Date:
February 28th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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
061/08:16:57
974 3
0 5
5 5
5
N/A -4
4 -0
1 187
1
000/00:07:55
947 1
1 0
1 175
2
Coasting Arc #1 (Orbit 3328)
---------------------------------------
Vector Time (GMT): 2007/057/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3977889
96 A = 6707336
51 meter
Y = -1790648
33 meter E =
0006980
Z = -5088962
35 I = 51
39354
XDOT = 4553
367024 Wp = 241
82489
YDOT = -6060
906871 meter/sec RA = 315
56925 deg
ZDOT = -1428
357635 TA = 14
47878
MA = 14
45879
Ha = 184
436 n
mi
Hp = 175
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13050820
08 X = -3932850
34
Y = -5874830
48 feet Y = -1834879
38 meter
Z = -16696070
69 Z = -5108177
13
XDOT = 14938
868188 XDOT = 4627
741081
YDOT = -19884
865061 feet/sec YDOT = -6009
572703 meter/sec
ZDOT = -4686
212713 ZDOT = -1406
057359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7814419
67 X = -2381835
11
Y = -11889056
37 feet Y = -3623784
38 meter
Z = -16768467
38 Z = -5111028
86
XDOT = 22406
974577 XDOT = 6829
645851
YDOT = -8243
363727 feet/sec YDOT = -2512
577264 meter/sec
ZDOT = -4603
208766 ZDOT = -1403
058032
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 07057
49733439
00020000 00000-0 20000-3 0 9000
2 25544 51
6357 316
0153 0020843 253
6996 106
1877 15
78712949 33295
Satellite: ISS
Catalog Number: 25544
Epoch time: 07057
49733439 = yrday
fracday
Element set: 900
Inclination: 51
6357 deg
RA of node: 316
0153 deg
Eccentricity:
0020843
Arg of perigee: 253
6996 deg
Mean anomaly: 106
1877 deg
Mean motion: 15
78712949 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3329
Checksum: 317
Coasting Arc #2 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2007/058/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4525274
62 A = 6718818
37 meter
Y = 4944061
14 meter E =
0018297
Z = -307155
71 I = 51
41249
XDOT = -3360
054135 Wp = 223
49613
YDOT = -3461
660349 meter/sec RA = 310
37208 deg
ZDOT = -6018
248197 TA = 319
86148
MA = 319
99649
Ha = 184
444 n
mi
Hp = 175
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14846701
52 X = -4578731
43
Y = 16220673
03 feet Y = 4893158
10 meter
Z = -1007728
69 Z = -329268
70
XDOT = -11023
799654 XDOT = -3291
860858
YDOT = -11357
153375 feet/sec YDOT = -3498
853019 meter/sec
ZDOT = -19744
908782 ZDOT = -6034
405286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21108946
36 X = -6434006
85
Y = 6146073
05 feet Y = 1873323
07 meter
Z = -1090167
99 Z = -332283
20
XDOT = -2974
319661 XDOT = -906
572633
YDOT = -13835
298983 feet/sec YDOT = -4216
999130 meter/sec
ZDOT = -19806
036292 ZDOT = -6036
879862
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 07058
51013645
00020000 00000-0 20000-3 0 9015
2 25544 51
6358 310
7773 0020980 257
2942 102
5878 15
78691807 33456
Satellite: ISS
Catalog Number: 25544
Epoch time: 07058
51013645 = yrday
fracday
Element set: 901
Inclination: 51
6358 deg
RA of node: 310
7773 deg
Eccentricity:
0020980
Arg of perigee: 257
2942 deg
Mean anomaly: 102
5878 deg
Mean motion: 15
78691807 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3345
Checksum: 303
Coasting Arc #3 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2007/059/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1835970
47 A = 6708028
62 meter
