[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 25th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
093/19:41:52
242 -0
7 1
6 1
6
N/A 1
4 0
0 228
1
000/00:03:44
484 0
0 -0
1 214
2
Coasting Arc #1 (Orbit 2168)
---------------------------------------
Vector Time (GMT): 2013/084/08:45:56
146
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4159101
47 A = 6789889
09 meter
Y = 4100478
23 meter E =
0016422
Z = -3472912
21 I = 51
74441
XDOT = -5797
870575 Wp = 77
24506
YDOT = -2028
656543 meter/sec RA = 163
36666 deg
ZDOT = 4569
958272 TA = 242
14849
MA = 242
31497
Ha = 228
274 n
mi
Hp = 213
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13645346
02 X = -4187774
38
Y = 13453012
58 feet Y = 4053807
70 meter
Z = -11394068
92 Z = -3493186
91
XDOT = -19021
885089 XDOT = -5796
954322
YDOT = -6655
697320 feet/sec YDOT = -2093
486179 meter/sec
ZDOT = 14993
301418 ZDOT = 4541
795393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19103636
23 X = -5822788
32
Y = -537046
81 feet Y = -163691
87 meter
Z = -11478958
39 Z = -3498786
52
XDOT = -8417
390166 XDOT = -2565
620523
YDOT = -17030
700125 feet/sec YDOT = -5190
957398 meter/sec
ZDOT = 14876
151879 ZDOT = 4534
251093
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 13084
37258221
00016717 00000-0 10270-3 0 9003
2 25544 51
6452 164
4341 0011668 69
6810 290
5595 15
52157295 21695
Satellite: ISS
Catalog Number: 25544
Epoch time: 13084
37258221 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 164
4341 deg
Eccentricity:
0011668
Arg of perigee: 69
6810 deg
Mean anomaly: 290
5595 deg
Mean motion: 15
52157295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2169
Checksum: 312
Coasting Arc #2 (Orbit 2184)
---------------------------------------
Vector Time (GMT): 2013/085/08:45:56
146
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4795670
31 A = 6792181
62 meter
Y = -4061795
89 meter E =
0024483
Z = 2554958
90 I = 51
78122
XDOT = 4962
610548 Wp = 90
18288
YDOT = 2509
232216 meter/sec RA = 158
40724 deg
ZDOT = -5282
113218 TA = 61
17377
MA = 60
92820
Ha = 228
273 n
mi
Hp = 213
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15733826
49 X = 4828322
46
Y = -13326101
99 feet Y = -4007984
72 meter
Z = 8382411
10 Z = 2578335
77
XDOT = 16281
530668 XDOT = 4959
842026
YDOT = 8232
389160 feet/sec YDOT = 2564
710961 meter/sec
ZDOT = -17329
767775 ZDOT = -5258
012416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20500258
19 X = 6248478
70
Y = 1796719
64 feet Y = 547640
15 meter
Z = 8480231
07 Z = 2584774
43
XDOT = 5787
887570 XDOT = 1764
148131
YDOT = 15949
939363 feet/sec YDOT = 4861
541518 meter/sec
ZDOT = -17229
586603 ZDOT = -5251
577997
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 13085
40270675
00016717 00000-0 10270-3 0 9016
2 25544 51
6451 159
3135 0011695 73
9786 286
2653 15
52178960 21855
Satellite: ISS
Catalog Number: 25544
Epoch time: 13085
40270675 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 159
3135 deg
Eccentricity:
0011695
Arg of perigee: 73
9786 deg
Mean anomaly: 286
2653 deg
Mean motion: 15
52178960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2185
Checksum: 325
Coasting Arc #3 (Orbit 2199)
---------------------------------------
Vector Time (GMT): 2013/086/08:45:56
146
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5231241
26 A = 6793813
04 meter
Y = 4023183
84 meter E =
0018563
Z = -1603450
31 I = 51
81544
XDOT = -4067
439247 Wp = 61
53657
