Date:
January 15th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 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 2618)
---------------------------------------
Vector Time (GMT): 2007/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6410964
73 A = 6723159
11 meter
Y = 1709236
22 meter E =
0029357
Z = -1090100
29 I = 51
60649
XDOT = -2163
991737 Wp = 99
73864
YDOT = 4437
967382 meter/sec RA = 187
44786 deg
ZDOT = -5907
363867 TA = 92
19938
MA = 91
86319
Ha = 193
914 n
mi
Hp = 170
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21033348
86 X = 6396670
82
Y = 5607730
37 feet Y = 1780847
37 meter
Z = -3576444
52 Z = -1058990
54
XDOT = -7099
710424 XDOT = -2184
760121
YDOT = 14560
260439 feet/sec YDOT = 4413
652812 meter/sec
ZDOT = -19381
115049 ZDOT = -5917
926549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2261085
59 X = 689178
89
Y = 21669280
73 feet Y = 6604796
77 meter
Z = -3459642
18 Z = -1054498
94
XDOT = -14515
907904 XDOT = -4424
448729
YDOT = -1510
440076 feet/sec YDOT = -460
382135 meter/sec
ZDOT = -19420
121490 ZDOT = -5919
253030
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 07012
52978138
00020000 00000-0 20000-3 0 9002
2 25544 51
6293 188
2643 0023174 82
9664 277
4135 15
77000317 26190
Satellite: ISS
Catalog Number: 25544
Epoch time: 07012
52978138 = yrday
fracday
Element set: 900
Inclination: 51
6293 deg
RA of node: 188
2643 deg
Eccentricity:
0023174
Arg of perigee: 82
9664 deg
Mean anomaly: 277
4135 deg
Mean motion: 15
77000317 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2619
Checksum: 294
Coasting Arc #2 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2007/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2735243
52 A = 6713377
12 meter
Y = -3732004
84 meter E =
0029129
Z = 4841088
95 I = 51
60107
XDOT = 7051
658442 Wp = 81
24592
YDOT = 2125
601703 meter/sec RA = 182
25753 deg
ZDOT = -2329
388246 TA = 31
47098
MA = 31
29704
Ha = 193
883 n
mi
Hp = 170
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8973896
08 X = 2753255
01
Y = -12244110
38 feet Y = -3701317
63 meter
Z = 15882837
75 Z = 4854420
06
XDOT = 23135
362341 XDOT = 7038
681267
YDOT = 6973
758868 feet/sec YDOT = 2204
384956 meter/sec
ZDOT = -7642
349888 ZDOT = -2295
162730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14672140
44 X = 4472068
41
Y = 3688246
94 feet Y = 1124177
67 meter
Z = 15932316
67 Z = 4856170
12
XDOT = 2425
575417 XDOT = 739
315387
YDOT = 23037
672356 feet/sec YDOT = 7021
882534 meter/sec
ZDOT = -7513
806648 ZDOT = -2290
208266
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 07013
54369497
00020000 00000-0 20000-3 0 9018
2 25544 51
6285 183
0328 0023147 87
4316 272
9498 15
76970599 26355
Satellite: ISS
Catalog Number: 25544
Epoch time: 07013
54369497 = yrday
fracday
Element set: 901
Inclination: 51
6285 deg
RA of node: 183
0328 deg
Eccentricity:
0023147
Arg of perigee: 87
4316 deg
Mean anomaly: 272
9498 deg
Mean motion: 15
76970599 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2635
Checksum: 325
Coasting Arc #3 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2007/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5710701
20 A = 6719998
56 meter
Y = -2002735
17 meter E =
0036498
Z = 2888567
49 I = 51
65261
XDOT = 4053
758301 Wp = 87
92510
YDOT = -4201
151467 meter/sec RA = 177
14046 deg
ZDOT = 5048
296274 TA = 305
39083
MA = 305
73124
Ha = 193
896 n
mi
Hp = 170
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18735896
32 X = -5701913
96
Y = -6570653
44 feet Y = -2066546
63 meter
Z = 9476927
