[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 28th 2011
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) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 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 2142)
---------------------------------------
Vector Time (GMT): 2011/299/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5805280
11 A = 6770372
88 meter
Y = -1321438
03 meter E =
0022243
Z = -3197977
89 I = 51
43104
XDOT = -1289
532833 Wp = 359
50222
YDOT = -5872
539585 meter/sec RA = 218
18407 deg
ZDOT = 4789
058743 TA = 323
25340
MA = 323
40569
Ha = 218
939 n
mi
Hp = 203
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19046194
58 X = -5774536
43
Y = -4335426
60 feet Y = -1386184
49 meter
Z = -10492053
43 Z = -3226105
98
XDOT = -4230
750766 XDOT = -1247
034125
YDOT = -19266
862157 feet/sec YDOT = -5886
722075 meter/sec
ZDOT = 15712
134985 ZDOT = 4782
897539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10225539
49 X = 3116744
44
Y = -16570309
54 feet Y = -5050630
35 meter
Z = -10606593
27 Z = -3232889
63
XDOT = 18423
398178 XDOT = 5615
451765
YDOT = 1372
530952 feet/sec YDOT = 418
347434 meter/sec
ZDOT = 15687
290845 ZDOT = 4781
486249
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 11299
61045853
00016717 00000-0 10270-3 0 9001
2 25544 51
6426 219
1816 0022145 347
2534 12
8059 15
59122807 21431
Satellite: ISS
Catalog Number: 25544
Epoch time: 11299
61045853 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 219
1816 deg
Eccentricity:
0022145
Arg of perigee: 347
2534 deg
Mean anomaly: 12
8059 deg
Mean motion: 15
59122807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2143
Checksum: 296
Coasting Arc #2 (Orbit 2158)
---------------------------------------
Vector Time (GMT): 2011/300/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5689451
10 A = 6774735
53 meter
Y = 3694076
67 meter E =
0014151
Z = 26221
40 I = 51
47012
XDOT = -2575
663451 Wp = 22
62713
YDOT = 4017
217609 meter/sec RA = 213
17143 deg
ZDOT = -5992
587978 TA = 157
08976
MA = 157
02657
Ha = 219
092 n
mi
Hp = 202
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18666178
15 X = 5647592
97
Y = 12119674
11 feet Y = 3757465
56 meter
Z = 86028
21 Z = 53759
78
XDOT = -8450
339406 XDOT = -2591
281616
YDOT = 13179
847797 feet/sec YDOT = 3988
327536 meter/sec
ZDOT = -19660
721713 ZDOT = -6005
138904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17251897
61 X = -5258378
39
Y = 14058908
41 feet Y = 4285155
28 meter
Z = 198069
59 Z = 60371
61
XDOT = -8970
342931 XDOT = -2734
160525
YDOT = -10707
982102 feet/sec YDOT = -3263
792945 meter/sec
ZDOT = -19712
039075 ZDOT = -6008
229510
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 11300
63597418
00016717 00000-0 10270-3 0 9016
2 25544 51
6424 214
0305 0021880 350
9999 9
0761 15
59156266 21598
Satellite: ISS
Catalog Number: 25544
Epoch time: 11300
63597418 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 214
0305 deg
Eccentricity:
0021880
Arg of perigee: 350
9999 deg
Mean anomaly: 9
0761 deg
Mean motion: 15
59156266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2159
Checksum: 308
Coasting Arc #3 (Orbit 2174)
---------------------------------------
Vector Time (GMT): 2011/301/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3590063
08 A = 6770344
82 meter
Y = -4770877
91 meter E =
0025450
Z = 3155791
77 I = 51
48127
XDOT = 5861
597680 Wp = 25
61176
YDOT = -1221
990141 meter/sec RA = 208
15970 deg
ZDOT = 4828
848958 TA = 11
06107
MA = 11
00522
Ha = 219
250 n
mi
Hp = 202
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11778422
19 X = -3551778
01
Y = -15652486
58 feet Y = -4810810
16 meter
Z = 10353647
55 Z = 3138443
76
XDOT = 19230
