Date:
January 9th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13131 97 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
022/09:06:27
407 1
5 3
3 3
3
N/A 2
7 0
0 185
5
000/00:00:54
813 1
2 0
0 179
7
Coasting Arc #1 (Orbit 3831)
---------------------------------------
Vector Time (GMT): 2010/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6084978
03 A = 6719701
46 meter
Y = -986375
36 meter E =
0016276
Z = 2667461
46 I = 51
48966
XDOT = -1393
512469 Wp = 105
14044
YDOT = 5521
699639 meter/sec RA = 330
65163 deg
ZDOT = 5190
242541 TA = 285
35844
MA = 285
53822
Ha = 186
929 n
mi
Hp = 177
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19963838
67 X = 6082597
59
Y = -3236139
62 feet Y = -918343
08 meter
Z = 8751513
97 Z = 2697016
33
XDOT = -4571
891303 XDOT = -1480
366706
YDOT = 18115
812465 feet/sec YDOT = 5505
630478 meter/sec
ZDOT = 17028
354794 ZDOT = 5183
262390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8967060
10 X = 2733159
92
Y = 18070914
19 feet Y = 5508014
65 meter
Z = 8868502
92 Z = 2703119
69
XDOT = -17370
353429 XDOT = -5294
483725
YDOT = 227
739012 feet/sec YDOT = 69
414851 meter/sec
ZDOT = 17000
799154 ZDOT = 5181
843582
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 10008
55792121
00016717 00000-0 10270-3 0 9008
2 25544 51
6441 330
8660 0007380 162
3038 197
8385 15
77270683 38323
Satellite: ISS
Catalog Number: 25544
Epoch time: 10008
55792121 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 330
8660 deg
Eccentricity:
0007380
Arg of perigee: 162
3038 deg
Mean anomaly: 197
8385 deg
Mean motion: 15
77270683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3832
Checksum: 305
Coasting Arc #2 (Orbit 3846)
---------------------------------------
Vector Time (GMT): 2010/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1999472
35 A = 6716470
44 meter
Y = -5122694
85 meter E =
0011852
Z = -3870114
38 I = 51
45253
XDOT = 6504
986537 Wp = 136
85436
YDOT = -539
975808 meter/sec RA = 325
42992 deg
ZDOT = 4074
333372 TA = 175
76333
MA = 175
75329
Ha = 186
851 n
mi
Hp = 177
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6559948
65 X = 2075406
87
Y = -16806741
62 feet Y = -5099910
58 meter
Z = -12697225
66 Z = -3860217
07
XDOT = 21341
819348 XDOT = 6490
748864
YDOT = -1771
574172 feet/sec YDOT = -467
313239 meter/sec
ZDOT = 13367
235474 ZDOT = 4105
899862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18037369
06 X = 5497790
09
Y = 1069800
03 feet Y = 326075
05 meter
Z = -12658114
98 Z = -3858193
45
XDOT = 8383
483625 XDOT = 2555
285809
YDOT = 18338
561702 feet/sec YDOT = 5589
593607 meter/sec
ZDOT = 13492
195260 ZDOT = 4112
421115
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 10009
50829878
00016717 00000-0 10270-3 0 9015
2 25544 51
6441 325
9619 0007153 165
3898 194
7475 15
77245513 38473
Satellite: ISS
Catalog Number: 25544
Epoch time: 10009
50829878 = yrday
fracday
Element set: 901
Inclination: 51
6441 deg
RA of node: 325
9619 deg
Eccentricity:
0007153
Arg of perigee: 165
3898 deg
Mean anomaly: 194
7475 deg
Mean motion: 15
77245513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3847
Checksum: 342
Coasting Arc #3 (Orbit 3862)
---------------------------------------
Vector Time (GMT): 2010/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5165512
54 A = 6714645
93 meter
Y = -162363
69 meter E =
0010412
Z = -4292935
09 I = 51
42369
XDOT = 3070
