Date:
October 9th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2332)
---------------------------------------
Vector Time (GMT): 2009/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3829572
25 A = 6718744
01 meter
Y = 1846411
07 meter E =
0019273
Z = -5218040
87 I = 51
94664
XDOT = -2082
586099 Wp = 122
21199
YDOT = 7325
432145 meter/sec RA = 99
63614 deg
ZDOT = 1056
473379 TA = 157
87917
MA = 157
79589
Ha = 191
317 n
mi
Hp = 181
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12564213
41 X = 3833989
68
Y = 6057779
10 feet Y = 1889259
90 meter
Z = -17119556
65 Z = -5199425
74
XDOT = -6832
631558 XDOT = -2169
477854
YDOT = 24033
570028 feet/sec YDOT = 7301
657684 meter/sec
ZDOT = 3466
120011 ZDOT = 1046
144290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13729485
86 X = -4184747
29
Y = -2927162
67 feet Y = -892199
18 meter
Z = -17046064
15 Z = -5195640
35
XDOT = 827
323133 XDOT = 252
168091
YDOT = -23968
651811 feet/sec YDOT = -7305
645072 meter/sec
ZDOT = 3425
802099 ZDOT = 1044
184480
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 09278
51413793
00020000 00000-0 20000-3 0 9008
2 25544 51
6363 100
3830 0008459 166
4947 193
6444 15
74606682 23331
Satellite: ISS
Catalog Number: 25544
Epoch time: 09278
51413793 = yrday
fracday
Element set: 900
Inclination: 51
6363 deg
RA of node: 100
3830 deg
Eccentricity:
0008459
Arg of perigee: 166
4947 deg
Mean anomaly: 193
6444 deg
Mean motion: 15
74606682 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2333
Checksum: 301
Coasting Arc #2 (Orbit 2348)
---------------------------------------
Vector Time (GMT): 2009/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1416284
58 A = 6729733
97 meter
Y = -6467925
90 meter E =
0017132
Z = -1151466
60 I = 51
98860
XDOT = 4486
818284 Wp = 155
29733
YDOT = 2029
529674 meter/sec RA = 94
53894 deg
ZDOT = -5927
994164 TA = 37
26264
MA = 37
14389
Ha = 191
083 n
mi
Hp = 181
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4646602
95 X = 1494098
55
Y = -21220229
33 feet Y = -6451653
15 meter
Z = -3777777
55 Z = -1144396
74
XDOT = 14720
532427 XDOT = 4492
588172
YDOT = 6658
561923 feet/sec YDOT = 2079
735869 meter/sec
ZDOT = -19448
799751 ZDOT = -5906
182697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 798330
64 X = 243331
18
Y = 21713105
90 feet Y = 6618154
68 meter
Z = -3750247
36 Z = -1143075
39
XDOT = -14445
641523 XDOT = -4403
031536
YDOT = -2786
566229 feet/sec YDOT = -849
345387 meter/sec
ZDOT = -19362
697006 ZDOT = -5901
750047
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 09279
52956944
00020000 00000-0 20000-3 0 9011
2 25544 51
6369 95
1632 0008221 170
2738 189
8586 15
74660228 23493
Satellite: ISS
Catalog Number: 25544
Epoch time: 09279
52956944 = yrday
fracday
Element set: 901
Inclination: 51
6369 deg
RA of node: 95
1632 deg
Eccentricity:
0008221
Arg of perigee: 170
2738 deg
Mean anomaly: 189
8586 deg
Mean motion: 15
74660228 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2349
Checksum: 326
Coasting Arc #3 (Orbit 2364)
---------------------------------------
Vector Time (GMT): 2009/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4017728
60 A = 6719122
82 meter
Y = -1681579
85 meter E =
0007380
Z = 5110937
41 I = 51
95325
XDOT = 1142
775767 Wp = 139
12519
YDOT = -7460
226605 meter/sec RA = 89
39745 deg
ZDOT = -1560
395799 TA = 325
74909
MA = 325
79666
Ha = 191
221 n
mi
Hp = 181
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13181524
28 X = -4023454
95
Y = -5516994
26 feet Y = -1726540
34 meter
Z = 16768167
35 Z = 5091404
89
XDOT = 3749
264329 XDOT = 1233
692705
YDOT = -24475
809071 feet/sec YDOT = -7446
939112 meter/sec
ZDOT = -5119
