Date:
January 17th 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 2666)
---------------------------------------
Vector Time (GMT): 2007/015/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6632001
16 A = 6722956
47 meter
Y = -97215
80 meter E =
0030493
Z = -1082012
15 I = 51
69394
XDOT = -871
071756 Wp = 108
85844
YDOT = 4851
122306 meter/sec RA = 171
75632 deg
ZDOT = -5919
680675 TA = 82
98140
MA = 82
63469
Ha = 193
752 n
mi
Hp = 170
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21758533
99 X = 6637851
51
Y = -318949
48 feet Y = -23020
21 meter
Z = -3549908
64 Z = -1049779
97
XDOT = -2857
846970 XDOT = -896
496468
YDOT = 15915
755596 feet/sec YDOT = 4841
240173 meter/sec
ZDOT = -19421
524525 ZDOT = -5923
973379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13915202
42 X = 4241353
70
Y = 16755471
80 feet Y = 5107067
81 meter
Z = -3429094
33 Z = -1045187
95
XDOT = -12895
580004 XDOT = -3930
572785
YDOT = 6832
339724 feet/sec YDOT = 2082
497148 meter/sec
ZDOT = -19436
993937 ZDOT = -5924
395752
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
57146547
00020000 00000-0 20000-3 0 9001
2 25544 51
6298 172
5721 0023016 95
0750 265
3042 15
77075813 26673
Satellite: ISS
Catalog Number: 25544
Epoch time: 07015
57146547 = yrday
fracday
Element set: 900
Inclination: 51
6298 deg
RA of node: 172
5721 deg
Eccentricity:
0023016
Arg of perigee: 95
0750 deg
Mean anomaly: 265
3042 deg
Mean motion: 15
77075813 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2667
Checksum: 286
Coasting Arc #2 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2007/016/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1645792
28 A = 6713151
93 meter
Y = -4324012
69 meter E =
0028505
Z = 4839783
07 I = 51
68976
XDOT = 7357
434546 Wp = 90
41451
YDOT = 154
269435 meter/sec RA = 166
57246 deg
ZDOT = -2352
483873 TA = 22
48123
MA = 22
35658
Ha = 193
751 n
mi
Hp = 170
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5399580
98 X = 1670511
22
Y = -14186393
33 feet Y = -4305471
04 meter
Z = 15878553
39 Z = 4847837
62
XDOT = 24138
564784 XDOT = 7366
590451
YDOT = 506
133318 feet/sec YDOT = 236
595907 meter/sec
ZDOT = -7718
122942 ZDOT = -2316
719672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14294221
94 X = 4356878
85
Y = -5014195
44 feet Y = -1528326
77 meter
Z = 15908197
62 Z = 4848818
63
XDOT = 14742
382927 XDOT = 4493
478316
YDOT = 17844
845531 feet/sec YDOT = 5439
108918 meter/sec
ZDOT = -7584
017468 ZDOT = -2311
608524
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
58531650
00020000 00000-0 20000-3 0 9017
2 25544 51
6306 167
3412 0023095 99
0192 261
3587 15
77058889 26835
Satellite: ISS
Catalog Number: 25544
Epoch time: 07016
58531650 = yrday
fracday
Element set: 901
Inclination: 51
6306 deg
RA of node: 167
3412 deg
Eccentricity:
0023095
Arg of perigee: 99
0192 deg
Mean anomaly: 261
3587 deg
Mean motion: 15
77058889 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2683
Checksum: 304
Coasting Arc #3 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2007/017/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6016757
14 A = 6719533
84 meter
Y = -423907
05 meter E =
0035789
Z = 2935427
56 I = 51
74077
XDOT = 2837
072029 Wp = 95
49756
YDOT = -5126
329079 meter/sec RA = 161
46169 deg
ZDOT = 5019
436542 TA = 298
37144
MA = 298
73183
Ha = 193
602 n
mi
Hp = 170
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19740016
86 X = -6025829
27
Y = -1390771
16 feet Y = -491240
94 meter
Z = 9630667
86 Z = 2906176
62
XDOT = 9307
979097 XDOT = 2869
801469
