Date:
May 22nd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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
143/15:22:00
000 0
0 0
0 0
0
N/A 0
0 0
0 191
6
000/00:00:00
000 0
0 0
0 183
0
146/06:34:55
368 1
4 -2
4 2
4
N/A -1
5 0
0 190
5
000/00:09:46
736 -1
3 0
1 182
4
Coasting Arc #1 (Orbit 1926)
---------------------------------------
Vector Time (GMT): 2010/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6250731
73 A = 6729610
55 meter
Y = -1021521
52 meter E =
0014226
Z = -2248654
45 I = 51
70298
XDOT = 2729
775135 Wp =
47364
YDOT = 4688
893631 meter/sec RA = 7
00010 deg
ZDOT = 5472
252683 TA = 334
29271
MA = 334
36335
Ha = 191
596 n
mi
Hp = 183
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20507650
05 X = 6272613
60
Y = -3351448
56 feet Y = -951499
63 meter
Z = -7377475
22 Z = -2218235
19
XDOT = 8955
955166 XDOT = 2650
556882
YDOT = 15383
509287 feet/sec YDOT = 4718
976330 meter/sec
ZDOT = 17953
584918 ZDOT = 5485
321850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7964921
58 X = 2427708
10
Y = -19238738
69 feet Y = -5863967
55 meter
Z = -7256308
73 Z = -2211722
90
XDOT = 16335
869193 XDOT = 4979
172930
YDOT = -10
236758 feet/sec YDOT = -3
120164 meter/sec
ZDOT = 18005
633150 ZDOT = 5488
116984
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 10141
50437152
00016717 00000-0 10270-3 0 9001
2 25544 51
6476 7
5061 0010505 338
1206 21
9508 15
74152520 19270
Satellite: ISS
Catalog Number: 25544
Epoch time: 10141
50437152 = yrday
fracday
Element set: 900
Inclination: 51
6476 deg
RA of node: 7
5061 deg
Eccentricity:
0010505
Arg of perigee: 338
1206 deg
Mean anomaly: 21
9508 deg
Mean motion: 15
74152520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1927
Checksum: 265
Coasting Arc #2 (Orbit 1942)
---------------------------------------
Vector Time (GMT): 2010/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2650206
07 A = 6721541
43 meter
Y = -3894089
81 meter E =
0015769
Z = -4807055
40 I = 51
64534
XDOT = 7069
422994 Wp = 30
25425
YDOT = -1732
005155 meter/sec RA = 1
90506 deg
ZDOT = -2484
586139 TA = 215
36512
MA = 215
46981
Ha = 191
575 n
mi
Hp = 183
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8694901
81 X = -2583112
68
Y = -12775885
20 feet Y = -3923350
58 meter
Z = -15771179
14 Z = -4819767
46
XDOT = 23193
644993 XDOT = 7100
334941
YDOT = -5682
431611 feet/sec YDOT = -1652
777678 meter/sec
ZDOT = -8151
529329 ZDOT = -2450
167602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15378346
99 X = -4687320
16
Y = 855350
49 feet Y = 260710
83 meter
Z = -15821803
66 Z = -4822485
75
XDOT = 7068
587926 XDOT = 2154
505600
YDOT = -21755
751751 feet/sec YDOT = -6631
153134 meter/sec
ZDOT = -8014
436965 ZDOT = -2442
800387
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 10142
52009207
00016717 00000-0 10270-3 0 9011
2 25544 51
6468 2
2889 0010494 341
6611 18
4173 15
74191751 19433
Satellite: ISS
Catalog Number: 25544
Epoch time: 10142
52009207 = yrday
fracday
Element set: 901
Inclination: 51
6468 deg
RA of node: 2
2889 deg
Eccentricity:
0010494
Arg of perigee: 341
6611 deg
Mean anomaly: 18
4173 deg
Mean motion: 15
74191751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1943
Checksum: 288
Coasting Arc #3 (Orbit 1958)
---------------------------------------
Vector Time (GMT): 2010/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6080847
07 A = 6729667
41 meter
Y = 1996861
09 meter E =
0011762
Z = 2081004
25 I = 51
64325
XDOT = -3287
987183 Wp = 63
31386
YDOT = -4205
728600 meter/sec RA = 356
73071 deg
ZDOT = -5542
841984 TA = 93
46289
MA = 93
32834
Ha = 191
709 n
mi
Hp = 183