963516 XDOT = 5851
368301
YDOT = -4009
154006 feet/sec YDOT = -1156
499411 meter/sec
ZDOT = 15842
680308 ZDOT = 4857
300448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18411113
07 X = 5611707
26
Y = -6798303
19 feet Y = -2072122
81 meter
Z = 10283169
37 Z = 3134310
02
XDOT = -2202
982232 XDOT = -671
468984
YDOT = 18133
061541 feet/sec YDOT = 5526
957158 meter/sec
ZDOT = 15958
674750 ZDOT = 4864
204064
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 11301
66144830
00016717 00000-0 10270-3 0 9027
2 25544 51
6418 208
8781 0022099 354
8681 5
2244 15
59226000 21750
Satellite: ISS
Catalog Number: 25544
Epoch time: 11301
66144830 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 208
8781 deg
Eccentricity:
0022099
Arg of perigee: 354
8681 deg
Mean anomaly: 5
2244 deg
Mean motion: 15
59226000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2175
Checksum: 291
Coasting Arc #4 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2011/302/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 178471
57 A = 6763299
45 meter
Y = 4475829
20 meter E =
0027823
Z = -5084306
72 I = 51
48476
XDOT = -7289
656230 Wp = 26
36899
YDOT = -1650
694020 meter/sec RA = 203
11475 deg
ZDOT = -1688
154273 TA = 227
15983
MA = 227
39395
Ha = 219
192 n
mi
Hp = 202
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 585536
66 X = 153107
84
Y = 14684479
02 feet Y = 4477683
30 meter
Z = -16680796
34 Z = -5083501
18
XDOT = -23916
194980 XDOT = -7262
455140
YDOT = -5415
662794 feet/sec YDOT = -1732
059288 meter/sec
ZDOT = -5538
563887 ZDOT = -1723
502105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14312461
20 X = -4362438
17
Y = -3351562
62 feet Y = -1021556
29 meter
Z = -16677716
45 Z = -5083367
97
XDOT = 11490
335827 XDOT = 3502
254360
YDOT = -20450
366334 feet/sec YDOT = -6233
271659 meter/sec
ZDOT = -5682
550317 ZDOT = -1732
041337
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 11302
62279206
00016717 00000-0 10270-3 0 9031
2 25544 51
6407 204
0484 0022008 357
9781 2
1282 15
59319572 21903
Satellite: ISS
Catalog Number: 25544
Epoch time: 11302
62279206 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 204
0484 deg
Eccentricity:
0022008
Arg of perigee: 357
9781 deg
Mean anomaly: 2
1282 deg
Mean motion: 15
59319572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 288
Coasting Arc #5 (Orbit 2205)
---------------------------------------
Vector Time (GMT): 2011/303/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3561558
45 A = 6763602
34 meter
Y = -2962645
54 meter E =
0025966
Z = 4931225
18 I = 51
51499
XDOT = 6264
095070 Wp = 13
35510
YDOT = 3861
697646 meter/sec RA = 198
04969 deg
ZDOT = -2177
056388 TA = 98
04104
MA = 97
74634
Ha = 219
111 n
mi
Hp = 201
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11684903
04 X = 3570467
26
Y = -9719965
69 feet Y = -2922768
34 meter
Z = 16178560
31 Z = 4948549
05
XDOT = 20551
493011 XDOT = 6231
023145
YDOT = 12669
611701 feet/sec YDOT = 3931
561741 meter/sec
ZDOT = -7142
573450 ZDOT = -2146
705178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6420190
41 X = 1956874
04
Y = 13693123
08 feet Y = 4173663
91 meter
Z = 16249308
95 Z = 4952789
37
XDOT = -16531
361155 XDOT = -5038
758880
YDOT = 16185
233475 feet/sec YDOT = 4933
259163 meter/sec
ZDOT = -7019
033937 ZDOT = -2139
401544
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 11303
64818722
00016717 00000-0 10270-3 0 9047
2 25544 51
6407 198
8957 0021913 1
5365 358
5854 15
59394457 22068
Satellite: ISS
Catalog Number: 25544
Epoch time: 11303
64818722 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 198
8957 deg
Eccentricity:
0021913
Arg of perigee: 1
5365 deg
Mean anomaly: 358
5854 deg
Mean motion: 15