YDOT = -16818
664956 feet/sec YDOT = -5094
421105 meter/sec
ZDOT = 16467
967658 ZDOT = 5033
297513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11891899
05 X = -3624650
83
Y = -15883541
20 feet Y = -4841303
36 meter
Z = 9520931
11 Z = 2901979
80
XDOT = 17592
766898 XDOT = 5362
275351
YDOT = -3159
320908 feet/sec YDOT = -962
961013 meter/sec
ZDOT = 16519
285660 ZDOT = 5035
078269
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
59914124
00020000 00000-0 20000-3 0 9021
2 25544 51
6319 162
1101 0022925 102
9916 257
3810 15
77160463 26999
Satellite: ISS
Catalog Number: 25544
Epoch time: 07017
59914124 = yrday
fracday
Element set: 902
Inclination: 51
6319 deg
RA of node: 162
1101 deg
Eccentricity:
0022925
Arg of perigee: 102
9916 deg
Mean anomaly: 257
3810 deg
Mean motion: 15
77160463 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2699
Checksum: 282
Coasting Arc #4 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2007/018/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3226293
31 A = 6717236
04 meter
Y = 4606910
09 meter E =
0028694
Z = -3703125
01 I = 51
76034
XDOT = -6286
642261 Wp = 105
61568
YDOT = -950
084775 meter/sec RA = 156
26008 deg
ZDOT = 4315
245708 TA = 209
94497
MA = 210
10941
Ha = 193
497 n
mi
Hp = 170
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10584951
79 X = -3259579
98
Y = 15114534
40 feet Y = 4570646
26 meter
Z = -12149360
28 Z = -3718878
19
XDOT = -20625
466736 XDOT = -6296
513205
YDOT = -3117
076032 feet/sec YDOT = -1020
441278 meter/sec
ZDOT = 14157
630275 ZDOT = 4284
681852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18276670
03 X = -5570729
03
Y = 2242570
61 feet Y = 683535
52 meter
Z = -12207846
63 Z = -3720951
65
XDOT = -11320
676103 XDOT = -3450
542076
YDOT = -16173
667894 feet/sec YDOT = -4929
733974 meter/sec
ZDOT = 14042
886304 ZDOT = 4280
271746
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
54958553
00020000 00000-0 20000-3 0 9032
2 25544 51
6324 157
2061 0022806 105
9956 254
3723 15
77139120 27144
Satellite: ISS
Catalog Number: 25544
Epoch time: 07018
54958553 = yrday
fracday
Element set: 903
Inclination: 51
6324 deg
RA of node: 157
2061 deg
Eccentricity:
0022806
Arg of perigee: 105
9956 deg
Mean anomaly: 254
3723 deg
Mean motion: 15
77139120 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2714
Checksum: 288
Coasting Arc #5 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2007/019/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4850926
23 A = 6714584
28 meter
Y = 1344774
69 meter E =
0030645
Z = -4467032
47 I = 51
77797
XDOT = -4450
306838 Wp = 98
58807
YDOT = 5364
696051 meter/sec RA = 151
15858 deg
ZDOT = -3241
057563 TA = 139
06900
MA = 138
83854
Ha = 193
437 n
mi
Hp = 170
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15915112
29 X = 4857227
64
Y = 4411990
47 feet Y = 1399056
18 meter
Z = -14655618
34 Z = -4443451
90
XDOT = -14600
744220 XDOT = -4494
220862
YDOT = 17600
708829 feet/sec YDOT = 5314
685064 meter/sec
ZDOT = -10633
390955 ZDOT = -3262
782603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7634475
09 X = 2326988
01
Y = 14732986
82 feet Y = 4490614
38 meter
Z = -14567000
30 Z = -4440021
69
XDOT = -21719
666582 XDOT = -6620
154374
YDOT = 737
484378 feet/sec YDOT = 224
785238 meter/sec
ZDOT = -10714
182603 ZDOT = -3265
682857
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
56336997
00020000 00000-0 20000-3 0 9048
2 25544 51
6332 151
9738 0022778 110
0065 250
3555 15
77175726 27300
Satellite: ISS
Catalog Number: 25544
Epoch time: 07019