408789 ZDOT = -1554
623000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14270421
91 X = 4349624
60
Y = 1767636
73 feet Y = 538775
68 meter
Z = 16691068
37 Z = 5087437
64
XDOT = 3027
718070 XDOT = 922
848468
YDOT = 23555
069123 feet/sec YDOT = 7179
585069 meter/sec
ZDOT = -5097
028052 ZDOT = -1553
574150
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 09280
54498765
00020000 00000-0 20000-3 0 9028
2 25544 51
6365 89
9427 0008440 173
9687 186
1579 15
74619741 23652
Satellite: ISS
Catalog Number: 25544
Epoch time: 09280
54498765 = yrday
fracday
Element set: 902
Inclination: 51
6365 deg
RA of node: 89
9427 deg
Eccentricity:
0008440
Arg of perigee: 173
9687 deg
Mean anomaly: 186
1579 deg
Mean motion: 15
74619741 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2365
Checksum: 342
Coasting Arc #4 (Orbit 2380)
---------------------------------------
Vector Time (GMT): 2009/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -595029
43 A = 6729143
94 meter
Y = 6511620
49 meter E =
0013028
Z = 1583824
37 I = 51
98681
XDOT = -4729
102866 Wp = 98
87089
YDOT = -1849
610241 meter/sec RA = 84
30726 deg
ZDOT = 5785
546717 TA = 278
51453
MA = 278
66215
Ha = 190
886 n
mi
Hp = 181
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1952196
29 X = -675493
39
Y = 21363584
27 feet Y = 6504516
63 meter
Z = 5196274
18 Z = 1580738
16
XDOT = -15515
429349 XDOT = -4736
174544
YDOT = -6068
275068 feet/sec YDOT = -1902
533363 meter/sec
ZDOT = 18981
452484 ZDOT = 5762
555012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4161095
69 X = -1268301
97
Y = -21048090
12 feet Y = -6415457
87 meter
Z = 5184424
13 Z = 1580212
48
XDOT = 15170
606639 XDOT = 4624
000903
YDOT = 1688
000532 feet/sec YDOT = 514
502562 meter/sec
ZDOT = 18890
704180 ZDOT = 5757
886634
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 09281
56038728
00020000 00000-0 20000-3 0 9031
2 25544 51
6372 84
7222 0008459 177
9998 182
1201 15
74686808 23819
Satellite: ISS
Catalog Number: 25544
Epoch time: 09281
56038728 = yrday
fracday
Element set: 903
Inclination: 51
6372 deg
RA of node: 84
7222 deg
Eccentricity:
0008459
Arg of perigee: 177
9998 deg
Mean anomaly: 182
1201 deg
Mean motion: 15
74686808 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2381
Checksum: 322
Coasting Arc #5 (Orbit 2395)
---------------------------------------
Vector Time (GMT): 2009/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4260155
63 A = 6719562
95 meter
Y = 1557125
78 meter E =
0016969
Z = -4971835
86 I = 51
95139
XDOT = -251
746946 Wp = 134
13698
YDOT = 7395
307120 meter/sec RA = 79
15820 deg
ZDOT = 2093
259356 TA = 156
12477
MA = 156
04598
Ha = 190
771 n
mi
Hp = 182
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13976888
54 X = 4266579
71
Y = 5108680
40 feet Y = 1604801
31 meter
Z = -16311797
44 Z = -4951124
00
XDOT = -825
941424 XDOT = -344
592718
YDOT = 24262
818636 feet/sec YDOT = 7391
972793 meter/sec
ZDOT = 6867
648805 ZDOT = 2091
810876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14956335
97 X = -4558691
20
Y = -648267
90 feet Y = -197592
06 meter
Z = -16230050
14 Z = -4946919
28
XDOT = -6505
174827 XDOT = -1982
777287
YDOT = -22313
119923 feet/sec YDOT = -6801
038953 meter/sec
ZDOT = 6862
286947 ZDOT = 2091
625061
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 09282
51231118
00020000 00000-0 20000-3 0 9046
2 25544 51
6382 79
8286 0008432 180
9292 179
1857 15
74701501 23964
Satellite: ISS
Catalog Number: 25544
Epoch time: 09282
51231118 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 79
8286 deg
Eccentricity:
0008432
Arg of perigee: 180
9292 deg
Mean anomaly: 179
1857 deg
Mean motion: 15
