Date:
November 16th 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 679)
---------------------------------------
Vector Time (GMT): 2010/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2548706
40 A = 6724577
69 meter
Y = 3619502
20 meter E =
0015359
Z = -5074322
07 I = 51
56251
XDOT = -7031
216256 Wp = 131
26320
YDOT = -2642
732482 meter/sec RA = 190
62157 deg
ZDOT = 1639
813964 TA = 154
57551
MA = 154
49987
Ha = 193
057 n
mi
Hp = 185
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8361897
65 X = -2564340
50
Y = 11875007
23 feet Y = 3590913
80 meter
Z = -16648038
29 Z = -5086741
68
XDOT = -23068
294802 XDOT = -7009
108162
YDOT = -8670
382158 feet/sec YDOT = -2721
236216 meter/sec
ZDOT = 5379
967073 ZDOT = 1605
709525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3962545
40 X = -1207783
84
Y = -13913054
71 feet Y = -4240699
08 meter
Z = -16697887
60 Z = -5089516
14
XDOT = 20319
425069 XDOT = 6193
360761
YDOT = -12106
097178 feet/sec YDOT = -3689
938420 meter/sec
ZDOT = 5243
068986 ZDOT = 1598
087427
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
51319319
00016717 00000-0 10270-3 0 9000
2 25544 51
6457 191
6120 0007383 193
9757 166
1202 15
72729061 6804
Satellite: ISS
Catalog Number: 25544
Epoch time: 10316
51319319 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 191
6120 deg
Eccentricity:
0007383
Arg of perigee: 193
9757 deg
Mean anomaly: 166
1202 deg
Mean motion: 15
72729061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 680
Checksum: 298
Coasting Arc #2 (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 = 6479322
37 A = 6735366
76 meter
Y = 1464696
15 meter E =
0015340
Z = -1054625
64 I = 51
62885
XDOT = -1979
154427 Wp = 166
42931
YDOT = 4516
674067 meter/sec RA = 185
51666 deg
ZDOT = -5918
406017 TA = 25
10742
MA = 25
03291
Ha = 193
039 n
mi
Hp = 186
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21257619
33 X = 6467585
55
Y = 4805433
55 feet Y = 1537086
22 meter
Z = -3460057
86 Z = -1023177
18
XDOT = -6493
288802 XDOT = -2000
762723
YDOT = 14818
484471 feet/sec YDOT = 4494
421269 meter/sec
ZDOT = -19417
342575 ZDOT = -5928
073265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16955022
76 X = -5167890
94
Y = 13724558
12 feet Y = 4183245
32 meter
Z = -3333808
49 Z = -1016144
83
XDOT = -6678
764035 XDOT = -2035
687278
YDOT = -12950
445956 feet/sec YDOT = -3947
295928 meter/sec
ZDOT = -19456
145130 ZDOT = -5930
233036
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
52984099
00016717 00000-0 10270-3 0 9016
2 25544 51
6457 186
4017 0007566 198
1485 161
9408 15
72723364 6967
Satellite: ISS
Catalog Number: 25544
Epoch time: 10317
52984099 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 186
4017 deg
Eccentricity:
0007566
Arg of perigee: 198
1485 deg
Mean anomaly: 161
9408 deg
Mean motion: 15
72723364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 337
Coasting Arc #3 (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 = 874510
63 A = 6723609
14 meter
Y = -4135325
19 meter E =
0005390
Z = 5228429
43 I = 51
62068
XDOT = 7633
943651 Wp = 181
66453
YDOT = 654
927976 meter/sec RA = 180
37296 deg
ZDOT = -764
166866 TA = 275
57779
MA = 275
63925
Ha = 192
641 n
mi
Hp = 186
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2869129
35 X = 895288
48
Y = -13567339
87 feet Y = -4125429
75 meter
Z = 17153639
86 Z = 5232728
30
XDOT = 25045
746885 XDOT = 7629
764984
YDOT = 2148
713833 feet/sec YDOT = 740
271968 meter/sec
ZDOT = -2507
109141 ZDOT = -727
