Date:
October 3rd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3875 01 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2754)
---------------------------------------
Vector Time (GMT): 2007/274/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3313017
95 A = 6719337
95 meter
Y = 3704049
03 meter E =
0011345
Z = 4516451
35 I = 51
30240
XDOT = -3000
529949 Wp = 62
98101
YDOT = 6411
711481 meter/sec RA = 274
91263 deg
ZDOT = -3046
417008 TA = 57
50400
MA = 57
39441
Ha = 188
800 n
mi
Hp = 180
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10869481
45 X = 3249412
01
Y = 12152391
84 feet Y = 3740741
39 meter
Z = 14817753
78 Z = 4532391
80
XDOT = -9844
258364 XDOT = -3057
204466
YDOT = 21035
798821 feet/sec YDOT = 6377
841006 meter/sec
ZDOT = -9994
806456 ZDOT = -3061
131429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9470836
33 X = -2886710
91
Y = -13202994
83 feet Y = -4024272
83 meter
Z = 14878718
63 Z = 4535033
44
XDOT = 10948
936342 XDOT = 3337
235797
YDOT = -19219
707221 feet/sec YDOT = -5858
166761 meter/sec
ZDOT = -10049
884640 ZDOT = -3063
204838
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 07274
50057236
00020000 00000-0 20000-3 0 9007
2 25544 51
6335 275
4361 0002743 53
6295 306
5122 15
75360614 27555
Satellite: ISS
Catalog Number: 25544
Epoch time: 07274
50057236 = yrday
fracday
Element set: 900
Inclination: 51
6335 deg
RA of node: 275
4361 deg
Eccentricity:
0002743
Arg of perigee: 53
6295 deg
Mean anomaly: 306
5122 deg
Mean motion: 15
75360614 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2755
Checksum: 274
Coasting Arc #2 (Orbit 2770)
---------------------------------------
Vector Time (GMT): 2007/275/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2412633
25 A = 6724268
02 meter
Y = -5482859
10 meter E =
0015694
Z = 3038333
65 I = 51
31752
XDOT = 3939
418201 Wp = 79
63089
YDOT = 4459
084053 meter/sec RA = 269
79077 deg
ZDOT = 4899
909909 TA = 315
78315
MA = 315
90846
Ha = 188
872 n
mi
Hp = 180
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7915463
43 X = 2459004
24
Y = -17988382
88 feet Y = -5455620
45 meter
Z = 9968286
26 Z = 3050166
92
XDOT = 12924
600397 XDOT = 3865
460108
YDOT = 14629
540855 feet/sec YDOT = 4502
723257 meter/sec
ZDOT = 16075
819912 ZDOT = 4918
868253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9382951
52 X = -2859923
62
Y = 17242750
24 feet Y = 5255590
27 meter
Z = 10012541
92 Z = 3051822
78
XDOT = -10265
677479 XDOT = -3128
978495
YDOT = -14998
622447 feet/sec YDOT = -4571
580122 meter/sec
ZDOT = 16148
340978 ZDOT = 4922
014330
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 07275
51553519
00020000 00000-0 20000-3 0 9015
2 25544 51
6332 270
2128 0002781 56
8079 303
3351 15
75356405 27713
Satellite: ISS
Catalog Number: 25544
Epoch time: 07275
51553519 = yrday
fracday
Element set: 901
Inclination: 51
6332 deg
RA of node: 270
2128 deg
Eccentricity:
0002781
Arg of perigee: 56
8079 deg
Mean anomaly: 303
3351 deg
Mean motion: 15
75356405 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2771
Checksum: 280
Coasting Arc #3 (Orbit 2785)
---------------------------------------
Vector Time (GMT): 2007/276/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3590814
03 A = 6721324
50 meter
Y = -4059358
94 meter E =
0009197
Z = -3983898
19 I = 51
30939
XDOT = 2568
665201 Wp = 95
06055
YDOT = -6106
957635 meter/sec RA = 264
57088 deg
ZDOT = 3914
370052 TA = 215
57936
MA = 215
64071
Ha = 188
891 n
mi
Hp = 180
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11780885
93 X = -3525801
60
Y = -13318106
76 feet Y = -4099149
