Date:
November 13th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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 648)
---------------------------------------
Vector Time (GMT): 2010/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4007038
65 A = 6726058
53 meter
Y = -2529019
52 meter E =
0006676
Z = 4767386
05 I = 51
50849
XDOT = 5799
039946 Wp = 124
28022
YDOT = 4382
530216 meter/sec RA = 200
87808 deg
ZDOT = -2550
461010 TA = 350
73826
MA = 350
75056
Ha = 193
381 n
mi
Hp = 185
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13146452
27 X = 4011861
34
Y = -8297308
12 feet Y = -2484183
75 meter
Z = 15641030
35 Z = 4786864
10
XDOT = 19025
721609 XDOT = 5761
992548
YDOT = 14378
379973 feet/sec YDOT = 4447
171589 meter/sec
ZDOT = -8367
654233 ZDOT = -2522
378538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2366600
33 X = -721339
78
Y = 15284711
71 feet Y = 4658780
13 meter
Z = 15719196
88 Z = 4791211
21
XDOT = -22271
829810 XDOT = -6788
453726
YDOT = 5037
252641 feet/sec YDOT = 1535
354605 meter/sec
ZDOT = -8254
958373 ZDOT = -2516
111312
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 10314
54332771
00016717 00000-0 10270-3 0 9008
2 25544 51
6459 201
7071 0007372 185
6325 174
4756 15
72640611 6495
Satellite: ISS
Catalog Number: 25544
Epoch time: 10314
54332771 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 201
7071 deg
Eccentricity:
0007372
Arg of perigee: 185
6325 deg
Mean anomaly: 174
4756 deg
Mean motion: 15
72640611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 649
Checksum: 297
Coasting Arc #2 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2010/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5686921
95 A = 6734649
83 meter
Y = -3109791
52 meter E =
0011748
Z = 1822008
55 I = 51
56603
XDOT = 3786
598520 Wp = 97
30966
YDOT = -3592
653520 meter/sec RA = 195
78182 deg
ZDOT = 5654
402434 TA = 282
90071
MA = 283
03191
Ha = 193
357 n
mi
Hp = 185
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18657880
42 X = -5660576
12
Y = -10202728
10 feet Y = -3173238
89 meter
Z = 5977718
33 Z = 1794444
96
XDOT = 12423
223491 XDOT = 3799
022394
YDOT = -11786
920997 feet/sec YDOT = -3550
240329 meter/sec
ZDOT = 18551
189088 ZDOT = 5672
827955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19865758
40 X = 6055083
16
Y = -7672951
60 feet Y = -2338715
65 meter
Z = 5867089
22 Z = 1788288
79
XDOT = 478
737298 XDOT = 145
919128
YDOT = 15564
325955 feet/sec YDOT = 4744
006551 meter/sec
ZDOT = 18625
139469 ZDOT = 5676
942510
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 10315
56004807
00016717 00000-0 10270-3 0 9018
2 25544 51
6458 196
4963 0007347 189
5014 170
6011 15
72645222 6657
Satellite: ISS
Catalog Number: 25544
Epoch time: 10315
56004807 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 196
4963 deg
Eccentricity:
0007347
Arg of perigee: 189
5014 deg
Mean anomaly: 170
6011 deg
Mean motion: 15
72645222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 299
Coasting Arc #3 (Orbit 679)
---------------------------------------
Vector Time (GMT): 2010/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2549498
29 A = 6724619
08 meter
Y = 3619233
69 meter E =
0015343
Z = -5074158
70 I = 51
56262
XDOT = -7030
847644 Wp = 131
26750
YDOT = -2643
184165 meter/sec RA = 190
62072 deg
ZDOT = 1640
604151 TA = 154
57897
MA = 154
50342
Ha = 193
074 n
mi
Hp = 185
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8364495
69 X = -2565130
11
Y = 11874126
29 feet Y = 3590636
45 meter
Z = -16647502
31 Z = -5086582
15
XDOT = -23067
085445 XDOT = -7008
738365
YDOT = -8671
864059 feet/sec YDOT = -2721
