Date:
July 4th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10494 81 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 820)
---------------------------------------
Vector Time (GMT): 2009/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2065539
19 A = 6720761
87 meter
Y = 3939609
98 meter E =
0014826
Z = -5048877
50 I = 51
35731
XDOT = -5557
731516 Wp = 109
03118
YDOT = -5047
406667 meter/sec RA = 232
51093 deg
ZDOT = -1673
508725 TA = 144
84375
MA = 144
74584
Ha = 191
647 n
mi
Hp = 182
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6776703
39 X = -2084912
46
Y = 12925229
59 feet Y = 3916404
36 meter
Z = -16564558
73 Z = -5058958
38
XDOT = -18234
027282 XDOT = -5492
747866
YDOT = -16559
733158 feet/sec YDOT = -5109
192873 meter/sec
ZDOT = -5490
514191 ZDOT = -1700
351193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13803555
36 X = 4207323
67
Y = 4598150
29 feet Y = 1401516
21 meter
Z = -16603877
51 Z = -5060861
86
XDOT = -13205
929689 XDOT = -4025
167369
YDOT = 19540
191309 feet/sec YDOT = 5955
850311 meter/sec
ZDOT = -5596
056185 ZDOT = -1705
677925
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 09182
51880199
00010596 00000-0 82463-4 0 9001
2 25544 51
6396 233
3229 0007827 173
9476 186
1783 15
74103705 8215
Satellite: ISS
Catalog Number: 25544
Epoch time: 09182
51880199 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 233
3229 deg
Eccentricity:
0007827
Arg of perigee: 173
9476 deg
Mean anomaly: 186
1783 deg
Mean motion: 15
74103705 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 821
Checksum: 326
Coasting Arc #2 (Orbit 836)
---------------------------------------
Vector Time (GMT): 2009/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5210667
55 A = 6730882
05 meter
Y = 4004725
39 meter E =
0019213
Z = 1399580
74 I = 51
41116
XDOT = -2010
116650 Wp = 139
05537
YDOT = 4655
298045 meter/sec RA = 227
32895 deg
ZDOT = -5806
302317 TA = 25
48944
MA = 25
39482
Ha = 191
418 n
mi
Hp = 182
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17095365
97 X = 5158699
83
Y = 13138862
81 feet Y = 4062703
31 meter
Z = 4591800
34 Z = 1424768
70
XDOT = -6594
870898 XDOT = -2033
817547
YDOT = 15273
287548 feet/sec YDOT = 4632
688219 meter/sec
ZDOT = -19049
548284 ZDOT = -5816
124266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10010557
16 X = 3051217
82
Y = -19072256
48 feet Y = -5813223
77 meter
Z = 4690806
16 Z = 1429757
72
XDOT = 14769
194673 XDOT = 4501
650536
YDOT = 3033
225115 feet/sec YDOT = 924
527015 meter/sec
ZDOT = -19087
815856 ZDOT = -5817
966273
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 09183
53455379
00010596 00000-0 82463-4 0 9013
2 25544 51
6397 228
1057 0007643 177
1499 182
9709 15
74144713 8377
Satellite: ISS
Catalog Number: 25544
Epoch time: 09183
53455379 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 228
1057 deg
Eccentricity:
0007643
Arg of perigee: 177
1499 deg
Mean anomaly: 182
9709 deg
Mean motion: 15
74144713 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 837
Checksum: 340
Coasting Arc #3 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2009/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1436047
93 A = 6720558
48 meter
Y = -4165821
87 meter E =
0011262
Z = 5073454
29 I = 51
39643
XDOT = 6343
649874 Wp = 159
65439
YDOT = 4085
040393 meter/sec RA = 222
20264 deg
ZDOT = 1547
218122 TA = 275
38620
MA = 275
51467
Ha = 191
401 n
mi
Hp = 182
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4711443
35 X = 1457878
19
Y = -13667394
59 feet Y = -4149642
03 meter
Z = 16645191
23 Z = 5080482
86
XDOT = 20812
499587 XDOT = 6289
982672
YDOT = 13402
363493 feet/sec YDOT = 4155
678435 meter/sec
ZDOT = 5076
174940 ZDOT = 1577
