Date:
September 9th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 3625)
---------------------------------------
Vector Time (GMT): 2010/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6472164
66 A = 6738824
23 meter
Y = 1538686
36 meter E =
0016065
Z = -1010058
72 I = 51
69883
XDOT = -1988
704170 Wp = 11
13223
YDOT = -4490
376558 meter/sec RA = 173
51392 deg
ZDOT = 5933
613451 TA = 337
84026
MA = 337
90962
Ha = 195
082 n
mi
Hp = 187
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21234136
03 X = -6483982
90
Y = 5048183
60 feet Y = 1466244
60 meter
Z = -3313840
93 Z = -1041528
81
XDOT = -6524
619980 XDOT = -1967
168146
YDOT = -14732
206554 feet/sec YDOT = -4512
494713 meter/sec
ZDOT = 19467
235733 ZDOT = 5924
005017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21794197
31 X = 6642871
34
Y = 731163
91 feet Y = 222858
76 meter
Z = -3439853
94 Z = -1048467
48
XDOT = 2568
825449 XDOT = 782
977997
YDOT = 14372
607976 feet/sec YDOT = 4380
770911 meter/sec
ZDOT = 19428
661752 ZDOT = 5921
856102
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 10249
50202464
00016717 00000-0 10270-3 0 9006
2 25544 51
6443 174
5581 0008694 339
8412 20
2406 15
71500402 36269
Satellite: ISS
Catalog Number: 25544
Epoch time: 10249
50202464 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 174
5581 deg
Eccentricity:
0008694
Arg of perigee: 339
8412 deg
Mean anomaly: 20
2406 deg
Mean motion: 15
71500402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3626
Checksum: 279
Coasting Arc #2 (Orbit 3641)
---------------------------------------
Vector Time (GMT): 2010/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3015506
44 A = 6728508
58 meter
Y = 3395424
03 meter E =
0015357
Z = -4977122
47 I = 51
69560
XDOT = -6768
914416 Wp = 40
82350
YDOT = 3023
310893 meter/sec RA = 168
42797 deg
ZDOT = -2030
714734 TA = 209
45924
MA = 209
54587
Ha = 195
205 n
mi
Hp = 187
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9893393
82 X = 3001491
73
Y = 11139842
63 feet Y = 3429066
47 meter
Z = -16329141
98 Z = -4962507
64
XDOT = -22207
724463 XDOT = -6792
353829
YDOT = 9918
998992 feet/sec YDOT = 2947
485610 meter/sec
ZDOT = -6662
449915 ZDOT = -2063
654889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6924263
80 X = -2110515
61
Y = -13264259
85 feet Y = -4042946
40 meter
Z = -16270531
46 Z = -4959257
99
XDOT = 22965
167981 XDOT = 6999
783201
YDOT = -3622
361332 feet/sec YDOT = -1104
095734 meter/sec
ZDOT = -6794
329611 ZDOT = -2070
911665
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 10250
51945794
00016717 00000-0 10270-3 0 9010
2 25544 51
6455 169
3528 0008645 344
1533 15
9358 15
71555147 36425
Satellite: ISS
Catalog Number: 25544
Epoch time: 10250
51945794 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 169
3528 deg
Eccentricity:
0008645
Arg of perigee: 344
1533 deg
Mean anomaly: 15
9358 deg
Mean motion: 15
71555147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3642
Checksum: 319
Coasting Arc #3 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2010/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5122976
96 A = 6736376
86 meter
Y = -3592010
09 meter E =
0012577
Z = 2494318
49 I = 51
75176
XDOT = 4689
863111 Wp = 66
67856
YDOT = 2973
469441 meter/sec RA = 163
27947 deg
ZDOT = -5324
256518 TA = 85
18727
MA = 85
04367
Ha = 195
277 n
mi
Hp = 187
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16807667
19 X = 5150645
86
Y = -11784810
01 feet Y = -3534566
94 meter
Z = 8183459
60 Z = 2519273
29
XDOT = 15386
689996 XDOT = 4682
128762
YDOT = 9755
477169 feet/sec YDOT = 3025
870541 meter/sec
ZDOT = -17468
033197 ZDOT = -5301
