Date:
June 28th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 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 741)
---------------------------------------
Vector Time (GMT): 2009/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2607367
25 A = 6731043
22 meter
Y = -5979252
36 meter E =
0008090
Z = -1670475
95 I = 51
33084
XDOT = 3967
158519 Wp = 98
58760
YDOT = -3315
104750 meter/sec RA = 258
26546 deg
ZDOT = 5696
173972 TA = 242
88589
MA = 242
96843
Ha = 192
393 n
mi
Hp = 182
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8554354
48 X = -2532197
69
Y = -19616969
68 feet Y = -6007988
92 meter
Z = -5480564
15 Z = -1682960
67
XDOT = 13015
611939 XDOT = 3976
263136
YDOT = -10876
327921 feet/sec YDOT = -3270
691602 meter/sec
ZDOT = 18688
234817 ZDOT = 5715
467790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18978081
89 X = -5784519
36
Y = 9863702
03 feet Y = 3006456
38 meter
Z = -5529814
96 Z = -1685487
60
XDOT = -11026
525144 XDOT = -3360
884864
YDOT = -10736
748123 feet/sec YDOT = -3272
560828 meter/sec
ZDOT = 18763
710279 ZDOT = 5719
178893
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 09177
50329257
00010596 00000-0 82463-4 0 9007
2 25544 51
6408 259
0793 0008034 156
0578 204
0960 15
73961083 7425
Satellite: ISS
Catalog Number: 25544
Epoch time: 09177
50329257 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 259
0793 deg
Eccentricity:
0008034
Arg of perigee: 156
0578 deg
Mean anomaly: 204
0960 deg
Mean motion: 15
73961083 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 742
Checksum: 312
Coasting Arc #2 (Orbit 757)
---------------------------------------
Vector Time (GMT): 2009/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3224737
62 A = 6721279
59 meter
Y = 3154193
40 meter E =
0016181
Z = -4994896
73 I = 51
30445
XDOT = -3548
812632 Wp = 105
93485
YDOT = -6563
570850 meter/sec RA = 253
13779 deg
ZDOT = -1863
029151 TA = 146
03470
MA = 145
93100
Ha = 192
235 n
mi
Hp = 182
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10579847
83 X = -3235504
62
Y = 10348403
53 feet Y = 3118072
94 meter
Z = -16387456
48 Z = -5010588
09
XDOT = -11643
086062 XDOT = -3466
103748
YDOT = -21534
025097 feet/sec YDOT = -6602
793057 meter/sec
ZDOT = -6112
300363 ZDOT = -1880
069056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11216940
09 X = 3418923
34
Y = 9549247
32 feet Y = 2910610
58 meter
Z = -16448814
43 Z = -5013598
64
XDOT = -19752
052421 XDOT = -6020
425578
YDOT = 12610
131212 feet/sec YDOT = 3843
567993 meter/sec
ZDOT = -6179
453293 ZDOT = -1883
497364
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 09178
51912051
00010596 00000-0 82463-4 0 9010
2 25544 51
6398 253
8623 0008105 160
1699 199
9780 15
73996256 7585
Satellite: ISS
Catalog Number: 25544
Epoch time: 09178
51912051 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 253
8623 deg
Eccentricity:
0008105
Arg of perigee: 160
1699 deg
Mean anomaly: 199
9780 deg
Mean motion: 15
73996256 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 758
Checksum: 345
Coasting Arc #3 (Orbit 773)
---------------------------------------
Vector Time (GMT): 2009/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3584623
62 A = 6730905
41 meter
Y = 5454746
98 meter E =
0020478
Z = 1593570
67 I = 51
34741
XDOT = -3368
989320 Wp = 133
06504
YDOT = 3898
671056 meter/sec RA = 247
94904 deg
ZDOT = -5734
269152 TA = 29
25464
MA = 29
14012
Ha = 192
039 n
mi
Hp = 182
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11760576
18 X = 3515620
06
Y = 17896151
50 feet Y = 5494446
32 meter
Z = 5228250
23 Z = 1610817
72
XDOT = -11053
114568 XDOT = -3384
478661
YDOT = 12790
915539 feet/sec YDOT = 3860
911138 meter/sec