47 Z = 2860846
15
XDOT = 13299
731958 XDOT = 4075
911313
YDOT = -13783
305338 feet/sec YDOT = -4155
696848 meter/sec
ZDOT = 16562
651816 ZDOT = 5068
042616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1238507
59 X = -377497
11
Y = -19865467
80 feet Y = -6054994
58 meter
Z = 9372765
88 Z = 2856819
04
XDOT = 16381
138105 XDOT = 4992
970895
YDOT = 6911
105716 feet/sec YDOT = 2106
505022 meter/sec
ZDOT = 16636
122946 ZDOT = 5070
690274
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 07014
55758515
00020000 00000-0 20000-3 0 9024
2 25544 51
6287 177
8015 0023146 91
3949 268
9867 15
77036227 26511
Satellite: ISS
Catalog Number: 25544
Epoch time: 07014
55758515 = yrday
fracday
Element set: 902
Inclination: 51
6287 deg
RA of node: 177
8015 deg
Eccentricity:
0023146
Arg of perigee: 91
3949 deg
Mean anomaly: 268
9867 deg
Mean motion: 15
77036227 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2651
Checksum: 317
Coasting Arc #4 (Orbit 2665)
---------------------------------------
Vector Time (GMT): 2007/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4263785
49 A = 6717258
63 meter
Y = 3606853
28 meter E =
0029318
Z = -3760648
36 I = 51
67341
XDOT = -5878
691636 Wp = 97
21404
YDOT = -2552
976478 meter/sec RA = 171
93294 deg
ZDOT = 4241
183783 TA = 217
38877
MA = 217
59312
Ha = 193
809 n
mi
Hp = 170
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13988797
54 X = -4285532
55
Y = 11833508
14 feet Y = 3559052
19 meter
Z = -12338085
18 Z = -3781413
98
XDOT = -19287
046051 XDOT = -5870
309702
YDOT = -8375
907081 feet/sec YDOT = -2618
669008 meter/sec
ZDOT = 13914
644957 ZDOT = 4212
645341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16448684
27 X = -5013558
97
Y = -7952593
16 feet Y = -2423950
39 meter
Z = -12415464
76 Z = -3784233
66
XDOT = -741
181442 XDOT = -225
912104
YDOT = -19897
811256 feet/sec YDOT = -6064
852871 meter/sec
ZDOT = 13807
337672 ZDOT = 4208
476522
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 07015
50808865
00020000 00000-0 20000-3 0 9035
2 25544 51
6297 172
8971 0023229 94
9107 265
4710 15
77057623 26663
Satellite: ISS
Catalog Number: 25544
Epoch time: 07015
50808865 = yrday
fracday
Element set: 903
Inclination: 51
6297 deg
RA of node: 172
8971 deg
Eccentricity:
0023229
Arg of perigee: 94
9107 deg
Mean anomaly: 265
4710 deg
Mean motion: 15
77057623 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2666
Checksum: 310
Coasting Arc #5 (Orbit 2681)
---------------------------------------
Vector Time (GMT): 2007/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4422771
17 A = 6715064
86 meter
Y = 2533273
26 meter E =
0031477
Z = -4398656
16 I = 51
69455
XDOT = -5619
431368 Wp = 90
68865
YDOT = 4032
115833 meter/sec RA = 166
82700 deg
ZDOT = -3348
993230 TA = 145
67691
MA = 145
47313
Ha = 193
754 n
mi
Hp = 170
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14510404
09 X = 4415482
63
Y = 8311263
97 feet Y = 2582691
05 meter
Z = -14431286
63 Z = -4377187
95
XDOT = -18436
454618 XDOT = -5647
832826
YDOT = 13228
726486 feet/sec YDOT = 3969
117926 meter/sec
ZDOT = -10987
510597 ZDOT = -3376
360451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1420630
33 X = -433008
12
Y = 16731307
34 feet Y = 5099702
48 meter
Z = -14350475
02 Z = -4374024
79
XDOT = -18499
100578 XDOT = -5638
525856
YDOT = -11023
073700 feet/sec YDOT = -3359
832864 meter/sec
ZDOT = -11089
597832 ZDOT = -3380
109419
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 07016
52193714
00020000 00000-0 20000-3 0 9049
2 25544 51
6300 167
6653 0023190 98
5231 261