090786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9115248
62 X = 2778327
78
Y = 10422315
42 feet Y = 3176721
74 meter
Z = 17170892
78 Z = 5233688
12
XDOT = -16135
136818 XDOT = -4917
989702
YDOT = 17968
199682 feet/sec YDOT = 5476
707263 meter/sec
ZDOT = -2358
255459 ZDOT = -718
796264
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
54645425
00016717 00000-0 10270-3 0 9027
2 25544 51
6456 181
1904 0007376 202
6905 157
3932 15
72826077 7125
Satellite: ISS
Catalog Number: 25544
Epoch time: 10318
54645425 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 181
1904 deg
Eccentricity:
0007376
Arg of perigee: 202
6905 deg
Mean anomaly: 157
3932 deg
Mean motion: 15
72826077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 306
Coasting Arc #4 (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 = -6719492
70 A = 6735329
54 meter
Y = 318609
32 meter E =
0006402
Z = 301537
51 I = 51
69025
XDOT = 48
345018 Wp = 72
48377
YDOT = -4782
450197 meter/sec RA = 175
25589 deg
ZDOT = 6027
714693 TA = 290
78777
MA = 290
85634
Ha = 192
397 n
mi
Hp = 186
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22045579
73 X = -6724020
88
Y = 1045306
16 feet Y = 243442
59 meter
Z = 989296
29 Z = 268882
65
XDOT = 158
612265 XDOT = 72
537617
YDOT = -15690
453401 feet/sec YDOT = -4781
774307 meter/sec
ZDOT = 19775
966839 ZDOT = 6028
008320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12216451
03 X = 3723574
27
Y = -18387517
59 feet Y = -5604515
36 meter
Z = 858183
60 Z = 261574
36
XDOT = 11277
426562 XDOT = 3437
359616
YDOT = 8433
780220 feet/sec YDOT = 2570
616211 meter/sec
ZDOT = 19777
138990 ZDOT = 6028
071964
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
56303584
00016717 00000-0 10270-3 0 9038
2 25544 51
6448 175
9784 0007380 207
2143 152
8633 15
72881728 7282
Satellite: ISS
Catalog Number: 25544
Epoch time: 10319
56303584 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 175
9784 deg
Eccentricity:
0007380
Arg of perigee: 207
2143 deg
Mean anomaly: 152
8633 deg
Mean motion: 15
72881728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 324
Coasting Arc #5 (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 = 760164
01 A = 6723163
67 meter
Y = 4103826
28 meter E =
0012787
Z = -5280401
46 I = 51
67876
XDOT = -7571
172591 Wp = 118
78937
YDOT = 1353
085134 meter/sec RA = 170
12916 deg
ZDOT = -44
468444 TA = 150
82414
MA = 150
75265
Ha = 192
146 n
mi
Hp = 186
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2493976
40 X = 739869
53
Y = 13463996
98 feet Y = 4112213
41 meter
Z = -17324151
79 Z = -5276757
81
XDOT = -24839
805088 XDOT = -7585
524303
YDOT = 4439
255688 feet/sec YDOT = 1268
339482 meter/sec
ZDOT = -145
893844 ZDOT = -81
284831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12485828
13 X = -3805680
41
Y = -5666576
16 feet Y = -1727172
41 meter
Z = -17309517
00 Z = -5275940
78
XDOT = 10328
057616 XDOT = 3147
991961
YDOT = -21921
142236 feet/sec YDOT = -6681
564153 meter/sec
ZDOT = -293
725983 ZDOT = -89
527680
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
51605266
00016717 00000-0 10270-3 0 9048
2 25544 51
6436 171
0918 0007313 211
3019 148
7709 15
72926425 7438
Satellite: ISS
Catalog Number: 25544
Epoch time: 10320
51605266 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 171
0918 deg
Eccentricity:
0007313
Arg of perigee: 211
3019 deg
Mean anomaly: 148
7709 deg
Mean motion: 15
72926425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 743
Checksum: 290