56336997 = yrday
fracday
Element set: 904
Inclination: 51
6332 deg
RA of node: 151
9738 deg
Eccentricity:
0022778
Arg of perigee: 110
0065 deg
Mean anomaly: 250
3555 deg
Mean motion: 15
77175726 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2730
Checksum: 300
Coasting Arc #6 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2007/020/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4390004
39 A = 6721542
03 meter
Y = -4717756
10 meter E =
0037021
Z = 1848195
04 I = 51
82666
XDOT = 4757
998430 Wp = 113
76718
YDOT = 2173
862889 meter/sec RA = 145
96948 deg
ZDOT = -5678
556388 TA = 45
70427
MA = 45
40122
Ha = 193
345 n
mi
Hp = 170
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14402901
55 X = 4433454
81
Y = -15478202
41 feet Y = -4668421
83 meter
Z = 6063632
02 Z = 1869626
20
XDOT = 15610
231071 XDOT = 4760
920926
YDOT = 7132
096091 feet/sec YDOT = 2227
086268 meter/sec
ZDOT = -18630
434344 ZDOT = -5655
435462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21117003
36 X = 6436462
62
Y = -341530
68 feet Y = -104098
55 meter
Z = 6143409
66 Z = 1872511
26
XDOT = 5702
791380 XDOT = 1738
210813
YDOT = 14738
151610 feet/sec YDOT = 4492
188611 meter/sec
ZDOT = -18543
422002 ZDOT = -5652
035026
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
57713245
00020000 00000-0 20000-3 0 9057
2 25544 51
6335 146
7425 0022868 113
6635 246
6933 15
77210147 27462
Satellite: ISS
Catalog Number: 25544
Epoch time: 07020
57713245 = yrday
fracday
Element set: 905
Inclination: 51
6335 deg
RA of node: 146
7425 deg
Eccentricity:
0022868
Arg of perigee: 113
6635 deg
Mean anomaly: 246
6933 deg
Mean motion: 15
77210147 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2746
Checksum: 291
Coasting Arc #7 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2007/021/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3401779
58 A = 6711005
04 meter
Y = -2501935
97 meter E =
0026220
Z = 5197859
00 I = 51
81572
XDOT = 5443
524926 Wp = 118
14284
YDOT = -5395
346776 meter/sec RA = 140
84790 deg
ZDOT = 949
809249 TA = 322
76469
MA = 322
94621
Ha = 193
243 n
mi
Hp = 170
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11160694
16 X = -3398799
28
Y = -8208451
34 feet Y = -2539960
15 meter
Z = 17053343
18 Z = 5181340
75
XDOT = 17859
333746 XDOT = 5498
838019
YDOT = -17701
268949 feet/sec YDOT = -5334
165024 meter/sec
ZDOT = 3116
172077 ZDOT = 976
387216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2102369
18 X = -640802
13
Y = -13771005
27 feet Y = -4197402
41 meter
Z = 16991048
79 Z = 5178871
67
XDOT = 24127
977681 XDOT = 7354
207597
YDOT = 347
442655 feet/sec YDOT = 105
900521 meter/sec
ZDOT = 3215
172105 ZDOT = 979
984458
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
59087005
00020000 00000-0 20000-3 0 9069
2 25544 51
6343 141
5110 0022670 117
2572 243
0905 15
77304630 27625
Satellite: ISS
Catalog Number: 25544
Epoch time: 07021
59087005 = yrday
fracday
Element set: 906
Inclination: 51
6343 deg
RA of node: 141
5110 deg
Eccentricity:
0022670
Arg of perigee: 117
2572 deg
Mean anomaly: 243
0905 deg
Mean motion: 15
77304630 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2762
Checksum: 256
Coasting Arc #8 (Orbit 2777)
---------------------------------------
Vector Time (GMT): 2007/022/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4946423
15 A = 6722809
49 meter
Y = 4547248
84 meter E =
0029099
Z = 255652
95 I = 51
87686
XDOT = -3033
077343 Wp = 95
93628
YDOT = -3672
476670 meter/sec RA = 135
69659 deg
ZDOT = 6048
643373 TA = 266
83400
MA = 267
16698