59394457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2206
Checksum: 329
Coasting Arc #6 (Orbit 2220)
---------------------------------------
Vector Time (GMT): 2011/304/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6107696
98 A = 6770628
77 meter
Y = 843760
52 meter E =
0024821
Z = -2768928
25 I = 51
56664
XDOT = -2987
275670 Wp = 14
35371
YDOT = -4874
428219 meter/sec RA = 193
01177 deg
ZDOT = 5137
345298 TA = 314
11359
MA = 314
31753
Ha = 219
157 n
mi
Hp = 201
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20038375
92 X = -6103227
03
Y = 2768243
17 feet Y = 775485
56 meter
Z = -9084410
26 Z = -2798588
90
XDOT = -9800
773196 XDOT = -2957
503402
YDOT = -15992
218567 feet/sec YDOT = -4907
667402 meter/sec
ZDOT = 16854
807407 ZDOT = 5122
905173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2108195
36 X = 642577
95
Y = -20063473
12 feet Y = -6115346
61 meter
Z = -9205365
20 Z = -2805795
31
XDOT = 16437
222190 XDOT = 5010
065323
YDOT = -5929
539374 feet/sec YDOT = -1807
323601 meter/sec
ZDOT = 16796
160032 ZDOT = 5119
469578
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 11304
60946043
00016717 00000-0 10270-3 0 9053
2 25544 51
6394 194
0647 0021868 4
9233 355
2133 15
59416221 22212
Satellite: ISS
Catalog Number: 25544
Epoch time: 11304
60946043 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 194
0647 deg
Eccentricity:
0021868
Arg of perigee: 4
9233 deg
Mean anomaly: 355
2133 deg
Mean motion: 15
59416221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2221
Checksum: 289
Coasting Arc #7 (Orbit 2236)
---------------------------------------
Vector Time (GMT): 2011/305/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6605624
36 A = 6773684
67 meter
Y = 1417219
25 meter E =
0016895
Z = -609388
92 I = 51
60671
XDOT = -1521
311207 Wp = 38
69832
YDOT = 4558
980260 meter/sec RA = 188
01039 deg
ZDOT = -5964
788392 TA = 147
88342
MA = 147
78038
Ha = 219
274 n
mi
Hp = 201
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21671995
95 X = 6592246
12
Y = 4649669
47 feet Y = 1491012
59 meter
Z = -1999307
47 Z = -577331
01
XDOT = -4991
178502 XDOT = -1543
201441
YDOT = 14957
284318 feet/sec YDOT = 4541
845661 meter/sec
ZDOT = -19569
515721 ZDOT = -5972
232134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9372536
59 X = -2856749
15
Y = 20098649
57 feet Y = 6126068
39 meter
Z = -1868664
76 Z = -569569
02
XDOT = -12025
518538 XDOT = -3665
378050
YDOT = -7405
097764 feet/sec YDOT = -2257
073799 meter/sec
ZDOT = -19600
069611 ZDOT = -5974
101218
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 11305
63477983
00016717 00000-0 10270-3 0 9060
2 25544 51
6390 188
9119 0021748 8
8843 351
2693 15
59472146 22373
Satellite: ISS
Catalog Number: 25544
Epoch time: 11305
63477983 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 188
9119 deg
Eccentricity:
0021748
Arg of perigee: 8
8843 deg
Mean anomaly: 351
2693 deg
Mean motion: 15
59472146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2237
Checksum: 337
Coasting Arc #8 (Orbit 2252)
---------------------------------------
Vector Time (GMT): 2011/306/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4653364
77 A = 6767840
25 meter
Y = -3186313
80 meter E =
0025944
Z = 3709561
93 I = 51
61707
XDOT = 5563
747735 Wp = 39
38874
YDOT = -3120
698241 meter/sec RA = 183
00054 deg
ZDOT = 4302
023770 TA = 5
12238
MA = 5
09588
Ha = 219
357 n
mi
Hp = 200
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15266944
80 X = -4635409
46
Y = -10453785
44 feet Y = -3238250
14 meter
Z = 12170478
78 Z = 3686999
36
XDOT = 18253
765534 XDOT = 5577
331867
YDOT = -10238
511290 feet/sec YDOT = -3058
405000 meter/sec
ZDOT = 14114
251213 ZDOT = 4329