92 meter
Z = -13070532
12 Z = -4001184
61
XDOT = 8427
379267 XDOT = 2617
747770
YDOT = -20035
950246 feet/sec YDOT = -6077
958967 meter/sec
ZDOT = 12842
421432 ZDOT = 3926
967888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10757729
16 X = 3278955
85
Y = 14096074
81 feet Y = 4296483
60 meter
Z = -13136665
83 Z = -4004055
74
XDOT = -8693
273614 XDOT = -2649
709798
YDOT = 18625
512782 feet/sec YDOT = 5677
056296 meter/sec
ZDOT = 12889
502711 ZDOT = 3928
720426
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 07276
46704841
00020000 00000-0 20000-3 0 9027
2 25544 51
6334 265
3160 0002770 58
5549 301
5885 15
75362691 27867
Satellite: ISS
Catalog Number: 25544
Epoch time: 07276
46704841 = yrday
fracday
Element set: 902
Inclination: 51
6334 deg
RA of node: 265
3160 deg
Eccentricity:
0002770
Arg of perigee: 58
5549 deg
Mean anomaly: 301
5885 deg
Mean motion: 15
75362691 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2786
Checksum: 306
Coasting Arc #4 (Orbit 2801)
---------------------------------------
Vector Time (GMT): 2007/277/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2123128
03 A = 6721955
07 meter
Y = 5142388
81 meter E =
0008919
Z = -3782251
04 I = 51
31440
XDOT = -4295
332723 Wp = 71
88002
YDOT = -4835
225541 meter/sec RA = 259
45223 deg
ZDOT = -4168
200644 TA = 154
19529
MA = 154
15077
Ha = 188
886 n
mi
Hp = 180
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6965643
14 X = -2162099
64
Y = 16871354
36 feet Y = 5118428
86 meter
Z = -12408960
09 Z = -3792659
93
XDOT = -14092
298961 XDOT = -4220
696831
YDOT = -15863
600855 feet/sec YDOT = -4882
841102 meter/sec
ZDOT = -13675
198962 ZDOT = -4188
886113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7763951
42 X = 2366452
39
Y = -16489913
92 feet Y = -5026125
76 meter
Z = -12447846
00 Z = -3794103
46
XDOT = 11968
589539 XDOT = 3648
026092
YDOT = 16004
876358 feet/sec YDOT = 4878
286314 meter/sec
ZDOT = -13754
345774 ZDOT = -4192
324592
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 07277
48198201
00020000 00000-0 20000-3 0 9038
2 25544 51
6320 260
0915 0002761 63
4316 296
7130 15
75392742 28026
Satellite: ISS
Catalog Number: 25544
Epoch time: 07277
48198201 = yrday
fracday
Element set: 903
Inclination: 51
6320 deg
RA of node: 260
0915 deg
Eccentricity:
0002761
Arg of perigee: 63
4316 deg
Mean anomaly: 296
7130 deg
Mean motion: 15
75392742 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2802
Checksum: 276
Coasting Arc #5 (Orbit 2817)
---------------------------------------
Vector Time (GMT): 2007/278/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3943523
56 A = 6723346
70 meter
Y = 4348910
19 meter E =
0015225
Z = 3264870
43 I = 51
32580
XDOT = -2317
432568 Wp = 86
78297
YDOT = 5647
499709 meter/sec RA = 254
23089 deg
ZDOT = -4703
812727 TA = 54
71463
MA = 54
57231
Ha = 188
744 n
mi
Hp = 180
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12938069
43 X = 3878740
13
Y = 14268078
04 feet Y = 4392646
77 meter
Z = 10711517
16 Z = 3283870
62
XDOT = -7603
125224 XDOT = -2357
561204
YDOT = 18528
542352 feet/sec YDOT = 5621
360361 meter/sec
ZDOT = -15432
456454 ZDOT = -4715
168471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12372863
50 X = -3771248
80
Y = -14707863
39 feet Y = -4482956
76 meter
Z = 10784215
08 Z = 3287028
75
XDOT = 7084
441469 XDOT = 2159
337760
YDOT = -17353
374246 feet/sec YDOT = -5289
308470 meter/sec
ZDOT = -15474
870000 ZDOT = -4716
740376
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 07278
49689932
00020000 00000-0 20000-3 0 9047
2 25544 51
6315 254
8673 0002751 63
1609 296
