Date:
December 21st 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
356/16:38:37
103 -3
0 6
6 6
6
N/A -4
0 -0
9 194
8
000/00:21:10
206 -4
4 -0
1 185
2
Coasting Arc #1 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2010/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829361
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5691589
60 A = 6730782
87 meter
Y = -2443362
72 meter E =
0012699
Z = -2621788
25 I = 51
63601
XDOT = 4078
486660 Wp = 25
56384
YDOT = 3897
438244 meter/sec RA = 356
34264 deg
ZDOT = 5242
339008 TA = 304
62483
MA = 304
74451
Ha = 193
045 n
mi
Hp = 183
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18673194
22 X = 5731224
95
Y = -8016281
88 feet Y = -2379493
90 meter
Z = -8601667
47 Z = -2594042
50
XDOT = 13380
861746 XDOT = 4009
135208
YDOT = 12786
870880 feet/sec YDOT = 3942
657726 meter/sec
ZDOT = 17199
274961 ZDOT = 5261
984561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7418824
77 X = 2261257
79
Y = 18968900
53 feet Y = 5781720
88 meter
Z = -8489964
22 Z = -2587741
09
XDOT = -11818
993780 XDOT = -3602
429304
YDOT = 12324
998087 feet/sec YDOT = 3756
659417 meter/sec
ZDOT = 17278
140437 ZDOT = 5266
377205
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 10354
50518175
00016717 00000-0 10270-3 0 9002
2 25544 51
6457 356
8496 0008440 10
4996 349
6342 15
73464744 12780
Satellite: ISS
Catalog Number: 25544
Epoch time: 10354
50518175 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 356
8496 deg
Eccentricity:
0008440
Arg of perigee: 10
4996 deg
Mean anomaly: 349
6342 deg
Mean motion: 15
73464744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1278
Checksum: 326
Coasting Arc #2 (Orbit 1293)
---------------------------------------
Vector Time (GMT): 2010/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829361
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4012254
47 A = 6724811
24 meter
Y = -2996698
47 meter E =
0016355
Z = -4504198
03 I = 51
58460
XDOT = 6107
704685 Wp = 43
76713
YDOT = -3456
165798 meter/sec RA = 351
25367 deg
ZDOT = -3136
379962 TA = 194
82601
MA = 194
87403
Ha = 193
065 n
mi
Hp = 183
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13163564
52 X = -3956566
07
Y = -9831687
91 feet Y = -3041253
82 meter
Z = -14777552
58 Z = -4523554
76
XDOT = 20038
401199 XDOT = 6161
134184
YDOT = -11339
126634 feet/sec YDOT = -3387
566522 meter/sec
ZDOT = -10289
960505 ZDOT = -3106
579541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10021046
91 X = 3054415
10
Y = -12931217
68 feet Y = -3941435
15 meter
Z = -14855295
57 Z = -4527894
09
XDOT = 10103
661815 XDOT = 3079
596121
YDOT = 19531
063731 feet/sec YDOT = 5953
068225 meter/sec
ZDOT = -10169
946906 ZDOT = -3099
799817
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 10355
52136217
00016717 00000-0 10270-3 0 9019
2 25544 51
6446 351
6347 0008476 13
7747 346
3645 15
73468064 12942
Satellite: ISS
Catalog Number: 25544
Epoch time: 10355
52136217 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 351
6347 deg
Eccentricity:
0008476
Arg of perigee: 13
7747 deg
Mean anomaly: 346
3645 deg
Mean motion: 15
73468064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1294
Checksum: 315
Coasting Arc #3 (Orbit 1309)
---------------------------------------
Vector Time (GMT): 2010/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829361
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4941855
04 A = 6730056
66 meter
Y = 3560864
62 meter E =
0016915
Z = 2856841
15 I = 51
57233
XDOT = -5027
488422 Wp = 68
53979
YDOT = -2891
422846 meter/sec RA = 346
07095 deg
ZDOT = -5062
685642 TA = 78
63742
MA = 78
44743
Ha = 193
135 n
mi
Hp = 183
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16213435
18 X = -4995183
93
Y = 11682626
72 feet Y = 3505303
22 meter
Z = 9372838
41 Z = 2832704
77
XDOT = -16494
384587 XDOT = -4970
188888
YDOT = -9486
295425 feet/sec YDOT = -2947
322111 meter/sec
ZDOT = -16609
861030 ZDOT = -5086