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19950285
67 X = -6112833
67
Y = 6551381
52 feet Y = 1928682
45 meter
Z = 6827441
77 Z = 2051385
53
XDOT = -10787
359523 XDOT = -3213
787110
YDOT = -13798
322177 feet/sec YDOT = -4242
081597 meter/sec
ZDOT = -18185
177114 ZDOT = -5558
635279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4242704
82 X = -1293176
43
Y = 20604148
09 feet Y = 6280144
34 meter
Z = 6709470
66 Z = 2045046
66
XDOT = -15778
563893 XDOT = -4809
306275
YDOT = 2724
970011 feet/sec YDOT = 830
570859 meter/sec
ZDOT = -18248
068668 ZDOT = -5562
011330
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 10143
53579521
00016717 00000-0 10270-3 0 9025
2 25544 51
6473 357
0720 0010578 345
8232 14
2633 15
74243056 19590
Satellite: ISS
Catalog Number: 25544
Epoch time: 10143
53579521 = yrday
fracday
Element set: 902
Inclination: 51
6473 deg
RA of node: 357
0720 deg
Eccentricity:
0010578
Arg of perigee: 345
8232 deg
Mean anomaly: 14
2633 deg
Mean motion: 15
74243056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1959
Checksum: 299
Coasting Arc #4 (Orbit 1960)
---------------------------------------
Vector Time (GMT): 2010/143/15:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 816784
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4351321
15 A = 6723891
49 meter
Y = -3006403
89 meter E =
0013687
Z = -4164875
98 I = 51
61708
XDOT = 5856
453736 Wp = 22
79990
YDOT = -3341
035565 meter/sec RA = 356
04983 deg
ZDOT = -3698
567161 TA = 209
31561
MA = 209
39247
Ha = 191
589 n
mi
Hp = 182
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14275988
03 X = -4297147
10
Y = -9863529
83 feet Y = -3054759
77 meter
Z = -13664291
28 Z = -4185883
61
XDOT = 19214
087062 XDOT = 5911
345753
YDOT = -10961
402772 feet/sec YDOT = -3275
238045 meter/sec
ZDOT = -12134
406697 ZDOT = -3669
982997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4163634
03 X = -1269075
65
Y = 16776884
52 feet Y = 5113594
40 meter
Z = -13747952
88 Z = -4190376
04
XDOT = -15886
303044 XDOT = -4842
145168
YDOT = -13815
236931 feet/sec YDOT = -4210
884216 meter/sec
ZDOT = -12020
553031 ZDOT = -3663
864564
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 10143
66275862
00016717 00000-0 10270-3 0 9031
2 25544 51
6447 356
4159 0010033 347
3896 12
7015 15
74234595 19617
Satellite: ISS
Catalog Number: 25544
Epoch time: 10143
66275862 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 356
4159 deg
Eccentricity:
0010033
Arg of perigee: 347
3896 deg
Mean anomaly: 12
7015 deg
Mean motion: 15
74234595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1961
Checksum: 312
Coasting Arc #5 (Orbit 1976)
---------------------------------------
Vector Time (GMT): 2010/144/15:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 816784
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4934911
85 A = 6727305
93 meter
Y = 3318980
65 meter E =
0014327
Z = 3144965
72 I = 51
59731
XDOT = -5150
967319 Wp = 51
90375
YDOT = -3053
951701 meter/sec RA = 350
85965 deg
ZDOT = -4836
108195 TA = 91
47474
MA = 91
31061
Ha = 191
712 n
mi
Hp = 182
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16190655
69 X = -4986936
46
Y = 10889044
13 feet Y = 3263504
36 meter
Z = 10318129
00 Z = 3120865
41
XDOT = -16899
499078 XDOT = -5092
941292
YDOT = -10019
526579 feet/sec YDOT = -3111
228019 meter/sec
ZDOT = -15866
496702 ZDOT = -4860
991360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16153964
74 X = 4923728
45
Y = 11033122
50 feet Y = 3362895
74 meter
Z = 10222134
36 Z = 3115706
55
XDOT = -2243
507585 XDOT = -683
821112
YDOT = 18149
193012 feet/sec YDOT = 5531
874030 meter/sec
ZDOT = -15965
587759 ZDOT = -4866