683770 meter/sec
ZDOT = 5382
559552 ZDOT = 1606
501506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3960216
92 X = -1207074
12
Y = -13914510
85 feet Y = -4241142
91 meter
Z = -16697367
04 Z = -5089357
47
XDOT = 20319
710315 XDOT = 6193
447704
YDOT = -12104
404720 feet/sec YDOT = -3689
422559 meter/sec
ZDOT = 5245
668662 ZDOT = 1598
879808
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 10316
51319190
00016717 00000-0 10270-3 0 9029
2 25544 51
6457 191
6111 0007376 194
0763 166
0195 15
72714842 6806
Satellite: ISS
Catalog Number: 25544
Epoch time: 10316
51319190 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 191
6111 deg
Eccentricity:
0007376
Arg of perigee: 194
0763 deg
Mean anomaly: 166
0195 deg
Mean motion: 15
72714842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 680
Checksum: 299
Coasting Arc #4 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2010/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6480702
81 A = 6735410
96 meter
Y = 1461610
14 meter E =
0015336
Z = -1050693
78 I = 51
62896
XDOT = -1973
435086 Wp = 166
42811
YDOT = 4517
948265 meter/sec RA = 185
51589 deg
ZDOT = -5919
311614 TA = 25
06493
MA = 24
99056
Ha = 193
056 n
mi
Hp = 186
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21262148
32 X = 6468981
29
Y = 4795308
85 feet Y = 1534015
74 meter
Z = -3447158
06 Z = -1019238
58
XDOT = -6474
524559 XDOT = -1995
053656
YDOT = 14822
664911 feet/sec YDOT = 4495
759367 meter/sec
ZDOT = -19420
313695 ZDOT = -5928
951102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16949834
33 X = -5166309
50
Y = 13734325
55 feet Y = 4186222
43 meter
Z = -3320881
62 Z = -1012204
72
XDOT = -6692
969637 XDOT = -2040
017145
YDOT = -12938
671923 feet/sec YDOT = -3943
707202 meter/sec
ZDOT = -19459
004808 ZDOT = -5931
104665
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 10317
52984892
00016717 00000-0 10270-3 0 9039
2 25544 51
6458 186
4009 0007558 198
2445 161
8448 15
72709077 6965
Satellite: ISS
Catalog Number: 25544
Epoch time: 10317
52984892 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 186
4009 deg
Eccentricity:
0007558
Arg of perigee: 198
2445 deg
Mean anomaly: 161
8448 deg
Mean motion: 15
72709077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 348
Coasting Arc #5 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2010/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 863412
06 A = 6723645
72 meter
Y = -4136298
96 meter E =
0005397
Z = 5229572
99 I = 51
62076
XDOT = 7635
567020 Wp = 181
85326
YDOT = 646
995732 meter/sec RA = 180
37244 deg
ZDOT = -754
228799 TA = 275
29395
MA = 275
35553
Ha = 192
658 n
mi
Hp = 186
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2832716
73 X = 884196
07
Y = -13570534
63 feet Y = -4126527
59 meter
Z = 17157391
71 Z = 5233817
96
XDOT = 25051
072901 XDOT = 7631
428655
YDOT = 2122
689409 feet/sec YDOT = 732
358102 meter/sec
ZDOT = -2474
503934 ZDOT = -717
144735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9139868
29 X = 2785831
85
Y = 10395268
53 feet Y = 3168477
85 meter
Z = 17174428
21 Z = 5234765
72
XDOT = -16119
518074 XDOT = -4913
229109
YDOT = 17986
256389 feet/sec YDOT = 5482
210947 meter/sec
ZDOT = -2325
618207 ZDOT = -708
848430
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 10318
54647144
00016717 00000-0 10270-3 0 9049
2 25544 51
6457 181
1896 0007369 202
7871 157
2966 15
72811623 7128
Satellite: ISS
Catalog Number: 25544
Epoch time: 10318
54647144 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 181
1896 deg
Eccentricity:
0007369
Arg of perigee: 202
7871 deg
Mean anomaly: 157
2966 deg
Mean motion: 15