YDOT = -3021
459783 meter/sec RA = 153
45377 deg
ZDOT = 5748
021205 TA = 280
98340
MA = 281
19217
Ha = 228
281 n
mi
Hp = 213
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17162865
03 X = -5268051
40
Y = 13199422
03 feet Y = 3964478
74 meter
Z = -5260663
74 Z = -1628953
33
XDOT = -13344
616953 XDOT = -4061
272806
YDOT = -9912
925798 feet/sec YDOT = -3066
909120 meter/sec
ZDOT = 18858
337288 ZDOT = 5728
277287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21474797
75 X = -6545518
35
Y = -2547131
43 feet Y = -776365
66 meter
Z = -5367349
84 Z = -1635968
23
XDOT = -2874
236570 XDOT = -876
067306
YDOT = -14932
580074 feet/sec YDOT = -4551
450407 meter/sec
ZDOT = 18776
360531 ZDOT = 5723
034690
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 13086
36843614
00016717 00000-0 10270-3 0 9022
2 25544 51
6456 154
5139 0011748 76
4396 283
8064 15
52195993 22007
Satellite: ISS
Catalog Number: 25544
Epoch time: 13086
36843614 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 154
5139 deg
Eccentricity:
0011748
Arg of perigee: 76
4396 deg
Mean anomaly: 283
8064 deg
Mean motion: 15
52195993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2200
Checksum: 323
Coasting Arc #4 (Orbit 2215)
---------------------------------------
Vector Time (GMT): 2013/087/08:45:56
146
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5559365
72 A = 6794754
53 meter
Y = -3864741
85 meter E =
0022535
Z = 497651
99 I = 51
84522
XDOT = 3085
770319 Wp = 106
63238
YDOT = 3638
054628 meter/sec RA = 148
50428 deg
ZDOT = -6000
427685 TA = 68
01877
MA = 67
77946
Ha = 228
289 n
mi
Hp = 213
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18239388
86 X = 5599751
43
Y = -12679599
23 feet Y = -3802347
64 meter
Z = 1632716
49 Z = 524757
73
XDOT = 10123
918371 XDOT = 3074
008188
YDOT = 11935
874763 feet/sec YDOT = 3672
495087 meter/sec
ZDOT = -19686
442536 ZDOT = -5985
466217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21956990
98 X = 6692490
85
Y = 3309843
46 feet Y = 1008840
29 meter
Z = 1746078
13 Z = 532204
61
XDOT = -513
051226 XDOT = -156
378014
YDOT = 14109
578353 feet/sec YDOT = 4300
599482 meter/sec
ZDOT = -19624
458949 ZDOT = -5981
535088
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 13087
39853583
00016717 00000-0 10270-3 0 9033
2 25544 51
6451 149
3934 0011733 80
7423 279
5055 15
52223444 22162
Satellite: ISS
Catalog Number: 25544
Epoch time: 13087
39853583 = yrday
fracday
Element set: 903
Inclination: 51
6451 deg
RA of node: 149
3934 deg
Eccentricity:
0011733
Arg of perigee: 80
7423 deg
Mean anomaly: 279
5055 deg
Mean motion: 15
52223444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2216
Checksum: 309
Coasting Arc #5 (Orbit 2231)
---------------------------------------
Vector Time (GMT): 2013/088/08:45:56
146
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5687279
65 A = 6794719
27 meter
Y = 3662206
78 meter E =
0023789
Z = 550789
11 I = 51
87108
XDOT = -2147
703688 Wp = 66
59139
YDOT = -4266
904763 meter/sec RA = 143
55696 deg
ZDOT = 5998
464435 TA = 299
33038
MA = 299
56783
Ha = 228
300 n
mi
Hp = 213
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18659053
96 X = -5730484
15
Y = 12015114
12 feet Y = 3598366
53 meter
Z = 1807050
89 Z = 523055
16
XDOT = -7046
271943 XDOT = -2128
969872
YDOT = -13999
031376 feet/sec YDOT = -4290
816317 meter/sec
ZDOT = 19680
001428 ZDOT = 5988
076953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21888231