311149
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 10144
67844276
00016717 00000-0 10270-3 0 9045
2 25544 51
6439 351
1976 0009959 350
3686 9
7285 15
74230142 19779
Satellite: ISS
Catalog Number: 25544
Epoch time: 10144
67844276 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 351
1976 deg
Eccentricity:
0009959
Arg of perigee: 350
3686 deg
Mean anomaly: 9
7285 deg
Mean motion: 15
74230142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1977
Checksum: 338
Coasting Arc #6 (Orbit 1992)
---------------------------------------
Vector Time (GMT): 2010/145/15:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 816784
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4622317
40 A = 6723255
11 meter
Y = 2331557
32 meter E =
0010579
Z = 4278423
63 I = 51
55554
XDOT = -5390
951058 Wp = 49
77371
YDOT = 4244
088691 meter/sec RA = 345
76717 deg
ZDOT = 3512
459014 TA = 4
65193
MA = 4
64210
Ha = 191
604 n
mi
Hp = 182
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15165083
33 X = 4575117
76
Y = 7649466
29 feet Y = 2382982
44 meter
Z = 14036822
93 Z = 4300764
89
XDOT = -17686
847304 XDOT = -5455
071769
YDOT = 13924
175495 feet/sec YDOT = 4183
444949 meter/sec
ZDOT = 11523
815664 ZDOT = 3486
113999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1199381
78 X = 365571
57
Y = -16868611
34 feet Y = -5141552
74 meter
Z = 14125789
17 Z = 4305540
54
XDOT = 18491
939137 XDOT = 5636
343049
YDOT = 10874
147673 feet/sec YDOT = 3314
440211 meter/sec
ZDOT = 11418
875896 ZDOT = 3480
473373
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 10145
69410890
00016717 00000-0 10270-3 0 9050
2 25544 51
6445 345
9799 0009935 353
9750 6
1292 15
74293803 19935
Satellite: ISS
Catalog Number: 25544
Epoch time: 10145
69410890 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 345
9799 deg
Eccentricity:
0009935
Arg of perigee: 353
9750 deg
Mean anomaly: 6
1292 deg
Mean motion: 15
74293803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1993
Checksum: 339
Coasting Arc #7 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2010/146/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3455476
85 A = 6719365
23 meter
Y = 3003612
64 meter E =
0006499
Z = 4913656
14 I = 51
53049
XDOT = -6351
561545 Wp = 27
47060
YDOT = 3796
184205 meter/sec RA = 342
48675 deg
ZDOT = 2150
691242 TA = 41
67002
MA = 41
62052
Ha = 190
499 n
mi
Hp = 182
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11336866
29 X = 3397762
99
Y = 9854372
17 feet Y = 3041930
50 meter
Z = 16120919
10 Z = 4930303
37
XDOT = -20838
456513 XDOT = -6403
986960
YDOT = 12454
672587 feet/sec YDOT = 3724
863857 meter/sec
ZDOT = 7056
073627 ZDOT = 2119
707917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7848965
35 X = 2392364
64
Y = 12723419
48 feet Y = 3878098
26 meter
Z = 16187203
60 Z = 4933859
66
XDOT = -22690
178826 XDOT = -6915
966506
YDOT = 5196
292032 feet/sec YDOT = 1583
829811 meter/sec
ZDOT = 6932
661296 ZDOT = 2113
075163
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 10146
32887326
00016717 00000-0 10270-3 0 9064
2 25544 51
6466 342
7241 0009407 347
1437 12
9485 15
74770676 20036
Satellite: ISS
Catalog Number: 25544
Epoch time: 10146
32887326 = yrday
fracday
Element set: 906
Inclination: 51
6466 deg
RA of node: 342
7241 deg
Eccentricity:
0009407
Arg of perigee: 347
1437 deg
Mean anomaly: 12
9485 deg
Mean motion: 15
74770676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 314
Coasting Arc #8 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2010/147/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5395325
34 A = 6728861
62 meter
Y = -3658942
81 meter E =
0016159