9836 15
75450830 28188
Satellite: ISS
Catalog Number: 25544
Epoch time: 07278
49689932 = yrday
fracday
Element set: 904
Inclination: 51
6315 deg
RA of node: 254
8673 deg
Eccentricity:
0002751
Arg of perigee: 63
1609 deg
Mean anomaly: 296
9836 deg
Mean motion: 15
75450830 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2818
Checksum: 327
Coasting Arc #6 (Orbit 2833)
---------------------------------------
Vector Time (GMT): 2007/279/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1966387
90 A = 6719591
53 meter
Y = -4689926
26 meter E =
0011397
Z = 4383811
10 I = 51
32177
XDOT = 4763
920875 Wp = 101
59000
YDOT = 5085
843646 meter/sec RA = 249
11124 deg
ZDOT = 3294
613237 TA = 315
16788
MA = 315
25991
Ha = 188
712 n
mi
Hp = 180
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6451403
86 X = 1997389
39
Y = -15386897
18 feet Y = -4667763
44 meter
Z = 14382582
35 Z = 4393439
38
XDOT = 15629
661665 XDOT = 4690
691466
YDOT = 16685
838735 feet/sec YDOT = 5138
707226 meter/sec
ZDOT = 10809
098546 ZDOT = 3317
578289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6640711
03 X = -2024088
72
Y = 15272269
70 feet Y = 4654987
81 meter
Z = 14418551
48 Z = 4394774
49
XDOT = -14158
305406 XDOT = -4315
451488
YDOT = -16473
440312 feet/sec YDOT = -5021
104607 meter/sec
ZDOT = 10896
956830 ZDOT = 3321
392442
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 07279
51180218
00020000 00000-0 20000-3 0 9055
2 25544 51
6309 249
6434 0002659 67
3144 292
8300 15
75463048 28349
Satellite: ISS
Catalog Number: 25544
Epoch time: 07279
51180218 = yrday
fracday
Element set: 905
Inclination: 51
6309 deg
RA of node: 249
6434 deg
Eccentricity:
0002659
Arg of perigee: 67
3144 deg
Mean anomaly: 292
8300 deg
Mean motion: 15
75463048 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2834
Checksum: 296
Coasting Arc #7 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2007/280/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4374260
53 A = 6725346
10 meter
Y = -4484643
32 meter E =
0008092
Z = -2444744
08 I = 51
35281
XDOT = 2248
798300 Wp = 56
56086
YDOT = -5086
591001 meter/sec RA = 243
89688 deg
ZDOT = 5324
238830 TA = 275
69797
MA = 275
79023
Ha = 188
816 n
mi
Hp = 180
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14351248
44 X = -4311911
28
Y = -14713396
73 feet Y = -4533210
34 meter
Z = -8020813
91 Z = -2465842
59
XDOT = 7377
947177 XDOT = 2279
645856
YDOT = -16688
290685 feet/sec YDOT = -5061
270819 meter/sec
ZDOT = 17467
975163 ZDOT = 5335
238831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14299554
26 X = 4358504
14
Y = 14719511
40 feet Y = 4486507
07 meter
Z = -8101516
11 Z = -2469342
11
XDOT = -6213
391876 XDOT = -1893
841844
YDOT = 15642
522366 feet/sec YDOT = 4767
840817 meter/sec
ZDOT = 17509
098228 ZDOT = 5336
773140
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 07280
46325957
00020000 00000-0 20000-3 0 9063
2 25544 51
6308 244
7457 0002859 71
3166 288
8308 15
75465961 28495
Satellite: ISS
Catalog Number: 25544
Epoch time: 07280
46325957 = yrday
fracday
Element set: 906
Inclination: 51
6308 deg
RA of node: 244
7457 deg
Eccentricity:
0002859
Arg of perigee: 71
3166 deg
Mean anomaly: 288
8308 deg
Mean motion: 15
75465961 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2849
Checksum: 330
Coasting Arc #8 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2007/281/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2027228
77 A = 6717590
46 meter
Y = 4173401
59 meter E =
0015121
Z = -4871855
77 I = 51
34094
XDOT = -5236
038432 Wp = 73
71333
YDOT = -5166
035173 meter/sec RA = 238
