Date:
May 25th 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
146/06:34:54
275 1
4 -2
4 2
4
N/A -1
5 0
0 190
6
000/00:09:48
549 -1
3 0
1 182
4
Coasting Arc #1 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2010/143/17:47:10
694
Vector Time (MET): N/A
Weight (LBS) : 816526
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1022699
64 A = 6719464
79 meter
Y = 4083118
63 meter E =
0008756
Z = 5237144
51 I = 51
60192
XDOT = -7597
015721 Wp = 358
14120
YDOT = 1100
455643 meter/sec RA = 355
51207 deg
ZDOT = 634
195155 TA = 85
87824
MA = 85
77816
Ha = 191
537 n
mi
Hp = 183
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3355313
78 X = 951523
99
Y = 13396058
48 feet Y = 4094156
74 meter
Z = 17182232
64 Z = 5241940
25
XDOT = -24924
592259 XDOT = -7611
837432
YDOT = 3610
418776 feet/sec YDOT = 1015
418372 meter/sec
ZDOT = 2080
692767 ZDOT = 597
252389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4510360
81 X = 1374757
98
Y = -13027386
01 feet Y = -3970747
26 meter
Z = 17201322
36 Z = 5242963
05
XDOT = 21975
847822 XDOT = 6698
238416
YDOT = 10124
225990 feet/sec YDOT = 3085
864082 meter/sec
ZDOT = 1933
554688 ZDOT = 589
347469
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
78971739
00016717 00000-0 10270-3 0 9007
2 25544 51
6473 355
7639 0010323 344
3768 15
7076 15
74259033 19634
Satellite: ISS
Catalog Number: 25544
Epoch time: 10143
78971739 = yrday
fracday
Element set: 900
Inclination: 51
6473 deg
RA of node: 355
7639 deg
Eccentricity:
0010323
Arg of perigee: 344
3768 deg
Mean anomaly: 15
7076 deg
Mean motion: 15
74259033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 325
Coasting Arc #2 (Orbit 1977)
---------------------------------------
Vector Time (GMT): 2010/144/17:47:10
694
Vector Time (MET): N/A
Weight (LBS) : 816526
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6537213
49 A = 6731397
71 meter
Y = -1482422
14 meter E =
0019425
Z = -463510
98 I = 51
61227
XDOT = 1461
897133 Wp = 16
04157
YDOT = 4588
950381 meter/sec RA = 350
36365 deg
ZDOT = 6019
519398 TA = 338
90940
MA = 338
98939
Ha = 191
739 n
mi
Hp = 182
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21447550
84 X = 6555556
03
Y = -4863589
70 feet Y = -1409216
53 meter
Z = -1520705
30 Z = -431708
20
XDOT = 4796
250435 XDOT = 1381
231749
YDOT = 15055
611487 feet/sec YDOT = 4604
846617 meter/sec
ZDOT = 19749
079391 ZDOT = 6026
425898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20802887
06 X = -6340719
98
Y = -7159680
63 feet Y = -2182270
66 meter
Z = -1394040
64 Z = -424903
59
XDOT = 3424
944432 XDOT = 1043
923063
YDOT = -13747
687566 feet/sec YDOT = -4190
295170 meter/sec
ZDOT = 19776
569704 ZDOT = 6027
898446
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
74191293
00016717 00000-0 10270-3 0 9014
2 25544 51
6478 350
8734 0010371 348
6008 11
4919 15
74247881 19781
Satellite: ISS
Catalog Number: 25544
Epoch time: 10144
74191293 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 350
8734 deg
Eccentricity:
0010371
Arg of perigee: 348
6008 deg
Mean anomaly: 11
4919 deg
Mean motion: 15
74247881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1978
Checksum: 319
Coasting Arc #3 (Orbit 1993)
---------------------------------------
Vector Time (GMT): 2010/145/17:47:10
694
Vector Time (MET): N/A
Weight (LBS) : 816526
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1503029
19 A = 6719305
20 meter
Y = -3921794
76 meter E =
0017473
Z = -5257140
00 I = 51
54230
XDOT = 7339
667842 Wp = 50
37537
YDOT = -2263
459834 meter/sec RA = 345
23048 deg
ZDOT = -399
835473 TA = 215
75948
MA = 215
87661
Ha = 191
766 n
mi
Hp = 182
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4931198
14 X = -1433524
54
Y = -12866780
70 feet Y = -3938213
29 meter
Z = -17247834
64 Z = -5264273
48
XDOT = 24080
275073 XDOT = 7366
375118
YDOT = -7426
049323 feet/sec YDOT = -2181