Y = 4205180
32 meter E =
0015515
Z = 4906639
64 I = 51
35920
XDOT = -5538
579298 Wp = 271
38144
YDOT = 4901
069281 meter/sec RA = 305
16116 deg
ZDOT = -2133
407898 TA = 199
37327
MA = 199
43231
Ha = 184
151 n
mi
Hp = 175
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6023525
16 X = 1764976
23
Y = 13796523
35 feet Y = 4225314
28 meter
Z = 16097899
07 Z = 4915386
02
XDOT = -18171
191923 XDOT = -5582
608717
YDOT = 16079
623624 feet/sec YDOT = 4838
887583 meter/sec
ZDOT = -6999
369745 ZDOT = -2160
420531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1843749
17 X = -561974
75
Y = 14904741
25 feet Y = 4542965
13 meter
Z = 16131290
83 Z = 4916817
44
XDOT = -22682
857052 XDOT = -6913
734829
YDOT = 4859
345022 feet/sec YDOT = 1481
128363 meter/sec
ZDOT = -7100
216409 ZDOT = -2164
145961
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 07059
52291442
00020000 00000-0 20000-3 0 9021
2 25544 51
6356 305
5390 0021035 261
8931 97
9848 15
78792999 33618
Satellite: ISS
Catalog Number: 25544
Epoch time: 07059
52291442 = yrday
fracday
Element set: 902
Inclination: 51
6356 deg
RA of node: 305
5390 deg
Eccentricity:
0021035
Arg of perigee: 261
8931 deg
Mean anomaly: 97
9848 deg
Mean motion: 15
78792999 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3361
Checksum: 321
Coasting Arc #4 (Orbit 3376)
---------------------------------------
Vector Time (GMT): 2007/060/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4889120
04 A = 6713906
65 meter
Y = -3257737
30 meter E =
0008192
Z = 3257944
33 I = 51
36354
XDOT = 875
655555 Wp = 261
37321
YDOT = 6023
046995 meter/sec RA = 300
01147 deg
ZDOT = 4717
464432 TA = 137
00524
MA = 136
94119
Ha = 184
050 n
mi
Hp = 175
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16040420
06 X = 4909359
12
Y = -10688114
51 feet Y = -3202951
15 meter
Z = 10688793
74 Z = 3281744
24
XDOT = 2872
885680 XDOT = 785
324002
YDOT = 19760
652870 feet/sec YDOT = 6032
334175 meter/sec
ZDOT = 15477
245513 ZDOT = 4721
498601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19167914
11 X = 5842380
22
Y = -1487188
23 feet Y = -453294
97 meter
Z = 10777778
95 Z = 3285067
02
XDOT = -7361
291667 XDOT = -2243
721700
YDOT = 17193
641372 feet/sec YDOT = 5240
621890 meter/sec
ZDOT = 15493
177716 ZDOT = 4722
320568
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 07060
53567398
00020000 00000-0 20000-3 0 9031
2 25544 51
6355 300
2997 0020939 265
9259 93
9513 15
78777089 33777
Satellite: ISS
Catalog Number: 25544
Epoch time: 07060
53567398 = yrday
fracday
Element set: 903
Inclination: 51
6355 deg
RA of node: 300
2997 deg
Eccentricity:
0020939
Arg of perigee: 265
9259 deg
Mean anomaly: 93
9513 deg
Mean motion: 15
78777089 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3377
Checksum: 340
Coasting Arc #5 (Orbit 3389)
---------------------------------------
Vector Time (GMT): 2007/061/08:20:55
947
Vector Time (MET): N/A
Weight (LBS) : 478907
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1896617
76 A = 6712281
11 meter
Y = -4523855
31 meter E =
0015629
Z = -4569948
90 I = 51
33473
XDOT = 5015
146389 Wp = 259
15699
YDOT = -5076
738928 meter/sec RA = 295
45170 deg
ZDOT = 2932
785126 TA = 40
03326
MA = 39
91817
Ha = 187
089 n
mi
Hp = 175
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6222499
21 X = -1823691
06
Y = -14842044
