Date:
March 19th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7104 18 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 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 3616)
---------------------------------------
Vector Time (GMT): 2007/075/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2882871
67 A = 6718605
18 meter
Y = -5407996
81 meter E =
0013060
Z = 2733399
56 I = 51
43406
XDOT = 5723
867161 Wp = 11
48497
YDOT = -453
335578 meter/sec RA = 221
10755 deg
ZDOT = 5148
360654 TA = 19
91226
MA = 19
86134
Ha = 186
177 n
mi
Hp = 178
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9458240
40 X = -2835462
51
Y = -17742771
68 feet Y = -5439969
43 meter
Z = 8967846
32 Z = 2719510
37
XDOT = 18779
091736 XDOT = 5703
501725
YDOT = -1487
321451 feet/sec YDOT = -389
441622 meter/sec
ZDOT = 16890
947028 ZDOT = 5176
117189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19899101
90 X = -6065246
26
Y = -3039296
04 feet Y = -926377
43 meter
Z = 8914872
37 Z = 2717253
10
XDOT = 9799
232146 XDOT = 2986
805958
YDOT = -14389
243405 feet/sec YDOT = -4385
841390 meter/sec
ZDOT = 16995
218792 ZDOT = 5180
142688
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 07075
72455025
00020000 00000-0 20000-3 0 9008
2 25544 51
6342 221
7093 0014909 313
4224 46
5699 15
77643706 36171
Satellite: ISS
Catalog Number: 25544
Epoch time: 07075
72455025 = yrday
fracday
Element set: 900
Inclination: 51
6342 deg
RA of node: 221
7093 deg
Eccentricity:
0014909
Arg of perigee: 313
4224 deg
Mean anomaly: 46
5699 deg
Mean motion: 15
77643706 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3617
Checksum: 291
Coasting Arc #2 (Orbit 3631)
---------------------------------------
Vector Time (GMT): 2007/076/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5564633
98 A = 6715499
84 meter
Y = -355590
79 meter E =
0010424
Z = -3730826
19 I = 51
44653
XDOT = -2460
050884 Wp = 336
45392
YDOT = -5951
888785 meter/sec RA = 215
88078 deg
ZDOT = 4241
877697 TA = 338
22226
MA = 338
26654
Ha = 186
248 n
mi
Hp = 178
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18256673
17 X = -5542120
78
Y = -1166636
44 feet Y = -417692
11 meter
Z = -12240243
41 Z = -3757803
99
XDOT = -8071
033084 XDOT = -2413
919088
YDOT = -19527
194176 feet/sec YDOT = -5979
140117 meter/sec
ZDOT = 13916
921579 ZDOT = 4230
039592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11606147
73 X = -3537553
83
Y = 14052412
29 feet Y = 4283175
27 meter
Z = -12341708
07 Z = -3761752
62
XDOT = -19572
558542 XDOT = -5965
715844
YDOT = -3997
768663 feet/sec YDOT = -1218
519888 meter/sec
ZDOT = 13871
570276 ZDOT = 4228
054620
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 07076
67468760
00020000 00000-0 20000-3 0 9014
2 25544 51
6340 216
8035 0014973 317
2946 42
7054 15
77689530 36329
Satellite: ISS
Catalog Number: 25544
Epoch time: 07076
67468760 = yrday
fracday
Element set: 901
Inclination: 51
6340 deg
RA of node: 216
8035 deg
Eccentricity:
0014973
Arg of perigee: 317
2946 deg
Mean anomaly: 42
7054 deg
Mean motion: 15
77689530 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3632
Checksum: 305
Coasting Arc #3 (Orbit 3647)
---------------------------------------
Vector Time (GMT): 2007/077/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1226345
34 A = 6713009
34 meter
Y = 4867934
45 meter E =
0015182
Z = -4464740
66 I = 51
46169
XDOT = -6917
417090 Wp = 359
06163
YDOT = -1178
239210 meter/sec RA = 210
75356 deg
ZDOT = -3169
565560 TA = 239
10946
MA = 239
25884
Ha = 186
630 n
mi
Hp = 178
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4023442