085699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13394577
91 X = 4082667
35
Y = -12852005
81 feet Y = -3917291
37 meter
Z = 12078618
15 Z = 3681562
81
XDOT = 5329
777781 XDOT = 1624
516268
YDOT = 18913
479655 feet/sec YDOT = 5764
828599 meter/sec
ZDOT = 14224
739041 ZDOT = 4335
700460
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 11306
66005956
00016717 00000-0 10270-3 0 9072
2 25544 51
6383 183
7574 0021740 12
3713 347
7972 15
59536258 22534
Satellite: ISS
Catalog Number: 25544
Epoch time: 11306
66005956 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 183
7574 deg
Eccentricity:
0021740
Arg of perigee: 12
3713 deg
Mean anomaly: 347
7972 deg
Mean motion: 15
59536258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2253
Checksum: 320
Coasting Arc #9 (Orbit 2267)
---------------------------------------
Vector Time (GMT): 2011/307/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1040164
80 A = 6761724
47 meter
Y = 4136303
80 meter E =
0030355
Z = -5267238
44 I = 51
62650
XDOT = -7568
429127 Wp = 42
85713
YDOT = 887
318310 meter/sec RA = 177
95438 deg
ZDOT = -778
690646 TA = 219
58137
MA = 219
80339
Ha = 219
288 n
mi
Hp = 200
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3412614
16 X = 1019422
04
Y = 13570550
52 feet Y = 4147819
43 meter
Z = -17280966
02 Z = -5262235
78
XDOT = -24830
804222 XDOT = -7574
006016
YDOT = 2911
149311 feet/sec YDOT = 802
652292 meter/sec
ZDOT = -2554
759338 ZDOT = -815
471961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13990290
89 X = -4264240
66
Y = 880856
41 feet Y = 268485
04 meter
Z = -17260747
84 Z = -5261075
94
XDOT = 1909
940663 XDOT = 582
149914
YDOT = -23896
630952 feet/sec YDOT = -7283
693114 meter/sec
ZDOT = -2704
794748 ZDOT = -824
421439
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 11307
62122432
00016717 00000-0 10270-3 0 9089
2 25544 51
6373 178
9256 0021631 16
2025 343
9817 15
59596156 22689
Satellite: ISS
Catalog Number: 25544
Epoch time: 11307
62122432 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 178
9256 deg
Eccentricity:
0021631
Arg of perigee: 16
2025 deg
Mean anomaly: 343
9817 deg
Mean motion: 15
59596156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2268
Checksum: 312
Coasting Arc #10 (Orbit 2283)
---------------------------------------
Vector Time (GMT): 2011/308/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3049427
04 A = 6764480
61 meter
Y = -3990131
84 meter E =
0028164
Z = 4530990
59 I = 51
66725
XDOT = 6821
671357 Wp = 33
00689
YDOT = 1635
236753 meter/sec RA = 172
89912 deg
ZDOT = -3118
790083 TA = 88
34589
MA = 88
02331
Ha = 219
202 n
mi
Hp = 200
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10004681
88 X = 3071807
86
Y = -13090983
72 feet Y = -3955905
96 meter
Z = 14865454
70 Z = 4545859
39
XDOT = 22380
811539 XDOT = 6818
029495
YDOT = 5364
949978 feet/sec YDOT = 1711
500381 meter/sec
ZDOT = -10232
250929 ZDOT = -3085
658954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11181940
59 X = 3408255
49
Y = 12025799
76 feet Y = 3665463
77 meter
Z = 14926272
22 Z = 4549527
77
XDOT = -8281
435667 XDOT = -2524
181591
YDOT = 20363
673332 feet/sec YDOT = 6206
847632 meter/sec
ZDOT = -10097
201081 ZDOT = -3077
626890
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 11308
64642893
00016717 00000-0 10270-3 0 9091
2 25544 51
6378 173
7713 0021527 19
6632 340
5349 15
59654276 22849
Satellite: ISS
Catalog Number: 25544
Epoch time: 11308
64642893 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node: 173
7713 deg
Eccentricity:
0021527
Arg of perigee: 19
6632 deg
Mean anomaly: 340
5349 deg
Mean motion: 15
59654276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2284
Checksum: 334