906010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14292454
87 X = -4356340
25
Y = -1951961
36 feet Y = -594957
82 meter
Z = 16672532
65 Z = 5081787
95
XDOT = 9096
356352 XDOT = 2772
569416
YDOT = -21896
634099 feet/sec YDOT = -6674
094073 meter/sec
ZDOT = 5196
769200 ZDOT = 1583
975252
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 09184
55030636
00010596 00000-0 82463-4 0 9022
2 25544 51
6389 222
8886 0007677 180
3851 179
7308 15
74131210 8539
Satellite: ISS
Catalog Number: 25544
Epoch time: 09184
55030636 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 222
8886 deg
Eccentricity:
0007677
Arg of perigee: 180
3851 deg
Mean anomaly: 179
7308 deg
Mean motion: 15
74131210 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 853
Checksum: 321
Coasting Arc #4 (Orbit 867)
---------------------------------------
Vector Time (GMT): 2009/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5830485
37 A = 6731014
23 meter
Y = -3107458
63 meter E =
0004880
Z = -1292841
83 I = 51
45519
XDOT = 1293
409790 Wp = 96
67092
YDOT = -4846
458788 meter/sec RA = 217
02526 deg
ZDOT = 5834
112056 TA = 249
11556
MA = 249
16781
Ha = 191
286 n
mi
Hp = 183
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19128889
00 X = -5789023
53
Y = -10195074
23 feet Y = -3172426
44 meter
Z = -4241607
06 Z = -1321066
17
XDOT = 4243
470439 XDOT = 1319
166602
YDOT = -15900
455342 feet/sec YDOT = -4831
852265 meter/sec
ZDOT = 19140
787586 ZDOT = 5840
457030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6049160
67 X = -1843784
17
Y = 20792031
43 feet Y = 6337411
18 meter
Z = -4352499
00 Z = -1326641
70
XDOT = -14893
829566 XDOT = -4539
639252
YDOT = -333
396091 feet/sec YDOT = -101
619129 meter/sec
ZDOT = 19165
412375 ZDOT = 5841
617692
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 09185
50257442
00010596 00000-0 82463-4 0 9035
2 25544 51
6393 217
9973 0007621 184
0064 176
1039 15
74136452 8683
Satellite: ISS
Catalog Number: 25544
Epoch time: 09185
50257442 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 217
9973 deg
Eccentricity:
0007621
Arg of perigee: 184
0064 deg
Mean anomaly: 176
1039 deg
Mean motion: 15
74136452 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 868
Checksum: 318
Coasting Arc #5 (Orbit 883)
---------------------------------------
Vector Time (GMT): 2009/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -836277
55 A = 6720458
26 meter
Y = 4285196
81 meter E =
0013574
Z = -5118887
64 I = 51
44383
XDOT = -6940
455480 Wp = 111
40931
YDOT = -3010
830525 meter/sec RA = 211
89943 deg
ZDOT = -1394
436033 TA = 145
23220
MA = 145
14342
Ha = 191
168 n
mi
Hp = 183
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2743692
77 X = -859266
73
Y = 14059044
65 feet Y = 4275717
56 meter
Z = -16794250
79 Z = -5123005
23
XDOT = -22770
523227 XDOT = -6899
498157
YDOT = -9878
052905 feet/sec YDOT = -3088
213471 meter/sec
ZDOT = -4574
921368 ZDOT = -1428
053678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14295111
74 X = 4357150
06
Y = -547216
54 feet Y = -166791
60 meter
Z = -16810168
96 Z = -5123739
50
XDOT = -4611
906731 XDOT = -1405
709172
YDOT = 23328
543189 feet/sec YDOT = 7110
539964 meter/sec
ZDOT = -4706
984011 ZDOT = -1434
688727
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 09186
51832632
00010596 00000-0 82463-4 0 9048
2 25544 51
6393 212
7795 0007598 188
1265 171
9777 15
74111609 8846
Satellite: ISS
Catalog Number: 25544
Epoch time: 09186
51832632 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 212
7795 deg
Eccentricity:
0007598
Arg of perigee: 188
1265 deg
Mean anomaly: 171
9777 deg
Mean motion: 15
74111609 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 884
