[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 4th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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 1603)
---------------------------------------
Vector Time (GMT): 2012/156/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4510747
95 A = 6776218
35 meter
Y = 2922849
68 meter E =
0013868
Z = -4132290
83 I = 51
60019
XDOT = -5695
940788 Wp = 61
44342
YDOT = -3465
776652 meter/sec RA = 184
59998 deg
ZDOT = 3782
316411 TA = 247
50377
MA = 247
65064
Ha = 221
009 n
mi
Hp = 208
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14799041
83 X = -4523022
67
Y = 9589401
82 feet Y = 2872339
78 meter
Z = -13557384
63 Z = -4154233
37
XDOT = -18687
469776 XDOT = -5675
136243
YDOT = -11370
658306 feet/sec YDOT = -3529
356513 meter/sec
ZDOT = 12409
174578 ZDOT = 3754
695450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7904814
75 X = 2409387
54
Y = 15684989
67 feet Y = 4780784
85 meter
Z = -13647928
31 Z = -4159888
55
XDOT = -12228
490782 XDOT = -3727
243990
YDOT = 16816
014420 feet/sec YDOT = 5125
521195 meter/sec
ZDOT = 12295
798421 ZDOT = 3747
759359
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 12156
54002340
00016717 00000-0 10270-3 0 9000
2 25544 51
6372 185
6542 0010492 27
5311 332
6396 15
56111042 16041
Satellite: ISS
Catalog Number: 25544
Epoch time: 12156
54002340 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 185
6542 deg
Eccentricity:
0010492
Arg of perigee: 27
5311 deg
Mean anomaly: 332
6396 deg
Mean motion: 15
56111042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 265
Coasting Arc #2 (Orbit 1619)
---------------------------------------
Vector Time (GMT): 2012/157/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6137685
97 A = 6781225
67 meter
Y = -1811561
41 meter E =
0019304
Z = 2235525
02 I = 51
64620
XDOT = 3268
470336 Wp = 76
23149
YDOT = 4291
479997 meter/sec RA = 179
60236 deg
ZDOT = -5452
014427 TA = 78
89961
MA = 78
68259
Ha = 221
064 n
mi
Hp = 208
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20136764
99 X = 6146627
34
Y = -5943442
95 feet Y = -1742876
41 meter
Z = 7334399
68 Z = 2265363
13
XDOT = 10723
327874 XDOT = 3246
723951
YDOT = 14079
658782 feet/sec YDOT = 4327
909425 meter/sec
ZDOT = -17887
186439 ZDOT = -5436
188352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4042172
84 X = -1232054
28
Y = -20558594
56 feet Y = -6266259
62 meter
Z = 7457363
18 Z = 2273004
30
XDOT = 13528
729996 XDOT = 4123
556903
YDOT = -9176
373810 feet/sec YDOT = -2796
958737 meter/sec
ZDOT = -17822
408590 ZDOT = -5432
270138
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 12157
56752869
00016717 00000-0 10270-3 0 9012
2 25544 51
6356 180
5148 0010562 31
6326 328
5461 15
56164620 16204
Satellite: ISS
Catalog Number: 25544
Epoch time: 12157
56752869 = yrday
fracday
Element set: 901
Inclination: 51
6356 deg
RA of node: 180
5148 deg
Eccentricity:
0010562
Arg of perigee: 31
6326 deg
Mean anomaly: 328
5461 deg
Mean motion: 15
56164620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1620
Checksum: 300
Coasting Arc #3 (Orbit 1635)
---------------------------------------
Vector Time (GMT): 2012/158/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6746067
03 A = 6783288
10 meter
Y = 585560
63 meter E =
0022470
Z = 62252
02 I = 51
68426
XDOT = -345
338013 Wp = 41
37684
YDOT = -4748
895453 meter/sec RA = 174
62291 deg
ZDOT = 6024
257288 TA = 319
29449
MA = 319
46220
Ha = 221
002 n
mi
Hp = 208
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22132765
85 X = -6752415
91
Y = 1921130
68 feet Y = 510086
43 meter
Z = 204238
92 Z = 29464
66
XDOT = -1132
998731 XDOT = -321
473652
YDOT = -15580
365660 feet/sec YDOT = -4752
624810 meter/sec
ZDOT = 19764