Coasting Arc #11 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2011/309/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5875530
70 A = 6771621
26 meter
Y = 2769549
45 meter E =
0028316
Z = -1868138
04 I = 51
72086
XDOT = -3567
761141 Wp = 27
78698
YDOT = -3796
025353 meter/sec RA = 167
88065 deg
ZDOT = 5652
161240 TA = 311
59727
MA = 311
83958
Ha = 219
195 n
mi
Hp = 200
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19276675
51 X = -5896988
45
Y = 9086448
33 feet Y = 2703725
60 meter
Z = -6129061
81 Z = -1896734
02
XDOT = -11705
253088 XDOT = -3552
505640
YDOT = -12454
151422 feet/sec YDOT = -3835
836696 meter/sec
ZDOT = 18543
836088 ZDOT = 5634
866036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5980275
10 X = -1822787
85
Y = -20419236
02 feet Y = -6223783
14 meter
Z = -6245820
26 Z = -1903726
02
XDOT = 12651
985539 XDOT = 3856
325192
YDOT = -9298
209188 feet/sec YDOT = -2834
094161 meter/sec
ZDOT = 18473
462965 ZDOT = 5630
711512
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 11309
60752466
00016717 00000-0 10270-3 0 9108
2 25544 51
6370 168
9390 0021471 23
5134 336
6999 15
59703190 22990
Satellite: ISS
Catalog Number: 25544
Epoch time: 11309
60752466 = yrday
fracday
Element set: 910
Inclination: 51
6370 deg
RA of node: 168
9390 deg
Eccentricity:
0021471
Arg of perigee: 23
5134 deg
Mean anomaly: 336
6999 deg
Mean motion: 15
59703190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 322
Coasting Arc #12 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2011/310/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6539033
94 A = 6771716
22 meter
Y = -614042
44 meter E =
0019655
Z = -1695866
75 I = 51
75127
XDOT = -1000
713331 Wp = 48
76258
YDOT = 5012
647894 meter/sec RA = 162
89100 deg
ZDOT = -5703
944080 TA = 149
80054
MA = 149
68711
Ha = 219
279 n
mi
Hp = 199
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21453523
42 X = 6553652
64
Y = -2014574
94 feet Y = -540837
29 meter
Z = -5563867
29 Z = -1664064
02
XDOT = -3283
180221 XDOT = -1028
982146
YDOT = 16445
695189 feet/sec YDOT = 5001
298996 meter/sec
ZDOT = -18713
727297 ZDOT = -5708
874516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -983957
62 X = -299910
28
Y = 21558548
49 feet Y = 6571045
58 meter
Z = -5434115
65 Z = -1656318
45
XDOT = -14274
223659 XDOT = -4350
783371
YDOT = -5347
970616 feet/sec YDOT = -1630
061444 meter/sec
ZDOT = -18734
065519 ZDOT = -5710
143170
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 11310
63265538
00016717 00000-0 10270-3 0 9113
2 25544 51
6369 163
7846 0021639 27
2948 332
9340 15
59797472 23151
Satellite: ISS
Catalog Number: 25544
Epoch time: 11310
63265538 = yrday
fracday
Element set: 911
Inclination: 51
6369 deg
RA of node: 163
7846 deg
Eccentricity:
0021639
Arg of perigee: 27
2948 deg
Mean anomaly: 332
9340 deg
Mean motion: 15
59797472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 328
Coasting Arc #13 (Orbit 2330)
---------------------------------------
Vector Time (GMT): 2011/311/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4687386
81 A = 6764327
15 meter
Y = -1896244
00 meter E =
0024611
Z = 4468176
25 I = 51
75464
XDOT = 5044
876040 Wp = 52
75618
YDOT = -4816
563421 meter/sec RA = 157
87778 deg
ZDOT = 3250
630327 TA = 4
71700
MA = 4
69385
Ha = 219
323 n
mi
Hp = 199
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15378565
66 X = -4687540
31
Y = -6221272
97 feet Y = -1948661
94 meter
Z = 14659370
88 Z = 4445404
13
XDOT = 16551
430576 XDOT = 5082
569538
YDOT = -15802
373428 feet/sec YDOT = -4759
937652 meter/sec
ZDOT = 10664
797662 ZDOT = 3275
230589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8055180
56 X = 2455219
04
Y = -14595579
73 feet Y = -4448732
