Date:
March 21st 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 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 3160)
---------------------------------------
Vector Time (GMT): 2009/077/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5090588
96 A = 6731840
65 meter
Y = 1278392
49 meter E =
0017775
Z = -4234416
91 I = 51
90061
XDOT = 1367
258186 Wp = 123
84208
YDOT = 6622
086070 meter/sec RA = 53
33696 deg
ZDOT = 3644
177932 TA = 183
22810
MA = 183
23959
Ha = 197
372 n
mi
Hp = 184
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16701407
34 X = 5096485
32
Y = 4194201
07 feet Y = 1335351
30 meter
Z = -13892443
92 Z = -4209672
68
XDOT = 4485
755205 XDOT = 1275
404647
YDOT = 21726
004166 feet/sec YDOT = 6636
862045 meter/sec
ZDOT = 11955
964345 ZDOT = 3650
596780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17154320
50 X = -5228636
89
Y = -2221619
82 feet Y = -677149
72 meter
Z = -13795724
76 Z = -4204936
91
XDOT = -7065
921893 XDOT = -2153
692993
YDOT = -19817
218761 feet/sec YDOT = -6040
288278 meter/sec
ZDOT = 11981
488954 ZDOT = 3651
957833
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 09077
04181804
00010596 00000-0 82463-4 0 9009
2 25544 51
6403 53
9169 0010078 135
3244 224
8732 15
71437771 31614
Satellite: ISS
Catalog Number: 25544
Epoch time: 09077
04181804 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 53
9169 deg
Eccentricity:
0010078
Arg of perigee: 135
3244 deg
Mean anomaly: 224
8732 deg
Mean motion: 15
71437771 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3161
Checksum: 293
Coasting Arc #2 (Orbit 3176)
---------------------------------------
Vector Time (GMT): 2009/078/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2473655
45 A = 6736614
28 meter
Y = -5736366
22 meter E =
0015246
Z = -2513128
28 I = 51
89844
XDOT = 5545
304286 Wp = 135
59402
YDOT = -66
873119 meter/sec RA = 48
28477 deg
ZDOT = -5335
567639 TA = 72
71890
MA = 72
55214
Ha = 197
242 n
mi
Hp = 184
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8115667
48 X = -2397118
38
Y = -18820099
15 feet Y = -5763600
19 meter
Z = -8245171
54 Z = -2524959
16
XDOT = 18193
255530 XDOT = 5571
558923
YDOT = -219
399997 feet/sec YDOT = -4
715617 meter/sec
ZDOT = -17505
143174 ZDOT = -5308
565023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10497925
06 X = 3199767
56
Y = 17580762
88 feet Y = 5358616
53 meter
Z = -8291766
42 Z = -2527330
41
XDOT = -16820
598307 XDOT = -5126
918364
YDOT = 1883
809324 feet/sec YDOT = 574
185082 meter/sec
ZDOT = -17399
694314 ZDOT = -5303
426827
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 09078
05929528
00010596 00000-0 82463-4 0 9015
2 25544 51
6402 48
7107 0010055 139
1814 221
0103 15
71468682 31770
Satellite: ISS
Catalog Number: 25544
Epoch time: 09078
05929528 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 48
7107 deg
Eccentricity:
0010055
Arg of perigee: 139
1814 deg
Mean anomaly: 221
0103 deg
Mean motion: 15
71468682 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3177
Checksum: 295
Coasting Arc #3 (Orbit 3192)
---------------------------------------
Vector Time (GMT): 2009/079/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4293845
22 A = 6728695
93 meter
Y = 1348485
17 meter E =
0012065
Z = 4991075
86 I = 51
85148
XDOT = -4238
282617 Wp = 112
61622
YDOT = -6119
144552 meter/sec RA = 43
14787 deg
ZDOT = -1993
692230 TA = 356
58709
MA = 356
59531
Ha = 197
377 n
mi
Hp = 184
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14087418
71 X = -4332850
54
Y = 4424163
94 feet Y = 1300250
95 meter