970278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11726685
29 X = -3574293
68
Y = -16237530
48 feet Y = -4949199
29 meter
Z = 9275602
58 Z = 2827203
67
XDOT = 8258
834022 XDOT = 2517
292610
YDOT = -15565
453644 feet/sec YDOT = -4744
350271 meter/sec
ZDOT = -16707
436081 ZDOT = -5092
426518
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 10356
53752554
00016717 00000-0 10270-3 0 9020
2 25544 51
6444 346
4201 0008630 16
7594 343
3852 15
73526322 13104
Satellite: ISS
Catalog Number: 25544
Epoch time: 10356
53752554 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 346
4201 deg
Eccentricity:
0008630
Arg of perigee: 16
7594 deg
Mean anomaly: 343
3852 deg
Mean motion: 15
73526322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1310
Checksum: 288
Coasting Arc #4 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2010/356/16:49:12
206
Vector Time (MET): N/A
Weight (LBS) : 828621
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6340062
80 A = 6735524
73 meter
Y = -176436
66 meter E =
0008317
Z = -2271690
43 I = 51
57140
XDOT = 2082
543703 Wp = 99
44374
YDOT = -5021
642507 meter/sec RA = 345
08470 deg
ZDOT = -5440
389398 TA = 106
05119
MA = 105
95958
Ha = 194
786 n
mi
Hp = 185
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20800730
96 X = -6326583
26
Y = -578860
44 feet Y = -247259
36 meter
Z = -7453052
59 Z = -2302457
51
XDOT = 6832
492463 XDOT = 2164
970096
YDOT = -16475
205074 feet/sec YDOT = -4997
892584 meter/sec
ZDOT = -17849
046580 ZDOT = -5430
072996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19639196
33 X = -5986027
04
Y = -6741464
23 feet Y = -2054798
30 meter
Z = -7576813
85 Z = -2309412
86
XDOT = 11044
000230 XDOT = 3366
211270
YDOT = -12225
567544 feet/sec YDOT = -3726
352988 meter/sec
ZDOT = -17807
346843 ZDOT = -5427
679318
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 10356
72809246
00016717 00000-0 10270-3 0 9033
2 25544 51
6452 345
4441 0004927 56
6233 303
5400 15
72011165 13139
Satellite: ISS
Catalog Number: 25544
Epoch time: 10356
72809246 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 345
4441 deg
Eccentricity:
0004927
Arg of perigee: 56
6233 deg
Mean anomaly: 303
5400 deg
Mean motion: 15
72011165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1313
Checksum: 276
Coasting Arc #5 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2010/357/16:49:12
206
Vector Time (MET): N/A
Weight (LBS) : 828621
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -648737
24 A = 6726920
25 meter
Y = 4459643
70 meter E =
0010721
Z = 4988171
79 I = 51
51318
XDOT = -7382
799076 Wp = 56
96972
YDOT = 1077
584547 meter/sec RA = 339
92185 deg
ZDOT = -1914
863120 TA = 51
59548
MA = 51
49926
Ha = 194
783 n
mi
Hp = 185
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2128403
01 X = -722788
96
Y = 14631376
98 feet Y = 4451974
47 meter
Z = 16365393
00 Z = 4984840
94
XDOT = -24221
781746 XDOT = -7384
998165
YDOT = 3535
382373 feet/sec YDOT = 995
013584 meter/sec
ZDOT = -6282
359318 ZDOT = -1950
733580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6257556
41 X = -1907303
19
Y = 13412469
10 feet Y = 4088120
58 meter
Z = 16351820
69 Z = 4984034
95
XDOT = -23222
329509 XDOT = -7078
166034
YDOT = -2964
316315 feet/sec YDOT = -903
523613 meter/sec
ZDOT = -6426
702674 ZDOT = -1958
858975
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 10357
74520496
00016717 00000-0 10270-3 0 9044
2 25544 51
6449 340
2368 0004908 59
5521 300
6125 15
72053258 13295
Satellite: ISS
Catalog Number: 25544
Epoch time: 10357
74520496 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 340
2368 deg
Eccentricity:
0004908
Arg of perigee: 59
5521 deg
Mean anomaly: 300
6125 deg
Mean motion: 15
72053258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1329
Checksum: 303
Coasting Arc #6 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2010/358/16:49:12
206
Vector Time (MET): N/A
Weight (LBS) : 828621
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6322187