623649 ZDOT = 6022
636827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 229524
55 X = 69959
08
Y = 22215632
07 feet Y = 6771324
65 meter
Z = 69218
03 Z = 21097
66
XDOT = -14009
321791 XDOT = -4270
041282
YDOT = 46
320158 feet/sec YDOT = 14
118384 meter/sec
ZDOT = 19758
352195 ZDOT = 6022
345749
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 12158
59501493
00016717 00000-0 10270-3 0 9022
2 25544 51
6360 175
3767 0010392 35
5455 324
6389 15
56211971 16360
Satellite: ISS
Catalog Number: 25544
Epoch time: 12158
59501493 = yrday
fracday
Element set: 902
Inclination: 51
6360 deg
RA of node: 175
3767 deg
Eccentricity:
0010392
Arg of perigee: 35
5455 deg
Mean anomaly: 324
6389 deg
Mean motion: 15
56211971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1636
Checksum: 316
Coasting Arc #4 (Orbit 1650)
---------------------------------------
Vector Time (GMT): 2012/159/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6294153
73 A = 6780938
55 meter
Y = 786936
95 meter E =
0011479
Z = -2413409
77 I = 51
70548
XDOT = -2648
156110 Wp = 68
42958
YDOT = 4787
619608 meter/sec RA = 169
64360 deg
ZDOT = -5361
673684 TA = 138
51287
MA = 138
42567
Ha = 221
177 n
mi
Hp = 208
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20650110
66 X = 6296609
98
Y = 2581814
14 feet Y = 857336
16 meter
Z = -7918011
07 Z = -2382827
12
XDOT = -8688
176213 XDOT = -2675
449765
YDOT = 15707
413411 feet/sec YDOT = 4757
854478 meter/sec
ZDOT = -17590
792928 ZDOT = -5374
603828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3798254
68 X = 1157708
03
Y = -20509587
81 feet Y = -6251322
36 meter
Z = -7792162
93 Z = -2375051
26
XDOT = 13676
952542 XDOT = 4168
735135
YDOT = 9215
734182 feet/sec YDOT = 2808
955779 meter/sec
ZDOT = -17644
430246 ZDOT = -5378
022339
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 12159
55827001
00016717 00000-0 10270-3 0 9036
2 25544 51
6351 170
5579 0010528 38
7651 321
4256 15
56191099 16515
Satellite: ISS
Catalog Number: 25544
Epoch time: 12159
55827001 = yrday
fracday
Element set: 903
Inclination: 51
6351 deg
RA of node: 170
5579 deg
Eccentricity:
0010528
Arg of perigee: 38
7651 deg
Mean anomaly: 321
4256 deg
Mean motion: 15
56191099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1651
Checksum: 305
Coasting Arc #5 (Orbit 1666)
---------------------------------------
Vector Time (GMT): 2012/160/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4821288
55 A = 6775676
33 meter
Y = -2141920
76 meter E =
0017491
Z = 4234002
18 I = 51
71784
XDOT = 5150
361990 Wp = 73
35684
YDOT = -4389
894356 meter/sec RA = 164
65147 deg
ZDOT = 3636
471146 TA = 339
52253
MA = 339
59257
Ha = 221
250 n
mi
Hp = 208
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15817875
83 X = -4817546
53
Y = -7027299
08 feet Y = -2195815
01 meter
Z = 13891083
27 Z = 4210589
53
XDOT = 16897
513090 XDOT = 5181
402846
YDOT = -14402
540539 feet/sec YDOT = -4332
126723 meter/sec
ZDOT = 11930
679612 ZDOT = 3661
566070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7685493
92 X = -2342538
55
Y = 15594404
26 feet Y = 4753174
42 meter
Z = 13794856
34 Z = 4204672
21
XDOT = -12548
193478 XDOT = -3824
689372
YDOT = -16851
772555 feet/sec YDOT = -5136
420275 meter/sec
ZDOT = 12034
380423 ZDOT = 3668
079153
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 12160
58572224
00016717 00000-0 10270-3 0 9046
2 25544 51
6349 165
4191 0010495 41
6762 318
5190 15
56233048 16676
Satellite: ISS
Catalog Number: 25544
Epoch time: 12160
58572224 = yrday
fracday
Element set: 904
Inclination: 51
6349 deg
RA of node: 165
4191 deg
Eccentricity:
0010495
Arg of perigee: 41
6762 deg
Mean anomaly: 318
5190 deg
Mean motion: 15
56233048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1667