Z = 16374920
80 Z = 4970121
82
XDOT = -13905
126697 XDOT = -4159
857440
YDOT = -20075
933570 feet/sec YDOT = -6166
101059 meter/sec
ZDOT = -6540
985005 ZDOT = -2014
090891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13358046
25 X = 4071532
50
Y = -6500889
31 feet Y = -1981471
06 meter
Z = 16293178
40 Z = 4966160
78
XDOT = 16246
684885 XDOT = 4951
989553
YDOT = 16795
513328 feet/sec YDOT = 5119
272463 meter/sec
ZDOT = -6621
064537 ZDOT = -2018
100471
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 09079
07676044
00010596 00000-0 82463-4 0 9021
2 25544 51
6408 43
5055 0010131 142
5838 217
6031 15
71454565 31934
Satellite: ISS
Catalog Number: 25544
Epoch time: 09079
07676044 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 43
5055 deg
Eccentricity:
0010131
Arg of perigee: 142
5838 deg
Mean anomaly: 217
6031 deg
Mean motion: 15
71454565 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3193
Checksum: 295
Coasting Arc #4 (Orbit 3208)
---------------------------------------
Vector Time (GMT): 2009/080/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4764241
00 A = 6738843
74 meter
Y = 4669799
26 meter E =
0016826
Z = 940470
27 I = 51
86487
XDOT = -3966
709280 Wp = 91
84538
YDOT = 2829
569076 meter/sec RA = 38
07206 deg
ZDOT = 5952
965566 TA = 278
37735
MA = 278
56807
Ha = 197
058 n
mi
Hp = 185
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15630711
94 X = 4707099
86
Y = 15320863
72 feet Y = 4722756
33 meter
Z = 3085532
39 Z = 963475
65
XDOT = -13014
138059 XDOT = -4026
973223
YDOT = 9283
363109 feet/sec YDOT = 2784
874321 meter/sec
ZDOT = 19530
726922 ZDOT = 5933
549053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17951156
09 X = -5471512
38
Y = -12499579
71 feet Y = -3809871
89 meter
Z = 3175694
13 Z = 967951
57
XDOT = 10481
366075 XDOT = 3194
720380
YDOT = -10035
602912 feet/sec YDOT = -3058
851768 meter/sec
ZDOT = 19455
087803 ZDOT = 5929
910762
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 09080
09420859
00010596 00000-0 82463-4 0 9037
2 25544 51
6417 38
2998 0010076 146
7810 213
3986 15
71517803 32090
Satellite: ISS
Catalog Number: 25544
Epoch time: 09080
09420859 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 38
2998 deg
Eccentricity:
0010076
Arg of perigee: 146
7810 deg
Mean anomaly: 213
3986 deg
Mean motion: 15
71517803 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3209
Checksum: 317
Coasting Arc #5 (Orbit 3223)
---------------------------------------
Vector Time (GMT): 2009/081/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2439961
00 A = 6727128
38 meter
Y = -3383540
73 meter E =
0021931
Z = -5294916
79 I = 51
80175
XDOT = 6365
791368 Wp = 114
15343
YDOT = 4296
199664 meter/sec RA = 32
95881 deg
ZDOT = 179
900016 TA = 157
60217
MA = 157
50626
Ha = 196
915 n
mi
Hp = 185
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8005121
40 X = 2503336
36
Y = -11100855
43 feet Y = -3355901
63 meter
Z = -17371774
24 Z = -5282909
49
XDOT = 20885
142284 XDOT = 6316
403518
YDOT = 14095
143255 feet/sec YDOT = 4367
109522 meter/sec
ZDOT = 590
223150 ZDOT = 210
704376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5926044
89 X = -1806258
48
Y = 12402100
36 feet Y = 3780160
19 meter
Z = -17325108
91 Z = -5280693
20
XDOT = -22212
688720 XDOT = -6770
427522
YDOT = -9583
188108 feet/sec YDOT = -2920
955735 meter/sec
ZDOT = 710
818115 ZDOT = 216
657361
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 09081
04805529
00010596 00000-0 82463-4 0 9045
2 25544 51
6419 33
4201 0009969 150
2534 209
9197 15
71545927 32248