233923 meter/sec
ZDOT = -1311
796172 ZDOT = -364
114068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2435180
61 X = -742243
05
Y = 13526286
58 feet Y = 4122812
15 meter
Z = -17276227
23 Z = -5265794
06
XDOT = -23508
678474 XDOT = -7165
445199
YDOT = -5768
207662 feet/sec YDOT = -1758
149695 meter/sec
ZDOT = -1169
522455 ZDOT = -356
470444
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
75757077
00016717 00000-0 10270-3 0 9025
2 25544 51
6477 345
6570 0010411 352
1265 7
9733 15
74294257 19941
Satellite: ISS
Catalog Number: 25544
Epoch time: 10145
75757077 = yrday
fracday
Element set: 902
Inclination: 51
6477 deg
RA of node: 345
6570 deg
Eccentricity:
0010411
Arg of perigee: 352
1265 deg
Mean anomaly: 7
9733 deg
Mean motion: 15
74294257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1994
Checksum: 320
Coasting Arc #4 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2010/146/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3444934
42 A = 6719315
69 meter
Y = 3009975
50 meter E =
0006673
Z = 4917316
90 I = 51
53080
XDOT = -6358
831121 Wp = 22
99124
YDOT = 3789
620739 meter/sec RA = 342
48747 deg
ZDOT = 2140
197383 TA = 46
25852
MA = 46
20330
Ha = 190
563 n
mi
Hp = 182
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11302278
27 X = 3387132
40
Y = 9875247
70 feet Y = 3048174
98 meter
Z = 16132929
45 Z = 4933912
69
XDOT = -20862
306827 XDOT = -6411
131624
YDOT = 12433
138909 feet/sec YDOT = 3718
219799 meter/sec
ZDOT = 7021
644958 ZDOT = 2109
179045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7809528
82 X = 2380344
38
Y = 12733294
45 feet Y = 3881108
15 meter
Z = 16199009
10 Z = 4937457
98
XDOT = -22705
810884 XDOT = -6920
731157
YDOT = 5171
312268 feet/sec YDOT = 1576
215979 meter/sec
ZDOT = 6898
093212 ZDOT = 2102
538811
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
32885173
00016717 00000-0 10270-3 0 9039
2 25544 51
6470 342
7250 0009854 345
5820 14
5062 15
74782757 20037
Satellite: ISS
Catalog Number: 25544
Epoch time: 10146
32885173 = yrday
fracday
Element set: 903
Inclination: 51
6470 deg
RA of node: 342
7250 deg
Eccentricity:
0009854
Arg of perigee: 345
5820 deg
Mean anomaly: 14
5062 deg
Mean motion: 15
74782757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 300
Coasting Arc #5 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2010/147/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5404056
78 A = 6728846
81 meter
Y = -3651183
76 meter E =
0016519
Z = -1615696
63 I = 51
53451
XDOT = 3939
490639 Wp = 10
20300
YDOT = 3299
610004 meter/sec RA = 337
30625 deg
ZDOT = 5744
872534 TA = 331
91156
MA = 332
00060
Ha = 190
835 n
mi
Hp = 182
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17729845
07 X = 5452332
22
Y = -11978949
35 feet Y = -3590482
21 meter
Z = -5300841
95 Z = -1589326
57
XDOT = 12924
838056 XDOT = 3874
392997
YDOT = 10825
492139 feet/sec YDOT = 3343
298883 meter/sec
ZDOT = 18848
007000 ZDOT = 5763
853276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20386867
36 X = 6213917
17
Y = -6581859
20 feet Y = -2006150
68 meter
Z = -5195799
06 Z = -1583679
55
XDOT = 8827
267084 XDOT = 2690
551007
YDOT = 12469
143242 feet/sec YDOT = 3800
594860 meter/sec
ZDOT = 18923
582038 ZDOT = 5767
907805
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
28072647
00016717 00000-0 10270-3 0 9040
2 25544 51
6473 337
8315 0009990 349
2649 10
8300 15
74786320 20188
Satellite: ISS
Catalog Number: 25544
Epoch time: 10147
28072647 = yrday
fracday
Element set: 904
Inclination: 51
6473 deg
RA of node: 337
8315 deg
Eccentricity:
0009990
Arg of perigee: 349
2649 deg
Mean anomaly: 10
8300 deg
Mean motion: 15
74786320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2018
Checksum: 312
Coasting Arc #6 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2010/148/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3405670