8563 15
77097885 26820
Satellite: ISS
Catalog Number: 25544
Epoch time: 07016
52193714 = yrday
fracday
Element set: 904
Inclination: 51
6300 deg
RA of node: 167
6653 deg
Eccentricity:
0023190
Arg of perigee: 98
5231 deg
Mean anomaly: 261
8563 deg
Mean motion: 15
77097885 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2682
Checksum: 301
Coasting Arc #6 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2007/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5403533
56 A = 6721576
35 meter
Y = -3441421
32 meter E =
0037141
Z = 1982332
05 I = 51
74402
XDOT = 4170
994383 Wp = 106
15779
YDOT = 3274
696455 meter/sec RA = 161
62967 deg
ZDOT = -5608
503442 TA = 51
72865
MA = 51
39509
Ha = 193
645 n
mi
Hp = 170
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17728128
48 X = 5431984
80
Y = -11290752
37 feet Y = -3380837
22 meter
Z = 6503714
07 Z = 2008650
51
XDOT = 13684
364772 XDOT = 4161
310841
YDOT = 10743
754772 feet/sec YDOT = 3321
285524 meter/sec
ZDOT = -18400
601843 ZDOT = -5588
264169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17865376
03 X = 5445366
61
Y = 11014009
18 feet Y = 3357070
00 meter
Z = 6601959
29 Z = 2012277
19
XDOT = -2869
420976 XDOT = -874
599513
YDOT = 15785
383678 feet/sec YDOT = 4811
384945 meter/sec
ZDOT = -18324
291566 ZDOT = -5585
244069
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 07017
53576399
00020000 00000-0 20000-3 0 9056
2 25544 51
6296 162
4326 0023117 102
4923 257
8830 15
77114188 26981
Satellite: ISS
Catalog Number: 25544
Epoch time: 07017
53576399 = yrday
fracday
Element set: 905
Inclination: 51
6296 deg
RA of node: 162
4326 deg
Eccentricity:
0023117
Arg of perigee: 102
4923 deg
Mean anomaly: 257
8830 deg
Mean motion: 15
77114188 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2698
Checksum: 309
Coasting Arc #7 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2007/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2797565
94 A = 6711488
61 meter
Y = -3221619
77 meter E =
0026783
Z = 5160442
79 I = 51
73875
XDOT = 6592
593690 Wp = 109
05197
YDOT = -3856
936316 meter/sec RA = 156
50617 deg
ZDOT = 1152
682689 TA = 329
91565
MA = 330
06923
Ha = 193
597 n
mi
Hp = 170
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9178365
93 X = -2786401
28
Y = -10569618
67 feet Y = -3252841
98 meter
Z = 16930586
58 Z = 5146879
23
XDOT = 21629
244389 XDOT = 6629
633141
YDOT = -12653
990537 feet/sec YDOT = -3783
007323 meter/sec
ZDOT = 3781
767353 ZDOT = 1184
798168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5256946
42 X = 1602317
27
Y = -13040610
85 feet Y = -3974778
19 meter
Z = 16879306
41 Z = 5144812
59
XDOT = 20083
049072 XDOT = 6121
313357
YDOT = 13203
325645 feet/sec YDOT = 4024
373657 meter/sec
ZDOT = 3901
712048 ZDOT = 1189
241832
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 07018
54956762
00020000 00000-0 20000-3 0 9065
2 25544 51
6310 157
2015 0022961 106
1175 254
2520 15
77187021 27143
Satellite: ISS
Catalog Number: 25544
Epoch time: 07018
54956762 = yrday
fracday
Element set: 906
Inclination: 51
6310 deg
RA of node: 157
2015 deg
Eccentricity:
0022961
Arg of perigee: 106
1175 deg
Mean anomaly: 254
2520 deg
Mean motion: 15
77187021 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2714
Checksum: 270
Coasting Arc #8 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2007/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5913886
11 A = 6723092
57 meter
Y = 3196072
12 meter E =
0030525
Z = 39540
02 I = 51
80510
XDOT = -2211
943679 Wp = 88
63382
YDOT = -4217
174082 meter/sec RA = 151