Satellite: ISS
Catalog Number: 25544
Epoch time: 09081
04805529 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 33
4201 deg
Eccentricity:
0009969
Arg of perigee: 150
2534 deg
Mean anomaly: 209
9197 deg
Mean motion: 15
71545927 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3224
Checksum: 313
Coasting Arc #6 (Orbit 3239)
---------------------------------------
Vector Time (GMT): 2009/082/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6136762
74 A = 6739033
94 meter
Y = -2680303
49 meter E =
0022706
Z = 631829
90 I = 51
81660
XDOT = 1386
194353 Wp = 139
39859
YDOT = -4615
432624 meter/sec RA = 27
84930 deg
ZDOT = -6012
342593 TA = 33
73794
MA = 33
59364
Ha = 196
848 n
mi
Hp = 185
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20133736
02 X = -6109404
31
Y = -8793646
61 feet Y = -2748775
33 meter
Z = 2072932
74 Z = 602084
57
XDOT = 4547
881735 XDOT = 1466
908355
YDOT = -15142
495484 feet/sec YDOT = -4599
480560 meter/sec
ZDOT = -19725
533442 ZDOT = -6005
412142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21500609
16 X = 6553385
67
Y = 4570358
82 feet Y = 1393045
37 meter
Z = 1956584
49 Z = 596366
95
XDOT = -1193
716758 XDOT = -363
844868
YDOT = 14202
421764 feet/sec YDOT = 4328
898154 meter/sec
ZDOT = -19698
779542 ZDOT = -6004
188004
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 09082
06547834
00010596 00000-0 82463-4 0 9051
2 25544 51
6422 28
2138 0010034 154
5401 205
6257 15
71542559 32404
Satellite: ISS
Catalog Number: 25544
Epoch time: 09082
06547834 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 28
2138 deg
Eccentricity:
0010034
Arg of perigee: 154
5401 deg
Mean anomaly: 205
6257 deg
Mean motion: 15
71542559 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3240
Checksum: 285
Coasting Arc #7 (Orbit 3255)
---------------------------------------
Vector Time (GMT): 2009/083/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 131034
83 A = 6727763
63 meter
Y = 4400487
70 meter E =
0014325
Z = 5083614
34 I = 51
75362
XDOT = -7335
030509 Wp = 147
20759
YDOT = -1682
789519 meter/sec RA = 22
76205 deg
ZDOT = 1631
781989 TA = 287
06026
MA = 287
21714
Ha = 196
610 n
mi
Hp = 185
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 429904
28 X = 57123
08
Y = 14437295
61 feet Y = 4401540
23 meter
Z = 16678524
75 Z = 5084070
96
XDOT = -24065
060726 XDOT = -7323
594939
YDOT = -5520
962989 feet/sec YDOT = -1764
750013 meter/sec
ZDOT = 5353
615449 ZDOT = 1596
176731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3466709
50 X = -1056653
05
Y = -14019016
21 feet Y = -4272996
14 meter
Z = 16680606
09 Z = 5084248
74
XDOT = 23697
294764 XDOT = 7222
935444
YDOT = 398
861953 feet/sec YDOT = 121
573123 meter/sec
ZDOT = 5214
453772 ZDOT = 1589
365510
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 09083
08288547
00010596 00000-0 82463-4 0 9068
2 25544 51
6431 23
0080 0009932 158
5355 201
6225 15
71608087 32567
Satellite: ISS
Catalog Number: 25544
Epoch time: 09083
08288547 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 23
0080 deg
Eccentricity:
0009932
Arg of perigee: 158
5355 deg
Mean anomaly: 201
6225 deg
Mean motion: 15
71608087 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3256
Checksum: 305
Coasting Arc #8 (Orbit 3270)
---------------------------------------
Vector Time (GMT): 2009/084/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6379705
03 A = 6737134
91 meter
Y = 234105
18 meter E =
0008536
Z = -2167358
66 I = 51
75718
XDOT = 1680
934170 Wp = 121
38669
YDOT = 5089
659972 meter/sec RA = 17
62127 deg
ZDOT = 5509