492405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19025076
69 X = -5798843
37
Y = 7601384
59 feet Y = 2316902
02 meter
Z = 8283347
39 Z = 2524764
29
XDOT = -12268
069287 XDOT = -3739
307519
YDOT = -11677
353284 feet/sec YDOT = -3559
257281 meter/sec
ZDOT = -17376
782990 ZDOT = -5296
443455
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 10251
53687584
00016717 00000-0 10270-3 0 9024
2 25544 51
6454 164
1475 0008630 347
5414 12
5533 15
71557543 36584
Satellite: ISS
Catalog Number: 25544
Epoch time: 10251
53687584 = yrday
fracday
Element set: 902
Inclination: 51
6454 deg
RA of node: 164
1475 deg
Eccentricity:
0008630
Arg of perigee: 347
5414 deg
Mean anomaly: 12
5533 deg
Mean motion: 15
71557543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 312
Coasting Arc #4 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2010/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4975274
20 A = 6731393
93 meter
Y = -1601798
66 meter E =
0010200
Z = 4230872
41 I = 51
76381
XDOT = 4670
832535 Wp = 56
10587
YDOT = -4939
808408 meter/sec RA = 158
21717 deg
ZDOT = 3621
816454 TA = 357
12117
MA = 357
12704
Ha = 195
507 n
mi
Hp = 187
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16323078
08 X = -4977545
62
Y = -5255244
94 feet Y = -1657447
44 meter
Z = 13880814
99 Z = 4206697
19
XDOT = 15324
253724 XDOT = 4708
129117
YDOT = -16206
720498 feet/sec YDOT = -4887
367463 meter/sec
ZDOT = 11882
599916 ZDOT = 3644
598415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14901605
51 X = 4542009
36
Y = 8641917
97 feet Y = 2634056
60 meter
Z = 13783936
64 Z = 4201343
89
XDOT = -17736
563834 XDOT = -5406
104657
YDOT = 11482
308198 feet/sec YDOT = 3499
807539 meter/sec
ZDOT = 11973
762122 ZDOT = 3649
602695
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 10252
55427770
00016717 00000-0 10270-3 0 9037
2 25544 51
6456 158
9418 0008673 351
4860 8
6153 15
71582820 36748
Satellite: ISS
Catalog Number: 25544
Epoch time: 10252
55427770 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 158
9418 deg
Eccentricity:
0008673
Arg of perigee: 351
4860 deg
Mean anomaly: 8
6153 deg
Mean motion: 15
71582820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 319
Coasting Arc #5 (Orbit 3688)
---------------------------------------
Vector Time (GMT): 2010/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2874913
58 A = 6732758
56 meter
Y = 4783887
31 meter E =
0008849
Z = -3763907
31 I = 51
79701
XDOT = -6393
403618 Wp = 35
84816
YDOT = -505
400554 meter/sec RA = 153
05969 deg
ZDOT = 4253
027249 TA = 278
79416
MA = 278
89436
Ha = 195
433 n
mi
Hp = 186
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9432131
17 X = -2909909
76
Y = 15695168
33 feet Y = 4751542
31 meter
Z = -12348777
25 Z = -3777959
11
XDOT = -20975
733655 XDOT = -6407
937492
YDOT = -1658
138300 feet/sec YDOT = -576
976333 meter/sec
ZDOT = 13953
501472 ZDOT = 4221
932701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12267806
09 X = 3739227
30
Y = -13543011
93 feet Y = -4127910
04 meter
Z = -12404977
58 Z = -3781037
17
XDOT = 19331
049090 XDOT = 5892
103763
YDOT = 4879
984003 feet/sec YDOT = 1487
419124 meter/sec
ZDOT = 13828
920620 ZDOT = 4215
055005
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 10253
50807703
00016717 00000-0 10270-3 0 9042
2 25544 51
6458 154
0616 0008732 354
6227 5
4840 15
71618019 36899
Satellite: ISS
Catalog Number: 25544
Epoch time: 10253
50807703 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 154
0616 deg
Eccentricity:
0008732
Arg of perigee: 354
6227 deg
Mean anomaly: 5
4840 deg
Mean motion: 15
71618019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3689
Checksum: 305
Coasting Arc #6 (Orbit 3704)