690914 Wp = 111
36584
YDOT = -6148
627743 meter/sec RA = 320
30571 deg
ZDOT = -3472
763385 TA = 123
45280
MA = 123
35320
Ha = 186
601 n
mi
Hp = 177
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16947219
63 X = -5142458
86
Y = -532689
27 feet Y = -219998
09 meter
Z = -14084432
70 Z = -4317973
04
XDOT = 10074
445256 XDOT = 3156
087695
YDOT = -20172
663199 feet/sec YDOT = -6113
811564 meter/sec
ZDOT = -11393
580658 ZDOT = -3457
639362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5023634
82 X = -1531203
89
Y = -16107544
74 feet Y = -4909579
64 meter
Z = -14183559
18 Z = -4323148
84
XDOT = 21207
841581 XDOT = 6464
150114
YDOT = 3335
641934 feet/sec YDOT = 1016
703662 meter/sec
ZDOT = -11333
791179 ZDOT = -3454
539551
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 10010
52201697
00016717 00000-0 10270-3 0 9023
2 25544 51
6448 320
7307 0007130 169
1610 190
9710 15
77299387 38632
Satellite: ISS
Catalog Number: 25544
Epoch time: 10010
52201697 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 320
7307 deg
Eccentricity:
0007130
Arg of perigee: 169
1610 deg
Mean anomaly: 190
9710 deg
Mean motion: 15
77299387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3863
Checksum: 299
Coasting Arc #4 (Orbit 3878)
---------------------------------------
Vector Time (GMT): 2010/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3215036
80 A = 6720958
67 meter
Y = 5519384
10 meter E =
0018579
Z = 2054507
43 I = 51
42292
XDOT = -5267
492133 Wp = 130
49784
YDOT = -995
864109 meter/sec RA = 315
08654 deg
ZDOT = -5546
766427 TA = 26
44367
MA = 26
34898
Ha = 186
553 n
mi
Hp = 177
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10548020
98 X = -3286496
91
Y = 18108215
56 feet Y = 5483031
84 meter
Z = 6740509
94 Z = 2038716
07
XDOT = -17281
798338 XDOT = -5229
019773
YDOT = -3267
270698 feet/sec YDOT = -1054
552483 meter/sec
ZDOT = -18198
052581 ZDOT = -5572
262356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20645084
18 X = -6292621
66
Y = -3713028
99 feet Y = -1131731
24 meter
Z = 6678069
07 Z = 2035475
45
XDOT = -3109
658085 XDOT = -947
823784
YDOT = -15745
382542 feet/sec YDOT = -4799
192599 meter/sec
ZDOT = -18299
008033 ZDOT = -5577
537649
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 10011
53571856
00016717 00000-0 10270-3 0 9033
2 25544 51
6453 315
5002 0007121 173
0142 187
1124 15
77313508 38792
Satellite: ISS
Catalog Number: 25544
Epoch time: 10011
53571856 = yrday
fracday
Element set: 903
Inclination: 51
6453 deg
RA of node: 315
5002 deg
Eccentricity:
0007121
Arg of perigee: 173
0142 deg
Mean anomaly: 187
1124 deg
Mean motion: 15
77313508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3879
Checksum: 279
Coasting Arc #5 (Orbit 3894)
---------------------------------------
Vector Time (GMT): 2010/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3973294
86 A = 6710889
97 meter
Y = 1660167
36 meter E =
0009887
Z = 5145700
67 I = 51
36948
XDOT = -4159
537804 Wp = 159
65368
YDOT = 6388
419032 meter/sec RA = 309
93766 deg
ZDOT = 1140
909669 TA = 279
36842
MA = 279
48020
Ha = 186
208 n
mi
Hp = 178
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13035744
29 X = 3929438
73
Y = 5446743
30 feet Y = 1704353
19 meter
Z = 16882220
04 Z = 5164896
37
XDOT = -13646
777572 XDOT = -4236
207343
YDOT = 20959
380026 feet/sec YDOT = 6341
475787 meter/sec
ZDOT = 3743
141959 ZDOT = 1120