98 feet Y = -4544656
86 meter
Z = -14993270
68 Z = -4578985
01
XDOT = 16453
892353 XDOT = 5057
295948
YDOT = -16655
967610 feet/sec YDOT = -5020
420918 meter/sec
ZDOT = 9621
998444 ZDOT = 2957
250672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12874024
24 X = 3924002
59
Y = -9603567
27 feet Y = -2927167
30 meter
Z = -15027806
12 Z = -4580475
31
XDOT = 19480
296259 XDOT = 5937
594300
YDOT = 10856
591538 feet/sec YDOT = 3309
089101 meter/sec
ZDOT = 9713
243356 ZDOT = 2960
596575
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 07061
35852438
00020000 00000-0 20000-3 0 9045
2 25544 51
6336 296
0427 0025244 271
5988 88
2285 15
77766744 33905
Satellite: ISS
Catalog Number: 25544
Epoch time: 07061
35852438 = yrday
fracday
Element set: 904
Inclination: 51
6336 deg
RA of node: 296
0427 deg
Eccentricity:
0025244
Arg of perigee: 271
5988 deg
Mean anomaly: 88
2285 deg
Mean motion: 15
77766744 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3390
Checksum: 322
Coasting Arc #6 (Orbit 3405)
---------------------------------------
Vector Time (GMT): 2007/062/08:20:55
947
Vector Time (MET): N/A
Weight (LBS) : 478907
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4379355
91 A = 6715750
11 meter
Y = 3626969
75 meter E =
0019988
Z = -3559196
19 I = 51
33609
XDOT = -1487
528120 Wp = 279
28683
YDOT = -6148
980246 meter/sec RA = 290
31455 deg
ZDOT = -4411
564813 TA = 303
51721
MA = 303
70802
Ha = 187
054 n
mi
Hp = 175
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14367965
59 X = -4402298
24
Y = 11899507
07 feet Y = 3577868
80 meter
Z = -11677152
84 Z = -3580526
55
XDOT = -4880
341602 XDOT = -1397
228758
YDOT = -20173
819704 feet/sec YDOT = -6165
110066 meter/sec
ZDOT = -14473
637838 ZDOT = -4418
571233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15240083
18 X = -4645177
35
Y = -10672863
98 feet Y = -3253088
94 meter
Z = -11756804
04 Z = -3583473
87
XDOT = 17424
968671 XDOT = 5311
130451
YDOT = -8821
269942 feet/sec YDOT = -2688
723078 meter/sec
ZDOT = -14500
769806 ZDOT = -4419
834637
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 07062
37192274
00020000 00000-0 20000-3 0 9054
2 25544 51
6339 290
8090 0025228 275
6971 84
1318 15
77807114 34062
Satellite: ISS
Catalog Number: 25544
Epoch time: 07062
37192274 = yrday
fracday
Element set: 905
Inclination: 51
6339 deg
RA of node: 290
8090 deg
Eccentricity:
0025228
Arg of perigee: 275
6971 deg
Mean anomaly: 84
1318 deg
Mean motion: 15
77807114 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3406
Checksum: 298
Coasting Arc #7 (Orbit 3421)
---------------------------------------
Vector Time (GMT): 2007/063/08:20:55
947
Vector Time (MET): N/A
Weight (LBS) : 478907
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 753964
82 A = 6717723
38 meter
Y = 6032476
82 meter E =
0011804
Z = 2870819
04 I = 51
33359
XDOT = -4983
038524 Wp = 280
14910
YDOT = 3011
126318 meter/sec RA = 285
07738 deg
ZDOT = -5034
104419 TA = 226
69746
MA = 226
79596
Ha = 187
197 n
mi
Hp = 175
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2473637
87 X = 672507
15
Y = 19791590
60 feet Y = 6040452
87 meter
Z = 9418697
64 Z = 2874283
33
XDOT = -16348
551588 XDOT = -4991
884780
YDOT = 9879
023353 feet/sec YDOT = 2955
353287 meter/sec
ZDOT = -16516
090613 ZDOT = -5058
333246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18327189
