Date:
December 17th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 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
356/16:34:17
359 -5
0 7
0 7
1
N/A -3
2 -0
9 195
5
000/00:18:34
719 -4
0 -0
2 184
6
Coasting Arc #1 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2010/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 604880
30 A = 6723381
98 meter
Y = 4474846
41 meter E =
0006006
Z = 4976934
05 I = 51
75964
XDOT = -7329
297556 Wp = 34
42683
YDOT = -1248
112481 meter/sec RA = 22
00696 deg
ZDOT = 2016
659426 TA = 36
12384
MA = 36
08328
Ha = 192
645 n
mi
Hp = 184
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1984515
41 X = 530619
46
Y = 14681254
62 feet Y = 4481194
97 meter
Z = 16328523
78 Z = 4979692
53
XDOT = -24046
251823 XDOT = -7324
592868
YDOT = -4094
857222 feet/sec YDOT = -1330
046941 meter/sec
ZDOT = 6616
336700 ZDOT = 1981
064642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14801954
29 X = -4511635
67
Y = 149709
88 feet Y = 45631
57 meter
Z = 16339460
32 Z = 4980267
51
XDOT = 6906
132086 XDOT = 2104
989060
YDOT = -22358
192503 feet/sec YDOT = -6814
777075 meter/sec
ZDOT = 6473
206824 ZDOT = 1973
033440
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 10349
55102650
00016717 00000-0 10270-3 0 9008
2 25544 51
6462 22
2606 0008344 350
5796 9
5209 15
73295571 12001
Satellite: ISS
Catalog Number: 25544
Epoch time: 10349
55102650 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 22
2606 deg
Eccentricity:
0008344
Arg of perigee: 350
5796 deg
Mean anomaly: 9
5209 deg
Mean motion: 15
73295571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 283
Coasting Arc #2 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2010/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6421322
32 A = 6732398
28 meter
Y = 322409
30 meter E =
0014159
Z = -1970850
09 I = 51
76261
XDOT = 1462
417893 Wp = 14
27035
YDOT = 5066
458289 meter/sec RA = 16
85209 deg
ZDOT = 5615
535846 TA = 323
82085
MA = 323
91655
Ha = 192
742 n
mi
Hp = 184
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21067330
44 X = 6426813
98
Y = 1057773
30 feet Y = 394247
27 meter
Z = -6466043
61 Z = -1939641
53
XDOT = 4797
958968 XDOT = 1378
375508
YDOT = 16622
238482 feet/sec YDOT = 5082
341533 meter/sec
ZDOT = 18423
674036 ZDOT = 5622
436663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3170251
33 X = -966292
60
Y = 20892779
64 feet Y = 6368119
24 meter
Z = -6340526
91 Z = -1932592
60
XDOT = -15486
027003 XDOT = -4720
141030
YDOT = 3227
453986 feet/sec YDOT = 983
727975 meter/sec
ZDOT = 18451
244995 ZDOT = 5623
939474
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 10350
50379138
00016717 00000-0 10270-3 0 9013
2 25544 51
6472 17
3738 0008336 354
4270 5
6799 15
73350690 12155
Satellite: ISS
Catalog Number: 25544
Epoch time: 10350
50379138 = yrday
fracday
Element set: 901
Inclination: 51
6472 deg
RA of node: 17
3738 deg
Eccentricity:
0008336
Arg of perigee: 354
4270 deg
Mean anomaly: 5
6799 deg
Mean motion: 15
73350690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1215
Checksum: 302
Coasting Arc #3 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2010/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1906152
28 A = 6723871
57 meter
Y = -4290632
79 meter E =
0016389
Z = -4827381
06 I = 51
70454
XDOT = 7271
494075 Wp = 42
61692
YDOT = -463
459402 meter/sec RA = 11
76543 deg
ZDOT = -2452
332233 TA = 203
36417
MA = 203
43873