Z = -1628803
29 I = 51
53409
XDOT = 3955
346921 Wp = 11
57838
YDOT = 3288
593047 meter/sec RA = 337
30540 deg
ZDOT = 5739
737434 TA = 330
38705
MA = 330
47845
Ha = 190
766 n
mi
Hp = 182
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17701198
62 X = 5443751
87
Y = -12004405
53 feet Y = -3598338
05 meter
Z = -5343842
82 Z = -1602475
28
XDOT = 12976
859977 XDOT = 3890
396239
YDOT = 10789
347267 feet/sec YDOT = 3332
460063 meter/sec
ZDOT = 18831
159560 ZDOT = 5758
795563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20366561
48 X = 6207727
94
Y = -6614471
66 feet Y = -2016090
96 meter
Z = -5238967
37 Z = -1596837
25
XDOT = 8885
180884 XDOT = 2708
203133
YDOT = 12450
228407 feet/sec YDOT = 3794
829618 meter/sec
ZDOT = 18907
042862 ZDOT = 5762
866664
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 10147
28075520
00016717 00000-0 10270-3 0 9076
2 25544 51
6469 337
8306 0009543 350
8050 9
2937 15
74774592 20187
Satellite: ISS
Catalog Number: 25544
Epoch time: 10147
28075520 = yrday
fracday
Element set: 907
Inclination: 51
6469 deg
RA of node: 337
8306 deg
Eccentricity:
0009543
Arg of perigee: 350
8050 deg
Mean anomaly: 9
2937 deg
Mean motion: 15
74774592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2018
Checksum: 317
Coasting Arc #9 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2010/148/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3422678
62 A = 6718512
63 meter
Y = -2773154
39 meter E =
0017713
Z = -5086498
75 I = 51
47293
XDOT = 6000
102636 Wp = 45
54195
YDOT = -4556
269405 meter/sec RA = 332
18223 deg
ZDOT = -1544
467108 TA = 209
53331
MA = 209
63348
Ha = 190
783 n
mi
Hp = 181
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11229260
56 X = -3366704
72
Y = -9098275
55 feet Y = -2811115
00 meter
Z = -16687988
04 Z = -5102990
85
XDOT = 19685
376104 XDOT = 6058
108556
YDOT = -14948
390437 feet/sec YDOT = -4488
848100 meter/sec
ZDOT = -5067
149304 ZDOT = -1515
178091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8372061
34 X = -2551804
30
Y = -11687064
32 feet Y = -3562217
20 meter
Z = -16753655
48 Z = -5106514
19
XDOT = 22079
308291 XDOT = 6729
773167
YDOT = -8678
288955 feet/sec YDOT = -2645
142473 meter/sec
ZDOT = -4950
471070 ZDOT = -1508
903582
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 10148
29607790
00016717 00000-0 10270-3 0 9089
2 25544 51
6475 332
6107 0009596 354
9281 5
1783 15
74824632 20348
Satellite: ISS
Catalog Number: 25544
Epoch time: 10148
29607790 = yrday
fracday
Element set: 908
Inclination: 51
6475 deg
RA of node: 332
6107 deg
Eccentricity:
0009596
Arg of perigee: 354
9281 deg
Mean anomaly: 5
1783 deg
Mean motion: 15
74824632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2034
Checksum: 321
Coasting Arc #10 (Orbit 2049)
---------------------------------------
Vector Time (GMT): 2010/149/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5074464
70 A = 6729414
35 meter
Y = 4292521
43 meter E =
0011274
Z = 1051542
88 I = 51
48312
XDOT = -3853
247212 Wp = 80
29089
YDOT = -3096
420022 meter/sec RA = 327
00592 deg
ZDOT = -5899
290767 TA = 88
18848
MA = 88
05936
Ha = 190
924 n
mi
Hp = 181
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16648506
22 X = -5127195
54
Y = 14083075
54 feet Y = 4235480
72 meter
Z = 3449943
84 Z = 1026763
59
XDOT = -12641
887177 XDOT = -3789
678177
YDOT = -10158
858339 feet/sec YDOT = -3139
152860 meter/sec
ZDOT = -19354
628502 ZDOT = -5917
856134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19602922
81 X = -5974970
87
Y = 9586584
32 feet Y = 2921990
90 meter
Z = 3351224
70 Z = 1021453
29
XDOT = -8968
363899 XDOT = -2733
557317
YDOT = -11481