04 X = -5586127
22
Y = 7853636
24 feet Y = 2393788
33 meter
Z = 9432515
46 Z = 2875030
71
XDOT = -13454
478377 XDOT = -4100
925009
YDOT = -11512
962866 feet/sec YDOT = -3509
151082 meter/sec
ZDOT = -16606
706989 ZDOT = -5061
724290
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 07063
38530126
00020000 00000-0 20000-3 0 9069
2 25544 51
6334 285
5746 0025259 279
5084 80
3227 15
77818991 34228
Satellite: ISS
Catalog Number: 25544
Epoch time: 07063
38530126 = yrday
fracday
Element set: 906
Inclination: 51
6334 deg
RA of node: 285
5746 deg
Eccentricity:
0025259
Arg of perigee: 279
5084 deg
Mean anomaly: 80
3227 deg
Mean motion: 15
77818991 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3422
Checksum: 309
Coasting Arc #8 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2007/064/08:20:55
947
Vector Time (MET): N/A
Weight (LBS) : 478907
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4292533
40 A = 6710355
29 meter
Y = -1449348
73 meter E =
0020022
Z = 4966344
81 I = 51
30304
XDOT = 276
512498 Wp = 277
17103
YDOT = 7439
274295 meter/sec RA = 279
92828 deg
ZDOT = 1941
188585 TA = 154
01695
MA = 153
91630
Ha = 187
240 n
mi
Hp = 174
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14083114
83 X = 4284295
99
Y = -4755081
14 feet Y = -1401392
82 meter
Z = 16293782
20 Z = 4987177
72
XDOT = 907
193235 XDOT = 183
875130
YDOT = 24407
067897 feet/sec YDOT = 7441
848632 meter/sec
ZDOT = 6368
728955 ZDOT = 1942
306155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8681719
81 X = 2646188
20
Y = 11959206
12 feet Y = 3645166
03 meter
Z = 16371847
43 Z = 4990139
10
XDOT = -22184
599024 XDOT = -6761
865783
YDOT = 7419
951622 feet/sec YDOT = 2261
601255 meter/sec
ZDOT = 6373
925921 ZDOT = 1942
772621
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 07064
39865850
00020000 00000-0 20000-3 0 9077
2 25544 51
6334 280
3390 0025301 283
4570 76
3776 15
77867583 34380
Satellite: ISS
Catalog Number: 25544
Epoch time: 07064
39865850 = yrday
fracday
Element set: 907
Inclination: 51
6334 deg
RA of node: 280
3390 deg
Eccentricity:
0025301
Arg of perigee: 283
4570 deg
Mean anomaly: 76
3776 deg
Mean motion: 15
77867583 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3438
Checksum: 319
Coasting Arc #9 (Orbit 3452)
---------------------------------------
Vector Time (GMT): 2007/065/08:20:55
947
Vector Time (MET): N/A
Weight (LBS) : 478907
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 220098
90 A = 6721094
36 meter
Y = -6693018
77 meter E =
0023140
Z = -414027
53 I = 51
33606
XDOT = 4838
770329 Wp = 314
00563
YDOT = -224
112478 meter/sec RA = 274
71896 deg
ZDOT = 6004
024672 TA = 41
46157
MA = 41
28622
Ha = 187
412 n
mi
Hp = 174
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 722109
26 X = 296936
08
Y = -21958722
99 feet Y = -6690127
92 meter
Z = -1358358
04 Z = -412771
06
XDOT = 15875
230738 XDOT = 4811
750634
YDOT = -735
277158 feet/sec YDOT = -170
153175 meter/sec
ZDOT = 19698
243675 ZDOT = 6027
465528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21088821
75 X = 6427872
87
Y = -6162703
01 feet Y = -1878391
88 meter
Z = -1354541
29 Z = -412864
19
XDOT = 5171
539612 XDOT = 1576
285274
YDOT = 13209
824799 feet/sec YDOT = 4026
354599 meter/sec
ZDOT = 19786
269493 ZDOT = 6030
854941
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 07065