72 X = -6671533
03
Y = -3719444
23 feet Y = -1133686
60 meter
Z = 1691077
15 Z = 515440
32
XDOT = 3876
626215 XDOT = 1181
595670
YDOT = -13573
031142 feet/sec YDOT = -4137
059892 meter/sec
ZDOT = 19637
148677 ZDOT = 5985
402917
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 13088
42862312
00016717 00000-0 10270-3 0 9049
2 25544 51
6453 144
2732 0011831 83
6434 276
6073 15
52239306 22327
Satellite: ISS
Catalog Number: 25544
Epoch time: 13088
42862312 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 144
2732 deg
Eccentricity:
0011831
Arg of perigee: 83
6434 deg
Mean anomaly: 276
6073 deg
Mean motion: 15
52239306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2232
Checksum: 290
Coasting Arc #6 (Orbit 2246)
---------------------------------------
Vector Time (GMT): 2013/089/08:45:56
146
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5706897
53 A = 6793622
34 meter
Y = -3286801
44 meter E =
0017562
Z = -1666814
05 I = 51
89105
XDOT = 1189
095579 Wp = 109
23260
YDOT = 4942
662706 meter/sec RA = 138
61068 deg
ZDOT = -5730
016794 TA = 88
93685
MA = 88
73565
Ha = 228
284 n
mi
Hp = 213
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18723417
11 X = 5751324
12
Y = -10783469
31 feet Y = -3222735
07 meter
Z = -5468550
02 Z = -1638981
94
XDOT = 3901
232215 XDOT = 1161
572483
YDOT = 16216
084994 feet/sec YDOT = 4955
805522 meter/sec
ZDOT = -18799
267698 ZDOT = -5724
307502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21199480
87 X = 6461601
77
Y = 4323271
02 feet Y = 1317733
01 meter
Z = -5352189
88 Z = -1631347
48
XDOT = -7400
244434 XDOT = -2255
594503
YDOT = 13270
542605 feet/sec YDOT = 4044
861386 meter/sec
ZDOT = -18775
990611 ZDOT = -5722
921938
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 13089
39431770
00016717 00000-0 10270-3 0 9057
2 25544 51
6447 139
4726 0011784 87
5150 272
7351 15
52263542 22475
Satellite: ISS
Catalog Number: 25544
Epoch time: 13089
39431770 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 139
4726 deg
Eccentricity:
0011784
Arg of perigee: 87
5150 deg
Mean anomaly: 272
7351 deg
Mean motion: 15
52263542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2247
Checksum: 316
Coasting Arc #7 (Orbit 2262)
---------------------------------------
Vector Time (GMT): 2013/090/08:45:56
146
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5566143
22 A = 6791810
15 meter
Y = 2838525
52 meter E =
0025260
Z = 2636724
36 I = 51
90786
XDOT = -347
414029 Wp = 83
62622
YDOT = -5589
704825 meter/sec RA = 133
66288 deg
ZDOT = 5243
840690 TA = 305
97862
MA = 306
21260
Ha = 228
287 n
mi
Hp = 213
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18261624
73 X = -5610279
14
Y = 9312747
78 feet Y = 2776034
80 meter
Z = 8650670
48 Z = 2609576
89
XDOT = -1139
809806 XDOT = -310
356334
YDOT = -18338
926590 feet/sec YDOT = -5593
382272 meter/sec
ZDOT = 17204
201739 ZDOT = 5242
243358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19980403
71 X = -6090027
05
Y = -4790415
43 feet Y = -1460118
62 meter
Z = 8537194
87 Z = 2602137
00
XDOT = 10596
363724 XDOT = 3229
771663
YDOT = -13308
363847 feet/sec YDOT = -4056
389301 meter/sec
ZDOT = 17198
142613 ZDOT = 5241
993869
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 13090
42437989
00016717 00000-0 10270-3 0 9062
2 25544 51
6450 134
3519 0011840 90
9169 269
3339 15
52293250 22639
Satellite: ISS
Catalog Number: 25544
Epoch time: 13090
