Date:
October 20th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5112 86 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 3038)
---------------------------------------
Vector Time (GMT): 2007/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1417947
93 A = 6715415
68 meter
Y = 4057666
64 meter E =
0016813
Z = -5174294
63 I = 51
60781
XDOT = -7516
131739 Wp = 100
20250
YDOT = -1151
736299 meter/sec RA = 181
78861 deg
ZDOT = 1156
762083 TA = 180
85906
MA = 180
86195
Ha = 188
198 n
mi
Hp = 180
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4652060
14 X = -1438079
84
Y = 13312554
60 feet Y = 4041697
83 meter
Z = -16976032
26 Z = -5181231
99
XDOT = -24659
224864 XDOT = -7508
313652
YDOT = -3778
662399 feet/sec YDOT = -1235
742235 meter/sec
ZDOT = 3795
151191 ZDOT = 1120
267183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1945985
39 X = -593136
35
Y = -13935589
70 feet Y = -4247567
74 meter
Z = -17001880
05 Z = -5182173
04
XDOT = 22710
790532 XDOT = 6922
248954
YDOT = -7631
149366 feet/sec YDOT = -2325
974327 meter/sec
ZDOT = 3656
287493 ZDOT = 1114
436428
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 07292
51400141
00020000 00000-0 20000-3 0 9005
2 25544 51
6373 182
7218 0002420 107
1868 252
9561 15
75791420 30391
Satellite: ISS
Catalog Number: 25544
Epoch time: 07292
51400141 = yrday
fracday
Element set: 900
Inclination: 51
6373 deg
RA of node: 182
7218 deg
Eccentricity:
0002420
Arg of perigee: 107
1868 deg
Mean anomaly: 252
9561 deg
Mean motion: 15
75791420 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3039
Checksum: 268
Coasting Arc #2 (Orbit 3054)
---------------------------------------
Vector Time (GMT): 2007/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6461519
40 A = 6726028
04 meter
Y = 905782
04 meter E =
0010228
Z = -1619470
79 I = 51
67259
XDOT = -2090
001420 Wp = 137
00051
YDOT = 4676
528271 meter/sec RA = 176
66411 deg
ZDOT = -5751
826147 TA = 60
88273
MA = 60
78038
Ha = 188
205 n
mi
Hp = 180
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21199210
64 X = 6458777
77
Y = 2971725
86 feet Y = 978023
07 meter
Z = -5313224
36 Z = -1588087
00
XDOT = -6856
960039 XDOT = -2114
198045
YDOT = 15342
940523 feet/sec YDOT = 4653
021351 meter/sec
ZDOT = -18870
820692 ZDOT = -5762
038317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20160835
73 X = -6145022
73
Y = 7282383
58 feet Y = 2219670
52 meter
Z = -5193807
04 Z = -1583072
39
XDOT = -661
818679 XDOT = -201
722333
YDOT = -15249
805803 feet/sec YDOT = -4648
140809 meter/sec
ZDOT = -18909
038043 ZDOT = -5763
474795
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 07293
52867605
00020000 00000-0 20000-3 0 9010
2 25544 51
6376 177
4966 0002354 115
2480 244
8928 15
75778097 30551
Satellite: ISS
Catalog Number: 25544
Epoch time: 07293
52867605 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 177
4966 deg
Eccentricity:
0002354
Arg of perigee: 115
2480 deg
Mean anomaly: 244
8928 deg
Mean motion: 15
75778097 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3055
Checksum: 323
Coasting Arc #3 (Orbit 3070)
---------------------------------------
Vector Time (GMT): 2007/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2205148
36 A = 6716748
94 meter
Y = -4156894
28 meter E =
0008580
Z = 4787011
98 I = 51
67152
XDOT = 7226
728598 Wp = 71
78259
YDOT = 928
928212 meter/sec RA = 171
48211 deg
ZDOT = -2516
054726 TA = 42
83847
MA = 42
77164
Ha = 187
896 n
mi
Hp = 180
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7234738
71 X = 2228212
74
Y = -13638104
60 feet Y = -4132105