34650 deg
ZDOT = 6051
733402 TA = 271
79499
MA = 272
14458
Ha = 193
492 n
mi
Hp = 170
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19402513
47 X = -5949377
58
Y = 10485800
93 feet Y = 3129741
31 meter
Z = 129724
47 Z = 10725
33
XDOT = -7257
033069 XDOT = -2194
019623
YDOT = -13835
872973 feet/sec YDOT = -4241
809723 meter/sec
ZDOT = 19854
768380 ZDOT = 6041
031156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18318714
83 X = -5583544
28
Y = -12282124
36 feet Y = -3743591
51 meter
Z = 22061
74 Z = 6724
42
XDOT = 7913
926309 XDOT = 2412
164739
YDOT = -11629
579969 feet/sec YDOT = -3544
695974 meter/sec
ZDOT = 19814
082655 ZDOT = 6039
332393
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 07019
56335067
00020000 00000-0 20000-3 0 9078
2 25544 51
6324 151
9703 0023079 109
8076 250
5580 15
77198896 27309
Satellite: ISS
Catalog Number: 25544
Epoch time: 07019
56335067 = yrday
fracday
Element set: 907
Inclination: 51
6324 deg
RA of node: 151
9703 deg
Eccentricity:
0023079
Arg of perigee: 109
8076 deg
Mean anomaly: 250
5580 deg
Mean motion: 15
77198896 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2730
Checksum: 309
Coasting Arc #9 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2007/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1042261
10 A = 6711432
94 meter
Y = 4195928
61 meter E =
0036987
Z = -5165587
79 I = 51
79104
XDOT = -6801
914046 Wp = 108
40627
YDOT = 3311
266764 meter/sec RA = 146
18703 deg
ZDOT = 1313
506042 TA = 174
18983
MA = 174
14681
Ha = 193
368 n
mi
Hp = 170
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3419491
78 X = 1020356
89
Y = 13766169
97 feet Y = 4207461
69 meter
Z = -16947466
49 Z = -5160577
50
XDOT = -22315
990966 XDOT = -6844
816153
YDOT = 10863
736101 feet/sec YDOT = 3234
963990 meter/sec
ZDOT = 4309
403024 ZDOT = 1280
359408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10378079
48 X = -3163238
63
Y = 9703142
10 feet Y = 2957517
71 meter
Z = -16928126
88 Z = -5159693
07
XDOT = -19563
821437 XDOT = -5963
052774
YDOT = -13601
063326 feet/sec YDOT = -4145
604102 meter/sec
ZDOT = 4185
496578 ZDOT = 1275
739357
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 07020
51375126
00020000 00000-0 20000-3 0 9086
2 25544 51
6328 147
0663 0023017 113
2162 247
1430 15
77244454 27455
Satellite: ISS
Catalog Number: 25544
Epoch time: 07020
51375126 = yrday
fracday
Element set: 908
Inclination: 51
6328 deg
RA of node: 147
0663 deg
Eccentricity:
0023017
Arg of perigee: 113
2162 deg
Mean anomaly: 247
1430 deg
Mean motion: 15
77244454 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2745
Checksum: 263
Coasting Arc #10 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2007/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5838339
31 A = 6720811
57 meter
Y = -2477149
76 meter E =
0028826
Z = -2217040
98 I = 51
84635
XDOT = 218
824606 Wp = 121
61071
YDOT = 5383
833233 meter/sec RA = 141
06900 deg
ZDOT = -5506
026322 TA = 83
20159
MA = 82
87367
Ha = 193
337 n
mi
Hp = 170
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19154656
54 X = 5876374
91
Y = -8127131
75 feet Y = -2411649
42 meter
Z = -7273756
49 Z = -2188586
89
XDOT = 717
928498 XDOT = 185
352061
YDOT = 17663
494859 feet/sec YDOT = 5386
093375 meter/sec
ZDOT = -18064
390819 ZDOT = -5505
044333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16579084
21 X = 5053304
87
Y = 12634156
86 feet Y = 3850891
01 meter
Z = -7167336
91 Z = -2184604
29
XDOT = -14009
412540 XDOT = -4270
068942
YDOT = 8264
517310 feet/sec YDOT = 2519
024876 meter/sec
ZDOT = -18060