Ha = 193
118 n
mi
Hp = 171
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16228422
40 X = -4998145
39
Y = 14918795
42 feet Y = 4491645
98 meter
Z = 838756
39 Z = 231498
31
XDOT = -9951
041153 XDOT = -3021
168253
YDOT = -12048
807973 feet/sec YDOT = -3706
327805 meter/sec
ZDOT = 19844
630490 ZDOT = 6033
937878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22038013
32 X = -6717186
46
Y = -633269
63 feet Y = -193020
58 meter
Z = 748732
89 Z = 228213
78
XDOT = 1149
371336 XDOT = 350
328383
YDOT = -14044
586818 feet/sec YDOT = -4280
790062 meter/sec
ZDOT = 19788
978628 ZDOT = 6031
680686
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
60458888
00020000 00000-0 20000-3 0 9074
2 25544 51
6344 136
2797 0022688 120
5828 239
7579 15
77290320 27784
Satellite: ISS
Catalog Number: 25544
Epoch time: 07022
60458888 = yrday
fracday
Element set: 907
Inclination: 51
6344 deg
RA of node: 136
2797 deg
Eccentricity:
0022688
Arg of perigee: 120
5828 deg
Mean anomaly: 239
7579 deg
Mean motion: 15
77290320 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2778
Checksum: 330
Coasting Arc #9 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2007/023/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1893598
22 A = 6711420
83 meter
Y = 3958793
04 meter E =
0035762
Z = -5109068
97 I = 51
85806
XDOT = -5764
261331 Wp = 115
91746
YDOT = 4818
581198 meter/sec RA = 130
53638 deg
ZDOT = 1590
581722 TA = 169
38926
MA = 169
31360
Ha = 192
959 n
mi
Hp = 171
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6212592
59 X = 1874008
15
Y = 12988166
14 feet Y = 3979858
87 meter
Z = -16762037
31 Z = -5099917
57
XDOT = -18911
618540 XDOT = -5825
441587
YDOT = 15808
993432 feet/sec YDOT = 4753
779912 meter/sec
ZDOT = 5218
443971 ZDOT = 1562
430968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4305332
25 X = -1312265
27
Y = 13781150
11 feet Y = 4200494
55 meter
Z = -16727183
78 Z = -5098445
62
XDOT = -23622
789034 XDOT = -7200
226098
YDOT = -1146
659939 feet/sec YDOT = -349
501949 meter/sec
ZDOT = 5113
458690 ZDOT = 1558
582209
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
55492763
00020000 00000-0 20000-3 0 9080
2 25544 51
6340 131
3748 0022614 124
0572 236
2744 15
77342700 27939
Satellite: ISS
Catalog Number: 25544
Epoch time: 07023
55492763 = yrday
fracday
Element set: 908
Inclination: 51
6340 deg
RA of node: 131
3748 deg
Eccentricity:
0022614
Arg of perigee: 124
0572 deg
Mean anomaly: 236
2744 deg
Mean motion: 15
77342700 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2793
Checksum: 281
Coasting Arc #10 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2007/024/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5019429
71 A = 6720046
09 meter
Y = -3717922
01 meter E =
0028036
Z = -2468158
10 I = 51
90398
XDOT = 1355
870395 Wp = 128
97784
YDOT = 5357
365785 meter/sec RA = 125
42652 deg
ZDOT = -5370
345350 TA = 78
85910
MA = 78
54401
Ha = 192
943 n
mi
Hp = 171
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16467945
25 X = 5072620
68
Y = -12197906
84 feet Y = -3661494
48 meter
Z = -8097631
57 Z = -2443644
95
XDOT = 4448
393684 XDOT = 1321
950588
YDOT = 17576
659401 feet/sec YDOT = 5372
338355 meter/sec
ZDOT = -17619
243273 ZDOT = -5363
840891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20424061
61 X = 6225253
98
Y = 2076816
15 feet Y = 633013
56 meter
Z = -8006143
33 Z = -2440272
49
XDOT = -8304
058198 XDOT = -2531
076939
YDOT = 14576
631507 feet/sec YDOT = 4442
957283 meter/sec
ZDOT = -17594
139506 ZDOT = -5362
693721