34866335
00020000 00000-0 20000-3 0 9083
2 25544 51
6337 275
4308 0025381 287
3970 72
4420 15
77878022 34532
Satellite: ISS
Catalog Number: 25544
Epoch time: 07065
34866335 = yrday
fracday
Element set: 908
Inclination: 51
6337 deg
RA of node: 275
4308 deg
Eccentricity:
0025381
Arg of perigee: 287
3970 deg
Mean anomaly: 72
4420 deg
Mean motion: 15
77878022 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3453
Checksum: 307
Coasting Arc #10 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2007/066/08:20:55
947
Vector Time (MET): N/A
Weight (LBS) : 478907
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4141800
54 A = 6709218
10 meter
Y = -1078983
99 meter E =
0011719
Z = -5157743
90 I = 51
29599
XDOT = 741
013761 Wp = 308
21053
YDOT = -7614
277826 meter/sec RA = 269
52557 deg
ZDOT = 1003
457953 TA = 331
35050
MA = 331
41484
Ha = 187
424 n
mi
Hp = 174
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13588584
46 X = -4104372
16
Y = -3539973
73 feet Y = -1125091
07 meter
Z = -16921731
95 Z = -5177773
61
XDOT = 2431
147511 XDOT = 821
228052
YDOT = -24981
226464 feet/sec YDOT = -7605
542815 meter/sec
ZDOT = 3292
184886 ZDOT = 1007
253223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1089672
69 X = -332132
24
Y = -13908147
62 feet Y = -4239203
40 meter
Z = -16997120
26 Z = -5180722
26
XDOT = 23373
224791 XDOT = 7124
158916
YDOT = -5848
312946 feet/sec YDOT = -1782
565786 meter/sec
ZDOT = 3305
411272 ZDOT = 1007
489356
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 07066
36198151
00020000 00000-0 20000-3 0 9091
2 25544 51
6341 270
1959 0025373 291
3223 68
5234 15
77936992 34695
Satellite: ISS
Catalog Number: 25544
Epoch time: 07066
36198151 = yrday
fracday
Element set: 909
Inclination: 51
6341 deg
RA of node: 270
1959 deg
Eccentricity:
0025373
Arg of perigee: 291
3223 deg
Mean anomaly: 68
5234 deg
Mean motion: 15
77936992 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3469
Checksum: 318
Coasting Arc #11 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2007/067/08:20:55
947
Vector Time (MET): N/A
Weight (LBS) : 478907
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1087417
98 A = 6719048
15 meter
Y = 6279833
10 meter E =
0019857
Z = -2122856
24 I = 51
33089
XDOT = -4684
138848 Wp = 287
48425
YDOT = -2685
065371 meter/sec RA = 264
36439 deg
ZDOT = -5495
446862 TA = 276
39133
MA = 276
61743
Ha = 187
804 n
mi
Hp = 174
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3567644
28 X = -1147246
75
Y = 20603126
96 feet Y = 6267338
32 meter
Z = -6964751
44 Z = -2128284
62
XDOT = -15367
909606 XDOT = -4627
070161
YDOT = -8809
269590 feet/sec YDOT = -2737
127304 meter/sec
ZDOT = -18029
681307 ZDOT = -5518
063506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20556832
50 X = -6265722
54
Y = 3789589
18 feet Y = 1155066
78 meter
Z = -6984292
41 Z = -2128812
33
XDOT = 3282
702292 XDOT = 1000
567659
YDOT = -15869
150078 feet/sec YDOT = -4836
916944 meter/sec
ZDOT = -18115
006798 ZDOT = -5521
454072
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 07067
37527948
00020000 00000-0 20000-3 0 9105
2 25544 51
6344 264
9610 0025492 294
9798 64
8720 15
77927968 34851
Satellite: ISS
Catalog Number: 25544
Epoch time: 07067
37527948 = yrday
fracday
Element set: 910
Inclination: 51
6344 deg
RA of node: 264
9610 deg
