Date:
May 28th 2008
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) : 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
There are no maneuvers
Coasting Arc #1 (Orbit 2510)
---------------------------------------
Vector Time (GMT): 2008/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -349081
28 A = 6716966
92 meter
Y = -5133013
80 meter E =
0004289
Z = 4316856
63 I = 51
88658
XDOT = 5994
074916 Wp = 54
36039
YDOT = -3350
068737 meter/sec RA = 127
27410 deg
ZDOT = -3493
876828 TA = 70
85879
MA = 70
81236
Ha = 184
306 n
mi
Hp = 182
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1145279
80 X = -312627
71
Y = -16840596
45 feet Y = -5136714
15 meter
Z = 14162915
45 Z = 4315248
69
XDOT = 19665
600118 XDOT = 6048
063061
YDOT = -10991
039163 feet/sec YDOT = -3282
737256 meter/sec
ZDOT = -11462
850486 ZDOT = -3464
626856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15638079
21 X = -4766486
54
Y = -6368461
49 feet Y = -1941107
06 meter
Z = 14156224
97 Z = 4314817
37
XDOT = -1567
218172 XDOT = -477
688099
YDOT = -21418
059055 feet/sec YDOT = -6528
224400 meter/sec
ZDOT = -11350
674925 ZDOT = -3459
685717
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 08147
54139827
00020000 00000-0 20000-3 0 9008
2 25544 51
6344 127
9894 0005720 264
0314 96
0198 15
76494201 25110
Satellite: ISS
Catalog Number: 25544
Epoch time: 08147
54139827 = yrday
fracday
Element set: 900
Inclination: 51
6344 deg
RA of node: 127
9894 deg
Eccentricity:
0005720
Arg of perigee: 264
0314 deg
Mean anomaly: 96
0198 deg
Mean motion: 15
76494201 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2511
Checksum: 290
Coasting Arc #2 (Orbit 2526)
---------------------------------------
Vector Time (GMT): 2008/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5010029
38 A = 6719085
13 meter
Y = 2520979
94 meter E =
0006198
Z = 3696187
85 I = 51
91113
XDOT = -3
177535 Wp = 103
68919
YDOT = -6370
559180 meter/sec RA = 122
18878 deg
ZDOT = 4333
262994 TA = 300
67043
MA = 300
73150
Ha = 184
194 n
mi
Hp = 181
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16437104
26 X = -5055802
48
Y = 8270931
57 feet Y = 2464698
59 meter
Z = 12126600
57 Z = 3671738
16
XDOT = -10
424985 XDOT = 47
009031
YDOT = -20900
784711 feet/sec YDOT = -6370
314583 meter/sec
ZDOT = 14216
742105 ZDOT = 4333
368758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 412138
15 X = 125619
71
Y = 18457600
85 feet Y = 5625876
74 meter
Z = 12032799
34 Z = 3667597
24
XDOT = -17583
525929 XDOT = -5359
458703
YDOT = -8891
436052 feet/sec YDOT = -2710
109709 meter/sec
ZDOT = 14216
523022 ZDOT = 4333
196217
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 08148
55561753
00020000 00000-0 20000-3 0 9018
2 25544 51
6348 122
7614 0005811 266
9112 93
1387 15
76543799 25277
Satellite: ISS
Catalog Number: 25544
Epoch time: 08148
55561753 = yrday
fracday
Element set: 901
Inclination: 51
6348 deg
RA of node: 122
7614 deg
Eccentricity:
0005811
Arg of perigee: 266
9112 deg
Mean anomaly: 93
1387 deg
Mean motion: 15
76543799 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2527
Checksum: 307
Coasting Arc #3 (Orbit 2541)
---------------------------------------
Vector Time (GMT): 2008/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -269479
41 A = 6720750
26 meter
Y = 5937264
81 meter E =
0001697
Z = -3135217
18 I = 51
93092
XDOT = -5481
080157 Wp = 315
32968
YDOT = 2330
562033 meter/sec RA = 117
00253 deg
ZDOT = 4884
169119 TA = 8
32485
MA = 8
32203
Ha = 184
215 n
mi
Hp = 181
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -884118
80 X = -320620