Ha = 192
784 n
mi
Hp = 184
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6253780
46 X = -1834581
09
Y = -14076879
23 feet Y = -4311547
84 meter
Z = -15837864
38 Z = -4836467
89
XDOT = 23856
607857 XDOT = 7288
049274
YDOT = -1520
536097 feet/sec YDOT = -382
052351 meter/sec
ZDOT = -8045
709425 ZDOT = -2416
966666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14541310
68 X = 4432191
50
Y = -4966354
98 feet Y = -1513745
00 meter
Z = -15874251
13 Z = -4838471
74
XDOT = -836
044937 XDOT = -254
826497
YDOT = 22887
369822 feet/sec YDOT = 6976
070322 meter/sec
ZDOT = -7903
444442 ZDOT = -2408
969866
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 10351
52005128
00016717 00000-0 10270-3 0 9022
2 25544 51
6472 12
1605 0008392 358
2612 1
8521 15
73355054 12313
Satellite: ISS
Catalog Number: 25544
Epoch time: 10351
52005128 = yrday
fracday
Element set: 902
Inclination: 51
6472 deg
RA of node: 12
1605 deg
Eccentricity:
0008392
Arg of perigee: 358
2612 deg
Mean anomaly: 1
8521 deg
Mean motion: 15
73355054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 259
Coasting Arc #4 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2010/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6225738
42 A = 6731633
08 meter
Y = 1110482
99 meter E =
0014374
Z = 2302780
17 I = 51
69945
XDOT = -2850
165027 Wp = 72
50028
YDOT = -4648
413708 meter/sec RA = 6
59971 deg
ZDOT = -5432
019608 TA = 81
65113
MA = 81
48819
Ha = 192
908 n
mi
Hp = 183
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20425650
98 X = -6248879
96
Y = 3643316
90 feet Y = 1040733
35 meter
Z = 7555053
05 Z = 2272479
08
XDOT = -9350
935127 XDOT = -2771
585668
YDOT = -15250
701143 feet/sec YDOT = -4679
845905 meter/sec
ZDOT = -17821
586640 ZDOT = -5445
675614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2283118
90 X = -695894
64
Y = -20666294
12 feet Y = -6299086
45 meter
Z = 7433132
44 Z = 2265618
77
XDOT = 14321
918570 XDOT = 4365
320780
YDOT = -8050
236816 feet/sec YDOT = -2453
712181 meter/sec
ZDOT = -17876
333064 ZDOT = -5448
706318
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 10352
53628796
00016717 00000-0 10270-3 0 9037
2 25544 51
6458 6
9467 0008524 2
8984 357
2227 15
73408687 12474
Satellite: ISS
Catalog Number: 25544
Epoch time: 10352
53628796 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 6
9467 deg
Eccentricity:
0008524
Arg of perigee: 2
8984 deg
Mean anomaly: 357
2227 deg
Mean motion: 15
73408687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 335
Coasting Arc #5 (Orbit 1262)
---------------------------------------
Vector Time (GMT): 2010/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3042196
01 A = 6724304
10 meter
Y = 3766861
42 meter E =
0009365
Z = 4656993
71 I = 51
64407
XDOT = -6868
887754 Wp = 58
37680
YDOT = 2055
263284 meter/sec RA = 1
51234 deg
ZDOT = 2825
380896 TA = 3
75224
MA = 3
74522
Ha = 192
927 n
mi
Hp = 183
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9980958
04 X = 2977225
12
Y = 12358469
22 feet Y = 3800517
12 meter
Z = 15278850
76 Z = 4671615
59
XDOT = -22535
720977 XDOT = -6905
084892
YDOT = 6742
989776 feet/sec YDOT = 1978
248435 meter/sec
ZDOT = 9269
622361 ZDOT = 2791
923908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12827923
23 X = -3909951
00
Y = 9273597
23 feet Y = 2826592
44 meter
Z = 15337514
32 Z = 4674874
36
XDOT = -4954
383943 XDOT = -1510
096226
YDOT = -21957
824603 feet/sec YDOT = -6692