002990 ZDOT = -5504
688911
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 07021
52749019
00020000 00000-0 20000-3 0 9095
2 25544 51
6332 141
8332 0022961 117
0252 243
3260 15
77264366 27615
Satellite: ISS
Catalog Number: 25544
Epoch time: 07021
52749019 = yrday
fracday
Element set: 909
Inclination: 51
6332 deg
RA of node: 141
8332 deg
Eccentricity:
0022961
Arg of perigee: 117
0252 deg
Mean anomaly: 243
3260 deg
Mean motion: 15
77264366 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2761
Checksum: 272
Coasting Arc #11 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2007/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 553181
84 A = 6715012
60 meter
Y = -5162633
20 meter E =
0030628
Z = 4227653
98 I = 51
84879
XDOT = 6435
071678 Wp = 106
75388
YDOT = -2282
710048 meter/sec RA = 135
87923 deg
ZDOT = -3616
886474 TA = 19
83634
MA = 19
71750
Ha = 193
271 n
mi
Hp = 170
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1814901
03 X = 590333
35
Y = -16937772
95 feet Y = -5156239
60 meter
Z = 13870255
83 Z = 4230431
37
XDOT = 21112
439888 XDOT = 6477
688742
YDOT = -7489
206195 feet/sec YDOT = -2210
511108 meter/sec
ZDOT = -11866
425441 ZDOT = -3585
522226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15447768
58 X = 4708479
86
Y = -7160873
19 feet Y = -2182634
15 meter
Z = 13879998
42 Z = 4230623
52
XDOT = 16736
769711 XDOT = 5101
367408
YDOT = 13251
421035 feet/sec YDOT = 4039
033132 meter/sec
ZDOT = -11749
057049 ZDOT = -3581
112589
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 07022
54120747
00020000 00000-0 20000-3 0 9101
2 25544 51
6336 136
6021 0023005 120
5357 239
8082 15
77274638 27773
Satellite: ISS
Catalog Number: 25544
Epoch time: 07022
54120747 = yrday
fracday
Element set: 910
Inclination: 51
6336 deg
RA of node: 136
6021 deg
Eccentricity:
0023005
Arg of perigee: 120
5357 deg
Mean anomaly: 239
8082 deg
Mean motion: 15
77274638 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2777
Checksum: 276
Coasting Arc #12 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2007/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5255785
36 A = 6715936
54 meter
Y = 1357780
65 meter E =
0033356
Z = 3940217
77 I = 51
87251
XDOT = 1382
991443 Wp = 116
69429
YDOT = -6435
248916 meter/sec RA = 130
78487 deg
ZDOT = 4021
634538 TA = 291
61551
MA = 291
97053
Ha = 193
100 n
mi
Hp = 170
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17243390
28 X = -5289718
12
Y = 4454660
94 feet Y = 1298817
74 meter
Z = 12927223
66 Z = 3914603
27
XDOT = 4537
373500 XDOT = 1435
312535
YDOT = -21113
021377 feet/sec YDOT = -6419
491063 meter/sec
ZDOT = 13194
339036 ZDOT = 4028
479951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12891519
54 X = -3929335
16
Y = -12387819
64 feet Y = -3775807
43 meter
Z = 12831300
50 Z = 3910980
39
XDOT = 19403
879482 XDOT = 5914
302466
YDOT = -6361
197145 feet/sec YDOT = -1938
892890 meter/sec
ZDOT = 13219
178089 ZDOT = 4029
205482
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 07023
55489887
00020000 00000-0 20000-3 0 9117
2 25544 51
6339 131
3700 0022850 124
4653 235
8675 15
77366077 27932
Satellite: ISS
Catalog Number: 25544
Epoch time: 07023
55489887 = yrday
fracday
Element set: 911
Inclination: 51
6339 deg
RA of node: 131
3700 deg
Eccentricity:
0022850
Arg of perigee: 124
4653 deg
Mean anomaly: 235
8675 deg
Mean motion: 15
77366077 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2793
Checksum: 311
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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