517527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -424047
22 X = -129249
59
Y = 14030147
92 feet Y = 4276389
09 meter
Z = 16958246
62 Z = 5168873
57
XDOT = -23452
039535 XDOT = -7148
181650
YDOT = -5174
380571 feet/sec YDOT = -1577
151198 meter/sec
ZDOT = 3662
498851 ZDOT = 1116
329650
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 10012
54940097
00016717 00000-0 10270-3 0 9043
2 25544 51
6456 310
2699 0007130 178
5312 181
5875 15
77380205 38955
Satellite: ISS
Catalog Number: 25544
Epoch time: 10012
54940097 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 310
2699 deg
Eccentricity:
0007130
Arg of perigee: 178
5312 deg
Mean anomaly: 181
5875 deg
Mean motion: 15
77380205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3895
Checksum: 312
Coasting Arc #6 (Orbit 3910)
---------------------------------------
Vector Time (GMT): 2010/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3913193
78 A = 6722597
57 meter
Y = -5463287
64 meter E =
0009123
Z = 126827
32 I = 51
39018
XDOT = 3837
616545 Wp = 79
79513
YDOT = 2896
903164 meter/sec RA = 304
74938 deg
ZDOT = 6016
239273 TA = 281
58856
MA = 281
69096
Ha = 186
231 n
mi
Hp = 178
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12838562
27 X = 3973378
30
Y = -17924172
06 feet Y = -5419191
51 meter
Z = 416100
12 Z = 145982
76
XDOT = 12590
605462 XDOT = 3775
712360
YDOT = 9504
275471 feet/sec YDOT = 2939
470764 meter/sec
ZDOT = 19738
317825 ZDOT = 6034
732097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21435430
82 X = 6533519
31
Y = 5153459
52 feet Y = 1570774
46 meter
Z = 491858
96 Z = 149918
61
XDOT = -3740
324746 XDOT = -1140
050982
YDOT = 13570
124197 feet/sec YDOT = 4136
173855 meter/sec
ZDOT = 19811
586875 ZDOT = 6038
571679
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 10013
56306950
00016717 00000-0 10270-3 0 9051
2 25544 51
6454 305
0384 0007048 181
5960 178
5184 15
77368121 39118
Satellite: ISS
Catalog Number: 25544
Epoch time: 10013
56306950 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 305
0384 deg
Eccentricity:
0007048
Arg of perigee: 181
5960 deg
Mean anomaly: 178
5184 deg
Mean motion: 15
77368121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3911
Checksum: 303
Coasting Arc #7 (Orbit 3925)
---------------------------------------
Vector Time (GMT): 2010/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2742176
77 A = 6711172
62 meter
Y = -3424152
44 meter E =
0016242
Z = -5092225
10 I = 51
33628
XDOT = 4692
686525 Wp = 126
46249
YDOT = -5923
830895 meter/sec RA = 299
55449 deg
ZDOT = 1450
010520 TA = 157
53775
MA = 157
46656
Ha = 186
052 n
mi
Hp = 178
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8996642
94 X = -2678946
91
Y = -11234095
94 feet Y = -3454462
95 meter
Z = -16706775
25 Z = -5105393
13
XDOT = 15395
953166 XDOT = 4751
535338
YDOT = -19435
140730 feet/sec YDOT = -5871
025628 meter/sec
ZDOT = 4757
252363 ZDOT = 1472
949357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6848140
44 X = 2087313
20
Y = -12589698
46 feet Y = -3837340
09 meter
Z = -16758976
72 Z = -5108136
10
XDOT = 22985
149615 XDOT = 7005
873603
YDOT = 6021
775579 feet/sec YDOT = 1835
437196 meter/sec
ZDOT = 4847
980815 ZDOT = 1477
664552
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 10014
51336680
00016717 00000-0 10270-3 0 9061
2 25544 51
6461 300
1342 0007009 185
3121 174
7970 15
77393284 39269
Satellite: ISS
Catalog Number: 25544