42437989 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 134
3519 deg
Eccentricity:
0011840
Arg of perigee: 90
9169 deg
Mean anomaly: 269
3339 deg
Mean motion: 15
52293250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2263
Checksum: 315
Coasting Arc #8 (Orbit 2277)
---------------------------------------
Vector Time (GMT): 2013/091/08:45:56
146
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5348316
09 A = 6789378
77 meter
Y = -2195065
35 meter E =
0016908
Z = -3573985
78 I = 51
91973
XDOT = -448
996196 Wp = 91
71689
YDOT = 6183
376176 meter/sec RA = 128
71318 deg
ZDOT = -4488
418693 TA = 130
19805
MA = 130
04994
Ha = 228
237 n
mi
Hp = 213
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17546968
79 X = 5389825
83
Y = -7201657
98 feet Y = -2135025
21 meter
Z = -11725675
12 Z = -3547903
05
XDOT = -1473
084633 XDOT = -496
303011
YDOT = 20286
667245 feet/sec YDOT = 6178
090471 meter/sec
ZDOT = -14725
783114 ZDOT = -4490
715126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18181388
15 X = 5541687
11
Y = 5633919
15 feet Y = 1717218
56 meter
Z = -11616691
78 Z = -3540767
66
XDOT = -13546
347129 XDOT = -4128
926605
YDOT = 13459
795706 feet/sec YDOT = 4102
545731 meter/sec
ZDOT = -14736
031320 ZDOT = -4491
542346
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 13091
39005297
00016717 00000-0 10270-3 0 9073
2 25544 51
6445 129
5515 0011792 94
4058 265
8441 15
52290887 22781
Satellite: ISS
Catalog Number: 25544
Epoch time: 13091
39005297 = yrday
fracday
Element set: 907
Inclination: 51
6445 deg
RA of node: 129
5515 deg
Eccentricity:
0011792
Arg of perigee: 94
4058 deg
Mean anomaly: 265
8441 deg
Mean motion: 15
52290887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2278
Checksum: 328
Coasting Arc #9 (Orbit 2293)
---------------------------------------
Vector Time (GMT): 2013/092/08:45:56
146
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5031746
96 A = 6786832
72 meter
Y = 1477433
37 meter E =
0021648
Z = 4292721
27 I = 51
93060
XDOT = 1104
337379 Wp = 102
04364
YDOT = -6698
039604 meter/sec RA = 123
76003 deg
ZDOT = 3580
125615 TA = 311
52617
MA = 311
71168
Ha = 228
240 n
mi
Hp = 213
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16508356
18 X = -5068746
87
Y = 4847222
36 feet Y = 1420958
55 meter
Z = 14083731
19 Z = 4268187
51
XDOT = 3623
154129 XDOT = 1161
762906
YDOT = -21975
195551 feet/sec YDOT = -6685
368942 meter/sec
ZDOT = 11745
818948 ZDOT = 3585
630218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16009347
13 X = -4879649
00
Y = -6526694
36 feet Y = -1989336
44 meter
Z = 13981270
96 Z = 4261491
39
XDOT = 15973
142219 XDOT = 4868
613748
YDOT = -13829
487419 feet/sec YDOT = -4215
227765 meter/sec
ZDOT = 11769
510801 ZDOT = 3587
346892
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 13092
42009062
00016717 00000-0 10270-3 0 9083
2 25544 51
6450 124
4305 0011773 97
9050 262
3438 15
52339310 22948
Satellite: ISS
Catalog Number: 25544
Epoch time: 13092
42009062 = yrday
fracday
Element set: 908
Inclination: 51
6450 deg
RA of node: 124
4305 deg
Eccentricity:
0011773
Arg of perigee: 97
9050 deg
Mean anomaly: 262
3438 deg
Mean motion: 15
52339310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 285
Coasting Arc #10 (Orbit 2308)
---------------------------------------
Vector Time (GMT): 2013/093/08:45:56
146
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4690644
54 A = 6784663
39 meter
Y = -589823
91 meter E =
0022722