72811623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 321
Coasting Arc #6 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2010/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6719608
31 A = 6735373
96 meter
Y = 329380
14 meter E =
0006365
Z = 288056
24 I = 51
69036
XDOT = 28
638665 Wp = 72
19649
YDOT = -4781
484457 meter/sec RA = 175
25527 deg
ZDOT = 6028
575694 TA = 290
92862
MA = 290
99673
Ha = 192
414 n
mi
Hp = 186
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22045959
03 X = -6724191
43
Y = 1080643
49 feet Y = 254211
81 meter
Z = 945066
40 Z = 255400
68
XDOT = 93
958875 XDOT = 52
817747
YDOT = -15687
284964 feet/sec YDOT = -4781
029011 meter/sec
ZDOT = 19778
791646 ZDOT = 6028
773553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12188046
89 X = 3714916
69
Y = -18408537
35 feet Y = -5610922
18 meter
Z = 813950
94 Z = 248092
25
XDOT = 11311
637995 XDOT = 3447
787261
YDOT = 8381
865602 feet/sec YDOT = 2554
792636 meter/sec
ZDOT = 19779
579279 ZDOT = 6028
815764
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 10319
56306230
00016717 00000-0 10270-3 0 9051
2 25544 51
6449 175
9777 0007373 207
3154 152
7621 15
72867178 7289
Satellite: ISS
Catalog Number: 25544
Epoch time: 10319
56306230 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 175
9777 deg
Eccentricity:
0007373
Arg of perigee: 207
3154 deg
Mean anomaly: 152
7621 deg
Mean motion: 15
72867178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 324
Coasting Arc #7 (Orbit 742)
---------------------------------------
Vector Time (GMT): 2010/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 783153
64 A = 6723206
17 meter
Y = 4099706
47 meter E =
0012751
Z = -5280269
65 I = 51
67885
XDOT = -7568
094808 Wp = 118
59180
YDOT = 1369
354276 meter/sec RA = 170
12897 deg
ZDOT = -65
384266 TA = 150
82301
MA = 150
75172
Ha = 192
163 n
mi
Hp = 186
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2569401
72 X = 762902
89
Y = 13450480
54 feet Y = 4108350
93 meter
Z = -17323719
33 Z = -5276514
20
XDOT = -24829
707374 XDOT = -7582
527066
YDOT = 4492
632138 feet/sec YDOT = 1284
642591 meter/sec
ZDOT = -214
515308 ZDOT = -102
185897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12518413
71 X = -3815612
50
Y = -5597227
31 feet Y = -1706034
88 meter
Z = -17308635
64 Z = -5275672
14
XDOT = 10283
494400 XDOT = 3134
409093
YDOT = -21941
058978 feet/sec YDOT = -6687
634777 meter/sec
ZDOT = -362
288178 ZDOT = -110
425437
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 10320
51608784
00016717 00000-0 10270-3 0 9068
2 25544 51
6437 171
0912 0007306 211
4062 148
6665 15
72911980 7434
Satellite: ISS
Catalog Number: 25544
Epoch time: 10320
51608784 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 171
0912 deg
Eccentricity:
0007306
Arg of perigee: 211
4062 deg
Mean anomaly: 148
6665 deg
Mean motion: 15
72911980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 743
Checksum: 296
Coasting Arc #8 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2010/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6397386
15 A = 6735111
84 meter
Y = -2035928
25 meter E =
0015479
Z = 394718
24 I = 51
74925
XDOT = 1790
282443 Wp = 158
94610
YDOT = 4444
458866 meter/sec RA = 165
00332 deg
ZDOT = -6033
230016 TA = 16
76768
MA = 16
71657
Ha = 191
964 n
mi
Hp = 186
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20988799
70 X = 6417759
29
Y = -6679554
62 feet Y = -1964274
92 meter
Z = 1295007
34 Z = 425846
98
XDOT = 5873
630061 XDOT = 1769
759678
YDOT = 14581
557959 feet/sec YDOT = 4464
364163 meter/sec
ZDOT = -19794
061731 ZDOT = -6024
582439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6320896