Epoch time: 10014
51336680 = yrday
fracday
Element set: 906
Inclination: 51
6461 deg
RA of node: 300
1342 deg
Eccentricity:
0007009
Arg of perigee: 185
3121 deg
Mean anomaly: 174
7970 deg
Mean motion: 15
77393284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3926
Checksum: 294
Coasting Arc #8 (Orbit 3941)
---------------------------------------
Vector Time (GMT): 2010/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4190278
81 A = 6719998
54 meter
Y = 4691855
85 meter E =
0011223
Z = -2347545
00 I = 51
35307
XDOT = -2497
714741 Wp = 164
69473
YDOT = -4916
895604 meter/sec RA = 294
40593 deg
ZDOT = -5385
201089 TA = 41
89915
MA = 41
81331
Ha = 185
825 n
mi
Hp = 178
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13747633
90 X = -4231028
87
Y = 15393227
85 feet Y = 4644770
07 meter
Z = -7701919
30 Z = -2367999
40
XDOT = -8194
602168 XDOT = -2416
387804
YDOT = -16131
547257 feet/sec YDOT = -4944
371261 meter/sec
ZDOT = -17667
982577 ZDOT = -5397
137658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19641986
08 X = -5986877
36
Y = -6236059
57 feet Y = -1900750
96 meter
Z = -7782827
66 Z = -2372205
87
XDOT = 10977
081092 XDOT = 3345
814317
YDOT = -12532
495479 feet/sec YDOT = -3819
904622 meter/sec
ZDOT = -17715
344064 ZDOT = -5399
636871
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 10015
52700104
00016717 00000-0 10270-3 0 9070
2 25544 51
6466 294
9033 0007016 189
3378 170
7657 15
77420552 39422
Satellite: ISS
Catalog Number: 25544
Epoch time: 10015
52700104 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 294
9033 deg
Eccentricity:
0007016
Arg of perigee: 189
3378 deg
Mean anomaly: 170
7657 deg
Mean motion: 15
77420552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3942
Checksum: 306
Coasting Arc #9 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2010/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1680324
72 A = 6715143
31 meter
Y = 5067636
80 meter E =
0009776
Z = 4062375
63 I = 51
32468
XDOT = -4837
373208 Wp = 116
00197
YDOT = 4651
705822 meter/sec RA = 289
17658 deg
ZDOT = -3799
086117 TA = 13
13586
MA = 13
11042
Ha = 185
683 n
mi
Hp = 178
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5512876
37 X = 1603798
83
Y = 16626104
99 feet Y = 5085998
97 meter
Z = 13328004
04 Z = 4070352
98
XDOT = -15870
647008 XDOT = -4870
575067
YDOT = 15261
502041 feet/sec YDOT = 4597
426124 meter/sec
ZDOT = -12464
193296 ZDOT = -3822
665755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12762360
93 X = -3889967
61
Y = 11962249
12 feet Y = 3646093
53 meter
Z = 13359700
75 Z = 4072036
79
XDOT = -19641
517604 XDOT = -5986
734566
YDOT = -6920
475193 feet/sec YDOT = -2109
360839 meter/sec
ZDOT = -12557
473385 ZDOT = -3827
517888
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 10016
54061882
00016717 00000-0 10270-3 0 9087
2 25544 51
6458 289
6726 0006978 192
9237 167
1750 15
77441645 39580
Satellite: ISS
Catalog Number: 25544
Epoch time: 10016
54061882 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 289
6726 deg
Eccentricity:
0006978
Arg of perigee: 192
9237 deg
Mean anomaly: 167
1750 deg
Mean motion: 15
77441645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 351
Coasting Arc #10 (Orbit 3973)
---------------------------------------
Vector Time (GMT): 2010/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4206080
94 A = 6714835
80 meter
Y = -3232346
86 meter E =
0012293