Checksum: 344
Coasting Arc #6 (Orbit 899)
---------------------------------------
Vector Time (GMT): 2009/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6268711
38 A = 6731211
77 meter
Y = 2127101
88 meter E =
0017997
Z = 1156236
83 I = 51
50483
XDOT = -586
739821 Wp = 145
20668
YDOT = 4944
187588 meter/sec RA = 206
72792 deg
ZDOT = -5884
334564 TA = 22
09373
MA = 22
01626
Ha = 191
005 n
mi
Hp = 183
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20566638
39 X = 6238843
13
Y = 6978680
69 feet Y = 2197035
04 meter
Z = 3793427
93 Z = 1186617
80
XDOT = -1924
999412 XDOT = -613
398228
YDOT = 16221
087888 feet/sec YDOT = 4937
478427 meter/sec
ZDOT = -19305
559593 ZDOT = -5887
248694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1862854
84 X = 567798
16
Y = -21617094
46 feet Y = -6588890
39 meter
Z = 3912760
29 Z = 1192609
34
XDOT = 14607
208787 XDOT = 4452
277238
YDOT = -2255
037306 feet/sec YDOT = -687
335371 meter/sec
ZDOT = -19316
717977 ZDOT = -5887
735640
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 09187
53407813
00010596 00000-0 82463-4 0 9051
2 25544 51
6379 207
5619 0007490 191
0279 169
0721 15
74123877 9002
Satellite: ISS
Catalog Number: 25544
Epoch time: 09187
53407813 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 207
5619 deg
Eccentricity:
0007490
Arg of perigee: 191
0279 deg
Mean anomaly: 169
0721 deg
Mean motion: 15
74123877 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 900
Checksum: 323
Coasting Arc #7 (Orbit 915)
---------------------------------------
Vector Time (GMT): 2009/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 187483
00 A = 6720320
16 meter
Y = -4324803
38 meter E =
0009754
Z = 5140868
97 I = 51
49453
XDOT = 7371
150935 Wp = 171
06673
YDOT = 1835
822450 meter/sec RA = 201
60339 deg
ZDOT = 1265
778161 TA = 266
75295
MA = 266
86455
Ha = 190
917 n
mi
Hp = 183
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 615101
72 X = 210856
69
Y = -14188987
46 feet Y = -4322577
11 meter
Z = 16866368
00 Z = 5141835
71
XDOT = 24183
566061 XDOT = 7343
925781
YDOT = 6023
039534 feet/sec YDOT = 1918
098509 meter/sec
ZDOT = 4152
815490 ZDOT = 1301
520942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13848795
11 X = -4221112
75
Y = 3129995
87 feet Y = 954022
74 meter
Z = 16869916
56 Z = 5141950
57
XDOT = -129
612819 XDOT = -39
505987
YDOT = -23886
077334 feet/sec YDOT = -7280
476372 meter/sec
ZDOT = 4293
191179 ZDOT = 1308
564671
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 09188
54982962
00010596 00000-0 82463-4 0 9067
2 25544 51
6372 202
3439 0007412 195
1590 164
9352 15
74122066 9163
Satellite: ISS
Catalog Number: 25544
Epoch time: 09188
54982962 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 202
3439 deg
Eccentricity:
0007412
Arg of perigee: 195
1590 deg
Mean anomaly: 164
9352 deg
Mean motion: 15
74122066 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 916
Checksum: 320
Coasting Arc #8 (Orbit 930)
---------------------------------------
Vector Time (GMT): 2009/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6562815
06 A = 6731169
51 meter
Y = -1070763
73 meter E =
0003535
Z = -1045943
87 I = 51
56054
XDOT = -134
631578 Wp = 82
93198
YDOT = -4928
740707 meter/sec RA = 196
43840 deg
ZDOT = 5907
906198 TA = 265
62579
MA = 265
66619
Ha = 190
736 n
mi
Hp = 183
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21531545
48 X = -6545272
91
Y = -3513004
37 feet Y = -1144054
70 meter
Z = -3431574
37 Z = -1077783
09
XDOT = -441
704652 XDOT = -108
206627
YDOT = -16170
409144 feet/sec YDOT = -4930
099510 meter/sec
ZDOT = 19382
894352 ZDOT = 5907
315500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2479856
93 X = 755860