80 A = 6737248
28 meter
Y = -2048694
27 meter E =
0018748
Z = 1051786
92 I = 51
52028
XDOT = 596
417147 Wp = 58
11003
YDOT = 4907
063555 meter/sec RA = 334
81843 deg
ZDOT = 5906
064245 TA = 313
40834
MA = 313
56427
Ha = 194
813 n
mi
Hp = 185
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20742085
95 X = 6339517
47
Y = -6721437
88 feet Y = -1977898
96 meter
Z = 3450744
50 Z = 1082541
64
XDOT = 1956
749169 XDOT = 512
810868
YDOT = 16099
289880 feet/sec YDOT = 4913
265000 meter/sec
ZDOT = 19376
851199 ZDOT = 5908
759013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21761641
56 X = 6632948
35
Y = -986449
80 feet Y = -300669
90 meter
Z = 3574544
40 Z = 1089521
13
XDOT = -2565
550409 XDOT = -781
979765
YDOT = 14425
136189 feet/sec YDOT = 4396
781511 meter/sec
ZDOT = 19387
507513 ZDOT = 5909
312290
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 10358
76230439
00016717 00000-0 10270-3 0 9053
2 25544 51
6455 335
0287 0004977 63
4225 296
7447 15
72041659 13457
Satellite: ISS
Catalog Number: 25544
Epoch time: 10358
76230439 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 335
0287 deg
Eccentricity:
0004977
Arg of perigee: 63
4225 deg
Mean anomaly: 296
7447 deg
Mean motion: 15
72041659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 324
Coasting Arc #7 (Orbit 1359)
---------------------------------------
Vector Time (GMT): 2010/359/16:49:12
206
Vector Time (MET): N/A
Weight (LBS) : 828621
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1615921
84 A = 6725664
22 meter
Y = -3901644
69 meter E =
0019402
Z = -5251156
76 I = 51
45524
XDOT = 6814
799568 Wp = 87
24408
YDOT = -3511
664352 meter/sec RA = 329
67212 deg
ZDOT = 514
646296 TA = 187
65382
MA = 187
68347
Ha = 194
769 n
mi
Hp = 184
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5301580
83 X = -1546663
91
Y = -12800671
56 feet Y = -3919327
26 meter
Z = -17228204
61 Z = -5258838
90
XDOT = 22358
266298 XDOT = 6851
061132
YDOT = -11521
208503 feet/sec YDOT = -3435
254447 meter/sec
ZDOT = 1688
472100 ZDOT = 547
840059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1854224
45 X = -565167
61
Y = -13691782
25 feet Y = -4173255
23 meter
Z = -17258966
83 Z = -5260533
09
XDOT = 23511
540591 XDOT = 7166
317572
YDOT = -5470
400145 feet/sec YDOT = -1667
377964 meter/sec
ZDOT = 1822
133818 ZDOT = 555
386388
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 10359
71581971
00016717 00000-0 10270-3 0 9060
2 25544 51
6462 330
1465 0004936 67
1561 293
0122 15
72087326 13606
Satellite: ISS
Catalog Number: 25544
Epoch time: 10359
71581971 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 330
1465 deg
Eccentricity:
0004936
Arg of perigee: 67
1561 deg
Mean anomaly: 293
0122 deg
Mean motion: 15
72087326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1360
Checksum: 300
Coasting Arc #8 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2010/360/16:49:12
206
Vector Time (MET): N/A
Weight (LBS) : 828621
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5415599
56 A = 6737669
28 meter
Y = 3997433
91 meter E =
0015404
Z = 143726
75 I = 51
46976
XDOT = -2959
930441 Wp = 117
15030
YDOT = -3776
111118 meter/sec RA = 324
54198 deg
ZDOT = -6018
941899 TA = 61
28596
MA = 61
13123
Ha = 194
789 n
mi
Hp = 185
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17767715
09 X = -5460595
31
Y = 13114940
64 feet Y = 3936621
82 meter
Z = 471544
46 Z = 117308
91
XDOT = -9711
057877 XDOT = -2888
246548
YDOT = -12388
816003 feet/sec YDOT = -3808
809664 meter/sec
ZDOT = -19747
184708 ZDOT = -6033
147254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20326515
41 X = -6195521
90
Y = 8638007
49 feet Y = 2632864
68 meter
Z = 365129
77 Z = 111291
55
XDOT = -5829
696920 XDOT = -1776
891621
YDOT = -12793
838768 feet/sec YDOT = -3899
562057 meter/sec
ZDOT = -19804
196036 ZDOT = -6036
318952
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 10360
73288981
00016717 00000-0 10270-3 0 9070
2 25544 51
6462 324