74701501 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2396
Checksum: 302
Coasting Arc #6 (Orbit 2411)
---------------------------------------
Vector Time (GMT): 2009/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -135614
76 A = 6728173
52 meter
Y = -6391017
61 meter E =
0013616
Z = -2075570
98 I = 51
97416
XDOT = 5027
684629 Wp = 164
83715
YDOT = 1700
551748 meter/sec RA = 74
07526 deg
ZDOT = -5585
780804 TA = 38
24412
MA = 38
14762
Ha = 190
528 n
mi
Hp = 182
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -444930
33 X = -54056
32
Y = -20967905
54 feet Y = -6392078
10 meter
Z = -6809616
08 Z = -2076031
75
XDOT = 16495
028310 XDOT = 5035
430204
YDOT = 5579
238018 feet/sec YDOT = 1756
817632 meter/sec
ZDOT = -18326
052506 ZDOT = -5561
337126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7022249
29 X = 2140381
58
Y = 19761332
89 feet Y = 6023254
26 meter
Z = -6811727
69 Z = -2076214
60
XDOT = -16072
952905 XDOT = -4899
036045
YDOT = -548
410986 feet/sec YDOT = -167
155668 meter/sec
ZDOT = -18229
578123 ZDOT = -5556
375412
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 09283
52767957
00020000 00000-0 20000-3 0 9054
2 25544 51
6383 74
6082 0008241 185
0419 175
0663 15
74747494 24127
Satellite: ISS
Catalog Number: 25544
Epoch time: 09283
52767957 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 74
6082 deg
Eccentricity:
0008241
Arg of perigee: 185
0419 deg
Mean anomaly: 175
0663 deg
Mean motion: 15
74747494 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2412
Checksum: 313
Coasting Arc #7 (Orbit 2427)
---------------------------------------
Vector Time (GMT): 2009/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4529424
81 A = 6720353
21 meter
Y = -1385399
41 meter E =
0007129
Z = 4760862
88 I = 51
93805
XDOT = -566
257181 Wp = 130
32632
YDOT = -7217
926360 meter/sec RA = 68
91738 deg
ZDOT = -2641
072415 TA = 345
46490
MA = 345
48539
Ha = 190
616 n
mi
Hp = 182
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14860317
61 X = -4536724
04
Y = -4545273
64 feet Y = -1436090
89 meter
Z = 15619628
87 Z = 4738840
99
XDOT = -1857
799150 XDOT = -472
673008
YDOT = -23680
860762 feet/sec YDOT = -7223
735338 meter/sec
ZDOT = -8664
935744 ZDOT = -2643
595965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15611510
05 X = 4758388
26
Y = -690546
70 feet Y = -210478
64 meter
Z = 15532715
71 Z = 4734371
75
XDOT = 9535
848331 XDOT = 2906
526571
YDOT = 20590
857602 feet/sec YDOT = 6276
093397 meter/sec
ZDOT = -8675
214855 ZDOT = -2644
205488
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 09284
54303347
00020000 00000-0 20000-3 0 9067
2 25544 51
6383 69
3880 0008352 188
3627 171
7399 15
74719647 24289
Satellite: ISS
Catalog Number: 25544
Epoch time: 09284
54303347 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 69
3880 deg
Eccentricity:
0008352
Arg of perigee: 188
3627 deg
Mean anomaly: 171
7399 deg
Mean motion: 15
74719647 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2428
Checksum: 328
Coasting Arc #8 (Orbit 2443)
---------------------------------------
Vector Time (GMT): 2009/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 817392
15 A = 6727056
12 meter
Y = 6174062
80 meter E =
0012539
Z = 2540526
58 I = 51
95089
XDOT = -5366
187901 Wp = 112
75067
YDOT = -1487
485777 meter/sec RA = 63
83968 deg
ZDOT = 5316
037742 TA = 275
91116
MA = 276
05406
Ha = 190
192 n
mi
Hp = 182
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2681732
76 X = 735950
44
Y = 20256111
54 feet Y = 6182748
07 meter
Z = 8335060
95 Z = 2544299
50
XDOT = -17605
603351 XDOT = -5374
980298
YDOT = -4880
202682 feet/sec YDOT = -1547
542660 meter/sec
ZDOT = 17441
068706 ZDOT = 5289
