Date:
August 9th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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
226/07:56:41
848 3
0 9
9 10
0
N/A 9
2 0
1 195
5
000/00:17:19
697 -2
3 -0
2 188
4
Coasting Arc #1 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2008/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4423533
08 A = 6726146
56 meter
Y = -2086059
96 meter E =
0020119
Z = -4637181
60 I = 51
94439
XDOT = 260
107843 Wp = 56
57030
YDOT = 7092
780442 meter/sec RA = 106
82762 deg
ZDOT = -2940
898871 TA = 184
33366
MA = 184
35111
Ha = 195
143 n
mi
Hp = 182
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14512903
80 X = 4469057
46
Y = -6844028
73 feet Y = -2036338
62 meter
Z = -15213850
38 Z = -4615581
73
XDOT = 853
372189 XDOT = 195
062199
YDOT = 23270
277040 feet/sec YDOT = 7095
325622 meter/sec
ZDOT = -9648
618343 ZDOT = -2939
792802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15311437
24 X = -4666926
07
Y = -5054828
74 feet Y = -1540711
80 meter
Z = -15130596
34 Z = -4611805
76
XDOT = 14955
775151 XDOT = 4558
520266
YDOT = -16418
945226 feet/sec YDOT = -5004
494505 meter/sec
ZDOT = -9643
675171 ZDOT = -2939
392192
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 08221
52107477
00020000 00000-0 20000-3 0 9005
2 25544 51
6415 107
5232 0010205 42
4647 317
7304 15
72888549 36774
Satellite: ISS
Catalog Number: 25544
Epoch time: 08221
52107477 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 107
5232 deg
Eccentricity:
0010205
Arg of perigee: 42
4647 deg
Mean anomaly: 317
7304 deg
Mean motion: 15
72888549 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3677
Checksum: 281
Coasting Arc #2 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2008/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1049195
42 A = 6731797
68 meter
Y = -5995211
95 meter E =
0021340
Z = 2865216
27 I = 51
97067
XDOT = 4748
319153 Wp = 76
56304
YDOT = -3283
707744 meter/sec RA = 101
67738 deg
ZDOT = -5095
723446 TA = 70
70398
MA = 70
47330
Ha = 195
245 n
mi
Hp = 182
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3442242
20 X = -995996
66
Y = -19669330
56 feet Y = -6006647
44 meter
Z = 9400315
86 Z = 2860248
04
XDOT = 15578
474911 XDOT = 4809
439171
YDOT = -10773
319371 feet/sec YDOT = -3230
267155 meter/sec
ZDOT = -16718
252775 ZDOT = -5072
508032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10681653
51 X = -3255767
99
Y = 16882087
24 feet Y = 5145660
19 meter
Z = 9380561
96 Z = 2859195
28
XDOT = -17607
840367 XDOT = -5366
869744
YDOT = -1834
521954 feet/sec YDOT = -559
162291 meter/sec
ZDOT = -16628
859913 ZDOT = -5068
476502
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 08222
53763182
00020000 00000-0 20000-3 0 9019
2 25544 51
6414 102
3112 0010270 46
7075 313
4942 15
72889287 36936
Satellite: ISS
Catalog Number: 25544
Epoch time: 08222
53763182 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 102
3112 deg
Eccentricity:
0010270
Arg of perigee: 46
7075 deg
Mean anomaly: 313
4942 deg
Mean motion: 15
72889287 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3693
Checksum: 277
Coasting Arc #3 (Orbit 3708)
---------------------------------------
Vector Time (GMT): 2008/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3756041
39 A = 6727602
35 meter
Y = 3613854
15 meter E =
0017898
Z = 4236235
50 I = 51
96140
XDOT = -2111
309283 Wp = 77
87924
YDOT = -6464
023987 meter/sec RA = 96
62101 deg
ZDOT = 3633
237257 TA = 335
32723
MA = 335
41273
Ha = 195
390 n
mi
Hp = 182
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12322970
43 X = -3816751
65
Y = 11856476
88 feet Y = 3571512
09 meter
Z = 13898410
42 Z = 4217841
64
XDOT = -6926
867727 XDOT = -2056
520107
YDOT = -21207
427778 feet/sec YDOT = -6487
327860 meter/sec
ZDOT = 11920
069742 ZDOT = 3623
113060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17144108
20 X = 5225524
18
Y = -687465
37 feet Y = -209539
45 meter
Z = 13827668
00 Z = 4214673
21