Checksum: 306
Coasting Arc #6 (Orbit 1681)
---------------------------------------
Vector Time (GMT): 2012/161/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2643278
80 A = 6771689
15 meter
Y = 3421213
01 meter E =
0023575
Z = -5232132
40 I = 51
73380
XDOT = -6734
657586 Wp = 66
26942
YDOT = 3455
951657 meter/sec RA = 159
64163 deg
ZDOT = -1137
366232 TA = 192
79173
MA = 192
85165
Ha = 221
220 n
mi
Hp = 208
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8672174
54 X = 2630242
04
Y = 11224452
14 feet Y = 3450699
46 meter
Z = -17165788
72 Z = -5219322
83
XDOT = -22095
333286 XDOT = -6767
277165
YDOT = 11338
424070 feet/sec YDOT = 3380
458281 meter/sec
ZDOT = -3731
516510 ZDOT = -1170
161605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11436206
06 X = 3485755
61
Y = -8497446
15 feet Y = -2590021
59 meter
Z = -17113323
45 Z = -5216140
99
XDOT = 10171
234506 XDOT = 3100
192277
YDOT = 21510
905032 feet/sec YDOT = 6556
523854 meter/sec
ZDOT = -3866
861936 ZDOT = -1178
619518
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 12161
54894307
00016717 00000-0 10270-3 0 9053
2 25544 51
6350 160
6010 0010566 45
5088 314
6927 15
56239688 16826
Satellite: ISS
Catalog Number: 25544
Epoch time: 12161
54894307 = yrday
fracday
Element set: 905
Inclination: 51
6350 deg
RA of node: 160
6010 deg
Eccentricity:
0010566
Arg of perigee: 45
5088 deg
Mean anomaly: 314
6927 deg
Mean motion: 15
56239688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1682
Checksum: 313
Coasting Arc #7 (Orbit 1697)
---------------------------------------
Vector Time (GMT): 2012/162/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -92881
96 A = 6771898
72 meter
Y = -4421480
74 meter E =
0015365
Z = 5120446
36 I = 51
76308
XDOT = 7229
956852 Wp = 50
81294
YDOT = -2027
600118 meter/sec RA = 154
62592 deg
ZDOT = -1606
961242 TA = 54
71077
MA = 54
56715
Ha = 221
183 n
mi
Hp = 208
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -304730
84 X = -68307
07
Y = -14506170
41 feet Y = -4422382
48 meter
Z = 16799364
71 Z = 5120054
43
XDOT = 23720
330879 XDOT = 7259
898778
YDOT = -6652
231359 feet/sec YDOT = -1946
582698 meter/sec
ZDOT = -5272
182553 ZDOT = -1571
765979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14507724
55 X = -4421954
44
Y = 299203
38 feet Y = 91197
19 meter
Z = 16798121
96 Z = 5120067
57
XDOT = -6453
837943 XDOT = -1967
129805
YDOT = -22742
948221 feet/sec YDOT = -6932
050618 meter/sec
ZDOT = -5127
059357 ZDOT = -1562
727692
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 12162
57635989
00016717 00000-0 10270-3 0 9067
2 25544 51
6347 155
4616 0010530 48
5184 311
6873 15
56281196 16982
Satellite: ISS
Catalog Number: 25544
Epoch time: 12162
57635989 = yrday
fracday
Element set: 906
Inclination: 51
6347 deg
RA of node: 155
4616 deg
Eccentricity:
0010530
Arg of perigee: 48
5184 deg
Mean anomaly: 311
6873 deg
Mean motion: 15
56281196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1698
Checksum: 333
Coasting Arc #8 (Orbit 1712)
---------------------------------------
Vector Time (GMT): 2012/163/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2298101
15 A = 6776271
98 meter
Y = 4982349
15 meter E =
0015638
Z = -3986156
08 I = 51
80500
XDOT = -6531
578189 Wp = 73
91275
YDOT = 176
954010 meter/sec RA = 149
62296 deg
ZDOT = 4004
010834 TA = 237
68077
MA = 237
83229
Ha = 221
244 n
mi
Hp = 207
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7539701
95 X = -2334280
14
Y = 16346289
85 feet Y = 4956448
42 meter
Z = -13077939
89 Z = -3997407
60
XDOT = -21429
062301 XDOT = -6552
522075
YDOT = 580
557777 feet/sec YDOT = 103
796401 meter/sec
ZDOT = 13136
518485 ZDOT = 3972
229839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16417493