744939 meter/sec
ZDOT = 9134
967011 ZDOT = 2784
337945
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 10353
55250219
00016717 00000-0 10270-3 0 9042
2 25544 51
6452 1
7326 0008539 6
8264 353
3014 15
73419896 12639
Satellite: ISS
Catalog Number: 25544
Epoch time: 10353
55250219 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 1
7326 deg
Eccentricity:
0008539
Arg of perigee: 6
8264 deg
Mean anomaly: 353
3014 deg
Mean motion: 15
73419896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1263
Checksum: 295
Coasting Arc #6 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2010/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5691617
40 A = 6730747
98 meter
Y = -2443474
28 meter E =
0012808
Z = -2621410
03 I = 51
63607
XDOT = 4078
252199 Wp = 25
51575
YDOT = 3897
417563 meter/sec RA = 356
33858 deg
ZDOT = 5242
647633 TA = 304
67727
MA = 304
79791
Ha = 193
064 n
mi
Hp = 183
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18673285
42 X = 5731252
16
Y = -8016647
89 feet Y = -2379605
15 meter
Z = -8600426
59 Z = -2593664
14
XDOT = 13380
092517 XDOT = 4008
899496
YDOT = 12786
803028 feet/sec YDOT = 3942
634416 meter/sec
ZDOT = 17200
287511 ZDOT = 5262
292044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7419187
89 X = 2261368
47
Y = 18968995
90 feet Y = 5781749
95 meter
Z = -8488722
80 Z = -2587362
71
XDOT = -11818
894465 XDOT = -3602
399033
YDOT = 12324
198902 feet/sec YDOT = 3756
415825 meter/sec
ZDOT = 17279
148390 ZDOT = 5266
684429
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 10354
50518086
00016717 00000-0 10270-3 0 9058
2 25544 51
6458 356
8455 0008547 10
6281 349
5061 15
73477260 12787
Satellite: ISS
Catalog Number: 25544
Epoch time: 10354
50518086 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 356
8455 deg
Eccentricity:
0008547
Arg of perigee: 10
6281 deg
Mean anomaly: 349
5061 deg
Mean motion: 15
73477260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1278
Checksum: 319
Coasting Arc #7 (Orbit 1293)
---------------------------------------
Vector Time (GMT): 2010/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4005909
10 A = 6724730
23 meter
Y = -3000106
29 meter E =
0016470
Z = -4507557
08 I = 51
58462
XDOT = 6113
057050 Wp = 43
71512
YDOT = -3452
384045 meter/sec RA = 351
24945 deg
ZDOT = -3130
032757 TA = 194
94823
MA = 194
99697
Ha = 193
065 n
mi
Hp = 183
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13142746
39 X = -3950166
75
Y = -9842868
41 feet Y = -3044590
38 meter
Z = -14788573
09 Z = -4526882
85
XDOT = 20055
961450 XDOT = 6166
413029
YDOT = -11326
719309 feet/sec YDOT = -3383
725328 meter/sec
ZDOT = -10269
136343 ZDOT = -3100
206513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10031923
57 X = 3057730
30
Y = -12910174
19 feet Y = -3935021
09 meter
Z = -14866191
41 Z = -4531215
14
XDOT = 10092
536375 XDOT = 3076
205087
YDOT = 19547
524553 feet/sec YDOT = 5958
085484 meter/sec
ZDOT = -10149
019025 ZDOT = -3093
420999
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 10355
52134944
00016717 00000-0 10270-3 0 9069
2 25544 51
6446 351
6305 0008574 13
9548 346
1850 15
73491932 12942
Satellite: ISS
Catalog Number: 25544
Epoch time: 10355
52134944 = yrday
fracday
Element set: 906
Inclination: 51
6446 deg
RA of node: 351
6305 deg
Eccentricity:
0008574
Arg of perigee: 13
9548 deg
Mean anomaly: 346
1850 deg
Mean motion: 15
73491932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1294