72 X = 1193508
90
Y = 15970913
56 feet Y = 4881464
04 meter
Z = -14648099
28 Z = -4458863
45
XDOT = -22694
937958 XDOT = -6888
330738
YDOT = -3865
614206 feet/sec YDOT = -1255
431363 meter/sec
ZDOT = -10398
837140 ZDOT = -3203
099187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15447455
10 X = 4708384
31
Y = 5770749
90 feet Y = 1758924
57 meter
Z = -14625305
48 Z = -4457793
11
XDOT = -15700
598121 XDOT = -4785
542307
YDOT = 15227
823096 feet/sec YDOT = 4641
440480 meter/sec
ZDOT = -10525
069136 ZDOT = -3208
041073
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 07077
68814244
00020000 00000-0 20000-3 0 9029
2 25544 51
6337 211
5697 0015065 321
4426 38
5662 15
77697971 36487
Satellite: ISS
Catalog Number: 25544
Epoch time: 07077
68814244 = yrday
fracday
Element set: 902
Inclination: 51
6337 deg
RA of node: 211
5697 deg
Eccentricity:
0015065
Arg of perigee: 321
4426 deg
Mean anomaly: 38
5662 deg
Mean motion: 15
77697971 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3648
Checksum: 318
Coasting Arc #4 (Orbit 3663)
---------------------------------------
Vector Time (GMT): 2007/078/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6327180
93 A = 6720258
16 meter
Y = 1594389
75 meter E =
0007629
Z = 1621553
24 I = 51
51312
XDOT = 179
508054 Wp = 33
56386
YDOT = 5135
918319 meter/sec RA = 205
53929 deg
ZDOT = -5731
244150 TA = 128
49035
MA = 128
42190
Ha = 186
806 n
mi
Hp = 177
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20758467
62 X = 6301004
81
Y = 5230937
49 feet Y = 1664997
65 meter
Z = 5320056
56 Z = 1652226
77
XDOT = 588
937185 XDOT = 149
905353
YDOT = 16850
125720 feet/sec YDOT = 5137
759518 meter/sec
ZDOT = -18803
294454 ZDOT = -5730
444585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15906183
08 X = 4848204
60
Y = -14283811
67 feet Y = -4353705
80 meter
Z = 5435600
31 Z = 1656770
97
XDOT = 13329
232388 XDOT = 4062
750032
YDOT = 7665
851577 feet/sec YDOT = 2336
551561 meter/sec
ZDOT = -18799
548704 ZDOT = -5730
102445
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 07078
70157051
00020000 00000-0 20000-3 0 9030
2 25544 51
6343 206
3356 0015221 326
1620 33
8573 15
77774246 36648
Satellite: ISS
Catalog Number: 25544
Epoch time: 07078
70157051 = yrday
fracday
Element set: 903
Inclination: 51
6343 deg
RA of node: 206
3356 deg
Eccentricity:
0015221
Arg of perigee: 326
1620 deg
Mean anomaly: 33
8573 deg
Mean motion: 15
77774246 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3664
Checksum: 280
Coasting Arc #5 (Orbit 3679)
---------------------------------------
Vector Time (GMT): 2007/079/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1011895
28 A = 6709331
41 meter
Y = -4070365
93 meter E =
0013266
Z = 5240375
86 I = 51
50307
XDOT = 7322
591083 Wp = 337
25818
YDOT = 2356
903045 meter/sec RA = 200
38459 deg
ZDOT = 429
121532 TA = 108
73287
MA = 108
58887
Ha = 186
907 n
mi
Hp = 177
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3319866
41 X = 1031878
66
Y = -13354218
93 feet Y = -4058938
12 meter
Z = 17192834
19 Z = 5245340
58
XDOT = 24024
248959 XDOT = 7293
607026
YDOT = 7732
621540 feet/sec YDOT = 2438
626340 meter/sec
ZDOT = 1407
879041 ZDOT = 464
624085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9456599
36 X = -2882371
49
Y = -9965309
19 feet Y = -3037426
24 meter
Z = 17210914
12 Z = 5245886
62
XDOT = 18818
308040 XDOT = 5735
820290
YDOT = -15265
245663 feet/sec YDOT = -4652
846878 meter/sec
ZDOT = 1541
691156 ZDOT = 469
907464
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 07079
71497218
00020000 00000-0 20000-3 0 9045
2 25544 51
6345 201