ZDOT = -18813
219003 ZDOT = -5750
672755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16583395
59 X = 5054618
98
Y = -13522559
03 feet Y = -4121675
99 meter
Z = 5296166
45 Z = 1614271
53
XDOT = 12870
376789 XDOT = 3922
890845
YDOT = 8349
020621 feet/sec YDOT = 2544
781485 meter/sec
ZDOT = -18877
328837 ZDOT = -5753
809829
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 09179
53493290
00010596 00000-0 82463-4 0 9023
2 25544 51
6399 248
6453 0007976 162
5748 197
5691 15
74050708 7742
Satellite: ISS
Catalog Number: 25544
Epoch time: 09179
53493290 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 248
6453 deg
Eccentricity:
0007976
Arg of perigee: 162
5748 deg
Mean anomaly: 197
5691 deg
Mean motion: 15
74050708 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 774
Checksum: 355
Coasting Arc #4 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2009/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2642220
03 A = 6720979
12 meter
Y = -3622787
58 meter E =
0012581
Z = 5004115
76 I = 51
32654
XDOT = 4637
461999 Wp = 150
17732
YDOT = 5882
406682 meter/sec RA = 242
82142 deg
ZDOT = 1797
305605 TA = 282
36362
MA = 282
50441
Ha = 191
884 n
mi
Hp = 182
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8668700
88 X = 2658225
24
Y = -11885786
03 feet Y = -3593151
86 meter
Z = 16417702
63 Z = 5016990
07
XDOT = 15214
770338 XDOT = 4562
608293
YDOT = 19299
234521 feet/sec YDOT = 5933
846742 meter/sec
ZDOT = 5896
671933 ZDOT = 1819
653266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12834032
12 X = -3911812
99
Y = -7074758
67 feet Y = -2156386
44 meter
Z = 16467988
75 Z = 5019442
97
XDOT = 16808
501221 XDOT = 5123
231172
YDOT = -16464
412384 feet/sec YDOT = -5018
352895 meter/sec
ZDOT = 5984
618351 ZDOT = 1824
111673
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 09180
55072927
00010596 00000-0 82463-4 0 9038
2 25544 51
6399 243
4280 0007947 167
1954 192
9413 15
74078874 7904
Satellite: ISS
Catalog Number: 25544
Epoch time: 09180
55072927 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 243
4280 deg
Eccentricity:
0007947
Arg of perigee: 167
1954 deg
Mean anomaly: 192
9413 deg
Mean motion: 15
74078874 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 790
Checksum: 342
Coasting Arc #5 (Orbit 804)
---------------------------------------
Vector Time (GMT): 2009/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4479774
73 A = 6730946
72 meter
Y = -4788590
42 meter E =
0006402
Z = -1527449
38 I = 51
37424
XDOT = 2688
523962 Wp = 100
25800
YDOT = -4343
796024 meter/sec RA = 237
63493 deg
ZDOT = 5752
202912 TA = 242
86078
MA = 242
92608
Ha = 191
822 n
mi
Hp = 182
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14697423
66 X = -4418474
87
Y = -15710598
48 feet Y = -4838342
92 meter
Z = -5011316
87 Z = -1549063
91
XDOT = 8820
616674 XDOT = 2708
954014
YDOT = -14251
299290 feet/sec YDOT = -4313
617925 meter/sec
ZDOT = 18872
056798 ZDOT = 5765
312817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13538743
24 X = -4126608
94
Y = 16693719
04 feet Y = 5088245
56 meter
Z = -5096335
90 Z = -1553363
18
XDOT = -14098
363885 XDOT = -4297
181312
YDOT = -5675
952315 feet/sec YDOT = -1730
030266 meter/sec
ZDOT = 18923
229028 ZDOT = 5767
800208
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 09181
50302643
00010596 00000-0 82463-4 0 9046
2 25544 51
6394 238
5368 0007740 169
9758 190
1561 15
74060388 8056
Satellite: ISS
Catalog Number: 25544
Epoch time: 09181
50302643 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 238
5368 deg
Eccentricity:
0007740
Arg of perigee: 169
9758 deg
Mean anomaly: 190
1561 deg
Mean motion: 15
74060388 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 805