40
Y = 19479215
25 feet Y = 5933965
70 meter
Z = -10286145
60 Z = -3136649
96
XDOT = -17982
546448 XDOT = -5530
460052
YDOT = 7646
200895 feet/sec YDOT = 2268
992880 meter/sec
ZDOT = 16024
176901 ZDOT = 4857
422155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17405953
02 X = 5305334
48
Y = 8783667
73 feet Y = 2677261
92 meter
Z = -10291076
96 Z = -3136720
26
XDOT = 154
594045 XDOT = 47
120265
YDOT = 18349
094153 feet/sec YDOT = 5592
803898 meter/sec
ZDOT = 15921
513351 ZDOT = 4852
877269
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 08149
50643881
00020000 00000-0 20000-3 0 9028
2 25544 51
6346 117
8594 0005644 272
4513 87
6005 15
76509513 25426
Satellite: ISS
Catalog Number: 25544
Epoch time: 08149
50643881 = yrday
fracday
Element set: 902
Inclination: 51
6346 deg
RA of node: 117
8594 deg
Eccentricity:
0005644
Arg of perigee: 272
4513 deg
Mean anomaly: 87
6005 deg
Mean motion: 15
76509513 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2542
Checksum: 296
Coasting Arc #4 (Orbit 2557)
---------------------------------------
Vector Time (GMT): 2008/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4563784
80 A = 6715366
50 meter
Y = -1450384
66 meter E =
0006442
Z = -4713882
06 I = 51
92567
XDOT = -562
848006 Wp = 48
60323
YDOT = 7169
898454 meter/sec RA = 111
91358 deg
ZDOT = -2749
225954 TA = 194
41384
MA = 194
43222
Ha = 184
196 n
mi
Hp = 182
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14973047
24 X = 4602563
46
Y = -4758479
86 feet Y = -1399132
55 meter
Z = -15465492
33 Z = -4691616
90
XDOT = -1846
614192 XDOT = -629
625726
YDOT = 23523
288890 feet/sec YDOT = 7163
231248 meter/sec
ZDOT = -9019
770189 ZDOT = -2752
121834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1604555
37 X = 489068
48
Y = -15713000
41 feet Y = -4789322
52 meter
Z = -15379978
79 Z = -4687817
53
XDOT = 19736
554880 XDOT = 6015
701927
YDOT = 10859
942188 feet/sec YDOT = 3310
110379 meter/sec
ZDOT = -9030
215941 ZDOT = -2752
409819
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 08150
52063421
00020000 00000-0 20000-3 0 9039
2 25544 51
6351 112
6305 0005706 276
4036 83
6479 15
76544890 25583
Satellite: ISS
Catalog Number: 25544
Epoch time: 08150
52063421 = yrday
fracday
Element set: 903
Inclination: 51
6351 deg
RA of node: 112
6305 deg
Eccentricity:
0005706
Arg of perigee: 276
4036 deg
Mean anomaly: 83
6479 deg
Mean motion: 15
76544890 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2558
Checksum: 284
Coasting Arc #5 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2008/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 652216
13 A = 6723774
58 meter
Y = -6494615
44 meter E =
0008721
Z = 1593414
85 I = 51
96427
XDOT = 5003
952010 Wp = 127
68805
YDOT = -921
040745 meter/sec RA = 106
74403 deg
ZDOT = -5786
141121 TA = 34
78844
MA = 34
73145
Ha = 184
286 n
mi
Hp = 181
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2139816
70 X = 717050
83
Y = -21307793
45 feet Y = -6486959
64 meter
Z = 5227739
01 Z = 1596740
21
XDOT = 16417
165388 XDOT = 5041
987782
YDOT = -3021
787221 feet/sec YDOT = -864
870447 meter/sec
ZDOT = -18983
402627 ZDOT = -5761
739248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18899619
87 X = -5760604
14
Y = -10063688
70 feet Y = -3067412
32 meter
Z = 5239911
36 Z = 1597124
98
XDOT = 2763
499763 XDOT = 842
314728
YDOT = -15052
737274 feet/sec YDOT = -4588
074321 meter/sec
ZDOT = -18889
613214 ZDOT = -5757
554107
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 08151
53481646
00020000 00000-0 20000-3 0 9045
2 25544 51
6353 107
4020 0005766 280