1012 0015244 329
7569 30
2715 15
77810973 36803
Satellite: ISS
Catalog Number: 25544
Epoch time: 07079
71497218 = yrday
fracday
Element set: 904
Inclination: 51
6345 deg
RA of node: 201
1012 deg
Eccentricity:
0015244
Arg of perigee: 329
7569 deg
Mean anomaly: 30
2715 deg
Mean motion: 15
77810973 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3680
Checksum: 290
Coasting Arc #6 (Orbit 3695)
---------------------------------------
Vector Time (GMT): 2007/080/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6189273
45 A = 6721112
01 meter
Y = -2420841
50 meter E =
0022391
Z = 896564
03 I = 51
56931
XDOT = 2512
411479 Wp = 11
90436
YDOT = -4215
317615 meter/sec RA = 195
21735 deg
ZDOT = 5957
403178 TA = 357
92228
MA = 357
93157
Ha = 187
307 n
mi
Hp = 177
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20306015
27 X = -6166098
62
Y = -7942393
37 feet Y = -2489923
78 meter
Z = 2941483
04 Z = 866552
87
XDOT = 8242
819813 XDOT = 2530
420929
YDOT = -13829
782203 feet/sec YDOT = -4187
121337 meter/sec
ZDOT = 19545
286016 ZDOT = 5969
652543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17491381
41 X = -5331373
05
Y = 13043023
98 feet Y = 3975513
71 meter
Z = 2828302
10 Z = 862066
48
XDOT = -6481
520435 XDOT = -1975
567429
YDOT = -12943
654661 feet/sec YDOT = -3945
225941 meter/sec
ZDOT = 19590
737797 ZDOT = 5971
256881
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 07080
72835094
00020000 00000-0 20000-3 0 9057
2 25544 51
6338 195
8669 0015430 335
0252 25
0165 15
77788424 36961
Satellite: ISS
Catalog Number: 25544
Epoch time: 07080
72835094 = yrday
fracday
Element set: 905
Inclination: 51
6338 deg
RA of node: 195
8669 deg
Eccentricity:
0015430
Arg of perigee: 335
0252 deg
Mean anomaly: 25
0165 deg
Mean motion: 15
77788424 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3696
Checksum: 310
Coasting Arc #7 (Orbit 3710)
---------------------------------------
Vector Time (GMT): 2007/081/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3331361
35 A = 6711005
71 meter
Y = 3288013
56 meter E =
0012242
Z = -4810245
60 I = 51
56413
XDOT = -6602
126883 Wp = 29
00332
YDOT = -3134
918124 meter/sec RA = 190
01932 deg
ZDOT = 2442
594308 TA = 264
79681
MA = 264
93653
Ha = 187
309 n
mi
Hp = 176
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10929663
22 X = -3344513
40
Y = 10787446
08 feet Y = 3250686
71 meter
Z = -15781645
66 Z = -4826461
47
XDOT = -21660
521270 XDOT = -6578
446822
YDOT = -10285
164449 feet/sec YDOT = -3208
614314 meter/sec
ZDOT = 8013
760853 ZDOT = 2410
578681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3674276
03 X = 1119919
33
Y = 14846306
15 feet Y = 4525154
12 meter
Z = -15842151
36 Z = -4828687
74
XDOT = -18902
187314 XDOT = -5761
386693
YDOT = 13054
703480 feet/sec YDOT = 3979
073621 meter/sec
ZDOT = 7892
934266 ZDOT = 2405
766364
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 07081
67836519
00020000 00000-0 20000-3 0 9066
2 25544 51
6337 190
9598 0015422 338
4828 21
5687 15
77863271 37116
Satellite: ISS
Catalog Number: 25544
Epoch time: 07081
67836519 = yrday
fracday
Element set: 906
Inclination: 51
6337 deg
RA of node: 190
9598 deg
Eccentricity:
0015422
Arg of perigee: 338
4828 deg
Mean anomaly: 21
5687 deg
Mean motion: 15
77863271 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3711
Checksum: 324
Coasting Arc #8 (Orbit 3726)
---------------------------------------
Vector Time (GMT): 2007/082/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5048258
09 A = 6716481
69 meter
Y = 3021153
02 meter E =
0014126
Z = -3255732
02 I = 51
61179
XDOT = -5061
832045 Wp =
53215