XDOT = -8833
250959 XDOT = -2692
374892
YDOT = 19281
234362 feet/sec YDOT = 5876
920234 meter/sec
ZDOT = 11880
356236 ZDOT = 3621
132581
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 08223
55417803
00020000 00000-0 20000-3 0 9029
2 25544 51
6416 97
0990 0010278 49
9043 310
3019 15
72889668 37092
Satellite: ISS
Catalog Number: 25544
Epoch time: 08223
55417803 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 97
0990 deg
Eccentricity:
0010278
Arg of perigee: 49
9043 deg
Mean anomaly: 310
3019 deg
Mean motion: 15
72889668 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3709
Checksum: 303
Coasting Arc #4 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2008/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2570041
71 A = 6730114
99 meter
Y = 5176057
22 meter E =
0014297
Z = -3454487
43 I = 51
97204
XDOT = -3726
981676 Wp = 65
44025
YDOT = 4909
040768 meter/sec RA = 91
46638 deg
ZDOT = 4603
332754 TA = 253
91526
MA = 254
07272
Ha = 195
234 n
mi
Hp = 182
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8431895
37 X = 2528752
31
Y = 16981815
04 feet Y = 5204566
39 meter
Z = -11333620
18 Z = -3442102
05
XDOT = -12227
630171 XDOT = -3803
960301
YDOT = 16105
776799 feet/sec YDOT = 4866
932644 meter/sec
ZDOT = 15102
797748 ZDOT = 4585
040762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4545230
99 X = 1385386
41
Y = -18436728
67 feet Y = -5619514
90 meter
Z = -11285289
50 Z = -3439756
24
XDOT = 18473
715195 XDOT = 5630
788391
YDOT = -4605
660271 feet/sec YDOT = -1403
805251 meter/sec
ZDOT = 15032
557244 ZDOT = 4581
923448
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 08224
50717991
00020000 00000-0 20000-3 0 9037
2 25544 51
6414 92
2128 0010096 52
4688 307
7390 15
72918554 37248
Satellite: ISS
Catalog Number: 25544
Epoch time: 08224
50717991 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 92
2128 deg
Eccentricity:
0010096
Arg of perigee: 52
4688 deg
Mean anomaly: 307
7390 deg
Mean motion: 15
72918554 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3724
Checksum: 297
Coasting Arc #5 (Orbit 3739)
---------------------------------------
Vector Time (GMT): 2008/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2684372
87 A = 6728997
02 meter
Y = -4864552
14 meter E =
0015969
Z = -3814127
96 I = 51
96720
XDOT = 3633
429828 Wp = 63
57813
YDOT = 5302
276443 meter/sec RA = 86
41323 deg
ZDOT = -4211
926538 TA = 162
35538
MA = 162
29985
Ha = 195
207 n
mi
Hp = 182
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8806997
60 X = 2757097
66
Y = -15959816
74 feet Y = -4834126
93 meter
Z = -12513543
19 Z = -3800911
29
XDOT = 11920
701534 XDOT = 3594
329393
YDOT = 17395
920090 feet/sec YDOT = 5342
689346 meter/sec
ZDOT = -13818
656622 ZDOT = -4194
370003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16995986
01 X = -5180376
53
Y = 6684325
84 feet Y = 2037382
51 meter
Z = -12462903
67 Z = -3798693
04
XDOT = 2272
776695 XDOT = 692
742337
YDOT = -19818
111122 feet/sec YDOT = -6040
560270 meter/sec
ZDOT = -13750
330359 ZDOT = -4191
100693
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 08225
52370671
00020000 00000-0 20000-3 0 9041
2 25544 51
6408 87
0005 0009999 56
2913 303
9202 15
72922409 37402
Satellite: ISS
Catalog Number: 25544
Epoch time: 08225
52370671 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 87
0005 deg
Eccentricity:
0009999
Arg of perigee: 56
2913 deg
Mean anomaly: 303
9202 deg
Mean motion: 15
72922409 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3740
Checksum: 285
Coasting Arc #6 (Orbit 3752)
---------------------------------------
Vector Time (GMT): 2008/226/08:05:21
697
Vector Time (MET): N/A
Weight (LBS) : 661158
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4193090
84 A = 6730333
58 meter
Y = 1612181
79 meter E =
0013425
Z = -5023205
15 I = 51
94960
XDOT = -515
045425 Wp = 91
76376
YDOT = 7415
450712 meter/sec RA = 82
09915 deg
ZDOT = 1954
098321 TA = 197
04987
MA = 197