947288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9537181
59 X = -2906932
95
Y = -18063527
31 feet Y = -5505763
12 meter
Z = 8350217
65 Z = 2545146
34
XDOT = 16979
572246 XDOT = 5175
373621
YDOT = -911
519471 feet/sec YDOT = -277
831135 meter/sec
ZDOT = 17338
101880 ZDOT = 5284
653453
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 09285
55836654
00020000 00000-0 20000-3 0 9072
2 25544 51
6395 64
1676 0008377 193
1609 166
9337 15
74812621 24441
Satellite: ISS
Catalog Number: 25544
Epoch time: 09285
55836654 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 64
1676 deg
Eccentricity:
0008377
Arg of perigee: 193
1609 deg
Mean anomaly: 166
9337 deg
Mean motion: 15
74812621 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2444
Checksum: 325
Coasting Arc #9 (Orbit 2458)
---------------------------------------
Vector Time (GMT): 2009/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4858448
16 A = 6721231
39 meter
Y = 1204071
58 meter E =
0013086
Z = -4497321
13 I = 51
91697
XDOT = 1258
155583 Wp = 149
01144
YDOT = 6882
965276 meter/sec RA = 58
67410 deg
ZDOT = 3195
090777 TA = 152
87440
MA = 152
80597
Ha = 190
031 n
mi
Hp = 182
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15939790
55 X = 4866470
28
Y = 3950366
08 feet Y = 1258446
22 meter
Z = -14754990
59 Z = -4473699
19
XDOT = 4127
807030 XDOT = 1165
574265
YDOT = 22581
907075 feet/sec YDOT = 6896
517242 meter/sec
ZDOT = 10482
581290 ZDOT = 3200
977681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16361591
27 X = -4987013
02
Y = 2173212
81 feet Y = 662395
26 meter
Z = -14661771
36 Z = -4468907
91
XDOT = -11871
698488 XDOT = -3618
493699
YDOT = -18345
638895 feet/sec YDOT = -5591
750735 meter/sec
ZDOT = 10506
105042 ZDOT = 3202
260817
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 09286
51022909
00020000 00000-0 20000-3 0 9080
2 25544 51
6399 59
2740 0008192 196
9744 163
1146 15
74799033 24592
Satellite: ISS
Catalog Number: 25544
Epoch time: 09286
51022909 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 59
2740 deg
Eccentricity:
0008192
Arg of perigee: 196
9744 deg
Mean anomaly: 163
1146 deg
Mean motion: 15
74799033 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2459
Checksum: 324
Coasting Arc #10 (Orbit 2474)
---------------------------------------
Vector Time (GMT): 2009/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1346321
34 A = 6725772
73 meter
Y = -5841198
93 meter E =
0009047
Z = -3040612
75 I = 51
91638
XDOT = 5756
029943 Wp = 170
69256
YDOT = 1251
761749 meter/sec RA = 53
59886 deg
ZDOT = -4964
131150 TA = 44
38816
MA = 44
31568
Ha = 189
832 n
mi
Hp = 182
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4417064
77 X = -1266133
07
Y = -19164038
50 feet Y = -5855806
17 meter
Z = -9975763
62 Z = -3046958
02
XDOT = 18884
612675 XDOT = 5765
719837
YDOT = 4106
829885 feet/sec YDOT = 1316
182865 meter/sec
ZDOT = -16286
519521 ZDOT = -4936
144618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11332294
08 X = 3454083
24
Y = 16057549
00 feet Y = 4894340
94 meter
Z = -10001046
12 Z = -3048318
86
XDOT = -17941
341981 XDOT = -5468
521036
YDOT = 2608
819681 feet/sec YDOT = 795
168239 meter/sec
ZDOT = -16176
085721 ZDOT = -4930
470928
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 09287
52553124
00020000 00000-0 20000-3 0 9091
2 25544 51
6401 54
0528 0008153 200
9243 159
1588 15
74827912 24751
Satellite: ISS
Catalog Number: 25544
Epoch time: 09287
52553124 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 54
0528 deg
Eccentricity:
0008153
Arg of perigee: 200
9243 deg
Mean anomaly: 159
1588 deg
Mean motion: 15
74827912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2475
Checksum: 294