37 X = -1926609
21
Y = 21091539
61 feet Y = 6428701
27 meter
Z = 1420011
58 Z = 432819
53
XDOT = -13880
947424 XDOT = -4230
912775
YDOT = -2817
853535 feet/sec YDOT = -858
881757 meter/sec
ZDOT = -19759
334600 ZDOT = -6022
645186
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 10321
53261705
00016717 00000-0 10270-3 0 9070
2 25544 51
6439 165
8804 0007309 215
5267 144
5410 15
72942631 7599
Satellite: ISS
Catalog Number: 25544
Epoch time: 10321
53261705 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 165
8804 deg
Eccentricity:
0007309
Arg of perigee: 215
5267 deg
Mean anomaly: 144
5410 deg
Mean motion: 15
72942631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 303
Coasting Arc #9 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2010/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2286666
23 A = 6723311
74 meter
Y = -3555700
42 meter E =
0007547
Z = 5230307
04 I = 51
73760
XDOT = 6936
254876 Wp = 193
66183
YDOT = -3233
854833 meter/sec RA = 159
89348 deg
ZDOT = 827
090612 TA = 248
43270
MA = 248
51314
Ha = 191
840 n
mi
Hp = 186
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7502185
78 X = -2272144
36
Y = -11665683
78 feet Y = -3581190
19 meter
Z = 17159800
00 Z = 5219233
32
XDOT = 22756
741719 XDOT = 6967
882950
YDOT = -10609
759951 feet/sec YDOT = -3156
112631 meter/sec
ZDOT = 2713
551877 ZDOT = 860
864638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13924482
96 X = 4244182
41
Y = 62653
46 feet Y = 19096
78 meter
Z = 17115330
97 Z = 5216752
88
XDOT = -3637
334672 XDOT = -1108
659608
YDOT = 23812
383450 feet/sec YDOT = 7258
014475 meter/sec
ZDOT = 2849
193183 ZDOT = 868
434082
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 10322
54911410
00016717 00000-0 10270-3 0 9088
2 25544 51
6427 160
6675 0007273 219
4661 140
5972 15
72961038 7755
Satellite: ISS
Catalog Number: 25544
Epoch time: 10322
54911410 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 160
6675 deg
Eccentricity:
0007273
Arg of perigee: 219
4661 deg
Mean anomaly: 140
5972 deg
Mean motion: 15
72961038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 307
Coasting Arc #10 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2010/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5630221
04 A = 6734425
63 meter
Y = 3547055
41 meter E =
0002469
Z = -1025893
62 I = 51
80279
XDOT = -3339
385674 Wp = 20
58262
YDOT = -3586
571233 meter/sec RA = 154
75643 deg
ZDOT = 5932
822219 TA = 328
23808
MA = 328
25297
Ha = 191
491 n
mi
Hp = 186
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18471853
81 X = -5664482
67
Y = 11637320
91 feet Y = 3483903
37 meter
Z = -3365792
71 Z = -1053329
13
XDOT = -10955
989743 XDOT = -3327
853201
YDOT = -11766
965988 feet/sec YDOT = -3623
849998 meter/sec
ZDOT = 19464
639827 ZDOT = 5916
626880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 50262
41 X = 15319
98
Y = -21814676
83 feet Y = -6649113
50 meter
Z = -3475993
45 Z = -1059482
80
XDOT = 14274
697454 XDOT = 4350
927784
YDOT = -3054
959133 feet/sec YDOT = -931
151544 meter/sec
ZDOT = 19399
601616 ZDOT = 5912
998572
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 10323
50204833
00016717 00000-0 10270-3 0 9090
2 25544 51
6414 155
7799 0007355 223
9476 136
1103 15
73036687 7906
Satellite: ISS
Catalog Number: 25544
Epoch time: 10323
50204833 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 155
7799 deg
Eccentricity:
0007355
Arg of perigee: 223
9476 deg
Mean anomaly: 136
1103 deg
Mean motion: 15
73036687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 790
Checksum: 310