48 X = 5004052
01
Y = 7299919
57 feet Y = 2225015
48 meter
Z = -13124705
38 Z = -4000410
20
XDOT = 1323
644208 XDOT = 403
446754
YDOT = 20304
864195 feet/sec YDOT = 6188
922607 meter/sec
ZDOT = 13005
601360 ZDOT = 3964
107294
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 12163
53954651
00016717 00000-0 10270-3 0 9075
2 25544 51
6348 150
6441 0010628 52
0715 308
1398 15
56284145 17132
Satellite: ISS
Catalog Number: 25544
Epoch time: 12163
53954651 = yrday
fracday
Element set: 907
Inclination: 51
6348 deg
RA of node: 150
6441 deg
Eccentricity:
0010628
Arg of perigee: 52
0715 deg
Mean anomaly: 308
1398 deg
Mean motion: 15
56284145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1713
Checksum: 301
Coasting Arc #9 (Orbit 1728)
---------------------------------------
Vector Time (GMT): 2012/164/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4250770
14 A = 6781221
38 meter
Y = -4901042
83 meter E =
0021658
Z = 1956596
17 I = 51
84790
XDOT = 4858
593009 Wp = 88
13520
YDOT = 1953
732292 meter/sec RA = 144
64051 deg
ZDOT = -5607
437334 TA = 70
32279
MA = 70
08923
Ha = 221
173 n
mi
Hp = 207
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13946096
26 X = 4295753
94
Y = -16079536
85 feet Y = -4853256
75 meter
Z = 6419278
78 Z = 1977355
12
XDOT = 15940
265777 XDOT = 4863
624640
YDOT = 6409
882848 feet/sec YDOT = 2008
092735 meter/sec
ZDOT = -18397
104115 ZDOT = -5583
822013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16448212
36 X = -5013415
13
Y = -13468140
57 feet Y = -4105089
25 meter
Z = 6505209
15 Z = 1982787
75
XDOT = 4991
490187 XDOT = 1521
406209
YDOT = -15019
651586 feet/sec YDOT = -4577
989803 meter/sec
ZDOT = -18299
995004 ZDOT = -5577
838477
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 12164
56692655
00016717 00000-0 10270-3 0 9083
2 25544 51
6349 145
5040 0010589 55
2420 304
9729 15
56347126 17293
Satellite: ISS
Catalog Number: 25544
Epoch time: 12164
56692655 = yrday
fracday
Element set: 908
Inclination: 51
6349 deg
RA of node: 145
5040 deg
Eccentricity:
0010589
Arg of perigee: 55
2420 deg
Mean anomaly: 304
9729 deg
Mean motion: 15
56347126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1729
Checksum: 320
Coasting Arc #10 (Orbit 1744)
---------------------------------------
Vector Time (GMT): 2012/165/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5364148
76 A = 6782714
34 meter
Y = 4112063
75 meter E =
0023255
Z = 428589
84 I = 51
87727
XDOT = -2575
619147 Wp = 54
39032
YDOT = -4009
674495 meter/sec RA = 139
67457 deg
ZDOT = 6019
382915 TA = 310
22372
MA = 310
42696
Ha = 221
154 n
mi
Hp = 207
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17598913
27 X = -5411814
03
Y = 13491022
81 feet Y = 4051811
96 meter
Z = 1406134
64 Z = 402415
51
XDOT = -8450
194053 XDOT = -2559
831712
YDOT = -13155
100048 feet/sec YDOT = -4038
389005 meter/sec
ZDOT = 19748
631612 ZDOT = 6006
908529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14255340
52 X = 4345027
79
Y = 16994329
93 feet Y = 5179871
76 meter
Z = 1297950
66 Z = 395615
36
XDOT = -11523
361413 XDOT = -3512
320559
YDOT = 8103
329266 feet/sec YDOT = 2469
894760 meter/sec
ZDOT = 19697
591729 ZDOT = 6003
825959
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 12165
59428696
00016717 00000-0 10270-3 0 9090
2 25544 51
6347 140
3650 0010529 60
0473 300
1725 15
56386669 17454
Satellite: ISS
Catalog Number: 25544
Epoch time: 12165
59428696 = yrday
fracday
Element set: 909
Inclination: 51
6347 deg
RA of node: 140
3650 deg
Eccentricity:
0010529
Arg of perigee: 60
0473 deg
Mean anomaly: 300
1725 deg
Mean motion: 15
56386669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1745
Checksum: 318
Coasting Arc #11 (Orbit 1759)
---------------------------------------