Z = -4886407
46 I = 51
93871
XDOT = -1671
938539 Wp = 86
95295
YDOT = 7045
189272 meter/sec RA = 118
80389 deg
ZDOT = -2464
067629 TA = 158
94147
MA = 158
84777
Ha = 228
154 n
mi
Hp = 213
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15389253
73 X = 4720628
24
Y = -1935117
81 feet Y = -537202
81 meter
Z = -16031520
53 Z = -4863547
92
XDOT = -5485
362660 XDOT = -1738
625344
YDOT = 23114
138032 feet/sec YDOT = 7026
119588 meter/sec
ZDOT = -8084
211382 ZDOT = -2472
352136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13468839
71 X = 4105302
34
Y = 7887560
19 feet Y = 2404128
35 meter
Z = -15936129
16 Z = -4857332
17
XDOT = -17802
374444 XDOT = -5426
163730
YDOT = 14052
660079 feet/sec YDOT = 4283
250792 meter/sec
ZDOT = -8119
544406 ZDOT = -2474
837135
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 13093
38574183
00016717 00000-0 10270-3 0 9091
2 25544 51
6444 119
6301 0011774 101
1274 259
1202 15
52316829 23090
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
38574183 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 119
6301 deg
Eccentricity:
0011774
Arg of perigee: 101
1274 deg
Mean anomaly: 259
1202 deg
Mean motion: 15
52316829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2309
Checksum: 295
Coasting Arc #11 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2013/093/19:43:44
484
Vector Time (MET): N/A
Weight (LBS) : 907128
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3148707
18 A = 6783791
22 meter
Y = 2928671
88 meter E =
0024867
Z = -5268538
63 I = 51
94094
XDOT = -4112
327239 Wp = 99
73018
YDOT = 6355
942141 meter/sec RA = 116
51570 deg
ZDOT = 1075
672668 TA = 180
56057
MA = 180
56337
Ha = 228
129 n
mi
Hp = 214
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10330404
12 X = 3141317
16
Y = 9608503
54 feet Y = 2963841
03 meter
Z = -17285231
72 Z = -5253260
70
XDOT = -13491
887266 XDOT = -4188
320413
YDOT = 20852
828545 feet/sec YDOT = 6309
530678 meter/sec
ZDOT = 3529
109804 ZDOT = 1055
510419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1287704
01 X = 392492
18
Y = -14126910
86 feet Y = -4305882
43 meter
Z = -17221847
55 Z = -5249219
13
XDOT = 23742
816478 XDOT = 7236
810463
YDOT = -2033
715801 feet/sec YDOT = -619
876576 meter/sec
ZDOT = 3444
316496 ZDOT = 1049
827668
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 13093
83637600
00016717 00000-0 10270-3 0 9107
2 25544 51
6454 117
3907 0010595 101
5206 258
7136 15
52049025 23167
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
83637600 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 117
3907 deg
Eccentricity:
0010595
Arg of perigee: 101
5206 deg
Mean anomaly: 258
7136 deg
Mean motion: 15
52049025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 288
Coasting Arc #12 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2013/094/19:43:44
484
Vector Time (MET): N/A
Weight (LBS) : 907128
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2705579
88 A = 6784828
75 meter
Y = -3729561
09 meter E =
0015495
Z = 4967271
04 I = 51
95751
XDOT = 4230
449051 Wp = 87
48526
YDOT = -6013
354495 meter/sec RA = 111
55983 deg
ZDOT = -2204
170102 TA = 23
93540
MA = 23
86344
Ha = 228
103 n
mi
Hp = 214
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8876574
41 X = -2687803
59
Y = -12236092
83 feet Y = -3759716
77 meter
Z = 16296820
98 Z = 4954171
14
XDOT = 13879
426020 XDOT = 4308
084461
YDOT = -19728
853330 feet/sec YDOT = -5965
613055 meter/sec