514641 feet/sec YDOT = -3499
565663 meter/sec
ZDOT = -19428
554153 ZDOT = -5921
823306
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 10149
31138391
00016717 00000-0 10270-3 0 9090
2 25544 51
6474 327
3906 0009527 358
4586 1
6546 15
74810391 20509
Satellite: ISS
Catalog Number: 25544
Epoch time: 10149
31138391 = yrday
fracday
Element set: 909
Inclination: 51
6474 deg
RA of node: 327
3906 deg
Eccentricity:
0009527
Arg of perigee: 358
4586 deg
Mean anomaly: 1
6546 deg
Mean motion: 15
74810391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2050
Checksum: 313
Coasting Arc #11 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2010/150/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3317177
45 A = 6717814
40 meter
Y = 2664464
57 meter E =
0008574
Z = 5195045
81 I = 51
42042
XDOT = -5569
909254 Wp = 20
68858
YDOT = 5254
009758 meter/sec RA = 321
86782 deg
ZDOT = 869
301912 TA = 61
05755
MA = 60
97160
Ha = 190
880 n
mi
Hp = 181
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10883128
12 X = 3261899
70
Y = 8741681
67 feet Y = 2701249
25 meter
Z = 17044113
55 Z = 5211026
92
XDOT = -18273
980491 XDOT = -5632
469496
YDOT = 17237
564824 feet/sec YDOT = 5191
373773 meter/sec
ZDOT = 2852
040395 ZDOT = 842
092139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8511110
34 X = 2594186
43
Y = 10965722
94 feet Y = 3342352
35 meter
Z = 17107752
75 Z = 5214443
04
XDOT = -20932
440327 XDOT = -6380
207812
YDOT = 12004
556999 feet/sec YDOT = 3658
988973 meter/sec
ZDOT = 2743
633127 ZDOT = 836
259377
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 10150
32667019
00016717 00000-0 10270-3 0 9109
2 25544 51
6478 322
1704 0009654 1
7074 358
4121 15
74877948 20663
Satellite: ISS
Catalog Number: 25544
Epoch time: 10150
32667019 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 322
1704 deg
Eccentricity:
0009654
Arg of perigee: 1
7074 deg
Mean anomaly: 358
4121 deg
Mean motion: 15
74877948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 306
Coasting Arc #12 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2010/151/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4616201
96 A = 6729548
59 meter
Y = -4858444
57 meter E =
0020013
Z = -463919
74 I = 51
43734
XDOT = 3773
517505 Wp = 24
37915
YDOT = 3022
406650 meter/sec RA = 316
69897 deg
ZDOT = 6005
327654 TA = 330
55400
MA = 330
66660
Ha = 191
048 n
mi
Hp = 181
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15145019
56 X = 4672440
52
Y = -15939778
77 feet Y = -4806508
93 meter
Z = -1522046
41 Z = -441358
42
XDOT = 12380
306776 XDOT = 3710
267151
YDOT = 9916
032315 feet/sec YDOT = 3064
249728 meter/sec
ZDOT = 19702
518551 ZDOT = 6023
506274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18171908
46 X = 5538797
70
Y = -12389328
42 feet Y = -3776267
30 meter
Z = -1432157
09 Z = -436521
48
XDOT = 8995
798864 XDOT = 2741
919494
YDOT = 10952
778600 feet/sec YDOT = 3338
406917 meter/sec
ZDOT = 19774
913679 ZDOT = 6027
393689
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 10151
27848661
00016717 00000-0 10270-3 0 9119
2 25544 51
6482 317
2767 0009762 4
8982 355
2276 15
74896215 20815
Satellite: ISS
Catalog Number: 25544
Epoch time: 10151
27848661 = yrday
fracday
Element set: 911
Inclination: 51
6482 deg
RA of node: 317
2767 deg
Eccentricity:
0009762
Arg of perigee: 4
8982 deg
Mean anomaly: 355
2276 deg
Mean motion: 15
74896215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2081
Checksum: 328
Coasting Arc #13 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2010/152/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3264098
63 A = 6717444
26 meter
Y = -2647110
45 meter E =