Coasting Arc #11 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2009/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5194099
10 A = 6722404
64 meter
Y = -947112
13 meter E =
0008315
Z = 4152115
19 I = 51
88678
XDOT = -1816
894119 Wp = 124
61407
YDOT = -6482
489899 meter/sec RA = 48
42616 deg
ZDOT = -3750
876328 TA = 3
60243
MA = 3
59644
Ha = 189
818 n
mi
Hp = 183
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17041007
54 X = -5203292
83
Y = -3107323
27 feet Y = -1005246
65 meter
Z = 13622425
18 Z = 4126859
62
XDOT = -5960
938712 XDOT = -1726
049387
YDOT = -21268
011480 feet/sec YDOT = -6502
299869 meter/sec
ZDOT = -12306
024699 ZDOT = -3759
481706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16947257
66 X = 5165524
13
Y = -3942937
90 feet Y = -1201807
47 meter
Z = 13522779
39 Z = 4121743
16
XDOT = 13558
926070 XDOT = 4132
760666
YDOT = 15948
294463 feet/sec YDOT = 4861
040152 meter/sec
ZDOT = -12340
243551 ZDOT = -3761
306234
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 09288
54081707
00020000 00000-0 20000-3 0 9109
2 25544 51
6409 48
8326 0008076 204
1342 155
9445 15
74831586 24912
Satellite: ISS
Catalog Number: 25544
Epoch time: 09288
54081707 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 48
8326 deg
Eccentricity:
0008076
Arg of perigee: 204
1342 deg
Mean anomaly: 155
9445 deg
Mean motion: 15
74831586 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2491
Checksum: 303
Coasting Arc #12 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2009/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1776397
92 A = 6724193
75 meter
Y = 5457881
06 meter E =
0011286
Z = 3503008
61 I = 51
87415
XDOT = -6154
874178 Wp = 131
72805
YDOT = -917
285428 meter/sec RA = 43
35174 deg
ZDOT = 4533
678309 TA = 269
74274
MA = 269
87206
Ha = 189
350 n
mi
Hp = 183
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5828077
17 X = 1698217
57
Y = 17906433
93 feet Y = 5477308
96 meter
Z = 11492810
41 Z = 3511448
17
XDOT = -20193
156752 XDOT = -6166
183749
YDOT = -3009
466627 feet/sec YDOT = -986
175710 meter/sec
ZDOT = 14874
272666 ZDOT = 4503
749899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12636236
23 X = -3851524
80
Y = -13934164
66 feet Y = -4247133
39 meter
Z = 11526323
79 Z = 3513223
49
XDOT = 18698
356159 XDOT = 5699
258957
YDOT = -4705
208891 feet/sec YDOT = -1434
147670 meter/sec
ZDOT = 14756
204827 ZDOT = 4497
691231
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 09289
55608222
00020000 00000-0 20000-3 0 9119
2 25544 51
6420 43
6117 0008042 209
0429 151
0288 15
74921540 25079
Satellite: ISS
Catalog Number: 25544
Epoch time: 09289
55608222 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 43
6117 deg
Eccentricity:
0008042
Arg of perigee: 209
0429 deg
Mean anomaly: 151
0288 deg
Mean motion: 15
74921540 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2507
Checksum: 270
Coasting Arc #13 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2009/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5557908
35 A = 6723648
25 meter
Y = 634438
60 meter E =
0007888
Z = -3738063
04 I = 51
84960
XDOT = 2197
565170 Wp = 169
90035
YDOT = 6004
685624 meter/sec RA = 38
17413 deg
ZDOT = 4280
323452 TA = 145
14755
MA = 145
09587
Ha = 189
163 n
mi
Hp = 183
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18234607
44 X = 5568560
18
Y = 2081491
47 feet Y = 696649
70 meter
Z = -12263986
36 Z = -3711036
18
XDOT = 7209
859482 XDOT = 2109
462812
YDOT = 19700
412153 feet/sec YDOT = 6028
767795 meter/sec
ZDOT = 14043
055945 ZDOT = 4290
785068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17433760
32 X = -5313810
14
Y = 5958273
49 feet Y = 1816081