Vector Time (GMT): 2012/166/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5625310
16 A = 6779475
49 meter
Y = -2561705
77 meter E =
0013645
Z = -2799625
00 I = 51
88995
XDOT = 41
950526 Wp = 80
11980
YDOT = 5684
215714 meter/sec RA = 134
70593 deg
ZDOT = -5135
856511 TA = 131
50561
MA = 131
38843
Ha = 221
183 n
mi
Hp = 207
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18455741
99 X = 5667137
64
Y = -8404546
49 feet Y = -2498565
87 meter
Z = -9185121
38 Z = -2772195
97
XDOT = 137
632959 XDOT = 3
334377
YDOT = 18649
001685 feet/sec YDOT = 5684
469515 meter/sec
ZDOT = -16849
922935 ZDOT = -5135
745850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9524611
75 X = -2903101
66
Y = -17961064
91 feet Y = -5474532
59 meter
Z = -9071889
93 Z = -2765112
05
XDOT = 17288
330802 XDOT = 5269
483228
YDOT = -689
038426 feet/sec YDOT = -210
018912 meter/sec
ZDOT = -16849
970624 ZDOT = -5135
871046
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 12166
55742062
00016717 00000-0 10270-3 0 9105
2 25544 51
6355 135
5459 0010566 62
4289 297
7937 15
56402199 17608
Satellite: ISS
Catalog Number: 25544
Epoch time: 12166
55742062 = yrday
fracday
Element set: 910
Inclination: 51
6355 deg
RA of node: 135
5459 deg
Eccentricity:
0010566
Arg of perigee: 62
4289 deg
Mean anomaly: 297
7937 deg
Mean motion: 15
56402199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1760
Checksum: 327
Coasting Arc #12 (Orbit 1775)
---------------------------------------
Vector Time (GMT): 2012/167/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5006658
36 A = 6773949
11 meter
Y = 475829
10 meter E =
0017789
Z = 4522321
52 I = 51
89311
XDOT = 2254
576061 Wp = 87
75180
YDOT = -6619
262059 meter/sec RA = 129
72161 deg
ZDOT = 3182
434044 TA = 330
43338
MA = 330
53384
Ha = 221
173 n
mi
Hp = 207
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16426044
49 X = -5033575
67
Y = 1561119
10 feet Y = 419690
44 meter
Z = 14837012
85 Z = 4497933
87
XDOT = 7396
903088 XDOT = 2312
966761
YDOT = -21716
739040 feet/sec YDOT = -6593
723936 meter/sec
ZDOT = 10441
056576 ZDOT = 3193
527719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2853605
59 X = 869778
98
Y = 16342640
01 feet Y = 4981236
68 meter
Z = 14736486
46 Z = 4491681
07
XDOT = -21032
916481 XDOT = -6410
832943
YDOT = -5814
080574 feet/sec YDOT = -1772
131759 meter/sec
ZDOT = 10487
363426 ZDOT = 3196
548372
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 12167
58474198
00016717 00000-0 10270-3 0 9112
2 25544 51
6359 130
4070 0010345 66
6004 293
6237 15
56460035 17769
Satellite: ISS
Catalog Number: 25544
Epoch time: 12167
58474198 = yrday
fracday
Element set: 911
Inclination: 51
6359 deg
RA of node: 130
4070 deg
Eccentricity:
0010345
Arg of perigee: 66
6004 deg
Mean anomaly: 293
6237 deg
Mean motion: 15
56460035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1776
Checksum: 305
Coasting Arc #13 (Orbit 1790)
---------------------------------------
Vector Time (GMT): 2012/168/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3758680
05 A = 6770728
25 meter
Y = 1902179
33 meter E =
0024920
Z = -5322066
31 I = 51
90111
XDOT = -4014
293446 Wp = 79
33492
YDOT = 6496
509532 meter/sec RA = 124
71803 deg
ZDOT = -510
672479 TA = 185
78695
MA = 185
81580
Ha = 221
109 n
mi
Hp = 207
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12331627
46 X = 3762983
72
Y = 6240745
85 feet Y = 1944236
07 meter
Z = -17460847
48 Z = -5303795
94
XDOT = -13170
254088 XDOT = -4084
159640
YDOT = 21314
007650 feet/sec YDOT = 6451
228649 meter/sec
ZDOT = -1675
434643 ZDOT = -530
342630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5021636
11 X = 1530594
69
Y = -12977536
91 feet Y = -3955553
25 meter
Z = -17385736