39
Y = 21654681
50 feet Y = 6600346
92 meter
Z = -3556603
96 Z = -1084052
89
XDOT = -13828
387552 XDOT = -4214
892526
YDOT = 4757
581051 feet/sec YDOT = 1450
110704 meter/sec
ZDOT = 19380
291425 ZDOT = 5907
112826
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 09189
50209644
00010596 00000-0 82463-4 0 9074
2 25544 51
6378 197
4531 0007507 198
6194 161
4696 15
74171424 9311
Satellite: ISS
Catalog Number: 25544
Epoch time: 09189
50209644 = yrday
fracday
Element set: 907
Inclination: 51
6378 deg
RA of node: 197
4531 deg
Eccentricity:
0007507
Arg of perigee: 198
6194 deg
Mean anomaly: 161
4696 deg
Mean motion: 15
74171424 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 931
Checksum: 335
Coasting Arc #9 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2009/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 409758
41 A = 6720222
22 meter
Y = 4274739
17 meter E =
0012104
Z = -5178020
45 I = 51
55107
XDOT = -7587
570959 Wp = 112
27098
YDOT = -615
370047 meter/sec RA = 191
31518 deg
ZDOT = -1115
035849 TA = 147
10239
MA = 147
02699
Ha = 190
595 n
mi
Hp = 184
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1344351
74 X = 387080
55
Y = 14024734
79 feet Y = 4279195
33 meter
Z = -16988256
08 Z = -5176084
30
XDOT = -24893
605510 XDOT = -7574
709314
YDOT = -2018
930601 feet/sec YDOT = -700
146619 meter/sec
ZDOT = -3658
254097 ZDOT = -1151
864500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13009350
45 X = 3965250
02
Y = -5433595
45 feet Y = -1656159
89 meter
Z = -16980404
99 Z = -5175627
44
XDOT = 4857
102958 XDOT = 1480
444982
YDOT = 23445
836952 feet/sec YDOT = 7146
291103 meter/sec
ZDOT = -3802
857930 ZDOT = -1159
111097
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 09190
51784799
00010596 00000-0 82463-4 0 9087
2 25544 51
6370 192
2347 0007342 203
7648 156
3177 15
74111910 9478
Satellite: ISS
Catalog Number: 25544
Epoch time: 09190
51784799 = yrday
fracday
Element set: 908
Inclination: 51
6370 deg
RA of node: 192
2347 deg
Eccentricity:
0007342
Arg of perigee: 203
7648 deg
Mean anomaly: 156
3177 deg
Mean motion: 15
74111910 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 947
Checksum: 325
Coasting Arc #10 (Orbit 962)
---------------------------------------
Vector Time (GMT): 2009/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6658745
52 A = 6731414
91 meter
Y = -9307
17 meter E =
0016217
Z = 913175
88 I = 51
61828
XDOT = 826
700021 Wp = 151
26652
YDOT = 4828
867975 meter/sec RA = 186
15591 deg
ZDOT = -5949
433398 TA = 18
75232
MA = 18
69265
Ha = 190
356 n
mi
Hp = 184
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21846277
97 X = 6653918
74
Y = -30535
35 feet Y = 65127
70 meter
Z = 2995983
84 Z = 945511
81
XDOT = 2712
270409 XDOT = 801
542149
YDOT = 15842
742700 feet/sec YDOT = 4837
972752 meter/sec
ZDOT = -19519
138446 ZDOT = -5945
477814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6694438
75 X = -2040464
93
Y = -20776634
04 feet Y = -6332718
05 meter
Z = 3122928
21 Z = 951868
52
XDOT = 12707
857222 XDOT = 3873
354881
YDOT = -7040
104332 feet/sec YDOT = -2145
823800 meter/sec
ZDOT = -19503
321590 ZDOT = -5944
612421
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 09191
53359957
00010596 00000-0 82463-4 0 9095
2 25544 51
6367 187
0167 0007172 207
8234 152
2546 15
74131149 9632
Satellite: ISS
Catalog Number: 25544
Epoch time: 09191
53359957 = yrday
fracday
Element set: 909
Inclination: 51
6367 deg
RA of node: 187
0167 deg
Eccentricity:
0007172
Arg of perigee: 207
8234 deg
Mean anomaly: 152
2546 deg
Mean motion: 15
74131149 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 963
Checksum: 327