204024 TA = 214
45123
MA = 214
50660
Ha = 196
541 n
mi
Hp = 185
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20930790
78 X = 6387141
64
Y = 768061
60 feet Y = 305488
11 meter
Z = -7110756
75 Z = -2136348
22
XDOT = 5514
875887 XDOT = 1597
133262
YDOT = 16698
359489 feet/sec YDOT = 5107
989191 meter/sec
ZDOT = 18074
816351 ZDOT = 5517
165854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20567598
92 X = -6269004
15
Y = 4167679
31 feet Y = 1270308
65 meter
Z = -6989642
82 Z = -2130443
13
XDOT = -8868
730504 XDOT = -2703
189058
YDOT = -13465
958028 feet/sec YDOT = -4104
424007 meter/sec
ZDOT = 18106
252496 ZDOT = 5518
785761
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 09084
03669432
00010596 00000-0 82463-4 0 9071
2 25544 51
6434 18
1281 0009750 161
7822 198
3691 15
71567098 32713
Satellite: ISS
Catalog Number: 25544
Epoch time: 09084
03669432 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 18
1281 deg
Eccentricity:
0009750
Arg of perigee: 161
7822 deg
Mean anomaly: 198
3691 deg
Mean motion: 15
71567098 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3271
Checksum: 324
Coasting Arc #9 (Orbit 3286)
---------------------------------------
Vector Time (GMT): 2009/085/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2752626
12 A = 6730315
80 meter
Y = -4224432
42 meter E =
0013065
Z = -4464642
91 I = 51
70628
XDOT = 6891
779255 Wp = 117
86953
YDOT = -1083
703540 meter/sec RA = 12
55329 deg
ZDOT = -3236
818318 TA = 119
76699
MA = 119
63697
Ha = 196
403 n
mi
Hp = 185
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9030925
61 X = -2683494
82
Y = -13859686
42 feet Y = -4254827
85 meter
Z = -14647778
58 Z = -4477846
77
XDOT = 22610
824329 XDOT = 6919
109060
YDOT = -3555
457808 feet/sec YDOT = -1006
483194 meter/sec
ZDOT = -10619
482672 ZDOT = -3203
271591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12138741
02 X = 3699888
26
Y = 11170407
41 feet Y = 3404740
18 meter
Z = -14699622
69 Z = -4480444
99
XDOT = -20238
862501 XDOT = -6168
805290
YDOT = 8247
605871 feet/sec YDOT = 2513
870270 meter/sec
ZDOT = -10488
560470 ZDOT = -3196
913231
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 09085
05407562
00010596 00000-0 82463-4 0 9089
2 25544 51
6435 12
9224 0009902 166
1138 194
0298 15
71600117 32874
Satellite: ISS
Catalog Number: 25544
Epoch time: 09085
05407562 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 12
9224 deg
Eccentricity:
0009902
Arg of perigee: 166
1138 deg
Mean anomaly: 194
0298 deg
Mean motion: 15
71600117 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3287
Checksum: 303
Coasting Arc #10 (Orbit 3302)
---------------------------------------
Vector Time (GMT): 2009/086/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5395412
21 A = 6733846
43 meter
Y = 2047405
64 meter E =
0017234
Z = 3448524
86 I = 51
68902
XDOT = -4534
056657 Wp = 123
02119
YDOT = -4232
202796 meter/sec RA = 7
39206 deg
ZDOT = -4573
917476 TA = 16
15411
MA = 16
09923
Ha = 196
375 n
mi
Hp = 185
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17701483
63 X = -5434658
03
Y = 6717210
09 feet Y = 1986851
91 meter
Z = 11314057
92 Z = 3422218
29
XDOT = -14875
513968 XDOT = -4464
175109
YDOT = -13885
179776 feet/sec YDOT = -4282
515007 meter/sec
ZDOT = -15006
290933 ZDOT = -4595
773838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15320715
23 X = 4669754
00
Y = -11227190
51 feet Y = -3422047
67 meter
Z = 11211477
11 Z = 3417258
22
XDOT = 17146
507878 XDOT = 5226
255601
YDOT = 8303
693718 feet/sec YDOT = 2530
965845 meter/sec
ZDOT = -15091