---------------------------------------
Vector Time (GMT): 2010/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5910649
56 A = 6734747
43 meter
Y = -777178
10 meter E =
0008601
Z = -3145516
63 I = 51
82998
XDOT = -1844
819135 Wp = 28
11127
YDOT = 5659
843638 meter/sec RA = 148
00496 deg
ZDOT = -4862
904642 TA = 188
30017
MA = 188
31441
Ha = 195
533 n
mi
Hp = 186
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19391894
87 X = 5934181
27
Y = -2549796
92 feet Y = -710950
30 meter
Z = -10319936
45 Z = -3116745
28
XDOT = -6052
556218 XDOT = -1884
348152
YDOT = 18569
040806 feet/sec YDOT = 5638
992438 meter/sec
ZDOT = -15954
411554 ZDOT = -4871
963211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19593892
14 X = -5972218
32
Y = -996017
95 feet Y = -303586
27 meter
Z = -10204679
23 Z = -3110386
23
XDOT = 9132
852329 XDOT = 2783
693390
YDOT = -15762
634146 feet/sec YDOT = -4804
450888 meter/sec
ZDOT = -15990
600944 ZDOT = -4873
935168
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 10254
52544768
00016717 00000-0 10270-3 0 9055
2 25544 51
6458 148
8558 0008718 357
5553 2
5565 15
71627664 37050
Satellite: ISS
Catalog Number: 25544
Epoch time: 10254
52544768 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 148
8558 deg
Eccentricity:
0008718
Arg of perigee: 357
5553 deg
Mean anomaly: 2
5565 deg
Mean motion: 15
71627664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3705
Checksum: 339
Coasting Arc #7 (Orbit 3720)
---------------------------------------
Vector Time (GMT): 2010/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 329646
43 A = 6729309
63 meter
Y = -4843439
04 meter E =
0014469
Z = 4659407
72 I = 51
83717
XDOT = 6764
099858 Wp = 30
79796
YDOT = -2305
386077 meter/sec RA = 142
85498 deg
ZDOT = -2858
925626 TA = 87
47616
MA = 87
31053
Ha = 195
569 n
mi
Hp = 186
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1081517
16 X = 361147
42
Y = -15890548
02 feet Y = -4839576
41 meter
Z = 15286770
72 Z = 4661085
87
XDOT = 22191
928667 XDOT = 6803
264631
YDOT = -7563
602615 feet/sec YDOT = -2229
526992 meter/sec
ZDOT = -9379
677251 ZDOT = -2825
970158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3570869
22 X = -1088400
94
Y = 15515313
16 feet Y = 4729067
45 meter
Z = 15293413
78 Z = 4661432
52
XDOT = -22051
940919 XDOT = -6721
431592
YDOT = 4092
061178 feet/sec YDOT = 1247
260247 meter/sec
ZDOT = -9247
669821 ZDOT = -2818
689761
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 10255
54280140
00016717 00000-0 10270-3 0 9060
2 25544 51
6453 143
6496 0008863 1
2616 358
8567 15
71698815 37216
Satellite: ISS
Catalog Number: 25544
Epoch time: 10255
54280140 = yrday
fracday
Element set: 906
Inclination: 51
6453 deg
RA of node: 143
6496 deg
Eccentricity:
0008863
Arg of perigee: 1
2616 deg
Mean anomaly: 358
8567 deg
Mean motion: 15
71698815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 320
Coasting Arc #8 (Orbit 3736)
---------------------------------------
Vector Time (GMT): 2010/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5632314
45 A = 6737458
60 meter
Y = 3204819
40 meter E =
0020058
Z = 1797790
92 I = 51
88766
XDOT = -1060
952806 Wp = 42
91189
YDOT = -5075
142947 meter/sec RA = 137
79025 deg
ZDOT = 5700
704725 TA = 336
95074
MA = 337
04061
Ha = 195
797 n
mi
Hp = 186
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18478721
93 X = -5676466
11
Y = 10514499
36 feet Y = 3141588
67 meter
Z = 5898264
18 Z = 1770321
66
XDOT = -3480
816292 XDOT = -1031
815922
YDOT = -16650
731452 feet/sec YDOT = -5086
844101 meter/sec
ZDOT = 18703
099493 ZDOT = 5695
621489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19851764
14 X = 6050817