YDOT = 3335
454510 meter/sec RA = 184
89496 deg
ZDOT = -4739
902069 TA = 217
61900
MA = 217
71789
Ha = 187
472 n
mi
Hp = 176
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16562526
54 X = 5029915
70
Y = 9911919
37 feet Y = 3077502
88 meter
Z = -10681535
50 Z = -3231252
14
XDOT = -16607
060515 XDOT = -5075
727758
YDOT = 10943
092223 feet/sec YDOT = 3278
772527 meter/sec
ZDOT = -15550
859808 ZDOT = -4764
526262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16890088
13 X = 5148098
86
Y = -9447513
77 feet Y = -2879602
20 meter
Z = -10589052
75 Z = -3227543
28
XDOT = 538
242891 XDOT = 164
056433
YDOT = 18546
271806 feet/sec YDOT = 5652
903647 meter/sec
ZDOT = -15642
987222 ZDOT = -4767
982505
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 07082
69168992
00020000 00000-0 20000-3 0 9073
2 25544 51
6340 185
7250 0015418 342
9580 17
1065 15
77928428 37271
Satellite: ISS
Catalog Number: 25544
Epoch time: 07082
69168992 = yrday
fracday
Element set: 907
Inclination: 51
6340 deg
RA of node: 185
7250 deg
Eccentricity:
0015418
Arg of perigee: 342
9580 deg
Mean anomaly: 17
1065 deg
Mean motion: 15
77928428 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3727
Checksum: 316
Coasting Arc #9 (Orbit 3742)
---------------------------------------
Vector Time (GMT): 2007/083/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5339362
67 A = 6716367
59 meter
Y = -2551021
19 meter E =
0017222
Z = 3185155
69 I = 51
63988
XDOT = 4685
110988 Wp = 33
12168
YDOT = 3775
509883 meter/sec RA = 179
67738 deg
ZDOT = -4803
581148 TA = 109
68910
MA = 109
50321
Ha = 187
578 n
mi
Hp = 175
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17517594
08 X = 5352018
87
Y = -8369492
09 feet Y = -2491242
69 meter
Z = 10449985
86 Z = 3211124
97
XDOT = 15371
099041 XDOT = 4665
879340
YDOT = 12386
843447 feet/sec YDOT = 3827
793892 meter/sec
ZDOT = -15759
780670 ZDOT = -4780
867661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1139081
55 X = 347192
06
Y = -19328056
21 feet Y = -5891191
53 meter
Z = 10547295
43 Z = 3214815
65
XDOT = 16916
998745 XDOT = 5156
301217
YDOT = -7602
949044 feet/sec YDOT = -2317
378869 meter/sec
ZDOT = -15673
825449 ZDOT = -4777
381997
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 07083
70498716
00020000 00000-0 20000-3 0 9087
2 25544 51
6330 180
4899 0015565 346
8049 13
2706 15
77981847 37438
Satellite: ISS
Catalog Number: 25544
Epoch time: 07083
70498716 = yrday
fracday
Element set: 908
Inclination: 51
6330 deg
RA of node: 180
4899 deg
Eccentricity:
0015565
Arg of perigee: 346
8049 deg
Mean anomaly: 13
2706 deg
Mean motion: 15
77981847 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3743
Checksum: 327
Coasting Arc #10 (Orbit 3758)
---------------------------------------
Vector Time (GMT): 2007/084/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2936767
82 A = 6710571
51 meter
Y = -3576650
06 meter E =
0012258
Z = 4852281
25 I = 51
64867
XDOT = 6906
962726 Wp = 16
71809
YDOT = -2515
278739 meter/sec RA = 174
55538 deg
ZDOT = 2336
392636 TA = 50
61414
MA = 50
50564
Ha = 187
794 n
mi
Hp = 175
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9635065
02 X = -2920126
25
Y = -11734416
22 feet Y = -3609397
61 meter
Z = 15919557
90 Z = 4838054
96
XDOT = 22660
638864 XDOT = 6923
225912
YDOT = -8252
226835 feet/sec YDOT = -2437
950291 meter/sec
ZDOT = 7665
330170 ZDOT = 2369
985893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14925911
04 X = -4549417
68
Y = 3076524
88 feet Y = 937724
78 meter
Z = 15865544
42 Z = 4835817
94
XDOT = 3556
055467 XDOT = 1083
885706
YDOT = -22755