09502
Ha = 195
495 n
mi
Hp = 188
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13756859
72 X = 4199152
96
Y = 5289310
33 feet Y = 1659105
71 meter
Z = -16480331
85 Z = -5002820
56
XDOT = -1689
781578 XDOT = -607
420406
YDOT = 24328
906537 feet/sec YDOT = 7409
174499 meter/sec
ZDOT = 6411
083729 ZDOT = 1951
372594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7001403
45 X = 2134027
77
Y = -13069185
85 feet Y = -3983487
85 meter
Z = -16401404
27 Z = -4999148
02
XDOT = 22961
155047 XDOT = 6998
560058
YDOT = 4284
211754 feet/sec YDOT = 1305
827743 meter/sec
ZDOT = 6401
213437 ZDOT = 1951
089856
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 08226
34963786
00020000 00000-0 20000-3 0 9058
2 25544 51
6410 82
7661 0002952 15
7003 344
4250 15
70857388 37535
Satellite: ISS
Catalog Number: 25544
Epoch time: 08226
34963786 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 82
7661 deg
Eccentricity:
0002952
Arg of perigee: 15
7003 deg
Mean anomaly: 344
4250 deg
Mean motion: 15
70857388 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3753
Checksum: 295
Coasting Arc #7 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2008/227/08:05:21
697
Vector Time (MET): N/A
Weight (LBS) : 661158
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -944746
62 A = 6740915
44 meter
Y = -6631857
48 meter E =
0009402
Z = -725836
66 I = 51
98023
XDOT = 4809
315100 Wp = 124
99117
YDOT = -34
499640 meter/sec RA = 77
03280 deg
ZDOT = -6004
301833 TA = 62
86801
MA = 62
77215
Ha = 195
512 n
mi
Hp = 188
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3099562
41 X = -866992
00
Y = -21758062
59 feet Y = -6641987
37 meter
Z = -2381353
86 Z = -730237
81
XDOT = 15778
592847 XDOT = 4838
510702
YDOT = -113
187796 feet/sec YDOT = 19
444605 meter/sec
ZDOT = -19699
152994 ZDOT = -5980
867708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21965216
63 X = -6694998
03
Y = 682409
92 feet Y = 207998
54 meter
Z = -2398957
26 Z = -731202
17
XDOT = 1678
981900 XDOT = 511
753683
YDOT = -14205
947066 feet/sec YDOT = -4329
972666 meter/sec
ZDOT = -19608
581187 ZDOT = -5976
695546
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 08227
36750027
00020000 00000-0 20000-3 0 9064
2 25544 51
6413 77
5630 0002876 19
3589 340
7681 15
70852560 37691
Satellite: ISS
Catalog Number: 25544
Epoch time: 08227
36750027 = yrday
fracday
Element set: 906
Inclination: 51
6413 deg
RA of node: 77
5630 deg
Eccentricity:
0002876
Arg of perigee: 19
3589 deg
Mean anomaly: 340
7681 deg
Mean motion: 15
70852560 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3769
Checksum: 307
Coasting Arc #8 (Orbit 3784)
---------------------------------------
Vector Time (GMT): 2008/228/08:05:21
697
Vector Time (MET): N/A
Weight (LBS) : 661158
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3817076
00 A = 6728929
53 meter
Y = 1650466
98 meter E =
0004036
Z = 5286968
37 I = 51
93238
XDOT = -2642
723480 Wp = 58
96825
YDOT = -7223
128932 meter/sec RA = 71
93903 deg
ZDOT = 348
741908 TA = 27
74426
MA = 27
72273
Ha = 195
569 n
mi
Hp = 188
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12523215
23 X = -3860930
70
Y = 5414917
91 feet Y = 1607536
73 meter
Z = 17345696
75 Z = 5268318
97
XDOT = -8670
352624 XDOT = -2563
450975
YDOT = -23697
929567 feet/sec YDOT = -7252
238171 meter/sec
ZDOT = 1144
166366 ZDOT = 336
095955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4224270
27 X = 1287557
58
Y = 13068979
69 feet Y = 3983425
01 meter
Z = 17273759
35 Z = 5265041
85
XDOT = -23445
890251 XDOT = -7146
307348
YDOT = 6139
570712 feet/sec YDOT = 1871
341153 meter/sec
ZDOT = 1094
640922 ZDOT = 333
646553
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 08228
38535227
00020000 00000-0 20000-3 0 9071
2 25544 51
6410 72
3600 0002931 20
4381 339
6897 15
70918556 37855
Satellite: ISS
Catalog Number: 25544
Epoch time: 08228
38535227 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 72
3600 deg