Checksum: 322
Coasting Arc #6 (Orbit 820)
---------------------------------------
Vector Time (GMT): 2009/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2068622
23 A = 6720795
96 meter
Y = 3936775
94 meter E =
0014895
Z = -5049952
88 I = 51
35743
XDOT = -5556
378362 Wp = 108
83886
YDOT = -5050
070739 meter/sec RA = 232
50723 deg
ZDOT = -1669
548277 TA = 145
07518
MA = 144
97737
Ha = 191
676 n
mi
Hp = 182
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6786818
33 X = -2087958
35
Y = 12915931
56 feet Y = 3913536
05 meter
Z = -16568086
87 Z = -5060048
65
XDOT = -18229
587802 XDOT = -5491
384262
YDOT = -16568
473553 feet/sec YDOT = -5111
841756 meter/sec
ZDOT = -5477
520594 ZDOT = -1696
384146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13795932
68 X = 4205000
28
Y = 4609562
72 feet Y = 1404994
72 meter
Z = -16607464
18 Z = -5061955
08
XDOT = -13214
408017 XDOT = -4027
751564
YDOT = 19537
789433 feet/sec YDOT = 5955
118219 meter/sec
ZDOT = -5583
036861 ZDOT = -1701
709635
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
51879537
00010596 00000-0 82463-4 0 9050
2 25544 51
6396 233
3190 0007806 173
3889 186
7378 15
74090202 8214
Satellite: ISS
Catalog Number: 25544
Epoch time: 09182
51879537 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 233
3190 deg
Eccentricity:
0007806
Arg of perigee: 173
3889 deg
Mean anomaly: 186
7378 deg
Mean motion: 15
74090202 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 821
Checksum: 334
Coasting Arc #7 (Orbit 836)
---------------------------------------
Vector Time (GMT): 2009/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5209943
70 A = 6730861
07 meter
Y = 4006609
14 meter E =
0019241
Z = 1396808
44 I = 51
41130
XDOT = -2013
037175 Wp = 138
84810
YDOT = 4652
943245 meter/sec RA = 227
32533 deg
ZDOT = -5807
185156 TA = 25
72808
MA = 25
63249
Ha = 191
413 n
mi
Hp = 182
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17092991
13 X = 5157968
44
Y = 13145043
11 feet Y = 4064578
93 meter
Z = 4582704
86 Z = 1421992
86
XDOT = -6604
452674 XDOT = -2036
707234
YDOT = 15265
561827 feet/sec YDOT = 4630
300932 meter/sec
ZDOT = -19052
444739 ZDOT = -5817
021219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10017044
36 X = 3053195
12
Y = -19071031
02 feet Y = -5812850
25 meter
Z = 4681696
92 Z = 1426981
22
XDOT = 14763
316746 XDOT = 4499
858944
YDOT = 3043
502140 feet/sec YDOT = 927
659452 meter/sec
ZDOT = -19090
767791 ZDOT = -5818
866023
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
53454838
00010596 00000-0 82463-4 0 9067
2 25544 51
6397 228
1018 0007616 176
5639 183
5577 15
74153309 8374
Satellite: ISS
Catalog Number: 25544
Epoch time: 09183
53454838 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 228
1018 deg
Eccentricity:
0007616
Arg of perigee: 176
5639 deg
Mean anomaly: 183
5577 deg
Mean motion: 15
74153309 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 837
Checksum: 341
Coasting Arc #8 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2009/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1445532
03 A = 6720460
03 meter
Y = -4159504
74 meter E =
0011243
Z = 5075733
26 I = 51
39651
XDOT = 6341
094076 Wp = 159
28693
YDOT = 4093
110938 meter/sec RA = 222
19878 deg
ZDOT = 1536
956391 TA = 275
85514
MA = 275
98329
Ha = 191
362 n
mi
Hp = 182
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4742559
17 X = 1467279
88
Y = -13646669
08 feet Y = -4143219
30 meter
Z = 16652668
19 Z = 5082807
71
XDOT = 20804
114422 XDOT = 6287
386667
YDOT = 13428
841661 feet/sec YDOT = 4163
720178 meter/sec
ZDOT = 5042
507844 ZDOT = 1567
631767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14277966