85 Z = -5299172
59
XDOT = 21528
306617 XDOT = 6561
827857
YDOT = 10695
129159 feet/sec YDOT = 3259
875368 meter/sec
ZDOT = -1757
087327 ZDOT = -535
560217
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 12168
54784021
00016717 00000-0 10270-3 0 9129
2 25544 51
6361 125
5876 0010428 69
5705 290
6567 15
56444119 17918
Satellite: ISS
Catalog Number: 25544
Epoch time: 12168
54784021 = yrday
fracday
Element set: 912
Inclination: 51
6361 deg
RA of node: 125
5876 deg
Eccentricity:
0010428
Arg of perigee: 69
5705 deg
Mean anomaly: 290
6567 deg
Mean motion: 15
56444119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1791
Checksum: 321
Coasting Arc #14 (Orbit 1806)
---------------------------------------
Vector Time (GMT): 2012/169/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2083649
16 A = 6772186
68 meter
Y = -4138221
91 meter E =
0016843
Z = 4928088
13 I = 51
92366
XDOT = 5078
824035 Wp = 67
61020
YDOT = -5290
868633 meter/sec RA = 119
71314 deg
ZDOT = -2283
012389 TA = 44
64108
MA = 44
50558
Ha = 221
152 n
mi
Hp = 207
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6836119
30 X = -2061159
52
Y = -13576843
52 feet Y = -4161397
61 meter
Z = 16168268
14 Z = 4918019
76
XDOT = 16662
808515 XDOT = 5148
700555
YDOT = -17358
492891 feet/sec YDOT = -5233
683011 meter/sec
ZDOT = -7490
198127 ZDOT = -2258
170671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12707482
92 X = -3873240
79
Y = 8420840
28 feet Y = 2566672
12 meter
Z = 16127164
30 Z = 4915559
68
XDOT = -18517
847146 XDOT = -5644
239810
YDOT = -13718
053357 feet/sec YDOT = -4181
262663 meter/sec
ZDOT = -7387
326415 ZDOT = -2251
657091
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 12169
57512429
00016717 00000-0 10270-3 0 9135
2 25544 51
6368 120
4482 0010447 73
3862 286
8438 15
56481303 18078
Satellite: ISS
Catalog Number: 25544
Epoch time: 12169
57512429 = yrday
fracday
Element set: 913
Inclination: 51
6368 deg
RA of node: 120
4482 deg
Eccentricity:
0010447
Arg of perigee: 73
3862 deg
Mean anomaly: 286
8438 deg
Mean motion: 15
56481303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1807
Checksum: 317
Coasting Arc #15 (Orbit 1821)
---------------------------------------
Vector Time (GMT): 2012/170/12:44:24
279
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 345676
44 A = 6777227
09 meter
Y = 5799402
57 meter E =
0015296
Z = -3500776
54 I = 51
95524
XDOT = -5340
681751 Wp = 82
43422
YDOT = 3061
332222 meter/sec RA = 114
72331 deg
ZDOT = 4563
042019 TA = 236
61872
MA = 236
76518
Ha = 221
039 n
mi
Hp = 207
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1134109
07 X = 297806
67
Y = 19026911
33 feet Y = 5803001
08 meter
Z = -11485487
32 Z = -3499212
55
XDOT = -17521
921756 XDOT = -5396
683539
YDOT = 10043
740887 feet/sec YDOT = 3001
295518 meter/sec
ZDOT = 14970
610300 ZDOT = 4536
961649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18708874
62 X = 5702464
98
Y = -3663723
84 feet Y = -1116703
03 meter
Z = -11479595
60 Z = -3498980
74
XDOT = 11978
882344 XDOT = 3651
163339
YDOT = 14795
689985 feet/sec YDOT = 4509
726308 meter/sec
ZDOT = 14862
827013 ZDOT = 4530
189673
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 12170
53818436
00016717 00000-0 10270-3 0 9141
2 25544 51
6370 115
6295 0010372 76
6556 283
5754 15
56504537 18229
Satellite: ISS
Catalog Number: 25544
Epoch time: 12170
53818436 = yrday
fracday
Element set: 914
Inclination: 51
6370 deg
RA of node: 115
6295 deg
Eccentricity:
0010372
Arg of perigee: 76
6556 deg
Mean anomaly: 283
5754 deg
Mean motion: 15
56504537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1822
Checksum: 314
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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