Coasting Arc #6 (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 = 6404139
30 A = 6735080
53 meter
Y = -2018845
99 meter E =
0015489
Z = 371641
34 I = 51
74919
XDOT = 1758
138546 Wp = 159
18202
YDOT = 4454
675556 meter/sec RA = 165
00380 deg
ZDOT = -6035
178857 TA = 16
78276
MA = 16
73156
Ha = 191
950 n
mi
Hp = 186
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21010955
72 X = 6424433
03
Y = -6623510
47 feet Y = -1947117
59 meter
Z = 1219295
75 Z = 402802
70
XDOT = 5768
171082 XDOT = 1737
513393
YDOT = 14615
077283 feet/sec YDOT = 4474
220828 meter/sec
ZDOT = -19800
455569 ZDOT = -6026
687688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6379921
37 X = -1944600
03
Y = 21078589
66 feet Y = 6424754
13 meter
Z = 1344430
96 Z = 409782
56
XDOT = -13850
096844 XDOT = -4221
509518
YDOT = -2919
501235 feet/sec YDOT = -889
863977 meter/sec
ZDOT = -19766
356527 ZDOT = -6024
785469
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
53257253
00016717 00000-0 10270-3 0 9051
2 25544 51
6438 165
8810 0007318 215
4177 144
6501 15
72956584 7598
Satellite: ISS
Catalog Number: 25544
Epoch time: 10321
53257253 = yrday
fracday
Element set: 905
Inclination: 51
6438 deg
RA of node: 165
8810 deg
Eccentricity:
0007318
Arg of perigee: 215
4177 deg
Mean anomaly: 144
6501 deg
Mean motion: 15
72956584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 313
Coasting Arc #7 (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 = -2254576
21 A = 6723251
56 meter
Y = -3570578
98 meter E =
0007512
Z = 5234012
37 I = 51
73746
XDOT = 6950
000854 Wp = 193
96406
YDOT = -3212
318179 meter/sec RA = 159
89336 deg
ZDOT = 795
430967 TA = 248
43355
MA = 248
51362
Ha = 191
823 n
mi
Hp = 186
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7396903
58 X = -2239908
35
Y = -11714497
98 feet Y = -3595709
09 meter
Z = 17171956
61 Z = 5223094
90
XDOT = 22801
840073 XDOT = 6981
540881
YDOT = -10539
101638 feet/sec YDOT = -3134
422753 meter/sec
ZDOT = 2609
681651 ZDOT = 829
271559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13907406
36 X = 4238977
46
Y = 177370
10 feet Y = 54062
41 meter
Z = 17128115
11 Z = 5220649
49
XDOT = -3713
120910 XDOT = -1131
759253
YDOT = 23812
963297 feet/sec YDOT = 7258
191213 meter/sec
ZDOT = 2745
590269 ZDOT = 836
855914
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
54906020
00016717 00000-0 10270-3 0 9067
2 25544 51
6426 160
6680 0007281 219
3639 140
6995 15
72975833 7757
Satellite: ISS
Catalog Number: 25544
Epoch time: 10322
54906020 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 160
6680 deg
Eccentricity:
0007281
Arg of perigee: 219
3639 deg
Mean anomaly: 140
6995 deg
Mean motion: 15
72975833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 318
Coasting Arc #8 (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 = -5648195
93 A = 6734413
78 meter
Y = 3527510
07 meter E =
0002540
Z = -993729
59 I = 51
80281
XDOT = -3299
427531 Wp = 21
88746
YDOT = -3611
660649 meter/sec RA = 154
75674 deg
ZDOT = 5940
000923 TA = 327
28798
MA = 327
30370
Ha = 191
474 n
mi
Hp = 186
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18530826
55 X = -5682393
91
Y = 11573195
76 feet Y = 3464157
37 meter
Z = -3260267
67 Z = -1021252
27
XDOT = -10824
893476 XDOT = -3287
652348
YDOT = -11849
280344 feet/sec YDOT = -3648
491221 meter/sec
ZDOT = 19488
192004 ZDOT = 5924
000294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 136328
48 X = 41552
92
Y = -21830683
35 feet Y = -6653992
29 meter
Z = -3370818
47 Z = -1027425