9385 0004871 72
4073 287
7621 15
72069924 13768
Satellite: ISS
Catalog Number: 25544
Epoch time: 10360
73288981 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 324
9385 deg
Eccentricity:
0004871
Arg of perigee: 72
4073 deg
Mean anomaly: 287
7621 deg
Mean motion: 15
72069924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 332
Coasting Arc #9 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2010/361/16:49:12
206
Vector Time (MET): N/A
Weight (LBS) : 828621
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3434875
31 A = 6725625
35 meter
Y = 2520129
93 meter E =
0007521
Z = 5197859
15 I = 51
40581
XDOT = -5339
429522 Wp = 92
24732
YDOT = 5485
594098 meter/sec RA = 319
41518 deg
ZDOT = 867
424033 TA = 349
46217
MA = 349
47792
Ha = 194
598 n
mi
Hp = 184
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11269275
96 X = 3381189
27
Y = 8268142
83 feet Y = 2558240
29 meter
Z = 17053343
67 Z = 5214415
47
XDOT = -17517
813393 XDOT = -5404
587400
YDOT = 17997
355963 feet/sec YDOT = 5425
521009 meter/sec
ZDOT = 2845
879373 ZDOT = 841
327222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9127828
74 X = 2782162
20
Y = 10477047
80 feet Y = 3193404
17 meter
Z = 17119857
14 Z = 5218132
46
XDOT = -20230
735188 XDOT = -6166
328085
YDOT = 13139
724470 feet/sec YDOT = 4004
988018 meter/sec
ZDOT = 2740
709781 ZDOT = 835
368341
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 10361
74994273
00016717 00000-0 10270-3 0 9081
2 25544 51
6462 319
7306 0004865 74
5567 285
6133 15
72139918 13921
Satellite: ISS
Catalog Number: 25544
Epoch time: 10361
74994273 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 319
7306 deg
Eccentricity:
0004865
Arg of perigee: 74
5567 deg
Mean anomaly: 285
6133 deg
Mean motion: 15
72139918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 336
Coasting Arc #10 (Orbit 1406)
---------------------------------------
Vector Time (GMT): 2010/362/16:49:12
206
Vector Time (MET): N/A
Weight (LBS) : 828621
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3767330
04 A = 6736643
80 meter
Y = -5413731
28 meter E =
0012949
Z = -1353845
98 I = 51
42064
XDOT = 4698
112645 Wp = 50
94008
YDOT = 1826
229795 meter/sec RA = 314
25756 deg
ZDOT = 5815
887773 TA = 294
15523
MA = 294
29056
Ha = 194
687 n
mi
Hp = 184
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12360006
71 X = 3834164
15
Y = -17761585
57 feet Y = -5371228
94 meter
Z = -4441751
91 Z = -1335382
32
XDOT = 15413
755396 XDOT = 4649
089674
YDOT = 5991
567570 feet/sec YDOT = 1878
492406 meter/sec
ZDOT = 19080
996631 ZDOT = 5838
592276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15661393
50 X = 4773592
74
Y = -14953940
76 feet Y = -4557961
15 meter
Z = -4367294
00 Z = -1331151
21
XDOT = 12717
825397 XDOT = 3876
393181
YDOT = 7764
282580 feet/sec YDOT = 2366
553331 meter/sec
ZDOT = 19172
265373 ZDOT = 5843
706486
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 10362
70341761
00016717 00000-0 10270-3 0 9097
2 25544 51
6462 314
8478 0004841 77
3254 282
8449 15
72159790 14071
Satellite: ISS
Catalog Number: 25544
Epoch time: 10362
70341761 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 314
8478 deg
Eccentricity:
0004841
Arg of perigee: 77
3254 deg
Mean anomaly: 282
8449 deg
Mean motion: 15
72159790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1407
Checksum: 322
Coasting Arc #11 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2010/363/16:49:12
206
Vector Time (MET): N/A
Weight (LBS) : 828621
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4575964
88 A = 6726807
56 meter
Y = -595360
37 meter E =
0017376
Z = -4910434
78 I = 51
36690
XDOT = 3184
523786 Wp = 75
48442
YDOT = -6650
558843 meter/sec RA = 309
14831 deg
ZDOT = -2163
381719 TA = 173
40260
MA = 173
37970
Ha = 194
610 n
mi
Hp = 184
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15013008
13 X = -4545113
28
Y = -1953282
06 feet Y = -646358
62 meter
Z = -16110350
34 Z = -4932590
00
XDOT = 10447