76756 deg
ZDOT = -2248
231001 TA = 174
31263
MA = 174
29544
Ha = 188
797 n
mi
Hp = 180
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6651013
04 X = -2050078
88
Y = 13692262
43 feet Y = 4150603
81 meter
Z = -15983778
78 Z = -4881759
98
XDOT = -17178
603778 XDOT = -5166
960289
YDOT = -16948
934295 feet/sec YDOT = -5224
201465 meter/sec
ZDOT = -7376
085960 ZDOT = -2273
499708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6330440
18 X = 1929518
17
Y = -13800469
73 feet Y = -4206383
18 meter
Z = -16020854
26 Z = -4883156
38
XDOT = 16412
317312 XDOT = 5002
474317
YDOT = 16197
490272 feet/sec YDOT = 4936
995035 meter/sec
ZDOT = -7472
720683 ZDOT = -2277
685264
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 07281
47813175
00020000 00000-0 20000-3 0 9070
2 25544 51
6311 239
5203 0002781 74
1704 285
9766 15
75486865 28653
Satellite: ISS
Catalog Number: 25544
Epoch time: 07281
47813175 = yrday
fracday
Element set: 907
Inclination: 51
6311 deg
RA of node: 239
5203 deg
Eccentricity:
0002781
Arg of perigee: 74
1704 deg
Mean anomaly: 285
9766 deg
Mean motion: 15
75486865 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2865
Checksum: 315
Coasting Arc #9 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2007/282/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4772286
82 A = 6726859
24 meter
Y = 4499929
80 meter E =
0016156
Z = 1461642
19 I = 51
38929
XDOT = -2435
091759 Wp = 111
85173
YDOT = 4474
844611 meter/sec RA = 233
56822 deg
ZDOT = -5780
952012 TA = 51
98671
MA = 51
84096
Ha = 188
694 n
mi
Hp = 180
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15657108
99 X = 4714512
74
Y = 14763549
22 feet Y = 4552973
30 meter
Z = 4795414
02 Z = 1484685
59
XDOT = -7989
146190 XDOT = -2456
865926
YDOT = 14681
248725 feet/sec YDOT = 4447
491806 meter/sec
ZDOT = -18966
377993 ZDOT = -5792
835126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16122332
39 X = -4914086
91
Y = -14224103
17 feet Y = -4335506
65 meter
Z = 4883516
18 Z = 1488495
73
XDOT = 6341
855752 XDOT = 1932
997633
YDOT = -13764
976927 feet/sec YDOT = -4195
564967 meter/sec
ZDOT = -19010
928111 ZDOT = -5794
530888
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 07282
49298712
00020000 00000-0 20000-3 0 9088
2 25544 51
6315 234
2958 0002738 74
6879 285
4587 15
75533052 28811
Satellite: ISS
Catalog Number: 25544
Epoch time: 07282
49298712 = yrday
fracday
Element set: 908
Inclination: 51
6315 deg
RA of node: 234
2958 deg
Eccentricity:
0002738
Arg of perigee: 74
6879 deg
Mean anomaly: 285
4587 deg
Mean motion: 15
75533052 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2881
Checksum: 331
Coasting Arc #10 (Orbit 2896)
---------------------------------------
Vector Time (GMT): 2007/283/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2268993
23 A = 6716072
28 meter
Y = -3650612
59 meter E =
0006014
Z = 5155758
99 I = 51
37196
XDOT = 5685
411257 Wp = 106
14486
YDOT = 5087
760825 meter/sec RA = 228
42644 deg
ZDOT = 1097
671407 TA = 333
33665
MA = 333
36756
Ha = 188
572 n
mi
Hp = 180
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7444203
50 X = 2284600
05
Y = -11977075
44 feet Y = -3625151
76 meter
Z = 16915219
77 Z = 5166820
17
XDOT = 18652
924073 XDOT = 5622
764203
YDOT = 16692
128691 feet/sec YDOT = 5150
988121 meter/sec
ZDOT = 3601
284145 ZDOT = 1125
139099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6726633
97 X = -2050278
03
Y = 12337422
98 feet Y = 3760446
53 meter
Z = 16956755
33 Z = 5168419
02
XDOT = -18562
169332 XDOT = -5657
749212
YDOT = -15226
635383 feet/sec YDOT = -4641
078465 meter/sec
ZDOT = 3706