47
XDOT = 14272
938794 XDOT = 4350
391744
YDOT = -2906
561052 feet/sec YDOT = -885
919809 meter/sec
ZDOT = 19423
935892 ZDOT = 5920
415660
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
50198562
00016717 00000-0 10270-3 0 9079
2 25544 51
6414 155
7803 0007361 223
8520 136
2059 15
73051028 7905
Satellite: ISS
Catalog Number: 25544
Epoch time: 10323
50198562 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 155
7803 deg
Eccentricity:
0007361
Arg of perigee: 223
8520 deg
Mean anomaly: 136
2059 deg
Mean motion: 15
73051028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 790
Checksum: 288
Coasting Arc #9 (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 = 3429681
07 A = 6723356
99 meter
Y = 2674829
27 meter E =
0008616
Z = -5133615
15 I = 51
79213
XDOT = -5871
208081 Wp = 105
52342
YDOT = 4756
977205 meter/sec RA = 149
66106 deg
ZDOT = -1448
132123 TA = 150
64194
MA = 150
59351
Ha = 191
282 n
mi
Hp = 186
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11252234
50 X = 3424454
65
Y = 8775686
57 feet Y = 2713153
12 meter
Z = -16842569
40 Z = -5116965
79
XDOT = -19262
493703 XDOT = -5916
930144
YDOT = 15606
880595 feet/sec YDOT = 4691
066270 meter/sec
ZDOT = -4751
089642 ZDOT = -1476
766067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13403259
00 X = -4085313
34
Y = 5121135
37 feet Y = 1560922
06 meter
Z = -16775703
28 Z = -5113234
36
XDOT = -2932
776519 XDOT = -893
910283
YDOT = -23570
144110 feet/sec YDOT = -7184
179925 meter/sec
ZDOT = -4866
126155 ZDOT = -1483
195252
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
51840924
00016717 00000-0 10270-3 0 9088
2 25544 51
6404 150
5674 0007277 227
0176 133
0377 15
73111476 8062
Satellite: ISS
Catalog Number: 25544
Epoch time: 10324
51840924 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 150
5674 deg
Eccentricity:
0007277
Arg of perigee: 227
0176 deg
Mean anomaly: 133
0377 deg
Mean motion: 15
73111476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 294
Coasting Arc #10 (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 = 4546791
15 A = 6733390
76 meter
Y = -4713969
43 meter E =
0012706
Z = 1527142
45 I = 51
85316
XDOT = 4457
202151 Wp = 148
88406
YDOT = 2416
818013 meter/sec RA = 144
51841 deg
ZDOT = -5799
645949 TA = 14
33287
MA = 14
29685
Ha = 190
789 n
mi
Hp = 187
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14917293
81 X = 4591746
91
Y = -15465778
96 feet Y = -4662873
24 meter
Z = 5010309
87 Z = 1549340
17
XDOT = 14623
366636 XDOT = 4458
019990
YDOT = 7929
192955 feet/sec YDOT = 2466
666204 meter/sec
ZDOT = -19027
709807 ZDOT = -5777
990054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5805826
30 X = 1769615
86
Y = 20666556
11 feet Y = 6299166
30 meter
Z = 5099511
53 Z = 1554331
11
XDOT = -12788
423495 XDOT = -3897
911481
YDOT = 8274
770459 feet/sec YDOT = 2522
150036 meter/sec
ZDOT = -18940
726611 ZDOT = -5773
133471
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
53479768
00016717 00000-0 10270-3 0 9096
2 25544 51
6409 145
3542 0007282 233
5439 126
5053 15
73205952 8222
Satellite: ISS
Catalog Number: 25544
Epoch time: 10325
53479768 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 145
3542 deg
Eccentricity:
0007282
Arg of perigee: 233
5439 deg
Mean anomaly: 126
5053 deg
Mean motion: 15
73205952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 822
Checksum: 312
Coasting Arc #11 (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 = -4260105
28 A = 6723829
14 meter
Y = -1506044
71 meter E =