77 X = -4351924
27
Y = -1986386
74 feet Y = -605450
68 meter
Z = 16680189
89 Z = 5084121
88
XDOT = 9121
393409 XDOT = 2780
200711
YDOT = -21894
646172 feet/sec YDOT = -6673
488153 meter/sec
ZDOT = 5163
053472 ZDOT = 1573
698698
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
55028767
00010596 00000-0 82463-4 0 9079
2 25544 51
6389 222
8846 0007647 179
7780 180
3388 15
74161915 8536
Satellite: ISS
Catalog Number: 25544
Epoch time: 09184
55028767 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 222
8846 deg
Eccentricity:
0007647
Arg of perigee: 179
7780 deg
Mean anomaly: 180
3388 deg
Mean motion: 15
74161915 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 853
Checksum: 355
Coasting Arc #9 (Orbit 867)
---------------------------------------
Vector Time (GMT): 2009/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5825568
98 A = 6730891
32 meter
Y = -3125465
82 meter E =
0005002
Z = -1270534
36 I = 51
45538
XDOT = 1322
248187 Wp = 95
59115
YDOT = -4831
004660 meter/sec RA = 217
02138 deg
ZDOT = 5840
620493 TA = 250
44528
MA = 250
49930
Ha = 191
213 n
mi
Hp = 183
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19112759
13 X = -5784014
51
Y = -10254152
94 feet Y = -3190378
14 meter
Z = -4168419
81 Z = -1298734
59
XDOT = 4338
084602 XDOT = 1347
798428
YDOT = -15849
752821 feet/sec YDOT = -4816
076805 meter/sec
ZDOT = 19162
140725 ZDOT = 5847
105065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6110204
79 X = -1862390
42
Y = 20788810
14 feet Y = 6336429
33 meter
Z = -4279218
19 Z = -1304305
70
XDOT = -14863
873664 XDOT = -4530
508693
YDOT = -431
839663 feet/sec YDOT = -131
624729 meter/sec
ZDOT = 19187
313989 ZDOT = 5848
293304
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
50253013
00010596 00000-0 82463-4 0 9080
2 25544 51
6393 217
9931 0007587 183
3810 176
7304 15
74188601 8683
Satellite: ISS
Catalog Number: 25544
Epoch time: 09185
50253013 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 217
9931 deg
Eccentricity:
0007587
Arg of perigee: 183
3810 deg
Mean anomaly: 176
7304 deg
Mean motion: 15
74188601 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 868
Checksum: 323
Coasting Arc #10 (Orbit 883)
---------------------------------------
Vector Time (GMT): 2009/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -886817
99 A = 6720200
26 meter
Y = 4262924
66 meter E =
0013756
Z = -5128825
63 I = 51
44378
XDOT = -6932
471305 Wp = 111
34769
YDOT = -3051
268208 meter/sec RA = 211
89448 deg
ZDOT = -1345
254250 TA = 145
77481
MA = 145
68608
Ha = 191
063 n
mi
Hp = 183
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2909507
85 X = -909506
09
Y = 13985973
29 feet Y = 4252881
92 meter
Z = -16826855
74 Z = -5133188
02
XDOT = -22744
328428 XDOT = -6891
301309
YDOT = -10010
722467 feet/sec YDOT = -3128
560691 meter/sec
ZDOT = -4413
563813 ZDOT = -1378
832600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14260708
53 X = 4346663
96
Y = -369489
64 feet Y = -112620
44 meter
Z = -16843735
59 Z = -5133970
61
XDOT = -4733
907685 XDOT = -1442
895063
YDOT = 23335
936001 feet/sec YDOT = 7112
793293 meter/sec
ZDOT = -4545
474526 ZDOT = -1385
460636
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
51824072
00010596 00000-0 82463-4 0 9092
2 25544 51
6393 212
7751 0007566 187
4975 172
6076 15
74186104 8845
Satellite: ISS
Catalog Number: 25544
Epoch time: 09186
51824072 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 212
7751 deg
Eccentricity:
0007566
Arg of perigee: 187
4975 deg
Mean anomaly: 172
6076 deg
Mean motion: 15
74186104 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 884
Checksum: 337
Coasting Arc #11 (Orbit 899)