71
Y = -7694877
36 feet Y = -2345398
62 meter
Z = 5788238
45 Z = 1764255
08
XDOT = 557
568569 XDOT = 169
946900
YDOT = 15548
735912 feet/sec YDOT = 4739
254706 meter/sec
ZDOT = 18682
652775 ZDOT = 5694
472566
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 10256
56014116
00016717 00000-0 10270-3 0 9072
2 25544 51
6454 138
4430 0008896 5
1776 354
9476 15
71675321 37373
Satellite: ISS
Catalog Number: 25544
Epoch time: 10256
56014116 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 138
4430 deg
Eccentricity:
0008896
Arg of perigee: 5
1776 deg
Mean anomaly: 354
9476 deg
Mean motion: 15
71675321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3737
Checksum: 319
Coasting Arc #9 (Orbit 3751)
---------------------------------------
Vector Time (GMT): 2010/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2067344
81 A = 6727061
38 meter
Y = 3765710
02 meter E =
0016653
Z = -5188766
49 I = 51
87489
XDOT = -5811
804620 Wp = 67
36194
YDOT = 4877
657356 meter/sec RA = 132
66272 deg
ZDOT = 1233
736278 TA = 214
35628
MA = 214
46408
Ha = 195
755 n
mi
Hp = 186
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6782627
33 X = 2050288
45
Y = 12354691
66 feet Y = 3788732
86 meter
Z = -17023512
10 Z = -5178764
79
XDOT = -19067
600458 XDOT = -5871
908817
YDOT = 16002
812847 feet/sec YDOT = 4812
330230 meter/sec
ZDOT = 4047
691200 ZDOT = 1205
356384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5230016
94 X = -1594109
16
Y = -13139795
75 feet Y = -4005009
75 meter
Z = -16983376
99 Z = -5176533
31
XDOT = 20040
268671 XDOT = 6108
273891
YDOT = -13021
467220 feet/sec YDOT = -3968
943209 meter/sec
ZDOT = 3934
023533 ZDOT = 1199
090373
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 10257
51388037
00016717 00000-0 10270-3 0 9085
2 25544 51
6453 133
5621 0008852 8
0121 352
1181 15
71726070 37526
Satellite: ISS
Catalog Number: 25544
Epoch time: 10257
51388037 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 133
5621 deg
Eccentricity:
0008852
Arg of perigee: 8
0121 deg
Mean anomaly: 352
1181 deg
Mean motion: 15
71726070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3752
Checksum: 285
Coasting Arc #10 (Orbit 3767)
---------------------------------------
Vector Time (GMT): 2010/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4325600
97 A = 6738677
98 meter
Y = -5154836
51 meter E =
0009556
Z = -363434
65 I = 51
93351
XDOT = 3432
650092 Wp = 90
26178
YDOT = 3296
770079 meter/sec RA = 127
57703 deg
ZDOT = -6040
882611 TA = 93
66602
MA = 93
55673
Ha = 195
818 n
mi
Hp = 186
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14191604
23 X = 4384687
31
Y = -16912193
26 feet Y = -5106134
68 meter
Z = -1192370
90 Z = -342277
30
XDOT = 11261
975368 XDOT = 3424
875368
YDOT = 10816
174800 feet/sec YDOT = 3335
112466 meter/sec
ZDOT = -19819
168671 ZDOT = -6024
225749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16004701
93 X = -4878233
15
Y = 15214082
77 feet Y = 4637252
43 meter
Z = -1107637
82 Z = -337608
01
XDOT = -8985
827803 XDOT = -2738
880314
YDOT = -10855
856798 feet/sec YDOT = -3308
865152 meter/sec
ZDOT = -19752
365287 ZDOT = -6020
520940
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 10258
53118853
00016717 00000-0 10270-3 0 9096
2 25544 51
6455 128
3560 0008684 11
8774 348
2591 15
71698351 37689
Satellite: ISS
Catalog Number: 25544
Epoch time: 10258
53118853 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 128
3560 deg
Eccentricity:
0008684
Arg of perigee: 11
8774 deg
Mean anomaly: 348
2591 deg
Mean motion: 15
71698351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3768
Checksum: 339
Coasting Arc #11 (Orbit 3783)
---------------------------------------