0007491
Z = 4982334
27 I = 51
84394
XDOT = 4473
702488 Wp = 187
13653
YDOT = -5926
173972 meter/sec RA = 139
43395 deg
ZDOT = 2026
904062 TA = 243
25875
MA = 243
33543
Ha = 190
787 n
mi
Hp = 187
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13976723
37 X = -4267151
66
Y = -4941091
56 feet Y = -1553723
69 meter
Z = 16346241
03 Z = 4961620
89
XDOT = 14677
501600 XDOT = 4529
790992
YDOT = -19442
827991 feet/sec YDOT = -5875
832947 meter/sec
ZDOT = 6649
947710 ZDOT = 2048
773465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11215494
52 X = 3418482
73
Y = -9833070
96 feet Y = -2997120
03 meter
Z = 16263030
96 Z = 4956971
84
XDOT = 9030
288535 XDOT = 2752
431946
YDOT = 21481
599208 feet/sec YDOT = 6547
591439 meter/sec
ZDOT = 6737
858386 ZDOT = 2053
699236
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
55115729
00016717 00000-0 10270-3 0 9105
2 25544 51
6401 140
1402 0007192 235
7378 124
3104 15
73183522 8386
Satellite: ISS
Catalog Number: 25544
Epoch time: 10326
55115729 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 140
1402 deg
Eccentricity:
0007192
Arg of perigee: 235
7378 deg
Mean anomaly: 124
3104 deg
Mean motion: 15
73183522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 838
Checksum: 275
Coasting Arc #12 (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 = -3236060
73 A = 6732515
65 meter
Y = 5555744
29 meter E =
0002276
Z = -1992659
94 I = 51
89718
XDOT = -5171
910254 Wp = 306
90889
YDOT = -998
965029 meter/sec RA = 134
28541 deg
ZDOT = 5610
867197 TA = 30
99263
MA = 30
97920
Ha = 190
481 n
mi
Hp = 187
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10616997
13 X = -3288265
40
Y = 18227507
52 feet Y = 5519265
05 meter
Z = -6537598
22 Z = -2008507
21
XDOT = -16968
209495 XDOT = -5187
612376
YDOT = -3277
444321 feet/sec YDOT = -1056
888883 meter/sec
ZDOT = 18408
356945 ZDOT = 5585
703289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10993422
72 X = -3350795
24
Y = -17979710
37 feet Y = -5480215
72 meter
Z = -6601327
21 Z = -2012084
53
XDOT = 9700
454648 XDOT = 2956
698577
YDOT = -12656
415995 feet/sec YDOT = -3857
675595 meter/sec
ZDOT = 18307
249823 ZDOT = 5580
049746
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
50396066
00016717 00000-0 10270-3 0 9117
2 25544 51
6408 135
2521 0007216 238
2877 121
7583 15
73261823 8539
Satellite: ISS
Catalog Number: 25544
Epoch time: 10327
50396066 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 135
2521 deg
Eccentricity:
0007216
Arg of perigee: 238
2877 deg
Mean anomaly: 121
7583 deg
Mean motion: 15
73261823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 853
Checksum: 300
Coasting Arc #13 (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 = 4687743
49 A = 6724109
68 meter
Y = 234078
59 meter E =
0004935
Z = -4819309
68 I = 51
89050
XDOT = -2906
730888 Wp = 86
00955
YDOT = 6670
778623 meter/sec RA = 129
21181 deg
ZDOT = -2505
223750 TA = 159
56118
MA = 159
54143
Ha = 190
249 n
mi
Hp = 187
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15379735
88 X = 4708189
27
Y = 767974
37 feet Y = 286614
63 meter
Z = -15811383
47 Z = -4796486
58
XDOT = -9536
518663 XDOT = -2968
938632
YDOT = 21885
756638 feet/sec YDOT = 6637
926277 meter/sec
ZDOT = -8219
238024 ZDOT = -2519
495203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7812263
73 X = -2381177
98
Y = 13378588
00 feet Y = 4077793
62 meter
Z = -15719663
67 Z = -4791353
49
XDOT = -14074
571879 XDOT = -4289
929509
YDOT = -17936
459308 feet/sec YDOT = -5467