96 meter
Z = 15705419
90 Z = 4797780
89
XDOT = 23709
739495 XDOT = 7228
026774
YDOT = 3047
664738 feet/sec YDOT = 1009
748764 meter/sec
ZDOT = -8254
772723 ZDOT = -2480
943698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 311976
10 X = 95090
32
Y = 15393872
71 feet Y = 4692052
40 meter
Z = 15745821
96 Z = 4799326
53
XDOT = -21160
807015 XDOT = -6449
813978
YDOT = 8756
791032 feet/sec YDOT = 2669
069907 meter/sec
ZDOT = -8121
172271 ZDOT = -2475
333308
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 07294
54332811
00020000 00000-0 20000-3 0 9020
2 25544 51
6377 172
2712 0002171 113
8420 246
2972 15
75888769 30710
Satellite: ISS
Catalog Number: 25544
Epoch time: 07294
54332811 = yrday
fracday
Element set: 902
Inclination: 51
6377 deg
RA of node: 172
2712 deg
Eccentricity:
0002171
Arg of perigee: 113
8420 deg
Mean anomaly: 246
2972 deg
Mean motion: 15
75888769 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3071
Checksum: 292
Coasting Arc #4 (Orbit 3086)
---------------------------------------
Vector Time (GMT): 2007/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6084640
11 A = 6723691
21 meter
Y = -753949
56 meter E =
0015453
Z = 2744460
36 I = 51
72254
XDOT = 2946
669687 Wp = 84
10990
YDOT = -4905
451067 meter/sec RA = 166
37876 deg
ZDOT = 5162
159443 TA = 307
25226
MA = 307
39312
Ha = 188
038 n
mi
Hp = 180
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19962730
03 X = -6089089
41
Y = -2473587
81 feet Y = -822016
19 meter
Z = 9004135
04 Z = 2714889
94
XDOT = 9667
551467 XDOT = 2976
226939
YDOT = -16093
999563 feet/sec YDOT = -4872
334210 meter/sec
ZDOT = 16936
218646 ZDOT = 5176
546638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18595930
86 X = 5668039
73
Y = -7799631
00 feet Y = -2377327
53 meter
Z = 8891613
26 Z = 2710163
72
XDOT = -876
544754 XDOT = -267
170841
YDOT = 17366
929941 feet/sec YDOT = 5293
440246 meter/sec
ZDOT = 16990
281433 ZDOT = 5178
637781
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 07295
55796360
00020000 00000-0 20000-3 0 9036
2 25544 51
6374 167
0454 0002180 115
9640 244
1749 15
75861882 30872
Satellite: ISS
Catalog Number: 25544
Epoch time: 07295
55796360 = yrday
fracday
Element set: 903
Inclination: 51
6374 deg
RA of node: 167
0454 deg
Eccentricity:
0002180
Arg of perigee: 115
9640 deg
Mean anomaly: 244
1749 deg
Mean motion: 15
75861882 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3087
Checksum: 310
Coasting Arc #5 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2007/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2906878
41 A = 6719242
40 meter
Y = 4436389
69 meter E =
0009941
Z = -4135607
16 I = 51
73570
XDOT = -6658
867425 Wp = 112
92893
YDOT = -862
883592 meter/sec RA = 161
18639 deg
ZDOT = 3758
144703 TA = 195
52137
MA = 195
55187
Ha = 187
820 n
mi
Hp = 180
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9537002
66 X = -2936180
29
Y = 14555084
29 feet Y = 4403719
23 meter
Z = -13568264
94 Z = -4149800
52
XDOT = -21846
677905 XDOT = -6666
980396
YDOT = -2830
982914 feet/sec YDOT = -937
391941 meter/sec
ZDOT = 12329
871073 ZDOT = 3725
775603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 677496
24 X = 206500
85
Y = -17346303
10 feet Y = -5287153
19 meter
Z = -13621654
80 Z = -4151880
38
XDOT = 19011
565308 XDOT = 5794
725106
YDOT = -8834
545847 feet/sec YDOT = -2692
769574 meter/sec
ZDOT = 12206
688808 ZDOT = 3720
598749
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 07296
50916362
00020000 00000-0 20000-3 0 9049
2 25544 51
6370 162
1462 0002062 122
7608 237
3755 15
75910738 31026