Vector Time (GMT): 2010/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3743564
94 A = 6726548
51 meter
Y = -1823150
37 meter E =
0009043
Z = 5278212
36 I = 51
91076
XDOT = 3841
001633 Wp = 32
52591
YDOT = -6662
086387 meter/sec RA = 122
47849 deg
ZDOT = 430
192756 TA = 53
44619
MA = 53
36298
Ha = 195
975 n
mi
Hp = 185
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12282037
21 X = -3748540
40
Y = -5981464
47 feet Y = -1865040
86 meter
Z = 17316969
70 Z = 5260014
16
XDOT = 12601
711394 XDOT = 3913
123047
YDOT = -21857
238802 feet/sec YDOT = -6618
730740 meter/sec
ZDOT = 1411
393555 ZDOT = 449
027591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11760451
74 X = 3584585
69
Y = 7130215
02 feet Y = 2173289
54 meter
Z = 17244001
96 Z = 5255971
80
XDOT = -14092
331607 XDOT = -4295
342674
YDOT = 19704
633505 feet/sec YDOT = 6005
972292 meter/sec
ZDOT = 1486
811504 ZDOT = 453
180146
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 10259
54847852
00016717 00000-0 10270-3 0 9108
2 25544 51
6454 123
1491 0008865 15
3945 344
7485 15
71759595 37843
Satellite: ISS
Catalog Number: 25544
Epoch time: 10259
54847852 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 123
1491 deg
Eccentricity:
0008865
Arg of perigee: 15
3945 deg
Mean anomaly: 344
7485 deg
Mean motion: 15
71759595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3784
Checksum: 345
Coasting Arc #12 (Orbit 3798)
---------------------------------------
Vector Time (GMT): 2010/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2252299
53 A = 6737962
43 meter
Y = 6242385
86 meter E =
0018135
Z = -1111119
91 I = 51
96394
XDOT = -4860
133577 Wp = 28
36418
YDOT = -707
288498 meter/sec RA = 117
36612 deg
ZDOT = 5932
951856 TA = 319
53344
MA = 319
66817
Ha = 195
931 n
mi
Hp = 185
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7389434
15 X = -2316538
06
Y = 20480268
56 feet Y = 6216840
08 meter
Z = -3645406
52 Z = -1122217
76
XDOT = -15945
320134 XDOT = -4880
684345
YDOT = -2320
500323 feet/sec YDOT = -761
752123 meter/sec
ZDOT = 19465
065144 ZDOT = 5909
291595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8939636
78 X = 2724801
29
Y = -19844450
54 feet Y = -6048588
53 meter
Z = -3689824
26 Z = -1124658
43
XDOT = 14384
091276 XDOT = 4384
271021
YDOT = 2911
218762 feet/sec YDOT = 887
339479 meter/sec
ZDOT = 19370
208907 ZDOT = 5904
039675
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 10260
50217355
00016717 00000-0 10270-3 0 9116
2 25544 51
6447 118
2676 0008940 17
9118 342
2357 15
71776596 37996
Satellite: ISS
Catalog Number: 25544
Epoch time: 10260
50217355 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 118
2676 deg
Eccentricity:
0008940
Arg of perigee: 17
9118 deg
Mean anomaly: 342
2357 deg
Mean motion: 15
71776596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 326
Coasting Arc #13 (Orbit 3814)
---------------------------------------
Vector Time (GMT): 2010/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4482731
16 A = 6727754
00 meter
Y = -625127
13 meter E =
0019478
Z = -4994595
37 I = 51
94155
XDOT = -1264
275914 Wp = 53
48652
YDOT = 7297
765693 meter/sec RA = 112
29598 deg
ZDOT = -2042
270734 TA = 196
75048
MA = 196
81489
Ha = 195
949 n
mi
Hp = 185
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14707123
24 X = 4513650
94
Y = -2050942
01 feet Y = -574825
92 meter
Z = -16386467
75 Z = -4972743
30
XDOT = -4147
886858 XDOT = -1335
866004
YDOT = 23942
800831 feet/sec YDOT = 7283
227412 meter/sec
ZDOT = -6700
363300 ZDOT = -2048
586814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14901282
13 X = -4541910
79
Y = 1149271
22 feet Y = 350297
87 meter