032797 meter/sec
ZDOT = -8276
660410 ZDOT = -2522
726093
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
52025259
00016717 00000-0 10270-3 0 9124
2 25544 51
6415 130
0393 0007031 242
4885 117
5563 15
73330627 8695
Satellite: ISS
Catalog Number: 25544
Epoch time: 10328
52025259 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 130
0393 deg
Eccentricity:
0007031
Arg of perigee: 242
4885 deg
Mean anomaly: 117
5563 deg
Mean motion: 15
73330627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 869
Checksum: 293
Coasting Arc #14 (Orbit 884)
---------------------------------------
Vector Time (GMT): 2010/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1826951
01 A = 6731526
28 meter
Y = -6021621
30 meter E =
0009503
Z = 2373622
98 I = 51
93391
XDOT = 5451
050753 Wp = 134
95512
YDOT = -485
040986 meter/sec RA = 124
05959 deg
ZDOT = -5419
564313 TA = 18
41147
MA = 18
37710
Ha = 189
908 n
mi
Hp = 187
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5993933
76 X = 1882619
36
Y = -19755975
40 feet Y = -6000880
23 meter
Z = 7787476
97 Z = 2382633
00
XDOT = 17884
024781 XDOT = 5482
396982
YDOT = -1591
341819 feet/sec YDOT = -423
908226 meter/sec
ZDOT = -17780
722812 ZDOT = -5393
006728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15036730
40 X = 4583195
42
Y = 14126434
62 feet Y = 4305737
27 meter
Z = 7823757
89 Z = 2384681
40
XDOT = -5559
532927 XDOT = -1694
545636
YDOT = 15718
140804 feet/sec YDOT = 4790
889317 meter/sec
ZDOT = -17673
973602 ZDOT = -5387
027154
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 10329
53650999
00016717 00000-0 10270-3 0 9132
2 25544 51
6411 124
8248 0007200 247
0951 112
9452 15
73360584 8853
Satellite: ISS
Catalog Number: 25544
Epoch time: 10329
53650999 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 124
8248 deg
Eccentricity:
0007200
Arg of perigee: 247
0951 deg
Mean anomaly: 112
9452 deg
Mean motion: 15
73360584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 885
Checksum: 309
Coasting Arc #15 (Orbit 900)
---------------------------------------
Vector Time (GMT): 2010/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4747635
75 A = 6724510
56 meter
Y = 1061416
32 meter E =
0005981
Z = 4644696
65 I = 51
92792
XDOT = 1282
105057 Wp = 173
96626
YDOT = -7011
172232 meter/sec RA = 118
99178 deg
ZDOT = 2906
575271 TA = 247
33858
MA = 247
40184
Ha = 189
576 n
mi
Hp = 187
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15576232
77 X = -4781715
12
Y = 3482337
02 feet Y = 1008134
46 meter
Z = 15238506
05 Z = 4621549
76
XDOT = 4206
381420 XDOT = 1346
290273
YDOT = -23002
533571 feet/sec YDOT = -6996
476335 meter/sec
ZDOT = 9536
008108 ZDOT = 2912
959089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3593353
59 X = 1095254
17
Y = -15641642
05 feet Y = -4767572
50 meter
Z = 15145448
46 Z = 4616332
69
XDOT = 17841
043926 XDOT = 5437
950189
YDOT = 13376
718038 feet/sec YDOT = 4077
223658 meter/sec
ZDOT = 9561
752077 ZDOT = 2914
422033
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 10330
55273316
00016717 00000-0 10270-3 0 9141
2 25544 51
6420 119
6108 0007191 251
1023 108
9361 15
73440938 9010
Satellite: ISS
Catalog Number: 25544
Epoch time: 10330
55273316 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 119
6108 deg
Eccentricity:
0007191
Arg of perigee: 251
1023 deg
Mean anomaly: 108
9361 deg
Mean motion: 15
73440938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 901
Checksum: 275
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