---------------------------------------
Vector Time (GMT): 2009/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6260938
72 A = 6731008
99 meter
Y = 2185971
59 meter E =
0018072
Z = 1085083
50 I = 51
50517
XDOT = -685
715882 Wp = 145
63190
YDOT = 4910
135013 meter/sec RA = 206
72335 deg
ZDOT = -5902
297478 TA = 22
46154
MA = 22
38252
Ha = 190
874 n
mi
Hp = 183
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20541137
54 X = 6230758
41
Y = 7171822
80 feet Y = 2255816
10 meter
Z = 3559985
23 Z = 1115425
95
XDOT = -2249
724021 XDOT = -711
898891
YDOT = 16109
366839 feet/sec YDOT = 4902
321705 meter/sec
ZDOT = -19364
493037 ZDOT = -5905
691280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2056162
04 X = 626718
19
Y = -21639842
33 feet Y = -6595823
94 meter
Z = 3679169
79 Z = 1121410
95
XDOT = 14574
648111 XDOT = 4442
352744
YDOT = -1927
450722 feet/sec YDOT = -587
486980 meter/sec
ZDOT = -19377
535536 ZDOT = -5906
272831
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
53393673
00010596 00000-0 82463-4 0 9105
2 25544 51
6379 207
5571 0007467 190
3651 169
7359 15
74220376 9005
Satellite: ISS
Catalog Number: 25544
Epoch time: 09187
53393673 = yrday
fracday
Element set: 910
Inclination: 51
6379 deg
RA of node: 207
5571 deg
Eccentricity:
0007467
Arg of perigee: 190
3651 deg
Mean anomaly: 169
7359 deg
Mean motion: 15
74220376 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 900
Checksum: 330
Coasting Arc #12 (Orbit 915)
---------------------------------------
Vector Time (GMT): 2009/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 319600
56 A = 6719877
03 meter
Y = -4290639
94 meter E =
0009552
Z = 5162237
07 I = 51
49428
XDOT = 7365
591235 Wp = 171
50104
YDOT = 1936
710593 meter/sec RA = 201
59639 deg
ZDOT = 1144
133342 TA = 267
50062
MA = 267
60998
Ha = 190
748 n
mi
Hp = 183
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1048558
28 X = 342478
61
Y = -14076902
70 feet Y = -4286939
03 meter
Z = 16936473
34 Z = 5163844
44
XDOT = 24165
325574 XDOT = 7337
829266
YDOT = 6354
037378 feet/sec YDOT = 2018
921501 meter/sec
ZDOT = 3753
718315 ZDOT = 1179
847829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13851222
91 X = -4221852
74
Y = 2682689
95 feet Y = 817683
90 meter
Z = 16942537
94 Z = 5164085
56
XDOT = 161
818075 XDOT = 49
322149
YDOT = -23955
185929 feet/sec YDOT = -7301
540671 meter/sec
ZDOT = 3893
988701 ZDOT = 1186
887756
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
54961781
00010596 00000-0 82463-4 0 9119
2 25544 51
6372 202
3387 0007395 194
4658 165
6295 15
74241960 9161
Satellite: ISS
Catalog Number: 25544
Epoch time: 09188
54961781 = yrday
fracday
Element set: 911
Inclination: 51
6372 deg
RA of node: 202
3387 deg
Eccentricity:
0007395
Arg of perigee: 194
4658 deg
Mean anomaly: 165
6295 deg
Mean motion: 15
74241960 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 916
Checksum: 340
Coasting Arc #13 (Orbit 930)
---------------------------------------
Vector Time (GMT): 2009/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6563230
19 A = 6730895
84 meter
Y = -1193518
16 meter E =
0003998
Z = -896952
41 I = 51
56104
XDOT = 80
890913 Wp = 80
29227
YDOT = -4891
599995 meter/sec RA = 196
43279 deg
ZDOT = 5940
135110 TA = 269
91227
MA = 269
95809
Ha = 190
539 n
mi
Hp = 183
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21532907
46 X = -6545039
12
Y = -3915742
00 feet Y = -1266810
17 meter
Z = -2942757
24 Z = -928792
09
XDOT = 265
390134 XDOT = 106
727972
YDOT = -16048
556415 feet/sec YDOT = -4890
551992 meter/sec
ZDOT = 19488
632252 ZDOT = 5940
589982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2093504
80 X = 638100
26
Y = 21768436
47 feet Y = 6635019