Satellite: ISS
Catalog Number: 25544
Epoch time: 07296
50916362 = yrday
fracday
Element set: 904
Inclination: 51
6370 deg
RA of node: 162
1462 deg
Eccentricity:
0002062
Arg of perigee: 122
7608 deg
Mean anomaly: 237
3755 deg
Mean motion: 15
75910738 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3102
Checksum: 277
Coasting Arc #6 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2007/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5499668
29 A = 6720592
93 meter
Y = 820734
97 meter E =
0007413
Z = -3780873
39 I = 51
76610
XDOT = -3686
174331 Wp = 89
17567
YDOT = 5274
120601 meter/sec RA = 156
09544 deg
ZDOT = -4224
020887 TA = 136
53560
MA = 136
47714
Ha = 187
785 n
mi
Hp = 180
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18043531
13 X = 5508449
26
Y = 2692700
03 feet Y = 882284
24 meter
Z = -12404440
24 Z = -3754133
99
XDOT = -12093
747806 XDOT = -3724
356286
YDOT = 17303
545278 feet/sec YDOT = 5232
685967 meter/sec
ZDOT = -13858
336244 ZDOT = -4242
021875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16816705
02 X = -5125731
69
Y = 7247942
27 feet Y = 2209172
80 meter
Z = -12302664
42 Z = -3749852
11
XDOT = 1632
577676 XDOT = 497
609676
YDOT = -19811
046804 feet/sec YDOT = -6038
407066 meter/sec
ZDOT = -13926
100918 ZDOT = -4244
675560
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 07297
52375837
00020000 00000-0 20000-3 0 9059
2 25544 51
6360 156
9205 0001982 128
8538 231
2803 15
75920614 31188
Satellite: ISS
Catalog Number: 25544
Epoch time: 07297
52375837 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 156
9205 deg
Eccentricity:
0001982
Arg of perigee: 128
8538 deg
Mean anomaly: 231
2803 deg
Mean motion: 15
75920614 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3118
Checksum: 299
Coasting Arc #7 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2007/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3467311
38 A = 6722009
27 meter
Y = -4792411
64 meter E =
0014484
Z = 3178643
57 I = 51
79791
XDOT = 5911
754761 Wp = 97
69522
YDOT = 1061
484234 meter/sec RA = 150
90357 deg
ZDOT = -4831
500654 TA = 45
26577
MA = 45
14796
Ha = 187
548 n
mi
Hp = 180
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11375693
51 X = 3505201
36
Y = -15723135
31 feet Y = -4753426
22 meter
Z = 10428620
63 Z = 3195580
55
XDOT = 19395
520869 XDOT = 5922
917037
YDOT = 3482
559822 feet/sec YDOT = 1127
655040 meter/sec
ZDOT = -15851
380097 ZDOT = -4802
753334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1009542
33 X = -307708
50
Y = 19346050
00 feet Y = 5896676
04 meter
Z = 10492411
00 Z = 3198086
87
XDOT = -16859
475361 XDOT = -5138
768090
YDOT = 7687
523086 feet/sec YDOT = 2343
157037 meter/sec
ZDOT = -15741
934621 ZDOT = -4798
141672
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 07298
53833183
00020000 00000-0 20000-3 0 9065
2 25544 51
6360 151
6942 0001851 128
0625 232
0706 15
76008661 31341
Satellite: ISS
Catalog Number: 25544
Epoch time: 07298
53833183 = yrday
fracday
Element set: 906
Inclination: 51
6360 deg
RA of node: 151
6942 deg
Eccentricity:
0001851
Arg of perigee: 128
0625 deg
Mean anomaly: 232
0706 deg
Mean motion: 15
76008661 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3134
Checksum: 278
Coasting Arc #8 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2007/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4788770
75 A = 6717566
89 meter
Y = -1098855
57 meter E =
0010434
Z = 4575521
77 I = 51
80534
XDOT = 4199
590580 Wp = 117
74189
YDOT = -5717
851429 meter/sec RA = 145
81097 deg
ZDOT = 3012
162808 TA = 302