ZDOT = -7231
529207 ZDOT = -2183
429974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4010540
62 X = -1222412
78
Y = 14635406
75 feet Y = 4460871
98 meter
Z = 16242609
03 Z = 4950747
23
XDOT = -23043
093152 XDOT = -7023
534793
YDOT = 1638
427222 feet/sec YDOT = 499
392617 meter/sec
ZDOT = -7144
352469 ZDOT = -2177
598632
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 13094
86658333
00016717 00000-0 10270-3 0 9118
2 25544 51
6451 112
2712 0010483 104
9709 255
2604 15
52097928 23328
Satellite: ISS
Catalog Number: 25544
Epoch time: 13094
86658333 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 112
2712 deg
Eccentricity:
0010483
Arg of perigee: 104
9709 deg
Mean anomaly: 255
2604 deg
Mean motion: 15
52097928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 300
Coasting Arc #13 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2013/095/19:43:44
484
Vector Time (MET): N/A
Weight (LBS) : 907128
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2346462
50 A = 6786721
89 meter
Y = 4504294
40 meter E =
0020039
Z = -4521632
56 I = 51
97452
XDOT = -4267
267279 Wp = 109
55617
YDOT = 5462
937600 meter/sec RA = 106
60680 deg
ZDOT = 3232
670770 TA = 192
86558
MA = 192
91678
Ha = 228
007 n
mi
Hp = 214
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7698367
77 X = 2317884
90
Y = 14777868
75 feet Y = 4530373
76 meter
Z = -14834752
48 Z = -4510303
58
XDOT = -14000
220730 XDOT = -4343
741243
YDOT = 17923
023621 feet/sec YDOT = 5414
791077 meter/sec
ZDOT = 10605
875229 ZDOT = 3211
754529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6476034
42 X = 1973895
29
Y = -15397912
84 feet Y = -4693283
83 meter
Z = -14788015
78 Z = -4507387
21
XDOT = 21655
262919 XDOT = 6600
524138
YDOT = -977
410035 feet/sec YDOT = -297
914579 meter/sec
ZDOT = 10518
016479 ZDOT = 3205
891423
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 13095
83239286
00016717 00000-0 10270-3 0 9129
2 25544 51
6456 107
4712 0010500 108
5278 251
7016 15
52083845 23477
Satellite: ISS
Catalog Number: 25544
Epoch time: 13095
83239286 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 107
4712 deg
Eccentricity:
0010500
Arg of perigee: 108
5278 deg
Mean anomaly: 251
7016 deg
Mean motion: 15
52083845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 300
Coasting Arc #14 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2013/096/19:43:44
484
Vector Time (MET): N/A
Weight (LBS) : 907128
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2001709
90 A = 6788934
84 meter
Y = -5203630
76 meter E =
0021133
Z = 3853597
19 I = 51
98966
XDOT = 4320
785362 Wp = 96
42537
YDOT = -4771
033035 meter/sec RA = 101
65761 deg
ZDOT = -4180
795088 TA = 37
38407
MA = 37
23722
Ha = 228
011 n
mi
Hp = 214
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6567289
68 X = -1962092
73
Y = -17072279
41 feet Y = -5225793
18 meter
Z = 12643035
39 Z = 3843969
91
XDOT = 14175
804994 XDOT = 4394
124099
YDOT = -15652
995522 feet/sec YDOT = -4722
305722 meter/sec
ZDOT = -13716
519318 ZDOT = -4159
626426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8699666
06 X = -2651658
21
Y = 16121614
43 feet Y = 4913868
08 meter
Z = 12603480
49 Z = 3841540
85
XDOT = -19987
517215 XDOT = -6092
195247
YDOT = -87
540142 feet/sec YDOT = -26
682235 meter/sec
ZDOT = -13627
678536 ZDOT = -4153
716418
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 13096
86257675
00016717 00000-0 10270-3 0 9136
2 25544 51
6453 102