9249 79
1266 15
76566433 25742
Satellite: ISS
Catalog Number: 25544
Epoch time: 08151
53481646 = yrday
fracday
Element set: 904
Inclination: 51
6353 deg
RA of node: 107
4020 deg
Eccentricity:
0005766
Arg of perigee: 280
9249 deg
Mean anomaly: 79
1266 deg
Mean motion: 15
76566433 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2574
Checksum: 299
Coasting Arc #6 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2008/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4204878
84 A = 6712915
12 meter
Y = 96802
83 meter E =
0002871
Z = 5234374
53 I = 51
93589
XDOT = 884
820165 Wp = 265
64528
YDOT = -7604
997938 meter/sec RA = 101
63340 deg
ZDOT = 851
622224 TA = 176
28407
MA = 176
28194
Ha = 184
470 n
mi
Hp = 181
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13795534
27 X = -4231076
93
Y = 317594
59 feet Y = 49634
37 meter
Z = 17173144
78 Z = 5213883
20
XDOT = 2902
953298 XDOT = 965
657580
YDOT = -24950
780635 feet/sec YDOT = -7594
651487 meter/sec
ZDOT = 2794
036168 ZDOT = 856
116226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4772032
65 X = -1454515
55
Y = 13051687
31 feet Y = 3978154
29 meter
Z = 17094317
66 Z = 5210348
02
XDOT = -21226
750032 XDOT = -6469
913410
YDOT = -11441
423611 feet/sec YDOT = -3487
345916 meter/sec
ZDOT = 2810
612460 ZDOT = 856
674678
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 08152
54898460
00020000 00000-0 20000-3 0 9054
2 25544 51
6360 102
1737 0005901 284
6329 75
4182 15
76609819 25908
Satellite: ISS
Catalog Number: 25544
Epoch time: 08152
54898460 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 102
1737 deg
Eccentricity:
0005901
Arg of perigee: 284
6329 deg
Mean anomaly: 75
4182 deg
Mean motion: 15
76609819 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2590
Checksum: 304
Coasting Arc #7 (Orbit 2605)
---------------------------------------
Vector Time (GMT): 2008/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -863283
65 A = 6724753
01 meter
Y = 6660608
38 meter E =
0011059
Z = 133589
39 I = 51
98049
XDOT = -4692
728947 Wp = 18
68064
YDOT = -732
507320 meter/sec RA = 96
49392 deg
ZDOT = 6069
657338 TA = 342
76582
MA = 342
80334
Ha = 184
565 n
mi
Hp = 181
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2832295
45 X = -938348
43
Y = 21852389
69 feet Y = 6650534
92 meter
Z = 438285
38 Z = 129214
11
XDOT = -15396
092345 XDOT = -4713
675092
YDOT = -2403
239240 feet/sec YDOT = -785
102118 meter/sec
ZDOT = 19913
573942 ZDOT = 6046
808574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19492321
33 X = 5941259
54
Y = 10276779
63 feet Y = 3132362
43 meter
Z = 422062
27 Z = 128644
58
XDOT = -6911
018005 XDOT = -2106
478288
YDOT = 12276
388359 feet/sec YDOT = 3741
843172 meter/sec
ZDOT = 19825
595812 ZDOT = 6042
841603
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 08153
56314086
00020000 00000-0 20000-3 0 9065
2 25544 51
6360 96
9444 0005853 288
6837 71
3692 15
76613608 26067
Satellite: ISS
Catalog Number: 25544
Epoch time: 08153
56314086 = yrday
fracday
Element set: 906
Inclination: 51
6360 deg
RA of node: 96
9444 deg
Eccentricity:
0005853
Arg of perigee: 288
6837 deg
Mean anomaly: 71
3692 deg
Mean motion: 15
76613608 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2606
Checksum: 314
Coasting Arc #8 (Orbit 2620)
---------------------------------------
Vector Time (GMT): 2008/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4032784
46 A = 6713071
46 meter
Y = 1387529
98 meter E =
0008745
Z = -5191724
64 I = 51
94430
XDOT = -1091
261714 Wp = 89
59412
YDOT = 7531
439270 meter/sec RA = 91
34999 deg