915101 ZDOT = -4600
015723
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 09086
07144310
00010596 00000-0 82463-4 0 9092
2 25544 51
6434 7
7170 0009826 168
8665 191
2716 15
71632803 33034
Satellite: ISS
Catalog Number: 25544
Epoch time: 09086
07144310 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 7
7170 deg
Eccentricity:
0009826
Arg of perigee: 168
8665 deg
Mean anomaly: 191
2716 deg
Mean motion: 15
71632803 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3303
Checksum: 306
Coasting Arc #11 (Orbit 3318)
---------------------------------------
Vector Time (GMT): 2009/087/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4988443
40 A = 6733572
78 meter
Y = 2929254
98 meter E =
0016839
Z = 3444422
39 I = 51
65940
XDOT = -5171
517403 Wp = 126
35601
YDOT = 3405
711517 meter/sec RA = 2
32801 deg
ZDOT = 4568
153515 TA = 274
35667
MA = 274
54905
Ha = 196
049 n
mi
Hp = 185
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16366284
11 X = 4938584
69
Y = 9610416
61 feet Y = 2984760
19 meter
Z = 11300598
40 Z = 3468535
11
XDOT = -16966
920612 XDOT = -5231
407744
YDOT = 11173
594217 feet/sec YDOT = 3347
546124 meter/sec
ZDOT = 14987
380300 ZDOT = 4542
884292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18359674
27 X = -5596028
72
Y = -4582206
74 feet Y = -1396656
61 meter
Z = 11394938
76 Z = 3473177
33
XDOT = 12840
910775 XDOT = 3913
909604
YDOT = -14220
259728 feet/sec YDOT = -4334
335165 meter/sec
ZDOT = 14888
942431 ZDOT = 4538
149653
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 09087
08879455
00010596 00000-0 82463-4 0 9101
2 25544 51
6435 2
5108 0009811 173
5483 186
5807 15
71676824 33190
Satellite: ISS
Catalog Number: 25544
Epoch time: 09087
08879455 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 2
5108 deg
Eccentricity:
0009811
Arg of perigee: 173
5483 deg
Mean anomaly: 186
5807 deg
Mean motion: 15
71676824 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3319
Checksum: 331
Coasting Arc #12 (Orbit 3333)
---------------------------------------
Vector Time (GMT): 2009/088/00:46:46
579
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3467337
68 A = 6730251
73 meter
Y = -3696127
82 meter E =
0016036
Z = -4443886
27 I = 51
61793
XDOT = 6585
113361 Wp = 143
82585
YDOT = 2255
316519 meter/sec RA = 357
16196 deg
ZDOT = 3255
474141 TA = 158
92162
MA = 158
85545
Ha = 195
925 n
mi
Hp = 186
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11375779
80 X = 3529998
55
Y = -12126403
60 feet Y = -3657003
94 meter
Z = -14579679
35 Z = -4426889
32
XDOT = 21604
702628 XDOT = 6543
589923
YDOT = 7399
332413 feet/sec YDOT = 2328
723127 meter/sec
ZDOT = 10680
689440 ZDOT = 3287
363987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7284354
58 X = -2220271
28
Y = 15010659
63 feet Y = 4575249
06 meter
Z = -14513557
66 Z = -4423732
38
XDOT = -21675
940719 XDOT = -6606
826731
YDOT = -49
912869 feet/sec YDOT = -15
213442 meter/sec
ZDOT = 10805
344590 ZDOT = 3293
469031
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 09088
04255061
00010596 00000-0 82463-4 0 9110
2 25544 51
6428 357
6307 0009725 176
5009 183
6223 15
71706859 33347
Satellite: ISS
Catalog Number: 25544
Epoch time: 09088
04255061 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 357
6307 deg
Eccentricity:
0009725
Arg of perigee: 176
5009 deg
Mean anomaly: 183
6223 deg
Mean motion: 15
71706859 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3334
Checksum: 317
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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