Checksum: 315
Coasting Arc #8 (Orbit 1309)
---------------------------------------
Vector Time (GMT): 2010/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4955212
43 A = 6729989
65 meter
Y = 3553286
79 meter E =
0016986
Z = 2842995
74 I = 51
57252
XDOT = -5010
116397 Wp = 68
56574
YDOT = -2903
715356 meter/sec RA = 346
06661 deg
ZDOT = -5072
884208 TA = 78
79024
MA = 78
59935
Ha = 193
115 n
mi
Hp = 182
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16257258
64 X = -5008388
33
Y = 11657765
05 feet Y = 3497576
87 meter
Z = 9327413
86 Z = 2818794
84
XDOT = -16437
389754 XDOT = -4952
631155
YDOT = -9526
625185 feet/sec YDOT = -2959
419317 meter/sec
ZDOT = -16643
320892 ZDOT = -5097
084002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11701938
86 X = -3566750
97
Y = -16281149
22 feet Y = -4962494
28 meter
Z = 9229918
79 Z = 2813279
25
XDOT = 8296
137965 XDOT = 2528
662852
YDOT = -15510
173616 feet/sec YDOT = -4727
500918 meter/sec
ZDOT = -16740
554153 ZDOT = -5102
520906
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 10356
53749346
00016717 00000-0 10270-3 0 9070
2 25544 51
6444 346
4157 0008716 16
9979 343
1475 15
73561800 13107
Satellite: ISS
Catalog Number: 25544
Epoch time: 10356
53749346 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 346
4157 deg
Eccentricity:
0008716
Arg of perigee: 16
9979 deg
Mean anomaly: 343
1475 deg
Mean motion: 15
73561800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1310
Checksum: 321
Coasting Arc #9 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2010/356/16:43:34
719
Vector Time (MET): N/A
Weight (LBS) : 812550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6562909
39 A = 6737772
36 meter
Y = 1475221
37 meter E =
0014531
Z = -332585
78 I = 51
57905
XDOT = -770
149745 Wp = 110
68873
YDOT = -4733
991813 meter/sec RA = 345
08396 deg
ZDOT = -6017
145158 TA = 72
92507
MA = 72
76595
Ha = 195
456 n
mi
Hp = 184
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21531854
95 X = -6577302
19
Y = 4839965
11 feet Y = 1401750
54 meter
Z = -1091160
71 Z = -364502
91
XDOT = -2526
738008 XDOT = -687
926141
YDOT = -15531
469203 feet/sec YDOT = -4742
143475 meter/sec
ZDOT = -19741
289889 ZDOT = -6020
687491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21938087
77 X = -6686729
15
Y = -2338700
27 feet Y = -712835
84 meter
Z = -1219613
85 Z = -371738
30
XDOT = 2542
876966 XDOT = 775
068899
YDOT = -13882
268248 feet/sec YDOT = -4231
315362 meter/sec
ZDOT = -19755
351763 ZDOT = -6021
431217
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 10356
72806308
00016717 00000-0 10270-3 0 9084
2 25544 51
6453 345
4403 0006699 61
1127 299
0706 15
72013406 13137
Satellite: ISS
Catalog Number: 25544
Epoch time: 10356
72806308 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 345
4403 deg
Eccentricity:
0006699
Arg of perigee: 61
1127 deg
Mean anomaly: 299
0706 deg
Mean motion: 15
72013406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1313
Checksum: 295
Coasting Arc #10 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2010/357/16:43:34
719
Vector Time (MET): N/A
Weight (LBS) : 812550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1799352
43 A = 6725544
02 meter
Y = 3787942
25 meter E =
0008658
Z = 5250736
49 I = 51
50942
XDOT = -7129
714212 Wp = 74
48131
YDOT = 2899
939219 meter/sec RA = 339
95641 deg
ZDOT = 353
000224 TA = 12
17353
MA = 12
15262
Ha = 195
282 n
mi