Z = 4116416
77 I = 51
31539
XDOT = 1417
729309 Wp = 139
26716
YDOT = 6598
453300 meter/sec RA = 284
04289 deg
ZDOT = 3717
279112 TA = 272
48873
MA = 272
62946
Ha = 185
528 n
mi
Hp = 178
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13799478
15 X = 4221916
69
Y = -10604812
54 feet Y = -3185223
69 meter
Z = 13505304
37 Z = 4136887
67
XDOT = 4651
342877 XDOT = 1325
781444
YDOT = 21648
468833 feet/sec YDOT = 6613
792848 meter/sec
ZDOT = 12195
797613 ZDOT = 3723
943350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15549899
89 X = 4739609
49
Y = 7674240
20 feet Y = 2339108
41 meter
Z = 13586299
83 Z = 4141104
19
XDOT = -16883
102585 XDOT = -5145
969668
YDOT = 12482
056299 feet/sec YDOT = 3804
530760 meter/sec
ZDOT = 12222
339291 ZDOT = 3725
369016
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 10017
55421914
00016717 00000-0 10270-3 0 9096
2 25544 51
6460 284
4408 0006941 197
1475 162
9457 15
77469437 39748
Satellite: ISS
Catalog Number: 25544
Epoch time: 10017
55421914 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 284
4408 deg
Eccentricity:
0006941
Arg of perigee: 197
1475 deg
Mean anomaly: 162
9457 deg
Mean motion: 15
77469437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3974
Checksum: 338
Coasting Arc #11 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2010/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -843935
96 A = 6719979
33 meter
Y = -6279657
72 meter E =
0002639
Z = -2243914
66 I = 51
32727
XDOT = 4802
359152 Wp = 143
20716
YDOT = -2586
786781 meter/sec RA = 278
81190 deg
ZDOT = 5434
239879 TA = 191
47819
MA = 191
48421
Ha = 185
358 n
mi
Hp = 178
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2768818
75 X = -762752
71
Y = -20602551
59 feet Y = -6288641
10 meter
Z = -7361924
75 Z = -2247817
50
XDOT = 15755
771497 XDOT = 4804
530181
YDOT = -8486
833270 feet/sec YDOT = -2533
072061 meter/sec
ZDOT = 17828
870995 ZDOT = 5457
574371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17116285
56 X = 5217043
84
Y = -11787033
93 feet Y = -3592687
94 meter
Z = -7377535
16 Z = -2248672
72
XDOT = 13810
257452 XDOT = 4209
366471
YDOT = 8839
810729 feet/sec YDOT = 2694
374310 meter/sec
ZDOT = 17921
218992 ZDOT = 5462
387549
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 10018
50445393
00016717 00000-0 10270-3 0 9101
2 25544 51
6462 279
5360 0006953 201
4022 158
6853 15
77515016 39895
Satellite: ISS
Catalog Number: 25544
Epoch time: 10018
50445393 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 279
5360 deg
Eccentricity:
0006953
Arg of perigee: 201
4022 deg
Mean anomaly: 158
6853 deg
Mean motion: 15
77515016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 310
Coasting Arc #12 (Orbit 4004)
---------------------------------------
Vector Time (GMT): 2010/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4187220
34 A = 6710543
54 meter
Y = 1164652
47 meter E =
0011642
Z = -5121718
85 I = 51
29227
XDOT = -545
478896 Wp = 108
76406
YDOT = -7572
298968 meter/sec RA = 273
65715 deg
ZDOT = -1282
019403 TA = 148
94998
MA = 148
88112
Ha = 185
059 n
mi
Hp = 178
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13737599
55 X = -4175052
59
Y = 3821038
29 feet Y = 1117896
68 meter
Z = -16803539
52 Z = -5142030
37
XDOT = -1789
628924 XDOT = -454
535876
YDOT = -24843
500550 feet/sec YDOT = -7577
890307 meter/sec
ZDOT = -4206
100402 ZDOT = -1284