ZDOT = 1166
913935 TA = 191
49383
MA = 191
51381
Ha = 184
768 n
mi
Hp = 181
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13230920
14 X = 4042190
12
Y = 4552263
71 feet Y = 1432680
43 meter
Z = -17033217
34 Z = -5172109
87
XDOT = -3580
254966 XDOT = -1181
067119
YDOT = 24709
446424 feet/sec YDOT = 7518
733815 meter/sec
ZDOT = 3828
457791 ZDOT = 1161
395719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8724974
35 X = 2659372
18
Y = -11055533
49 feet Y = -3369726
61 meter
Z = -16957619
15 Z = -5168682
32
XDOT = 21299
381726 XDOT = 6492
051550
YDOT = 10977
377815 feet/sec YDOT = 3345
904758 meter/sec
ZDOT = 3807
898717 ZDOT = 1160
647529
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 08154
51390000
00020000 00000-0 20000-3 0 9072
2 25544 51
6370 92
0425 0005915 292
7847 67
2692 15
76625164 26211
Satellite: ISS
Catalog Number: 25544
Epoch time: 08154
51390000 = yrday
fracday
Element set: 907
Inclination: 51
6370 deg
RA of node: 92
0425 deg
Eccentricity:
0005915
Arg of perigee: 292
7847 deg
Mean anomaly: 67
2692 deg
Mean motion: 15
76625164 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2621
Checksum: 285
Coasting Arc #9 (Orbit 2636)
---------------------------------------
Vector Time (GMT): 2008/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1058292
13 A = 6723098
88 meter
Y = -6364294
11 meter E =
0003035
Z = -1883751
26 I = 51
97891
XDOT = 4603
774507 Wp = 195
70310
YDOT = 2443
788198 meter/sec RA = 86
24458 deg
ZDOT = -5670
735351 TA = 5
13799
MA = 5
13487
Ha = 184
836 n
mi
Hp = 181
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3472087
04 X = 1138531
08
Y = -20880230
03 feet Y = -6352010
64 meter
Z = -6180286
30 Z = -1878416
46
XDOT = 15104
247071 XDOT = 4603
653343
YDOT = 8017
677814 feet/sec YDOT = 2495
270771 meter/sec
ZDOT = -18604
774773 ZDOT = -5648
369638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18699369
53 X = -5699567
83
Y = -9930732
50 feet Y = -3026887
27 meter
Z = -6160313
68 Z = -1877663
61
XDOT = 11692
164086 XDOT = 3563
771613
YDOT = -10530
090153 feet/sec YDOT = -3209
571479 meter/sec
ZDOT = -18518
493117 ZDOT = -5644
436702
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 08155
52803029
00020000 00000-0 20000-3 0 9085
2 25544 51
6381 86
8142 0005912 296
8592 63
1968 15
76653261 26376
Satellite: ISS
Catalog Number: 25544
Epoch time: 08155
52803029 = yrday
fracday
Element set: 908
Inclination: 51
6381 deg
RA of node: 86
8142 deg
Eccentricity:
0005912
Arg of perigee: 296
8592 deg
Mean anomaly: 63
1968 deg
Mean motion: 15
76653261 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2637
Checksum: 313
Coasting Arc #10 (Orbit 2652)
---------------------------------------
Vector Time (GMT): 2008/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4049090
55 A = 6715663
85 meter
Y = -2831194
72 meter E =
0007121
Z = 4549392
09 I = 51
95083
XDOT = 1360
492291 Wp = 23
80505
YDOT = -6924
152733 meter/sec RA = 81
07226 deg
ZDOT = -3090
146571 TA = 96
85867
MA = 96
77766
Ha = 185
033 n
mi
Hp = 181
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13284417
83 X = -4039231
04
Y = -9288696
60 feet Y = -2876419
88 meter
Z = 14925827
05 Z = 4529744
75
XDOT = 4463
557386 XDOT = 1452
829631
YDOT = -22717
036526 feet/sec YDOT = -6908
421941 meter/sec
ZDOT = -10138
276153 ZDOT = -3083
314536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12870410
17 X = -3922901
02
Y = 9968296
80 feet Y = 3038336
86 meter
Z = 14849968
21 Z = 4526270
31
XDOT = -19588
719081 XDOT = -5970
641576
YDOT = -10187
262660 feet/sec YDOT = -3105
077659 meter/sec