0019277
Z = -5254827
31 I = 51
37554
XDOT = 5003
983205 Wp = 58
42343
YDOT = -5837
432109 meter/sec RA = 311
54579 deg
ZDOT = -158
176472 TA = 210
01261
MA = 210
12324
Ha = 191
091 n
mi
Hp = 180
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10708985
01 X = -3208728
62
Y = -8684745
57 feet Y = -2683301
17 meter
Z = -17240247
07 Z = -5270550
17
XDOT = 16417
267732 XDOT = 5069
654908
YDOT = -19151
680149 feet/sec YDOT = -5781
107376 meter/sec
ZDOT = -518
951679 ZDOT = -133
708517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8722316
56 X = -2658562
09
Y = -10576638
05 feet Y = -3223759
28 meter
Z = -17302866
98 Z = -5273913
85
XDOT = 19049
727784 XDOT = 5806
357029
YDOT = -14969
522620 feet/sec YDOT = -4562
710495 meter/sec
ZDOT = -421
466801 ZDOT = -128
463081
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 10152
29373939
00016717 00000-0 10270-3 0 9124
2 25544 51
6480 312
0565 0009842 8
3363 351
7962 15
74934788 20971
Satellite: ISS
Catalog Number: 25544
Epoch time: 10152
29373939 = yrday
fracday
Element set: 912
Inclination: 51
6480 deg
RA of node: 312
0565 deg
Eccentricity:
0009842
Arg of perigee: 8
3363 deg
Mean anomaly: 351
7962 deg
Mean motion: 15
74934788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2097
Checksum: 329
Coasting Arc #14 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2010/153/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4122815
40 A = 6729571
48 meter
Y = 5315883
53 meter E =
0010143
Z = -207261
21 I = 51
39697
XDOT = -3686
957766 Wp = 84
66464
YDOT = -3083
974473 meter/sec RA = 306
38646 deg
ZDOT = -6009
234091 TA = 97
59368
MA = 97
47846
Ha = 191
220 n
mi
Hp = 180
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13526297
25 X = -4180945
32
Y = 17440562
76 feet Y = 5269454
76 meter
Z = -679990
83 Z = -227430
30
XDOT = -12096
318131 XDOT = -3623
006480
YDOT = -10118
026487 feet/sec YDOT = -3124
845871 meter/sec
ZDOT = -19715
334945 ZDOT = -6026
990361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16394581
35 X = -4997068
40
Y = 14772809
88 feet Y = 4502752
45 meter
Z = -760345
00 Z = -231753
16
XDOT = -8923
132743 XDOT = -2719
770860
YDOT = -10883
148952 feet/sec YDOT = -3317
183801 meter/sec
ZDOT = -19786
058193 ZDOT = -6030
790537
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 10153
30897580
00016717 00000-0 10270-3 0 9131
2 25544 51
6480 306
8366 0009688 12
1439 347
9956 15
74904960 21134
Satellite: ISS
Catalog Number: 25544
Epoch time: 10153
30897580 = yrday
fracday
Element set: 913
Inclination: 51
6480 deg
RA of node: 306
8366 deg
Eccentricity:
0009688
Arg of perigee: 12
1439 deg
Mean anomaly: 347
9956 deg
Mean motion: 15
74904960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 329
Coasting Arc #15 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2010/154/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3206350
44 A = 6717420
65 meter
Y = 2758933
31 meter E =
0012031
Z = 5214875
00 I = 51
33953
XDOT = -4395
943945 Wp = 25
50408
YDOT = 6299
159657 meter/sec RA = 301
21637 deg
ZDOT = -618
496031 TA = 70
46028
MA = 70
33040
Ha = 191
167 n
mi
Hp = 180
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10519522
43 X = 3149928
35
Y = 9051618
48 feet Y = 2794472
56 meter
Z = 17109169
93 Z = 5230314
70
XDOT = -14422
388272 XDOT = -4463
051031
YDOT = 20666
534308 feet/sec YDOT = 6249
626449 meter/sec
ZDOT = -2029
186452 ZDOT = -640
013780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8836008
33 X = 2693215
34
Y = 10602305
40 feet Y = 3231582
69 meter
Z = 17170670
41 Z = 5233620
34
XDOT = -16757
673537 XDOT = -5107
738894
YDOT = 17450
599203 feet/sec YDOT = 5318