Coasting Arc #11 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2009/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1027712
97 A = 6720133
86 meter
Y = -4136960
50 meter E =
0008106
Z = 5197020
78 I = 51
60941
XDOT = 7609
525550 Wp = 186
02112
YDOT = -643
118224 meter/sec RA = 181
03519 deg
ZDOT = 985
066591 TA = 254
54019
MA = 254
62973
Ha = 190
286 n
mi
Hp = 184
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3371761
72 X = -1006622
22
Y = -13572705
05 feet Y = -4148335
66 meter
Z = 17050593
11 Z = 5192078
97
XDOT = 24965
635008 XDOT = 7611
366245
YDOT = -2109
967927 feet/sec YDOT = -558
013877 meter/sec
ZDOT = 3231
845770 ZDOT = 1022
037539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11734449
55 X = -3576660
22
Y = 7652422
15 feet Y = 2332458
27 meter
Z = 17030941
07 Z = 5191030
84
XDOT = -9464
711320 XDOT = -2884
844010
YDOT = -22085
989630 feet/sec YDOT = -6731
809639 meter/sec
ZDOT = 3376
961131 ZDOT = 1029
297753
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 09192
54935142
00010596 00000-0 82463-4 0 9105
2 25544 51
6364 181
7989 0007190 212
7050 147
3669 15
74111287 9792
Satellite: ISS
Catalog Number: 25544
Epoch time: 09192
54935142 = yrday
fracday
Element set: 910
Inclination: 51
6364 deg
RA of node: 181
7989 deg
Eccentricity:
0007190
Arg of perigee: 212
7050 deg
Mean anomaly: 147
3669 deg
Mean motion: 15
74111287 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 979
Checksum: 327
Coasting Arc #12 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2009/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6589881
67 A = 6731424
64 meter
Y = 1108738
28 meter E =
0003142
Z = -800595
21 I = 51
67792
XDOT = -1500
608415 Wp = 48
82684
YDOT = -4621
614708 meter/sec RA = 175
88305 deg
ZDOT = 5968
561876 TA = 302
45215
MA = 302
48253
Ha = 190
093 n
mi
Hp = 184
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21620346
70 X = -6597900
89
Y = 3637592
78 feet Y = 1035001
61 meter
Z = -2626624
71 Z = -832627
88
XDOT = -4923
255956 XDOT = -1477
811080
YDOT = -15162
777913 feet/sec YDOT = -4638
268530 meter/sec
ZDOT = 19581
895917 ZDOT = 5961
326903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10724389
40 X = 3268793
89
Y = 19104522
11 feet Y = 5823058
34 meter
Z = -2752332
99 Z = -838911
10
XDOT = -11175
192522 XDOT = -3406
198681
YDOT = 9082
470073 feet/sec YDOT = 2768
336878 meter/sec
ZDOT = 19553
206903 ZDOT = 5959
817464
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 09193
50161815
00010596 00000-0 82463-4 0 9111
2 25544 51
6365 176
9079 0007207 214
9860 145
0830 15
74154175 9946
Satellite: ISS
Catalog Number: 25544
Epoch time: 09193
50161815 = yrday
fracday
Element set: 911
Inclination: 51
6365 deg
RA of node: 176
9079 deg
Eccentricity:
0007207
Arg of perigee: 214
9860 deg
Mean anomaly: 145
0830 deg
Mean motion: 15
74154175 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 994
Checksum: 317
Coasting Arc #13 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2009/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1581524
73 A = 6720036
03 meter
Y = 3928665
76 meter E =
0010595
Z = -5225641
49 I = 51
66886
XDOT = -7414
828566 Wp = 110
58845
YDOT = 1876
996095 meter/sec RA = 170
76360 deg
ZDOT = -837
957795 TA = 151
46043
MA = 151
40238
Ha = 189
919 n
mi
Hp = 185
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5188729
44 X = 1562861
23
Y = 12889323
34 feet Y = 3946247
44 meter
Z = -17144493
09 Z = -5218003
45
XDOT = -24326
865374 XDOT = -7431
195750
YDOT = 6158
123670 feet/sec YDOT = 1793
987707 meter/sec
ZDOT = -2749
205364 ZDOT = -874
018365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10181656
65 X = 3103368
95
Y = -9509318
84 feet Y = -2898440
38 meter
Z = -17114261
18 Z = -5216426
81