Coasting Arc #11 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2010/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3466149
46 A = 6723439
71 meter
Y = 2645163
70 meter E =
0008518
Z = -5124512
97 I = 51
79234
XDOT = -5843
184531 Wp = 105
19684
YDOT = 4778
577317 meter/sec RA = 149
66150 deg
ZDOT = -1489
882264 TA = 150
56049
MA = 150
51249
Ha = 191
300 n
mi
Hp = 186
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11371881
43 X = 3461207
83
Y = 8678358
60 feet Y = 2683896
96 meter
Z = -16812706
60 Z = -5107685
75
XDOT = -19170
552923 XDOT = -5888
947393
YDOT = 15677
747103 feet/sec YDOT = 4712
979533 meter/sec
ZDOT = -4888
065172 ZDOT = -1518
380164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13382390
92 X = -4078952
75
Y = 5273809
72 feet Y = 1607457
20 meter
Z = -16745125
94 Z = -5103914
39
XDOT = -3030
441968 XDOT = -923
678712
YDOT = -23529
388099 feet/sec YDOT = -7171
757493 meter/sec
ZDOT = -5002
555309 ZDOT = -1524
778858
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 10324
51848137
00016717 00000-0 10270-3 0 9105
2 25544 51
6405 150
5670 0007270 227
1197 132
9356 15
73096957 8067
Satellite: ISS
Catalog Number: 25544
Epoch time: 10324
51848137 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 150
5670 deg
Eccentricity:
0007270
Arg of perigee: 227
1197 deg
Mean anomaly: 132
9356 deg
Mean motion: 15
73096957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 306
Coasting Arc #12 (Orbit 821)
---------------------------------------
Vector Time (GMT): 2010/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4515365
71 A = 6733377
92 meter
Y = -4730837
16 meter E =
0012638
Z = 1567830
76 I = 51
85304
XDOT = 4498
926782 Wp = 148
35547
YDOT = 2373
284323 meter/sec RA = 144
51829 deg
ZDOT = -5785
327798 TA = 14
40055
MA = 14
36457
Ha = 190
806 n
mi
Hp = 187
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14814191
96 X = 4560314
76
Y = -15521119
31 feet Y = -4680092
44 meter
Z = 5143801
72 Z = 1589875
80
XDOT = 14760
258470 XDOT = 4500
158765
YDOT = 7786
365888 feet/sec YDOT = 2423
601418 meter/sec
ZDOT = -18980
734244 ZDOT = -5763
468196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5906127
49 X = 1800187
66
Y = 20604947
85 feet Y = 6280388
10 meter
Z = 5232390
09 Z = 1594832
50
XDOT = -12738
856694 XDOT = -3882
803520
YDOT = 8457
558864 feet/sec YDOT = 2577
863942 meter/sec
ZDOT = -18892
932453 ZDOT = -5758
565812
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 10325
53487927
00016717 00000-0 10270-3 0 9115
2 25544 51
6410 145
3539 0007279 233
6424 126
4067 15
73190979 8227
Satellite: ISS
Catalog Number: 25544
Epoch time: 10325
53487927 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 145
3539 deg
Eccentricity:
0007279
Arg of perigee: 233
6424 deg
Mean anomaly: 126
4067 deg
Mean motion: 15
73190979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 822
Checksum: 316
Coasting Arc #13 (Orbit 837)
---------------------------------------
Vector Time (GMT): 2010/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4294971
38 A = 6723937
50 meter
Y = -1459600
96 meter E =
0007505
Z = 4966305
10 I = 51
84424
XDOT = 4429
928434 Wp = 186
21157
YDOT = -5941
329552 meter/sec RA = 139
43465 deg
ZDOT = 2077
925024 TA = 243
67008
MA = 243
74718
Ha = 190
802 n
mi
Hp = 187
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14091113
46 X = -4302456
65
Y = -4788717
05 feet Y = -1507672
29 meter
Z = 16293651
90 Z = 4945421
27
XDOT = 14533
885939 XDOT = 4485
941808
YDOT = -19492
551023 feet/sec YDOT = -5891
478461 meter/sec
ZDOT = 6817
339318 ZDOT = 2099
581584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11138789
34 X = 3395102
99
Y = -10007274