Eccentricity:
0002931
Arg of perigee: 20
4381 deg
Mean anomaly: 339
6897 deg
Mean motion: 15
70918556 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3785
Checksum: 298
Coasting Arc #9 (Orbit 3799)
---------------------------------------
Vector Time (GMT): 2008/229/08:05:21
697
Vector Time (MET): N/A
Weight (LBS) : 661158
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3517612
23 A = 6740258
16 meter
Y = 5588818
13 meter E =
0011893
Z = -1323175
10 I = 51
96050
XDOT = -3470
447920 Wp = 33
94225
YDOT = 3566
075908 meter/sec RA = 66
83299 deg
ZDOT = 5871
112932 TA = 311
61269
MA = 311
71452
Ha = 195
568 n
mi
Hp = 188
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11540722
53 X = 3461283
35
Y = 18336017
48 feet Y = 5627839
18 meter
Z = -4341125
67 Z = -1306223
54
XDOT = -11385
983988 XDOT = -3538
586632
YDOT = 11699
724109 feet/sec YDOT = 3526
886191 meter/sec
ZDOT = 19262
181535 ZDOT = 5854
088456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19155368
83 X = 5838556
42
Y = -10150790
10 feet Y = -3093960
82 meter
Z = -4275101
32 Z = -1303050
88
XDOT = 10060
048490 XDOT = 3066
302780
YDOT = 10948
094752 feet/sec YDOT = 3336
979280 meter/sec
ZDOT = 19196
694572 ZDOT = 5851
152506
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 08229
33958336
00020000 00000-0 20000-3 0 9088
2 25544 51
6414 67
4817 0003012 24
2857 335
8446 15
70905500 38006
Satellite: ISS
Catalog Number: 25544
Epoch time: 08229
33958336 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 67
4817 deg
Eccentricity:
0003012
Arg of perigee: 24
2857 deg
Mean anomaly: 335
8446 deg
Mean motion: 15
70905500 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3800
Checksum: 286
Coasting Arc #10 (Orbit 3815)
---------------------------------------
Vector Time (GMT): 2008/230/08:05:21
697
Vector Time (MET): N/A
Weight (LBS) : 661158
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1949904
53 A = 6731034
22 meter
Y = -4315180
12 meter E =
0013958
Z = -4796914
49 I = 51
91733
XDOT = 5070
219693 Wp = 62
50557
YDOT = 5164
215096 meter/sec RA = 61
77374 deg
ZDOT = -2584
013738 TA = 182
20139
MA = 182
20754
Ha = 195
543 n
mi
Hp = 188
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6397324
57 X = 2021314
75
Y = -14157415
10 feet Y = -4292975
86 meter
Z = -15737908
42 Z = -4787268
60
XDOT = 16634
579046 XDOT = 5024
648222
YDOT = 16942
962912 feet/sec YDOT = 5220
658424 meter/sec
ZDOT = -8477
735362 ZDOT = -2559
493729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13755978
57 X = -4192822
27
Y = -7300086
97 feet Y = -2225066
51 meter
Z = -15701009
81 Z = -4785667
79
XDOT = 17352
677482 XDOT = 5289
096096
YDOT = -14665
513508 feet/sec YDOT = -4470
048517 meter/sec
ZDOT = -8382
492720 ZDOT = -2554
983781
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 08230
35741990
00020000 00000-0 20000-3 0 9099
2 25544 51
6416 62
2783 0003099 26
4096 333
7223 15
70930080 38165
Satellite: ISS
Catalog Number: 25544
Epoch time: 08230
35741990 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 62
2783 deg
Eccentricity:
0003099
Arg of perigee: 26
4096 deg
Mean anomaly: 333
7223 deg
Mean motion: 15
70930080 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3816
Checksum: 286
Coasting Arc #11 (Orbit 3831)
---------------------------------------
Vector Time (GMT): 2008/231/08:05:21
697
Vector Time (MET): N/A
Weight (LBS) : 661158
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5034457
07 A = 6736810
39 meter
Y = -3197113
93 meter E =
0014735
Z = 3122593
15 I = 51
92137
XDOT = 701
639455 Wp = 83
76204
YDOT = -5902
570153 meter/sec RA = 56
63675 deg
ZDOT = -4891
014326 TA = 60
13270
MA = 59
98635
Ha = 195
686 n
mi
Hp = 187
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16517247
61 X = -5013501
03
Y = -10489218
94 feet Y = -3253294
92 meter
Z = 10244728
17 Z = 3098187
06
XDOT = 2301
966717 XDOT = 791
350105
YDOT = -19365
387641 feet/sec YDOT = -5894
222485 meter/sec
ZDOT = -16046