XDOT = 13673
265110 XDOT = 4167
611205
YDOT = 19812
807606 feet/sec YDOT = 6038
943758 meter/sec
ZDOT = -2890
692771 ZDOT = -881
083157
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 09194
51736999
00010596 00000-0 82463-4 0 9125
2 25544 51
6367 171
6895 0007086 220
5975 139
4661 15
74111658 10109
Satellite: ISS
Catalog Number: 25544
Epoch time: 09194
51736999 = yrday
fracday
Element set: 912
Inclination: 51
6367 deg
RA of node: 171
6895 deg
Eccentricity:
0007086
Arg of perigee: 220
5975 deg
Mean anomaly: 139
4661 deg
Mean motion: 15
74111658 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1010
Checksum: 334
Coasting Arc #14 (Orbit 1025)
---------------------------------------
Vector Time (GMT): 2009/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6327110
85 A = 6731590
53 meter
Y = -2169439
55 meter E =
0014222
Z = 671851
30 I = 51
73758
XDOT = 2128
435609 Wp = 157
18579
YDOT = 4340
085296 meter/sec RA = 165
61793 deg
ZDOT = -6000
783035 TA = 15
50142
MA = 15
45791
Ha = 189
643 n
mi
Hp = 185
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20758237
71 X = 6347635
93
Y = -7117583
83 feet Y = -2098571
40 meter
Z = 2204236
54 Z = 702637
96
XDOT = 6983
056459 XDOT = 2108
896482
YDOT = 14239
124988 feet/sec YDOT = 4363
778060 meter/sec
ZDOT = -19687
608382 ZDOT = -5990
490149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14289925
77 X = -4355569
37
Y = -16637772
02 feet Y = -5071192
91 meter
Z = 2325006
40 Z = 708661
95
XDOT = 9387
698514 XDOT = 2861
370507
YDOT = -10821
182993 feet/sec YDOT = -3298
296576 meter/sec
ZDOT = -19646
924933 ZDOT = -5988
382720
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 09195
53312128
00010596 00000-0 82463-4 0 9133
2 25544 51
6369 166
4721 0007015 225
8534 134
2053 15
74130746 10266
Satellite: ISS
Catalog Number: 25544
Epoch time: 09195
53312128 = yrday
fracday
Element set: 913
Inclination: 51
6369 deg
RA of node: 166
4721 deg
Eccentricity:
0007015
Arg of perigee: 225
8534 deg
Mean anomaly: 134
2053 deg
Mean motion: 15
74130746 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1026
Checksum: 289
Coasting Arc #15 (Orbit 1041)
---------------------------------------
Vector Time (GMT): 2009/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2124545
35 A = 6719932
26 meter
Y = -3634288
70 meter E =
0006583
Z = 5240837
64 I = 51
72673
XDOT = 7021
694281 Wp = 204
30026
YDOT = -3077
730742 meter/sec RA = 160
50167 deg
ZDOT = 706
632900 TA = 238
95365
MA = 239
01829
Ha = 189
548 n
mi
Hp = 185
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6970293
14 X = -2109207
26
Y = -11923519
34 feet Y = -3657961
43 meter
Z = 17194349
20 Z = 5230553
44
XDOT = 23037
054729 XDOT = 7052
155426
YDOT = -10097
541803 feet/sec YDOT = -2999
039807 meter/sec
ZDOT = 2318
349408 ZDOT = 740
817954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8269754
32 X = -2520621
12
Y = 11124802
88 feet Y = 3390839
92 meter
Z = 17153742
12 Z = 5228460
60
XDOT = -17391
155308 XDOT = -5300
824138
YDOT = -16737
653461 feet/sec YDOT = -5101
636775 meter/sec
ZDOT = 2452
423110 ZDOT = 747
498564
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 09196
54887292
00010596 00000-0 82463-4 0 9145
2 25544 51
6369 161
2551 0007056 230
2861 129
7681 15
74123426 10429
Satellite: ISS
Catalog Number: 25544
Epoch time: 09196
54887292 = yrday
fracday
Element set: 914
Inclination: 51
6369 deg
RA of node: 161
2551 deg
Eccentricity:
0007056
Arg of perigee: 230
2861 deg
Mean anomaly: 129
7681 deg
Mean motion: 15
74123426 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1042
Checksum: 314
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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