76 meter
Z = -12157378
62 Z = -3705569
00
XDOT = -14443
021679 XDOT = -4402
233008
YDOT = -13479
331173 feet/sec YDOT = -4108
500142 meter/sec
ZDOT = 14084
556492 ZDOT = 4292
972819
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 09290
50788107
00020000 00000-0 20000-3 0 9128
2 25544 51
6423 38
7181 0007881 213
8082 146
2580 15
74899501 25225
Satellite: ISS
Catalog Number: 25544
Epoch time: 09290
50788107 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 38
7181 deg
Eccentricity:
0007881
Arg of perigee: 213
8082 deg
Mean anomaly: 146
2580 deg
Mean motion: 15
74899501 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2522
Checksum: 295
Coasting Arc #14 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2009/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2018962
34 A = 6722644
88 meter
Y = -5037950
22 meter E =
0004543
Z = -3965555
51 I = 51
82294
XDOT = 6558
566196 Wp = 154
39465
YDOT = 518
039321 meter/sec RA = 33
09757 deg
ZDOT = -4002
966391 TA = 74
23706
MA = 74
18696
Ha = 188
965 n
mi
Hp = 183
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6623892
19 X = -1943212
52
Y = -16528708
08 feet Y = -5060104
12 meter
Z = -13010352
73 Z = -3975179
66
XDOT = 21517
605629 XDOT = 6571
732205
YDOT = 1699
604071 feet/sec YDOT = 591
454481 meter/sec
ZDOT = -13133
091834 ZDOT = -3971
071975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13202001
92 X = 4023970
19
Y = 11907441
51 feet Y = 3629388
17 meter
Z = -13048501
78 Z = -3977183
34
XDOT = -19237
558766 XDOT = -5863
607912
YDOT = 7095
741994 feet/sec YDOT = 2162
782160 meter/sec
ZDOT = -13007
298135 ZDOT = -3964
624472
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 09291
52311522
00020000 00000-0 20000-3 0 9135
2 25544 51
6429 33
4978 0007887 217
2326 142
8291 15
74928773 25384
Satellite: ISS
Catalog Number: 25544
Epoch time: 09291
52311522 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 33
4978 deg
Eccentricity:
0007887
Arg of perigee: 217
2326 deg
Mean anomaly: 142
8291 deg
Mean motion: 15
74928773 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2538
Checksum: 311
Coasting Arc #15 (Orbit 2553)
---------------------------------------
Vector Time (GMT): 2009/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5882859
19 A = 6725008
32 meter
Y = -235763
18 meter E =
0010276
Z = 3235981
66 I = 51
80498
XDOT = -2412
110647 Wp = 129
25635
YDOT = -5538
613570 meter/sec RA = 27
91733 deg
ZDOT = -4784
947288 TA = 12
94563
MA = 12
91927
Ha = 188
876 n
mi
Hp = 183
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19300719
14 X = -5895505
92
Y = -773501
24 feet Y = -301619
39 meter
Z = 10616737
72 Z = 3207371
13
XDOT = -7913
748843 XDOT = -2326
752505
YDOT = -18171
304363 feet/sec YDOT = -5565
110091 meter/sec
ZDOT = -15698
645959 ZDOT = -4796
458179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17556646
38 X = 5351265
82
Y = -8201419
58 feet Y = -2499792
69 meter
Z = 10503907
27 Z = 3201590
94
XDOT = 14692
840158 XDOT = 4478
377680
YDOT = 11272
774259 feet/sec YDOT = 3435
941594 meter/sec
ZDOT = -15744
244453 ZDOT = -4798
845709
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 09292
53833261
00020000 00000-0 20000-3 0 9147
2 25544 51
6428 28
2779 0007684 220
5403 139
5189 15
74950670 25540
Satellite: ISS
Catalog Number: 25544
Epoch time: 09292
53833261 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 28
2779 deg
Eccentricity:
0007684
Arg of perigee: 220
5403 deg
Mean anomaly: 139
5189 deg
Mean motion: 15
74950670 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2554
Checksum: 309
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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