634927 ZDOT = -4887
387827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11160125
60 X = -3401606
28
Y = 16131479
67 feet Y = 4916875
00 meter
Z = 10150103
36 Z = 3093751
50
XDOT = -18074
652148 XDOT = -5509
153975
YDOT = -2372
074912 feet/sec YDOT = -723
008433 meter/sec
ZDOT = -16033
145720 ZDOT = -4886
902815
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 08231
37524910
00020000 00000-0 20000-3 0 9105
2 25544 51
6414 57
0748 0003143 31
1273 329
0074 15
70921369 38326
Satellite: ISS
Catalog Number: 25544
Epoch time: 08231
37524910 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 57
0748 deg
Eccentricity:
0003143
Arg of perigee: 31
1273 deg
Mean anomaly: 329
0074 deg
Mean motion: 15
70921369 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3832
Checksum: 263
Coasting Arc #12 (Orbit 3847)
---------------------------------------
Vector Time (GMT): 2008/232/08:05:21
697
Vector Time (MET): N/A
Weight (LBS) : 661158
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 854701
25 A = 6735324
69 meter
Y = 5620154
53 meter E =
0013844
Z = 3598677
82 I = 51
89978
XDOT = -5984
029343 Wp = 81
93778
YDOT = -1942
037810 meter/sec RA = 51
59276 deg
ZDOT = 4441
604282 TA = 320
88202
MA = 320
98202
Ha = 195
678 n
mi
Hp = 187
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2804137
97 X = 774310
70
Y = 18438827
21 feet Y = 5629262
90 meter
Z = 11806685
76 Z = 3602634
51
XDOT = -19632
642201 XDOT = -5983
444725
YDOT = -6371
515125 feet/sec YDOT = -2008
951292 meter/sec
ZDOT = 14572
192525 ZDOT = 4412
535615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18498807
00 X = 5638436
37
Y = -2296618
02 feet Y = -700009
17 meter
Z = 11822480
80 Z = 3603492
15
XDOT = -7006
703687 XDOT = -2135
643284
YDOT = 18209
388141 feet/sec YDOT = 5550
221505 meter/sec
ZDOT = 14459
660812 ZDOT = 4407
304616
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 08232
39306877
00020000 00000-0 20000-3 0 9119
2 25544 51
6418 51
8707 0003219 32
4876 327
6483 15
70921641 38482
Satellite: ISS
Catalog Number: 25544
Epoch time: 08232
39306877 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 51
8707 deg
Eccentricity:
0003219
Arg of perigee: 32
4876 deg
Mean anomaly: 327
6483 deg
Mean motion: 15
70921641 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3848
Checksum: 303
Coasting Arc #13 (Orbit 3862)
---------------------------------------
Vector Time (GMT): 2008/233/08:05:21
697
Vector Time (MET): N/A
Weight (LBS) : 661158
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5017400
73 A = 6732214
96 meter
Y = 156317
05 meter E =
0010727
Z = -4495518
66 I = 51
87040
XDOT = 2666
553014 Wp = 93
80277
YDOT = 6457
858663 meter/sec RA = 46
44857 deg
ZDOT = 3206
507347 TA = 208
19127
MA = 208
24938
Ha = 195
614 n
mi
Hp = 187
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16461288
47 X = 5037118
19
Y = 512851
22 feet Y = 212534
65 meter
Z = -14749076
97 Z = -4471096
34
XDOT = 8748
533511 XDOT = 2578
565450
YDOT = 21187
200339 feet/sec YDOT = 6487
185710 meter/sec
ZDOT = 10520
037227 ZDOT = 3219
247528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 622276
50 X = 189669
88
Y = -16541638
94 feet Y = -5041891
55 meter
Z = -14654666
81 Z = -4466742
44
XDOT = 20038
020629 XDOT = 6107
588688
YDOT = -8593
201720 feet/sec YDOT = -2619
207884 meter/sec
ZDOT = 10569
851569 ZDOT = 3221
690758
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 08233
34726565
00020000 00000-0 20000-3 0 9126
2 25544 51
6418 46
9923 0003114 32
7261 327
4093 15
70958805 38636
Satellite: ISS
Catalog Number: 25544
Epoch time: 08233
34726565 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 46
9923 deg
Eccentricity:
0003114
Arg of perigee: 32
7261 deg
Mean anomaly: 327
4093 deg
Mean motion: 15
70958805 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3863
Checksum: 294
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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