912685 XDOT = 3269
164246
YDOT = -21819
418777 feet/sec YDOT = -6614
474131 meter/sec
ZDOT = -7097
709052 ZDOT = -2147
706273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14315083
43 X = -4363237
43
Y = -4626582
15 feet Y = -1410182
24 meter
Z = -16199451
72 Z = -4937592
88
XDOT = 13935
557114 XDOT = 4247
557808
YDOT = -18511
782345 feet/sec YDOT = -5642
391259 meter/sec
ZDOT = -7034
425830 ZDOT = -2144
092993
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 10363
72044199
00016717 00000-0 10270-3 0 9107
2 25544 51
6457 309
6391 0004759 79
9889 280
1810 15
72183934 14239
Satellite: ISS
Catalog Number: 25544
Epoch time: 10363
72044199 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 309
6391 deg
Eccentricity:
0004759
Arg of perigee: 79
9889 deg
Mean anomaly: 280
1810 deg
Mean motion: 15
72183934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 330
Coasting Arc #12 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2010/364/16:49:12
206
Vector Time (MET): N/A
Weight (LBS) : 828621
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1741974
64 A = 6734827
18 meter
Y = 6033778
63 meter E =
0018524
Z = 2411390
83 I = 51
37561
XDOT = -5520
064768 Wp = 100
05830
YDOT = 554
015961 meter/sec RA = 303
96918 deg
ZDOT = -5342
324049 TA = 52
63101
MA = 52
46245
Ha = 194
653 n
mi
Hp = 184
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5715139
89 X = -1821030
14
Y = 19795861
64 feet Y = 6013856
52 meter
Z = 7911387
24 Z = 2402736
96
XDOT = -18110
448713 XDOT = -5499
897501
YDOT = 1817
637668 feet/sec YDOT = 492
400646 meter/sec
ZDOT = -17527
309873 ZDOT = -5369
091549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8938262
93 X = -2724382
54
Y = 18579538
74 feet Y = 5663043
41 meter
Z = 7876370
11 Z = 2400717
61
XDOT = -16704
540409 XDOT = -5091
543917
YDOT = -516
139105 feet/sec YDOT = -157
319199 meter/sec
ZDOT = -17635
005702 ZDOT = -5375
149738
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 10364
73745259
00016717 00000-0 10270-3 0 9115
2 25544 51
6458 304
4308 0004871 84
3204 275
8513 15
72193023 14395
Satellite: ISS
Catalog Number: 25544
Epoch time: 10364
73745259 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 304
4308 deg
Eccentricity:
0004871
Arg of perigee: 84
3204 deg
Mean anomaly: 275
8513 deg
Mean motion: 15
72193023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 304
Coasting Arc #13 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2010/365/16:49:12
206
Vector Time (MET): N/A
Weight (LBS) : 828621
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4861436
89 A = 6728943
60 meter
Y = -1587409
46 meter E =
0013898
Z = 4363249
17 I = 51
33938
XDOT = -754
422623 Wp = 102
33174
YDOT = 6901
419858 meter/sec RA = 298
87161 deg
ZDOT = 3339
515401 TA = 313
89116
MA = 314
00585
Ha = 194
519 n
mi
Hp = 184
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15949596
10 X = 4857630
41
Y = -5208036
30 feet Y = -1533067
82 meter
Z = 14315121
93 Z = 4386856
57
XDOT = -2475
139838 XDOT = -847
762284
YDOT = 22642
453602 feet/sec YDOT = 6892
461110 meter/sec
ZDOT = 10956
415358 ZDOT = 3335
624623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16458308
50 X = 5016492
43
Y = -2812079
68 feet Y = -857121
89 meter
Z = 14410144
45 Z = 4392212
03
XDOT = -6055
440628 XDOT = -1845
698303
YDOT = 20820
920002 feet/sec YDOT = 6346
216417 meter/sec
ZDOT = 10940
529945 ZDOT = 3334
673527
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 10365
75444764
00016717 00000-0 10270-3 0 9126
2 25544 51
6453 299
2216 0004817 87
1898 272
9815 15
72190570 14554
Satellite: ISS
Catalog Number: 25544
Epoch time: 10365
75444764 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 299
2216 deg
Eccentricity:
0004817
Arg of perigee: 87
1898 deg
Mean anomaly: 272
9815 deg
Mean motion: 15
72190570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 334
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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