914
Inclination: 51
6474 deg
RA of node: 63
3464 deg
Eccentricity:
0012975
Arg of perigee: 222
9075 deg
Mean anomaly: 137
1065 deg
Mean motion: 15
52482415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1360
Checksum: 294
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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