38775
MA = 302
48867
Ha = 187
768 n
mi
Hp = 180
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15711190
12 X = -4798355
12
Y = -3605169
19 feet Y = -1152459
88 meter
Z = 15011554
37 Z = 4552233
81
XDOT = 13778
184318 XDOT = 4248
583259
YDOT = -18759
355082 feet/sec YDOT = -5670
615280 meter/sec
ZDOT = 9882
423911 ZDOT = 3032
684195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15137100
17 X = 4613788
13
Y = -5775983
03 feet Y = -1760519
63 meter
Z = 14922859
07 Z = 4548487
44
XDOT = -1411
569754 XDOT = -430
246461
YDOT = 22117
657684 feet/sec YDOT = 6741
462062 meter/sec
ZDOT = 9959
740759 ZDOT = 3035
728983
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 07299
55288817
00020000 00000-0 20000-3 0 9077
2 25544 51
6344 146
4670 0001916 131
4374 228
6955 15
75963838 31504
Satellite: ISS
Catalog Number: 25544
Epoch time: 07299
55288817 = yrday
fracday
Element set: 907
Inclination: 51
6344 deg
RA of node: 146
4670 deg
Eccentricity:
0001916
Arg of perigee: 131
4374 deg
Mean anomaly: 228
6955 deg
Mean motion: 15
75963838 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3150
Checksum: 323
Coasting Arc #9 (Orbit 3164)
---------------------------------------
Vector Time (GMT): 2007/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3800023
64 A = 6724614
86 meter
Y = 5167244
45 meter E =
0006562
Z = -2017057
23 I = 51
85197
XDOT = -5056
727440 Wp = 56
60596
YDOT = -1539
606370 meter/sec RA = 140
63129 deg
ZDOT = 5599
003446 TA = 280
96973
MA = 281
04354
Ha = 187
468 n
mi
Hp = 180
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12467269
15 X = -3847723
27
Y = 16952901
75 feet Y = 5124483
80 meter
Z = -6617641
85 Z = -2035634
10
XDOT = -16590
313124 XDOT = -5066
335402
YDOT = -5051
202000 feet/sec YDOT = -1596
207456 meter/sec
ZDOT = 18369
433878 ZDOT = 5574
413612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 557651
31 X = 169972
12
Y = -21014072
03 feet Y = -6405089
15 meter
Z = -6687650
04 Z = -2038395
73
XDOT = 15064
974555 XDOT = 4591
804244
YDOT = -5399
319814 feet/sec YDOT = -1645
712679 meter/sec
ZDOT = 18275
726772 ZDOT = 5570
441520
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 07300
50401269
00020000 00000-0 20000-3 0 9084
2 25544 51
6333 141
5663 0001852 140
5864 219
5435 15
76020778 31650
Satellite: ISS
Catalog Number: 25544
Epoch time: 07300
50401269 = yrday
fracday
Element set: 908
Inclination: 51
6333 deg
RA of node: 141
5663 deg
Eccentricity:
0001852
Arg of perigee: 140
5864 deg
Mean anomaly: 219
5435 deg
Mean motion: 15
76020778 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3165
Checksum: 276
Coasting Arc #10 (Orbit 3180)
---------------------------------------
Vector Time (GMT): 2007/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4035275
22 A = 6715059
22 meter
Y = 1669527
35 meter E =
0014696
Z = -5113894
55 I = 51
84045
XDOT = -4461
426487 Wp = 85
13589
YDOT = 6075
629928 meter/sec RA = 135
52538 deg
ZDOT = -1539
472196 TA = 170
13514
MA = 170
10626
Ha = 187
430 n
mi
Hp = 180
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13239091
91 X = 4041149
53
Y = 5477451
92 feet Y = 1714685
23 meter
Z = -16777869
26 Z = -5094276
21
XDOT = -14637
226006 XDOT = -4521
554802
YDOT = 19933
169054 feet/sec YDOT = 6025
403631 meter/sec
ZDOT = -5050
761799 ZDOT = -1561
292163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14023314
64 X = -4274306
30
Y = 3335834
11 feet Y = 1016762
24 meter
Z = -16703047
28 Z = -5091088
81
XDOT = 468
650929 XDOT = 142
844803
YDOT = -23689
570738 feet/sec YDOT = -7220
581161 meter/sec
ZDOT = -5133