448620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9776893
54 X = -2979997
15
Y = -10248194
56 feet Y = -3123649
70 meter
Z = -16883950
25 Z = -5146228
04
XDOT = 20359
105422 XDOT = 6205
455333
YDOT = -12509
720811 feet/sec YDOT = -3812
962903 meter/sec
ZDOT = -4215
918994 ZDOT = -1285
012109
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 10019
51802161
00016717 00000-0 10270-3 0 9114
2 25544 51
6462 274
3041 0006870 205
9861 154
0960 15
77548224 40058
Satellite: ISS
Catalog Number: 25544
Epoch time: 10019
51802161 = yrday
fracday
Element set: 911
Inclination: 51
6462 deg
RA of node: 274
3041 deg
Eccentricity:
0006870
Arg of perigee: 205
9861 deg
Mean anomaly: 154
0960 deg
Mean motion: 15
77548224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4005
Checksum: 286
Coasting Arc #13 (Orbit 4020)
---------------------------------------
Vector Time (GMT): 2010/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 127975
80 A = 6722203
75 meter
Y = 6710768
07 meter E =
0015631
Z = -65378
76 I = 51
33039
XDOT = -4818
910872 Wp = 161
05639
YDOT = 37
292971 meter/sec RA = 268
46085 deg
ZDOT = -6020
605811 TA = 19
65840
MA = 19
59821
Ha = 185
057 n
mi
Hp = 179
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 419868
12 X = 53242
89
Y = 22016955
61 feet Y = 6711781
32 meter
Z = -214497
23 Z = -64938
43
XDOT = -15810
075040 XDOT = -4789
723193
YDOT = 122
352268 feet/sec YDOT = -16
431608 meter/sec
ZDOT = -19752
643736 ZDOT = -6043
944806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19054562
54 X = -5807830
66
Y = 11038437
09 feet Y = 3364515
63 meter
Z = -212568
65 Z = -64790
92
XDOT = -6907
399267 XDOT = -2105
375297
YDOT = -12279
215411 feet/sec YDOT = -3742
704857 meter/sec
ZDOT = -19845
075395 ZDOT = -6048
778980
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 10020
53157415
00016717 00000-0 10270-3 0 9124
2 25544 51
6460 269
0722 0007054 209
6311 150
4455 15
77512315 40218
Satellite: ISS
Catalog Number: 25544
Epoch time: 10020
53157415 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 269
0722 deg
Eccentricity:
0007054
Arg of perigee: 209
6311 deg
Mean anomaly: 150
4455 deg
Mean motion: 15
77512315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4021
Checksum: 266
Coasting Arc #14 (Orbit 4036)
---------------------------------------
Vector Time (GMT): 2010/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4234922
22 A = 6710480
04 meter
Y = 1102308
76 meter E =
0003002
Z = 5086976
68 I = 51
29389
XDOT = -258
179241 Wp = 186
17249
YDOT = 7569
516834 meter/sec RA = 263
26162 deg
ZDOT = -1428
346950 TA = 277
54832
MA = 277
58242
Ha = 184
573 n
mi
Hp = 179
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13894101
78 X = 4197569
96
Y = 3616498
55 feet Y = 1149457
20 meter
Z = 16689556
04 Z = 5107458
98
XDOT = -847
044753 XDOT = -335
865161
YDOT = 24834
372816 feet/sec YDOT = 7566
195389 meter/sec
ZDOT = -4686
177659 ZDOT = -1429
789693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3759351
61 X = 1145850
37
Y = 13757798
59 feet Y = 4193377
01 meter
Z = 16770708
40 Z = 5111711
92
XDOT = -20918
971168 XDOT = -6376
102412
YDOT = 11423
252414 feet/sec YDOT = 3481
807336 meter/sec
ZDOT = -4691
675131 ZDOT = -1430
022580
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 10021
54510686
00016717 00000-0 10270-3 0 9130
2 25544 51
6460 263
8398 0006909 215
5930 144
4776 15
77615029 40372
Satellite: ISS
Catalog Number: 25544