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 07024
56860154
00020000 00000-0 20000-3 0 9096
2 25544 51
6331 126
1421 0022598 128
0090 232
3119 15
77351959 28096
Satellite: ISS
Catalog Number: 25544
Epoch time: 07024
56860154 = yrday
fracday
Element set: 909
Inclination: 51
6331 deg
RA of node: 126
1421 deg
Eccentricity:
0022598
Arg of perigee: 128
0090 deg
Mean anomaly: 232
3119 deg
Mean motion: 15
77351959 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2809
Checksum: 284
Coasting Arc #11 (Orbit 2824)
---------------------------------------
Vector Time (GMT): 2007/025/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -570630
81 A = 6715304
04 meter
Y = -5309650
11 meter E =
0029980
Z = 4039425
45 I = 51
90466
XDOT = 5626
940135 Wp = 114
54400
YDOT = -3580
401344 meter/sec RA = 120
23652 deg
ZDOT = -3901
217181 TA = 15
41027
MA = 15
31917
Ha = 192
719 n
mi
Hp = 171
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1872148
32 X = -530837
72
Y = -17420111
91 feet Y = -5315808
90 meter
Z = 13252708
16 Z = 4036749
79
XDOT = 18461
089682 XDOT = 5685
509683
YDOT = -11746
723569 feet/sec YDOT = -3517
150121 meter/sec
ZDOT = -12799
268968 ZDOT = -3873
739697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10029019
09 X = 3056845
02
Y = -14375959
68 feet Y = -4381792
51 meter
Z = 13241981
39 Z = 4036155
93
XDOT = 20628
388237 XDOT = 6287
532735
YDOT = 2664
975466 feet/sec YDOT = 812
284522 meter/sec
ZDOT = -12696
631262 ZDOT = -3869
933209
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 07025
58225200
00020000 00000-0 20000-3 0 9108
2 25544 51
6335 120
9095 0022427 131
3263 228
9836 15
77421409 28252
Satellite: ISS
Catalog Number: 25544
Epoch time: 07025
58225200 = yrday
fracday
Element set: 910
Inclination: 51
6335 deg
RA of node: 120
9095 deg
Eccentricity:
0022427
Arg of perigee: 131
3263 deg
Mean anomaly: 228
9836 deg
Mean motion: 15
77421409 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2825
Checksum: 272
Coasting Arc #12 (Orbit 2840)
---------------------------------------
Vector Time (GMT): 2007/026/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4706983
73 A = 6714889
39 meter
Y = 2347015
47 meter E =
0031808
Z = 4164730
34 I = 51
91637
XDOT = -46
421820 Wp = 125
91407
YDOT = -6756
322234 meter/sec RA = 115
14516 deg
ZDOT = 3717
109216 TA = 286
14818
MA = 286
49806
Ha = 192
637 n
mi
Hp = 171
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15442860
02 X = -4753109
86
Y = 7700182
00 feet Y = 2294121
18 meter
Z = 13663813
46 Z = 4141752
17
XDOT = -152
302560 XDOT = 11
074925
YDOT = -22166
411528 feet/sec YDOT = -6756
520118 meter/sec
ZDOT = 12195
240209 ZDOT = 3717
022905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16816677
89 X = -5125723
42
Y = -4161104
48 feet Y = -1268304
64 meter
Z = 13577889
42 Z = 4138540
69
XDOT = 13862
276233 XDOT = 4225
221796
YDOT = -15824
652821 feet/sec YDOT = -4823
354180 meter/sec
ZDOT = 12194
050695 ZDOT = 3716
746652
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 07026
59588041
00020000 00000-0 20000-3 0 9116
2 25544 51
6332 115
6771 0022407 135
3834 224
9139 15
77453222 28415
Satellite: ISS
Catalog Number: 25544
Epoch time: 07026
59588041 = yrday
fracday
Element set: 911
Inclination: 51
6332 deg
RA of node: 115
6771 deg
Eccentricity:
0022407
Arg of perigee: 135
3834 deg
Mean anomaly: 224
9139 deg
Mean motion: 15
77453222 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2841
Checksum: 283
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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