Z = -16298868
96 Z = -4967895
26
XDOT = 5637
285529 XDOT = 1718
244629
YDOT = -22562
538632 feet/sec YDOT = -6877
061775 meter/sec
ZDOT = -6725
605720 ZDOT = -2049
964623
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 10261
51943247
00016717 00000-0 10270-3 0 9125
2 25544 51
6436 113
0604 0008883 21
5065 338
6468 15
71810304 38153
Satellite: ISS
Catalog Number: 25544
Epoch time: 10261
51943247 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 113
0604 deg
Eccentricity:
0008883
Arg of perigee: 21
5065 deg
Mean anomaly: 338
6468 deg
Mean motion: 15
71810304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3815
Checksum: 292
Coasting Arc #14 (Orbit 3830)
---------------------------------------
Vector Time (GMT): 2010/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -44178
32 A = 6735678
20 meter
Y = -6281184
59 meter E =
0017683
Z = 2424583
89 I = 51
97995
XDOT = 5066
077792 Wp = 75
49423
YDOT = -2129
438115 meter/sec RA = 107
16230 deg
ZDOT = -5387
412746 TA = 77
30554
MA = 77
10793
Ha = 195
948 n
mi
Hp = 185
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -144941
99 X = 14284
22
Y = -20607561
00 feet Y = -6281351
57 meter
Z = 7954671
54 Z = 2424511
72
XDOT = 16620
990130 XDOT = 5115
683938
YDOT = -6986
345523 feet/sec YDOT = -2072
509213 meter/sec
ZDOT = -17675
238668 ZDOT = -5362
681268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -704627
09 X = -214770
34
Y = 20596157
65 feet Y = 6277708
85 meter
Z = 7954317
60 Z = 2424476
01
XDOT = -15511
804276 XDOT = -4727
997943
YDOT = 6303
973843 feet/sec YDOT = 1921
451227 meter/sec
ZDOT = -17576
106380 ZDOT = -5357
197225
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 10262
53667393
00016717 00000-0 10270-3 0 9134
2 25544 51
6441 107
8535 0009001 24
5811 335
5779 15
71877905 38317
Satellite: ISS
Catalog Number: 25544
Epoch time: 10262
53667393 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 107
8535 deg
Eccentricity:
0009001
Arg of perigee: 24
5811 deg
Mean anomaly: 335
5779 deg
Mean motion: 15
71877905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3831
Checksum: 315
Coasting Arc #15 (Orbit 3846)
---------------------------------------
Vector Time (GMT): 2010/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4125771
97 A = 6730244
98 meter
Y = 3055149
06 meter E =
0014259
Z = 4337733
68 I = 51
96755
XDOT = -1334
528866 Wp = 70
64708
YDOT = -6746
332099 meter/sec RA = 102
11083 deg
ZDOT = 3477
674330 TA = 344
37639
MA = 344
42035
Ha = 196
201 n
mi
Hp = 185
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13535997
27 X = -4180700
40
Y = 10023454
92 feet Y = 3008705
46 meter
Z = 14231409
73 Z = 4317557
09
XDOT = -4378
375544 XDOT = -1275
884789
YDOT = -22133
635497 feet/sec YDOT = -6760
927401 meter/sec
ZDOT = 11409
692683 ZDOT = 3471
334256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13879260
05 X = 4230398
46
Y = -9661994
30 feet Y = -2944975
86 meter
Z = 14150544
17 Z = 4313085
86
XDOT = 3157
420777 XDOT = 962
381853
YDOT = 21230
524417 feet/sec YDOT = 6471
063842 meter/sec
ZDOT = 11384
207789 ZDOT = 3469
906534
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 10263
55390136
00016717 00000-0 10270-3 0 9146
2 25544 51
6426 102
6455 0008941 28
7673 331
3980 15
71837343 38475
Satellite: ISS
Catalog Number: 25544
Epoch time: 10263
55390136 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 102
6455 deg
Eccentricity:
0008941
Arg of perigee: 28
7673 deg
Mean anomaly: 331
3980 deg
Mean motion: 15
71837343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3847
Checksum: 315
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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