Hp = 184
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5903387
25 X = 1731354
37
Y = 12427632
06 feet Y = 3807682
84 meter
Z = 17226825
77 Z = 5259312
96
XDOT = -23391
450827 XDOT = -7163
326770
YDOT = 9514
236284 feet/sec YDOT = 2820
022480 meter/sec
ZDOT = 1158
137217 ZDOT = 318
283160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1730410
83 X = 527429
22
Y = 13605765
67 feet Y = 4147037
38 meter
Z = 17261180
85 Z = 5261207
92
XDOT = -24193
238522 XDOT = -7374
099102
YDOT = 1792
457339 feet/sec YDOT = 546
340997 meter/sec
ZDOT = 1018
363170 ZDOT = 310
397094
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 10357
74515935
00016717 00000-0 10270-3 0 9091
2 25544 51
6451 340
2328 0006590 64
2122 295
9720 15
72098184 13297
Satellite: ISS
Catalog Number: 25544
Epoch time: 10357
74515935 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 340
2328 deg
Eccentricity:
0006590
Arg of perigee: 64
2122 deg
Mean anomaly: 295
9720 deg
Mean motion: 15
72098184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1329
Checksum: 312
Coasting Arc #11 (Orbit 1343)
---------------------------------------
Vector Time (GMT): 2010/358/16:43:34
719
Vector Time (MET): N/A
Weight (LBS) : 812550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5678119
43 A = 6737270
84 meter
Y = -3492667
10 meter E =
0016310
Z = -936508
92 I = 51
52099
XDOT = 3234
678235 Wp = 49
84275
YDOT = 3689
101644 meter/sec RA = 334
81504 deg
ZDOT = 5931
903741 TA = 299
92086
MA = 300
08275
Ha = 195
438 n
mi
Hp = 184
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18629000
76 X = 5721302
41
Y = -11458881
58 feet Y = -3428929
41 meter
Z = -3072535
84 Z = -908820
40
XDOT = 10612
461401 XDOT = 3164
369830
YDOT = 12103
351852 feet/sec YDOT = 3724
880063 meter/sec
ZDOT = 19461
626446 ZDOT = 5947
447210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21161771
58 X = 6450107
98
Y = -5585509
54 feet Y = -1702463
31 meter
Z = -2961016
65 Z = -902517
87
XDOT = 6146
101340 XDOT = 1873
331688
YDOT = 13076
572555 feet/sec YDOT = 3985
739315 meter/sec
ZDOT = 19524
017447 ZDOT = 5950
920518
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 10358
69867049
00016717 00000-0 10270-3 0 9104
2 25544 51
6456 335
3504 0006713 67
6514 292
5359 15
72086252 13443
Satellite: ISS
Catalog Number: 25544
Epoch time: 10358
69867049 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 335
3504 deg
Eccentricity:
0006713
Arg of perigee: 67
6514 deg
Mean anomaly: 292
5359 deg
Mean motion: 15
72086252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1344
Checksum: 321
Coasting Arc #12 (Orbit 1359)
---------------------------------------
Vector Time (GMT): 2010/359/16:43:34
719
Vector Time (MET): N/A
Weight (LBS) : 812550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3694782
44 A = 6726341
67 meter
Y = -2501892
09 meter E =
0020284
Z = -5051380
63 I = 51
45847
XDOT = 5665
120937 Wp = 74
98677
YDOT = -4895
908232 meter/sec RA = 329
70629 deg
ZDOT = -1719
393972 TA = 178
38934
MA = 178
38280
Ha = 195
362 n
mi
Hp = 184
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12121989
64 X = -3641992
78
Y = -8208307
37 feet Y = -2542913
82 meter
Z = -16572771
09 Z = -5069201
66
XDOT = 18586
354780 XDOT = 5727
799272
YDOT = -16062
691050 feet/sec YDOT = -4832
206852 meter/sec
ZDOT = -5641
056337 ZDOT = -1691
721230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9333541
01 X = -2844863
30