995584 feet/sec YDOT = -6936
027454 meter/sec
ZDOT = 7791
334100 ZDOT = 2374
798634
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 07084
71825954
00020000 00000-0 20000-3 0 9098
2 25544 51
6327 175
2542 0015536 351
3113 8
7781 15
78000107 37593
Satellite: ISS
Catalog Number: 25544
Epoch time: 07084
71825954 = yrday
fracday
Element set: 909
Inclination: 51
6327 deg
RA of node: 175
2542 deg
Eccentricity:
0015536
Arg of perigee: 351
3113 deg
Mean anomaly: 8
7781 deg
Mean motion: 15
78000107 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3759
Checksum: 293
Coasting Arc #11 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2007/085/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6413415
36 A = 6720416
78 meter
Y = 1806901
16 meter E =
0024212
Z = -750428
62 I = 51
71198
XDOT = -1948
866447 Wp = 12
76234
YDOT = -4451
256779 meter/sec RA = 169
36622 deg
ZDOT = 5997
418905 TA = 339
04011
MA = 339
13919
Ha = 187
794 n
mi
Hp = 175
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21041388
99 X = -6429498
33
Y = 5928153
40 feet Y = 1735092
83 meter
Z = -2462036
14 Z = -781623
69
XDOT = -6393
918789 XDOT = -1928
081038
YDOT = -14603
860822 feet/sec YDOT = -4472
933826 meter/sec
ZDOT = 19676
571211 ZDOT = 5988
001950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4269319
05 X = -1301288
45
Y = 21425817
72 feet Y = 6530589
24 meter
Z = -2579132
68 Z = -786119
64
XDOT = -14402
186640 XDOT = -4389
786488
YDOT = -528
028756 feet/sec YDOT = -160
943165 meter/sec
ZDOT = 19640
519699 ZDOT = 5986
430404
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 07085
66817796
00020000 00000-0 20000-3 0 9100
2 25544 51
6337 170
3468 0015622 354
7473 5
3526 15
78048578 37740
Satellite: ISS
Catalog Number: 25544
Epoch time: 07085
66817796 = yrday
fracday
Element set: 910
Inclination: 51
6337 deg
RA of node: 170
3468 deg
Eccentricity:
0015622
Arg of perigee: 354
7473 deg
Mean anomaly: 5
3526 deg
Mean motion: 15
78048578 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3774
Checksum: 322
Coasting Arc #12 (Orbit 3789)
---------------------------------------
Vector Time (GMT): 2007/086/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 386454
96 A = 6708695
14 meter
Y = 4188782
78 meter E =
0020329
Z = -5236970
20 I = 51
70055
XDOT = -7508
325317 Wp = 45
37057
YDOT = 1548
881008 meter/sec RA = 164
20617 deg
ZDOT = 700
466770 TA = 231
19650
MA = 231
37821
Ha = 187
999 n
mi
Hp = 175
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1267896
84 X = 365026
55
Y = 13742725
64 feet Y = 4192984
38 meter
Z = -17181660
77 Z = -5235144
99
XDOT = -24633
613246 XDOT = -7528
489787
YDOT = 5081
630603 feet/sec YDOT = 1464
805986 meter/sec
ZDOT = 2298
119325 ZDOT = 663
942844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12947418
43 X = 3946373
14
Y = 4805272
95 feet Y = 1464647
19 meter
Z = -17174202
90 Z = -5234697
04
XDOT = -5898
358839 XDOT = -1797
819774
YDOT = 23432
129718 feet/sec YDOT = 7142
113138 meter/sec
ZDOT = 2160
926545 ZDOT = 658
650411
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 07086
68139866
00020000 00000-0 20000-3 0 9119
2 25544 51
6338 165
1113 0015693 358
4515 1
6599 15
78059274 37908
Satellite: ISS
Catalog Number: 25544
Epoch time: 07086
68139866 = yrday
fracday
Element set: 911
Inclination: 51
6338 deg
RA of node: 165
1113 deg
Eccentricity:
0015693
Arg of perigee: 358
4515 deg
Mean anomaly: 1
6599 deg
Mean motion: 15
78059274 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3790
Checksum: 319
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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