ZDOT = -10112
577159 ZDOT = -3082
313518
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 08156
54214762
00020000 00000-0 20000-3 0 9099
2 25544 51
6383 81
5861 0005907 300
7055 59
3527 15
76666596 26532
Satellite: ISS
Catalog Number: 25544
Epoch time: 08156
54214762 = yrday
fracday
Element set: 909
Inclination: 51
6383 deg
RA of node: 81
5861 deg
Eccentricity:
0005907
Arg of perigee: 300
7055 deg
Mean anomaly: 59
3527 deg
Mean motion: 15
76666596 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2653
Checksum: 313
Coasting Arc #11 (Orbit 2668)
---------------------------------------
Vector Time (GMT): 2008/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1366424
80 A = 6719440
65 meter
Y = 5608279
84 meter E =
0008237
Z = 3429935
05 I = 51
95830
XDOT = -4717
490314 Wp = 67
02215
YDOT = -3977
524243 meter/sec RA = 75
98677 deg
ZDOT = 4618
719808 TA = 333
41521
MA = 333
45743
Ha = 185
209 n
mi
Hp = 181
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4483020
99 X = -1445697
92
Y = 18399868
25 feet Y = 5592555
69 meter
Z = 11253067
76 Z = 3423105
66
XDOT = -15477
330427 XDOT = -4695
099307
YDOT = -13049
620219 feet/sec YDOT = -4030
153759 meter/sec
ZDOT = 15153
280211 ZDOT = 4595
855722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16356554
17 X = 4985477
71
Y = 9575802
22 feet Y = 2918704
52 meter
Z = 11227257
48 Z = 3422068
08
XDOT = -16227
362008 XDOT = -4946
099940
YDOT = 10033
686296 feet/sec YDOT = 3058
267583 meter/sec
ZDOT = 15064
936744 ZDOT = 4591
792720
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 08157
55625152
00020000 00000-0 20000-3 0 9102
2 25544 51
6386 76
3570 0005940 304
8885 55
1721 15
76684675 26692
Satellite: ISS
Catalog Number: 25544
Epoch time: 08157
55625152 = yrday
fracday
Element set: 910
Inclination: 51
6386 deg
RA of node: 76
3570 deg
Eccentricity:
0005940
Arg of perigee: 304
8885 deg
Mean anomaly: 55
1721 deg
Mean motion: 15
76684675 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2669
Checksum: 316
Coasting Arc #12 (Orbit 2683)
---------------------------------------
Vector Time (GMT): 2008/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4196294
57 A = 6719535
98 meter
Y = 4014416
03 meter E =
0003796
Z = -3376693
13 I = 51
95102
XDOT = -1835
949242 Wp = 1
81570
YDOT = 5844
952482 meter/sec RA = 70
80155 deg
ZDOT = 4671
107416 TA = 318
51813
MA = 318
54693
Ha = 185
328 n
mi
Hp = 181
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13767370
65 X = 4167496
14
Y = 13170656
27 feet Y = 4061181
07 meter
Z = -11078389
53 Z = -3356376
76
XDOT = -6023
455518 XDOT = -1923
863245
YDOT = 19176
353286 feet/sec YDOT = 5823
929336 meter/sec
ZDOT = 15325
155565 ZDOT = 4661
976076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16384119
37 X = 4993879
58
Y = -9813331
02 feet Y = -2991103
30 meter
Z = -10999843
75 Z = -3352752
38
XDOT = 16134
259212 XDOT = 4917
722208
YDOT = 9812
423518 feet/sec YDOT = 2990
826688 meter/sec
ZDOT = 15290
498884 ZDOT = 4660
544060
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 08158
50696147
00020000 00000-0 20000-3 0 9111
2 25544 51
6391 71
4549 0005974 308
1890 51
8736 15
76720608 26843
Satellite: ISS
Catalog Number: 25544
Epoch time: 08158
50696147 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 71
4549 deg
Eccentricity:
0005974
Arg of perigee: 308
1890 deg
Mean anomaly: 51
8736 deg
Mean motion: 15
76720608 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2684
Checksum: 316
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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