3511 0010527 111
9352 248
2919 15
52113825 23638
Satellite: ISS
Catalog Number: 25544
Epoch time: 13096
86257675 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 102
3511 deg
Eccentricity:
0010527
Arg of perigee: 111
9352 deg
Mean anomaly: 248
2919 deg
Mean motion: 15
52113825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 298
Coasting Arc #15 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2013/097/19:43:44
484
Vector Time (MET): N/A
Weight (LBS) : 907128
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1745369
38 A = 6791167
46 meter
Y = 5800245
32 meter E =
0014051
Z = -3086682
51 I = 52
00261
XDOT = -4341
694773 Wp = 103
16698
YDOT = 3923
034739 meter/sec RA = 96
71223 deg
ZDOT = 4932
590499 TA = 221
65197
MA = 221
75906
Ha = 227
858 n
mi
Hp = 214
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5726277
50 X = 1695374
40
Y = 19029676
25 feet Y = 5819483
22 meter
Z = -10126911
14 Z = -3078325
79
XDOT = -14244
405422 XDOT = -4409
201570
YDOT = 12870
848881 feet/sec YDOT = 3874
106327 meter/sec
ZDOT = 16183
039694 ZDOT = 4911
334418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10456298
82 X = 3187079
88
Y = -16919684
92 feet Y = -5157119
96 meter
Z = -10092731
97 Z = -3076264
71
XDOT = 17906
062541 XDOT = 5457
767862
YDOT = 1496
659286 feet/sec YDOT = 456
181750 meter/sec
ZDOT = 16093
925148 ZDOT = 4905
428385
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 13097
82836196
00016717 00000-0 10270-3 0 9145
2 25544 51
6454 97
5507 0010393 115
6875 244
5351 15
52122001 23782
Satellite: ISS
Catalog Number: 25544
Epoch time: 13097
82836196 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 97
5507 deg
Eccentricity:
0010393
Arg of perigee: 115
6875 deg
Mean anomaly: 244
5351 deg
Mean motion: 15
52122001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 311
Coasting Arc #16 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2013/098/19:47:44
484
Vector Time (MET): N/A
Weight (LBS) : 907128
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -373345
94 A = 6795006
00 meter
Y = -6732906
35 meter E =
0023761
Z = 744103
75 I = 52
01764
XDOT = 4705
067215 Wp = 124
00493
YDOT = -936
101756 meter/sec RA = 91
76880 deg
ZDOT = -5986
157997 TA = 47
99610
MA = 47
79401
Ha = 227
915 n
mi
Hp = 214
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1224888
25 X = -301644
07
Y = -22089587
78 feet Y = -6736680
35 meter
Z = 2441285
27 Z = 742465
03
XDOT = 15436
572229 XDOT = 4744
264569
YDOT = -3071
199988 feet/sec YDOT = -883
268291 meter/sec
ZDOT = -19639
625973 ZDOT = -5963
205714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15210977
56 X = -4636305
96
Y = 16065672
98 feet Y = 4896817
12 meter
Z = 2435246
66 Z = 742263
18
XDOT = -11742
659332 XDOT = -3579
162564
YDOT = -8094
018817 feet/sec YDOT = -2467
056935 meter/sec
ZDOT = -19543
782855 ZDOT = -5956
945014
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 13098
85852188
00016717 00000-0 10270-3 0 9159
2 25544 51
6453 92
4302 0010541 120
2940 239
9256 15
52100201 23946
Satellite: ISS
Catalog Number: 25544
Epoch time: 13098
85852188 = yrday
fracday
Element set: 915
Inclination: 51
6453 deg
RA of node: 92
4302 deg
Eccentricity:
0010541
Arg of perigee: 120
2940 deg
Mean anomaly: 239
9256 deg
Mean motion: 15
52100201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 289
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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