269990 ZDOT = 1129
671093
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 07283
50782635
00020000 00000-0 20000-3 0 9094
2 25544 51
6321 229
0719 0002633 78
6002 281
5458 15
75561619 28972
Satellite: ISS
Catalog Number: 25544
Epoch time: 07283
50782635 = yrday
fracday
Element set: 909
Inclination: 51
6321 deg
RA of node: 229
0719 deg
Eccentricity:
0002633
Arg of perigee: 78
6002 deg
Mean anomaly: 281
5458 deg
Mean motion: 15
75561619 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2897
Checksum: 308
Coasting Arc #11 (Orbit 2911)
---------------------------------------
Vector Time (GMT): 2007/284/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5116802
73 A = 6727582
55 meter
Y = -4338169
45 meter E =
0013399
Z = -433757
45 I = 51
43127
XDOT = 2822
647888 Wp = 49
57822
YDOT = -3916
499413 meter/sec RA = 223
24767 deg
ZDOT = 6002
936646 TA = 305
68792
MA = 305
81255
Ha = 188
624 n
mi
Hp = 180
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16787410
54 X = -5065805
21
Y = -14232839
39 feet Y = -4395103
32 meter
Z = -1423088
74 Z = -458491
29
XDOT = 9260
655801 XDOT = 2837
071108
YDOT = -12849
407522 feet/sec YDOT = -3884
853916 meter/sec
ZDOT = 19694
674037 ZDOT = 6016
684695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17712377
18 X = 5398732
57
Y = 13053146
98 feet Y = 3978599
20 meter
Z = -1517596
66 Z = -462563
46
XDOT = -7298
543743 XDOT = -2224
596133
YDOT = 12153
042990 feet/sec YDOT = 3704
247503 meter/sec
ZDOT = 19746
381642 ZDOT = 6018
697124
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 07284
45922344
00020000 00000-0 20000-3 0 9104
2 25544 51
6322 224
1738 0002713 83
6575 276
4898 15
75581709 29121
Satellite: ISS
Catalog Number: 25544
Epoch time: 07284
45922344 = yrday
fracday
Element set: 910
Inclination: 51
6322 deg
RA of node: 224
1738 deg
Eccentricity:
0002713
Arg of perigee: 83
6575 deg
Mean anomaly: 276
4898 deg
Mean motion: 15
75581709 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2912
Checksum: 307
Coasting Arc #12 (Orbit 2927)
---------------------------------------
Vector Time (GMT): 2007/285/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2714023
44 A = 6715579
45 meter
Y = 3202353
50 meter E =
0017660
Z = -5257130
44 I = 51
41367
XDOT = -5980
532197 Wp = 90
31748
YDOT = -4833
004699 meter/sec RA = 218
08746 deg
ZDOT = 143
803652 TA = 181
05138
MA = 181
05510
Ha = 188
601 n
mi
Hp = 180
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8904276
36 X = -2724092
04
Y = 10506409
11 feet Y = 3171947
18 meter
Z = -17247803
29 Z = -5270340
15
XDOT = -19621
168625 XDOT = -5926
742913
YDOT = -15856
314628 feet/sec YDOT = -4899
581636 meter/sec
ZDOT = 471
796758 ZDOT = 114
880359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7876822
00 X = 2400855
35
Y = -11220850
94 feet Y = -3420115
37 meter
Z = -17297562
48 Z = -5272297
04
XDOT = 20088
782717 XDOT = 6123
060972
YDOT = 13546
573769 feet/sec YDOT = 4128
995685 meter/sec
ZDOT = 361
308646 ZDOT = 110
126875
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 07285
47403054
00020000 00000-0 20000-3 0 9110
2 25544 51
6330 218
9490 0002615 85
1360 275
0102 15
75591522 29280
Satellite: ISS
Catalog Number: 25544
Epoch time: 07285
47403054 = yrday
fracday
Element set: 911
Inclination: 51
6330 deg
RA of node: 218
9490 deg
Eccentricity:
0002615
Arg of perigee: 85
1360 deg
Mean anomaly: 275
0102 deg
Mean motion: 15
75591522 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2928
Checksum: 272
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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