70 meter
Z = 14566564
19 Z = 4439888
77
XDOT = 12615
356432 XDOT = 3845
160640
YDOT = 17698
552120 feet/sec YDOT = 5394
518686 meter/sec
ZDOT = 10765
372925 ZDOT = 3281
285667
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 11311
65774873
00016717 00000-0 10270-3 0 9124
2 25544 51
6361 158
6292 0021354 31
0608 329
1805 15
59832709 23316
Satellite: ISS
Catalog Number: 25544
Epoch time: 11311
65774873 = yrday
fracday
Element set: 912
Inclination: 51
6361 deg
RA of node: 158
6292 deg
Eccentricity:
0021354
Arg of perigee: 31
0608 deg
Mean anomaly: 329
1805 deg
Mean motion: 15
59832709 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2331
Checksum: 304
Coasting Arc #14 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2011/312/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1231101
26 A = 6760808
82 meter
Y = 4053009
02 meter E =
0031464
Z = -5291077
95 I = 51
77138
XDOT = -7015
430400 Wp = 59
32925
YDOT = 2996
884285 meter/sec RA = 152
83046 deg
ZDOT = 681
978198 TA = 217
07020
MA = 217
28795
Ha = 219
251 n
mi
Hp = 199
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4039046
12 X = 1211391
93
Y = 13297273
68 feet Y = 4066665
63 meter
Z = -17359179
62 Z = -5285145
08
XDOT = -23016
503937 XDOT = -7051
733749
YDOT = 9832
297524 feet/sec YDOT = 2918
230473 meter/sec
ZDOT = 2237
461278 ZDOT = 647
808163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13656628
67 X = -4162540
42
Y = 2731465
49 feet Y = 832550
68 meter
Z = -17335169
10 Z = -5283759
54
XDOT = -7172
493419 XDOT = -2186
175994
YDOT = -22935
229617 feet/sec YDOT = -6990
657987 meter/sec
ZDOT = 2097
917418 ZDOT = 639
445229
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 11312
61874001
00016717 00000-0 10270-3 0 9136
2 25544 51
6364 153
7970 0021379 35
1450 325
1111 15
59876886 23461
Satellite: ISS
Catalog Number: 25544
Epoch time: 11312
61874001 = yrday
fracday
Element set: 913
Inclination: 51
6364 deg
RA of node: 153
7970 deg
Eccentricity:
0021379
Arg of perigee: 35
1450 deg
Mean anomaly: 325
1111 deg
Mean motion: 15
59876886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 301
Coasting Arc #15 (Orbit 2361)
---------------------------------------
Vector Time (GMT): 2011/313/14:29:27
145
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2601860
06 A = 6766753
75 meter
Y = -5050310
66 meter E =
0030671
Z = 3670185
18 I = 51
81743
XDOT = 6324
505420 Wp = 55
05630
YDOT = 62
909832 meter/sec RA = 147
79150 deg
ZDOT = -4354
108973 TA = 81
28630
MA = 80
93901
Ha = 219
196 n
mi
Hp = 199
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8536286
28 X = 2640310
69
Y = -16569260
68 feet Y = -5021000
05 meter
Z = 12041289
97 Z = 3682918
77
XDOT = 20749
689698 XDOT = 6344
483914
YDOT = 206
397086 feet/sec YDOT = 133
746011 meter/sec
ZDOT = -14285
134427 ZDOT = -4323
335203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15765616
22 X = 4805359
82
Y = 9878970
22 feet Y = 3011110
12 meter
Z = 12093491
63 Z = 3686096
25
XDOT = -1305
302681 XDOT = -397
856257
YDOT = 19588
244141 feet/sec YDOT = 5970
496814 meter/sec
ZDOT = -14159
581542 ZDOT = -4315
840454
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 11313
64375930
00016717 00000-0 10270-3 0 9148
2 25544 51
6355 148
6405 0021312 38
6890 321
5788 15
59918921 23625
Satellite: ISS
Catalog Number: 25544
Epoch time: 11313
64375930 = yrday
fracday
Element set: 914
Inclination: 51
6355 deg
RA of node: 148
6405 deg
Eccentricity:
0021312
Arg of perigee: 38
6890 deg
Mean anomaly: 321
5788 deg
Mean motion: 15
59918921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2362
Checksum: 317
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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