Y = -11172537
32 feet Y = -3405389
38 meter
Z = -16644371
61 Z = -5073204
47
XDOT = 21475
130037 XDOT = 6545
619635
YDOT = -9705
484465 feet/sec YDOT = -2958
231665 meter/sec
ZDOT = -5529
554506 ZDOT = -1685
408214
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 10359
71572614
00016717 00000-0 10270-3 0 9110
2 25544 51
6464 330
1423 0006755 71
6268 288
5629 15
72144540 13600
Satellite: ISS
Catalog Number: 25544
Epoch time: 10359
71572614 = yrday
fracday
Element set: 911
Inclination: 51
6464 deg
RA of node: 330
1423 deg
Eccentricity:
0006755
Arg of perigee: 71
6268 deg
Mean anomaly: 288
5629 deg
Mean motion: 15
72144540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1360
Checksum: 304
Coasting Arc #13 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2010/360/16:43:34
719
Vector Time (MET): N/A
Weight (LBS) : 812550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4100728
79 A = 6735713
05 meter
Y = 4924918
88 meter E =
0019991
Z = 2049616
18 I = 51
46365
XDOT = -5014
297482 Wp = 99
74286
YDOT = -1850
070409 meter/sec RA = 324
53989 deg
ZDOT = -5544
314624 TA = 57
33785
MA = 57
14515
Ha = 195
412 n
mi
Hp = 184
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13453834
62 X = -4165451
97
Y = 16157870
34 feet Y = 4878700
05 meter
Z = 6724462
52 Z = 2029538
07
XDOT = -16451
107223 XDOT = -4966
303889
YDOT = -6069
784808 feet/sec YDOT = -1905
874615 meter/sec
ZDOT = -18190
008608 ZDOT = -5568
557447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17176669
42 X = -5235448
84
Y = 12170724
20 feet Y = 3709636
74 meter
Z = 6643518
38 Z = 2024944
40
XDOT = -13359
445989 XDOT = -4071
959137
YDOT = -8794
876627 feet/sec YDOT = -2680
678396 meter/sec
ZDOT = -18287
466649 ZDOT = -5574
019835
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 10360
73276104
00016717 00000-0 10270-3 0 9120
2 25544 51
6460 324
9342 0006744 76
4271 283
7642 15
72135920 13763
Satellite: ISS
Catalog Number: 25544
Epoch time: 10360
73276104 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 324
9342 deg
Eccentricity:
0006744
Arg of perigee: 76
4271 deg
Mean anomaly: 283
7642 deg
Mean motion: 15
72135920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 297
Coasting Arc #14 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2010/361/16:43:34
719
Vector Time (MET): N/A
Weight (LBS) : 812550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4886685
40 A = 6728122
88 meter
Y = 619345
12 meter E =
0014305
Z = 4571966
48 I = 51
41499
XDOT = -3561
184398 Wp = 98
91489
YDOT = 6158
012698 meter/sec RA = 319
44476 deg
ZDOT = 2962
066347 TA = 321
57780
MA = 321
67958
Ha = 195
194 n
mi
Hp = 184
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16032432
42 X = 4857186
86
Y = 2031972
18 feet Y = 673825
77 meter
Z = 14999890
01 Z = 4595634
31
XDOT = -11683
675846 XDOT = -3644
168912
YDOT = 20203
453735 feet/sec YDOT = 6117
725219 meter/sec
ZDOT = 9718
065444 ZDOT = 2944
564966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14994778
19 X = 4570408
39
Y = 5784443
28 feet Y = 1763098
31 meter
Z = 15095076
80 Z = 4600979
41
XDOT = -15808
513264 XDOT = -4818
434843
YDOT = 15718
226339 feet/sec YDOT = 4790
915388 meter/sec
ZDOT = 9647
449197 ZDOT = 2940
542515
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 10361
74977216
00016717 00000-0 10270-3 0 9135
2 25544 51
6463 319
7260 0006728 79
2381 280
9538 15
72189562 13924
Satellite: ISS
Catalog Number: 25544