011480 ZDOT = -1564
541899
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 07301
51852742
00020000 00000-0 20000-3 0 9093
2 25544 51
6323 136
3391 0001901 142
9692 217
1603 15
76056710 31813
Satellite: ISS
Catalog Number: 25544
Epoch time: 07301
51852742 = yrday
fracday
Element set: 909
Inclination: 51
6323 deg
RA of node: 136
3391 deg
Eccentricity:
0001901
Arg of perigee: 142
9692 deg
Mean anomaly: 217
1603 deg
Mean motion: 15
76056710 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3181
Checksum: 268
Coasting Arc #11 (Orbit 3196)
---------------------------------------
Vector Time (GMT): 2007/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3935612
12 A = 6725941
22 meter
Y = -5407106
70 meter E =
0014983
Z = 642669
57 I = 51
89856
XDOT = 4207
575506 Wp = 130
16154
YDOT = 2337
395303 meter/sec RA = 130
37087 deg
ZDOT = -6018
847018 TA = 42
85645
MA = 42
73977
Ha = 187
249 n
mi
Hp = 180
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12912113
26 X = 3992660
65
Y = -17739851
36 feet Y = -5362777
53 meter
Z = 2108495
98 Z = 661927
43
XDOT = 13804
381581 XDOT = 4210
364869
YDOT = 7668
619762 feet/sec YDOT = 2384
462831 meter/sec
ZDOT = -19746
873420 ZDOT = -5998
399166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 258787
71 X = 78878
49
Y = 21932774
21 feet Y = 6685109
58 meter
Z = 2181099
47 Z = 664799
12
XDOT = -14140
631222 XDOT = -4310
064396
YDOT = 2148
675237 feet/sec YDOT = 654
916212 meter/sec
ZDOT = -19668
808043 ZDOT = -5995
052691
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 07302
53302045
00020000 00000-0 20000-3 0 9104
2 25544 51
6332 131
1123 0001677 144
9559 215
1716 15
76128094 31978
Satellite: ISS
Catalog Number: 25544
Epoch time: 07302
53302045 = yrday
fracday
Element set: 910
Inclination: 51
6332 deg
RA of node: 131
1123 deg
Eccentricity:
0001677
Arg of perigee: 144
9559 deg
Mean anomaly: 215
1716 deg
Mean motion: 15
76128094 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3197
Checksum: 264
Coasting Arc #12 (Orbit 3212)
---------------------------------------
Vector Time (GMT): 2007/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3338270
41 A = 6714169
07 meter
Y = -2455702
50 meter E =
0003697
Z = 5279694
51 I = 51
87550
XDOT = 4493
720142 Wp = 115
01404
YDOT = -6261
653404 meter/sec RA = 125
24173 deg
ZDOT = -72
614822 TA = 335
66343
MA = 335
68088
Ha = 187
455 n
mi
Hp = 180
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10952330
74 X = -3336210
54
Y = -8056766
72 feet Y = -2493021
78 meter
Z = 17321832
37 Z = 5263481
72
XDOT = 14743
176318 XDOT = 4563
757664
YDOT = -20543
482295 feet/sec YDOT = -6211
010477 meter/sec
ZDOT = -238
237606 ZDOT = -50
614237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13669843
74 X = 4166568
37
Y = -378964
70 feet Y = -115508
44 meter
Z = 17259857
27 Z = 5260804
50
XDOT = 862
817083 XDOT = 262
986647
YDOT = 24274
420847 feet/sec YDOT = 7398
843474 meter/sec
ZDOT = -155
287299 ZDOT = -47
331569
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 07303
54749603
00020000 00000-0 20000-3 0 9112
2 25544 51
6326 125
8846 0001915 149
2373 210
8904 15
76082192 32138
Satellite: ISS
Catalog Number: 25544
Epoch time: 07303
54749603 = yrday
fracday
Element set: 911
Inclination: 51
6326 deg
RA of node: 125
8846 deg
Eccentricity:
0001915
Arg of perigee: 149
2373 deg
Mean anomaly: 210
8904 deg
Mean motion: 15
76082192 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3213
Checksum: 282
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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