48 feet Y = -3050217
26 meter
Z = 16209756
67 Z = 4940733
83
XDOT = 9131
913601 XDOT = 2783
407266
YDOT = 21385
642521 feet/sec YDOT = 6518
343840 meter/sec
ZDOT = 6904
394951 ZDOT = 2104
459581
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 10326
55124832
00016717 00000-0 10270-3 0 9122
2 25544 51
6402 140
1400 0007190 235
8596 124
1885 15
73170095 8381
Satellite: ISS
Catalog Number: 25544
Epoch time: 10326
55124832 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 140
1400 deg
Eccentricity:
0007190
Arg of perigee: 235
8596 deg
Mean anomaly: 124
1885 deg
Mean motion: 15
73170095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 838
Checksum: 287
Coasting Arc #14 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2010/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3191239
44 A = 6732472
97 meter
Y = 5564130
97 meter E =
0002235
Z = -2041042
36 I = 51
89695
XDOT = -5208
207116 Wp = 303
23093
YDOT = -936
136435 meter/sec RA = 134
28552 deg
ZDOT = 5588
007339 TA = 34
10461
MA = 34
09025
Ha = 190
498 n
mi
Hp = 187
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10469945
66 X = -3243306
19
Y = 18255022
85 feet Y = 5528153
72 meter
Z = -6696333
21 Z = -2056671
55
XDOT = -17087
293689 XDOT = -5224
498050
YDOT = -3071
313763 feet/sec YDOT = -994
469472 meter/sec
ZDOT = 18333
357411 ZDOT = 5562
665675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11088068
98 X = -3379643
43
Y = -17862660
26 feet Y = -5444538
85 meter
Z = -6759185
96 Z = -2060199
88
XDOT = 9584
198114 XDOT = 2921
263585
YDOT = -12851
974354 feet/sec YDOT = -3917
281783 meter/sec
ZDOT = 18231
535446 ZDOT = 5556
972004
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 10327
50406066
00016717 00000-0 10270-3 0 9131
2 25544 51
6408 135
2519 0007209 238
3878 121
6582 15
73246979 8533
Satellite: ISS
Catalog Number: 25544
Epoch time: 10327
50406066 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 135
2519 deg
Eccentricity:
0007209
Arg of perigee: 238
3878 deg
Mean anomaly: 121
6582 deg
Mean motion: 15
73246979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 853
Checksum: 318
Coasting Arc #15 (Orbit 868)
---------------------------------------
Vector Time (GMT): 2010/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4714970
40 A = 6724251
80 meter
Y = 171018
41 meter E =
0004768
Z = -4795387
23 I = 51
89089
XDOT = -2848
686568 Wp = 85
53461
YDOT = 6673
251547 meter/sec RA = 129
21276 deg
ZDOT = -2564
736790 TA = 159
41607
MA = 159
39685
Ha = 190
266 n
mi
Hp = 187
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15469062
98 X = 4736003
08
Y = 561084
04 feet Y = 223862
20 meter
Z = -15732897
74 Z = -4772430
44
XDOT = -9346
084540 XDOT = -2910
637170
YDOT = 21893
869906 feet/sec YDOT = 6641
049732 meter/sec
ZDOT = -8414
490782 ZDOT = -2578
725635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7669610
05 X = -2337697
14
Y = 13552795
18 feet Y = 4130891
97 meter
Z = -15640640
03 Z = -4767267
08
XDOT = -14157
360832 XDOT = -4315
163581
YDOT = -17780
565618 feet/sec YDOT = -5419
516400 meter/sec
ZDOT = -8470
777435 ZDOT = -2581
892962
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 10328
52036213
00016717 00000-0 10270-3 0 9148
2 25544 51
6415 130
0393 0007024 242
6102 117
4346 15
73315836 8694
Satellite: ISS
Catalog Number: 25544
Epoch time: 10328
52036213 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 130
0393 deg
Eccentricity:
0007024
Arg of perigee: 242
6102 deg
Mean anomaly: 117
4346 deg
Mean motion: 15
73315836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 869
Checksum: 276
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list