Epoch time: 10021
54510686 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 263
8398 deg
Eccentricity:
0006909
Arg of perigee: 215
5930 deg
Mean anomaly: 144
4776 deg
Mean motion: 15
77615029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4037
Checksum: 316
Coasting Arc #15 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2010/022/09:06:54
813
Vector Time (MET): N/A
Weight (LBS) : 751525
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3111891
29 A = 6713958
37 meter
Y = -3647160
19 meter E =
0009253
Z = 4699352
82 I = 51
30207
XDOT = 3436
703439 Wp = 148
52829
YDOT = 6365
678430 meter/sec RA = 258
73091 deg
ZDOT = 2654
480139 TA = 275
22674
MA = 275
33232
Ha = 185
508 n
mi
Hp = 179
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10209617
08 X = 3129614
81
Y = -11965748
65 feet Y = -3612262
22 meter
Z = 15417824
20 Z = 4714513
18
XDOT = 11275
273750 XDOT = 3352
371014
YDOT = 20884
771753 feet/sec YDOT = 6403
638078 meter/sec
ZDOT = 8708
924339 ZDOT = 2670
970827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9506687
46 X = 2897638
34
Y = 12457387
27 feet Y = 3797011
64 meter
Z = 15477762
14 Z = 4717621
90
XDOT = -21903
023498 XDOT = -6676
041562
YDOT = 5771
972915 feet/sec YDOT = 1759
297345 meter/sec
ZDOT = 8774
424774 ZDOT = 2674
444671
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 10022
43196333
00016717 00000-0 10270-3 0 9149
2 25544 51
6444 259
2612 0004636 204
1981 155
8967 15
76991263 40517
Satellite: ISS
Catalog Number: 25544
Epoch time: 10022
43196333 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 259
2612 deg
Eccentricity:
0004636
Arg of perigee: 204
1981 deg
Mean anomaly: 155
8967 deg
Mean motion: 15
76991263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 310
Coasting Arc #16 (Orbit 4065)
---------------------------------------
Vector Time (GMT): 2010/023/09:06:54
813
Vector Time (MET): N/A
Weight (LBS) : 751525
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2894429
71 A = 6722805
96 meter
Y = -5908771
21 meter E =
0004257
Z = -1373444
60 I = 51
33949
XDOT = 3882
068682 Wp = 46
16207
YDOT = -3247
678744 meter/sec RA = 253
51527 deg
ZDOT = 5804
926906 TA = 298
66798
MA = 298
71077
Ha = 185
399 n
mi
Hp = 179
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9496160
48 X = -2821469
77
Y = -19385732
31 feet Y = -5940730
44 meter
Z = -4506051
84 Z = -1387328
66
XDOT = 12736
445808 XDOT = 3889
897203
YDOT = -10655
113989 feet/sec YDOT = -3204
223625 meter/sec
ZDOT = 19045
035780 ZDOT = 5823
804733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20879387
42 X = 6364037
29
Y = -5434577
02 feet Y = -1656459
08 meter
Z = -4561221
06 Z = -1390260
18
XDOT = 7541
446327 XDOT = 2298
632840
YDOT = 12965
060022 feet/sec YDOT = 3951
750295 meter/sec
ZDOT = 19119
710570 ZDOT = 5827
687782
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 10023
38249898
00016717 00000-0 10270-3 0 9150
2 25544 51
6447 254
3582 0004536 208
8795 151
2119 15
76998857 40666
Satellite: ISS
Catalog Number: 25544
Epoch time: 10023
38249898 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 254
3582 deg
Eccentricity:
0004536
Arg of perigee: 208
8795 deg
Mean anomaly: 151
2119 deg
Mean motion: 15
76998857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4066
Checksum: 350
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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