Epoch time: 10361
74977216 = yrday
fracday
Element set: 913
Inclination: 51
6463 deg
RA of node: 319
7260 deg
Eccentricity:
0006728
Arg of perigee: 79
2381 deg
Mean anomaly: 280
9538 deg
Mean motion: 15
72189562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 333
Coasting Arc #15 (Orbit 1406)
---------------------------------------
Vector Time (GMT): 2010/362/16:43:34
719
Vector Time (MET): N/A
Weight (LBS) : 812550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2055862
40 A = 6733143
99 meter
Y = -5628434
70 meter E =
0011082
Z = -3077385
08 I = 51
40966
XDOT = 5922
405728 Wp = 78
31668
YDOT = -496
225469 meter/sec RA = 314
25991 deg
ZDOT = 4881
111994 TA = 245
91710
MA = 246
03307
Ha = 195
222 n
mi
Hp = 184
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6744955
39 X = 2133597
21
Y = -18465993
12 feet Y = -5605009
95 meter
Z = -10096407
75 Z = -3067209
28
XDOT = 19430
464988 XDOT = 5903
802870
YDOT = -1628
036314 feet/sec YDOT = -430
101920 meter/sec
ZDOT = 16014
146961 ZDOT = 4909
837842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10739649
54 X = 3273445
18
Y = -16491695
48 feet Y = -5026668
78 meter
Z = -10055281
31 Z = -3064849
74
XDOT = 18010
102780 XDOT = 5489
479327
YDOT = 1928
108677 feet/sec YDOT = 587
687525 meter/sec
ZDOT = 16129
716945 ZDOT = 4916
337725
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 10362
70319994
00016717 00000-0 10270-3 0 9146
2 25544 51
6462 314
8429 0006589 82
0444 278
1465 15
72228547 14075
Satellite: ISS
Catalog Number: 25544
Epoch time: 10362
70319994 = yrday
fracday
Element set: 914
Inclination: 51
6462 deg
RA of node: 314
8429 deg
Eccentricity:
0006589
Arg of perigee: 82
0444 deg
Mean anomaly: 278
1465 deg
Mean motion: 15
72228547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1407
Checksum: 325
Coasting Arc #16 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2010/363/16:43:34
719
Vector Time (MET): N/A
Weight (LBS) : 812550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5263998
25 A = 6730340
10 meter
Y = 1482866
18 meter E =
0013282
Z = -3936095
74 I = 51
37985
XDOT = 1156
066251 Wp = 78
66085
YDOT = -6467
007226 meter/sec RA = 309
17031 deg
ZDOT = -3991
253611 TA = 149
72848
MA = 149
65169
Ha = 195
109 n
mi
Hp = 184
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17270335
46 X = -5261067
81
Y = 4865046
52 feet Y = 1424017
72 meter
Z = -12913699
92 Z = -3961661
06
XDOT = 3792
868278 XDOT = 1247
684459
YDOT = -21217
215307 feet/sec YDOT = -6453
566767 meter/sec
ZDOT = -13094
664079 ZDOT = -3985
415474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17825762
68 X = -5433292
46
Y = 1227756
72 feet Y = 374220
25 meter
Z = -13016589
76 Z = -3967456
56
XDOT = 8237
726870 XDOT = 2510
859150
YDOT = -18669
682173 feet/sec YDOT = -5690
519126 meter/sec
ZDOT = -13070
958715 ZDOT = -3984
028216
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 10363
72016835
00016717 00000-0 10270-3 0 9158
2 25544 51
6459 309
6339 0006433 86
1908 273
9990 15
72251450 14234
Satellite: ISS
Catalog Number: 25544
Epoch time: 10363
72016835 = yrday
fracday
Element set: 915
Inclination: 51
6459 deg
RA of node: 309
6339 deg
Eccentricity:
0006433
Arg of perigee: 86
1908 deg
Mean anomaly: 273
9990 deg
Mean motion: 15
72251450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 316
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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