942637 meter/sec
ZDOT = -2114
907999 ZDOT = -644
623958
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 10154
32419166
00016717 00000-0 10270-3 0 9145
2 25544 51
6478 301
6158 0009882 15
2973 344
8488 15
74985711 21292
Satellite: ISS
Catalog Number: 25544
Epoch time: 10154
32419166 = yrday
fracday
Element set: 914
Inclination: 51
6478 deg
RA of node: 301
6158 deg
Eccentricity:
0009882
Arg of perigee: 15
2973 deg
Mean anomaly: 344
8488 deg
Mean motion: 15
74985711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 331
Coasting Arc #16 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2010/155/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3533266
95 A = 6728953
29 meter
Y = -5645019
20 meter E =
0022403
Z = 867422
69 I = 51
36313
XDOT = 3700
844662 Wp = 39
21185
YDOT = 3239
241412 meter/sec RA = 296
06659 deg
ZDOT = 5939
601664 TA = 330
30590
MA = 330
43288
Ha = 191
236 n
mi
Hp = 180
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11592083
17 X = 3591914
19
Y = -18520404
21 feet Y = -5605180
28 meter
Z = 2845874
98 Z = 884729
20
XDOT = 12141
878811 XDOT = 3635
494275
YDOT = 10627
432455 feet/sec YDOT = 3280
260449 meter/sec
ZDOT = 19486
882100 ZDOT = 5957
421995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14104154
65 X = 4298946
34
Y = -16675054
71 feet Y = -5082556
68 meter
Z = 2914814
02 Z = 888435
31
XDOT = 9167
562228 XDOT = 2794
272967
YDOT = 11209
900998 feet/sec YDOT = 3416
777824 meter/sec
ZDOT = 19557
869291 ZDOT = 5961
238560
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 10155
33939063
00016717 00000-0 10270-3 0 9151
2 25544 51
6469 296
3949 0009899 18
6544 341
4981 15
75016796 21457
Satellite: ISS
Catalog Number: 25544
Epoch time: 10155
33939063 = yrday
fracday
Element set: 915
Inclination: 51
6469 deg
RA of node: 296
3949 deg
Eccentricity:
0009899
Arg of perigee: 18
6544 deg
Mean anomaly: 341
4981 deg
Mean motion: 15
75016796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2145
Checksum: 352
Coasting Arc #17 (Orbit 2159)
---------------------------------------
Vector Time (GMT): 2010/156/06:39:48
736
Vector Time (MET): N/A
Weight (LBS) : 816529
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3266401
14 A = 6717811
26 meter
Y = -2915521
38 meter E =
0018705
Z = -5108710
12 I = 51
31239
XDOT = 3711
832448 Wp = 69
16190
YDOT = -6589
375616 meter/sec RA = 290
88057 deg
ZDOT = 1397
942433 TA = 214
24324
MA = 214
36399
Ha = 191
315 n
mi
Hp = 179
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10716539
16 X = -3208739
18
Y = -9565358
85 feet Y = -2951725
31 meter
Z = -16760859
98 Z = -5124438
60
XDOT = 12177
927979 XDOT = 3778
449182
YDOT = -21618
686403 feet/sec YDOT = -6547
495358 meter/sec
ZDOT = 4586
425305 ZDOT = 1416
135760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9328255
99 X = -2843252
43
Y = -10826801
43 feet Y = -3300009
08 meter
Z = -16823517
46 Z = -5127808
12
XDOT = 13986
877446 XDOT = 4263
200245
YDOT = -19236
051557 feet/sec YDOT = -5863
148515 meter/sec
ZDOT = 4658
890052 ZDOT = 1420
029688
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 10156
29112427
00016717 00000-0 10270-3 0 9165
2 25544 51
6458 291
4997 0009957 22
0376 338
1214 15
75035546 21604
Satellite: ISS
Catalog Number: 25544
Epoch time: 10156
29112427 = yrday
fracday
Element set: 916
Inclination: 51
6458 deg
RA of node: 291
4997 deg
Eccentricity:
0009957
Arg of perigee: 22
0376 deg
Mean anomaly: 338
1214 deg
Mean motion: 15
75035546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2160
Checksum: 313
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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