44 meter
Z = -3067795
74 Z = -935064
14
XDOT = -13895
301356 XDOT = -4235
287853
YDOT = 4072
809999 feet/sec YDOT = 1241
392488 meter/sec
ZDOT = 19490
135291 ZDOT = 5940
593237
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
50180528
00010596 00000-0 82463-4 0 9129
2 25544 51
6378 197
4473 0007503 197
9571 162
1329 15
74313514 9312
Satellite: ISS
Catalog Number: 25544
Epoch time: 09189
50180528 = yrday
fracday
Element set: 912
Inclination: 51
6378 deg
RA of node: 197
4473 deg
Eccentricity:
0007503
Arg of perigee: 197
9571 deg
Mean anomaly: 162
1329 deg
Mean motion: 15
74313514 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 931
Checksum: 321
Coasting Arc #14 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2009/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 155193
88 A = 6719600
89 meter
Y = 4250651
41 meter E =
0012633
Z = -5211316
63 I = 51
55064
XDOT = -7600
229657 Wp = 113
43361
YDOT = -801
445039 meter/sec RA = 191
30515 deg
ZDOT = -886
669794 TA = 148
14243
MA = 148
06596
Ha = 190
367 n
mi
Hp = 183
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 509166
26 X = 132966
03
Y = 13945706
73 feet Y = 4252263
41 meter
Z = -17097495
51 Z = -5210616
05
XDOT = -24935
136671 XDOT = -7586
395691
YDOT = -2629
412857 feet/sec YDOT = -886
357766 meter/sec
ZDOT = -2909
021633 ZDOT = -923
557607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13174812
62 X = 4015682
89
Y = -4611817
50 feet Y = -1405681
97 meter
Z = -17094495
93 Z = -5210402
36
XDOT = 4345
852900 XDOT = 1324
615964
YDOT = 23654
081965 feet/sec YDOT = 7209
764183 meter/sec
ZDOT = -3053
868638 ZDOT = -930
819161
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
51745774
00010596 00000-0 82463-4 0 9133
2 25544 51
6371 192
2283 0007344 203
0439 157
0393 15
74274838 9478
Satellite: ISS
Catalog Number: 25544
Epoch time: 09190
51745774 = yrday
fracday
Element set: 913
Inclination: 51
6371 deg
RA of node: 192
2283 deg
Eccentricity:
0007344
Arg of perigee: 203
0439 deg
Mean anomaly: 157
0393 deg
Mean motion: 15
74274838 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 947
Checksum: 321
Coasting Arc #15 (Orbit 962)
---------------------------------------
Vector Time (GMT): 2009/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6685746
00 A = 6731074
37 meter
Y = 198657
55 meter E =
0016362
Z = 654767
27 I = 51
61896
XDOT = 447
887876 Wp = 153
71605
YDOT = 4823
631394 meter/sec RA = 186
14887 deg
ZDOT = -5994
442278 TA = 19
14456
MA = 19
08314
Ha = 190
120 n
mi
Hp = 184
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21934862
19 X = 6679846
99
Y = 651763
62 feet Y = 273388
40 meter
Z = 2148186
59 Z = 687231
79
XDOT = 1469
448413 XDOT = 423
035356
YDOT = 15825
562317 feet/sec YDOT = 4828
501786 meter/sec
ZDOT = -19666
805374 ZDOT = -5992
326192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6073295
29 X = -1851140
41
Y = -21074016
95 feet Y = -6423360
37 meter
Z = 2275648
19 Z = 693617
57
XDOT = 13049
041234 XDOT = 3977
347768
YDOT = -5897
525778 feet/sec YDOT = -1797
565857 meter/sec
ZDOT = -19658
210360 ZDOT = -5991
822518
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
53309538
00010596 00000-0 82463-4 0 9141
2 25544 51
6368 187
0095 0007195 206
9041 153
1751 15
74315892 9631
Satellite: ISS
Catalog Number: 25544
Epoch time: 09191
53309538 = yrday
fracday
Element set: 914
Inclination: 51
6368 deg
RA of node: 187
0095 deg
Eccentricity:
0007195
Arg of perigee: 206
9041 deg
Mean anomaly: 153
1751 deg
Mean motion: 15
74315892 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 963
Checksum: 322
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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