Eccentricity:
0025492
Arg of perigee: 294
9798 deg
Mean anomaly: 64
8720 deg
Mean motion: 15
77927968 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3485
Checksum: 348
Coasting Arc #12 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2007/068/08:20:55
947
Vector Time (MET): N/A
Weight (LBS) : 478907
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4015628
24 A = 6713396
28 meter
Y = 3509251
62 meter E =
0019381
Z = 4098805
76 I = 51
31680
XDOT = -1816
059502 Wp = 321
28226
YDOT = 6464
423308 meter/sec RA = 259
12988 deg
ZDOT = -3750
056085 TA = 167
39729
MA = 167
34877
Ha = 187
965 n
mi
Hp = 174
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13174633
34 X = 3956177
64
Y = 11513292
73 feet Y = 3553824
41 meter
Z = 13447525
48 Z = 4118169
05
XDOT = -5958
200467 XDOT = -1869
993599
YDOT = 21208
737886 feet/sec YDOT = 6443
813376 meter/sec
ZDOT = -12303
333613 ZDOT = -3759
009787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6011224
09 X = -1832221
10
Y = 16371239
48 feet Y = 4989953
79 meter
Z = 13520743
97 Z = 4121122
76
XDOT = -20711
455580 XDOT = -6312
851661
YDOT = 2597
718244 feet/sec YDOT = 791
784521 meter/sec
ZDOT = -12336
093316 ZDOT = -3760
041243
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 07068
38855554
00020000 00000-0 20000-3 0 9115
2 25544 51
6343 259
7254 0025556 299
4221 60
4394 15
78012249 35014
Satellite: ISS
Catalog Number: 25544
Epoch time: 07068
38855554 = yrday
fracday
Element set: 911
Inclination: 51
6343 deg
RA of node: 259
7254 deg
Eccentricity:
0025556
Arg of perigee: 299
4221 deg
Mean anomaly: 60
4394 deg
Mean motion: 15
78012249 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3501
Checksum: 301
Coasting Arc #13 (Orbit 3516)
---------------------------------------
Vector Time (GMT): 2007/069/08:20:55
947
Vector Time (MET): N/A
Weight (LBS) : 478907
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2143928
47 A = 6713003
12 meter
Y = -4766083
09 meter E =
0016146
Z = 4216367
91 I = 51
32223
XDOT = 4462
422706 Wp = 313
43344
YDOT = 5158
145554 meter/sec RA = 253
99030 deg
ZDOT = 3581
111442 TA = 100
11149
MA = 99
92930
Ha = 188
180 n
mi
Hp = 174
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7033886
06 X = 2176581
87
Y = -15636755
56 feet Y = -4741925
79 meter
Z = 13833228
05 Z = 4226862
53
XDOT = 14640
494443 XDOT = 4387
015596
YDOT = 16923
049719 feet/sec YDOT = 5207
625345 meter/sec
ZDOT = 11749
053289 ZDOT = 3602
606495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17105683
03 X = 5213812
19
Y = 552140
36 feet Y = 168292
38 meter
Z = 13872008
68 Z = 4228188
24
XDOT = -10143
638352 XDOT = -3091
780970
YDOT = 18629
785822 feet/sec YDOT = 5678
358719 meter/sec
ZDOT = 11830
508569 ZDOT = 3605
939012
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 07069
40181228
00020000 00000-0 20000-3 0 9120
2 25544 51
6345 254
4891 0025539 303
4682 56
4042 15
78001783 35176
Satellite: ISS
Catalog Number: 25544
Epoch time: 07069
40181228 = yrday
fracday
Element set: 912
Inclination: 51
6345 deg
RA of node: 254
4891 deg
Eccentricity:
0025539
Arg of perigee: 303
4682 deg
Mean anomaly: 56
4042 deg
Mean motion: 15
78001783 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3517
Checksum: 288
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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