86 A = 6718459
41 meter
Y = -2785889
51 meter E =
0017795
Z = -5090708
99 I = 51
47322
XDOT = 6013
004956 Wp = 44
03285
YDOT = -4545
934225 meter/sec RA = 332
18279 deg
ZDOT = -1525
530821 TA = 211
22650
MA = 211
33234
Ha = 190
854 n
mi
Hp = 181
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11173460
84 X = -3349535
37
Y = -9140057
44 feet Y = -2823659
02 meter
Z = -16701801
15 Z = -5107118
07
XDOT = 19727
706547 XDOT = 6070
802356
YDOT = -14914
482365 feet/sec YDOT = -4478
369807 meter/sec
ZDOT = -5005
022380 ZDOT = -1496
179629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8307057
54 X = -2531991
14
Y = -11712938
18 feet Y = -3570103
56 meter
Z = -16767137
89 Z = -5110623
63
XDOT = 22109
213389 XDOT = 6738
888241
YDOT = -8639
034400 feet/sec YDOT = -2633
177685 meter/sec
ZDOT = -4888
096577 ZDOT = -1489
891837
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
29604149
00016717 00000-0 10270-3 0 9051
2 25544 51
6479 332
6116 0010040 353
3892 6
7138 15
74836680 20346
Satellite: ISS
Catalog Number: 25544
Epoch time: 10148
29604149 = yrday
fracday
Element set: 905
Inclination: 51
6479 deg
RA of node: 332
6116 deg
Eccentricity:
0010040
Arg of perigee: 353
3892 deg
Mean anomaly: 6
7138 deg
Mean motion: 15
74836680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2034
Checksum: 301
Coasting Arc #7 (Orbit 2049)
---------------------------------------
Vector Time (GMT): 2010/149/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5088258
21 A = 6729397
62 meter
Y = 4281701
09 meter E =
0011023
Z = 1030840
18 I = 51
48354
XDOT = -3829
491849 Wp = 77
97233
YDOT = -3116
143727 meter/sec RA = 327
00676 deg
ZDOT = -5903
883522 TA = 90
73748
MA = 90
61117
Ha = 191
001 n
mi
Hp = 181
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16693760
54 X = -5140766
47
Y = 14047575
76 feet Y = 4224507
39 meter
Z = 3382021
59 Z = 1005994
42
XDOT = -12563
949637 XDOT = -3765
681716
YDOT = -10223
568657 feet/sec YDOT = -3158
609569 meter/sec
ZDOT = -19369
696596 ZDOT = -5922
332902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19637878
80 X = -5985625
46
Y = 9540936
80 feet Y = 2908077
54 meter
Z = 3283037
77 Z = 1000669
91
XDOT = -8880
051212 XDOT = -2706
639609
YDOT = -11522
795229 feet/sec YDOT = -3512
147986 meter/sec
ZDOT = -19443
160165 ZDOT = -5926
275218
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
31133983
00016717 00000-0 10270-3 0 9069
2 25544 51
6478 327
3915 0009973 356
9200 3
1900 15
74822548 20502
Satellite: ISS
Catalog Number: 25544
Epoch time: 10149
31133983 = yrday
fracday
Element set: 906
Inclination: 51
6478 deg
RA of node: 327
3915 deg
Eccentricity:
0009973
Arg of perigee: 356
9200 deg
Mean anomaly: 3
1900 deg
Mean motion: 15
74822548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2050
Checksum: 305
Coasting Arc #8 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2010/150/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3293218
26 A = 6717763
25 meter
Y = 2687040
61 meter E =
0008956
Z = 5198810
21 I = 51
42072
XDOT = -5588
335538 Wp = 17
83582
YDOT = 5238
914284 meter/sec RA = 321
86815 deg
ZDOT = 840
218842 TA = 64
19282
MA = 64
10045
Ha = 190
964 n
mi
Hp = 181
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10804521
84 X = 3237671
55
Y = 8815750
03 feet Y = 2723555
85 meter
Z = 17056463
93 Z = 5214674
27
XDOT = -18334
434181 XDOT = -5650
584330
YDOT = 17188
038988 feet/sec YDOT = 5176
073991 meter/sec
ZDOT = 2756
623496 ZDOT = 812
920306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8417496
33 X = 2565652
88
Y = 11020067
77 feet Y = 3358916
66 meter
Z = 17119636
81 Z = 5218065
30
XDOT = -20975
702014 XDOT = -6393
393974
YDOT = 11949
232822 feet/sec YDOT = 3642
126164 meter/sec
ZDOT = 2647
862767 ZDOT = 807
068571
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
32661842
00016717 00000-0 10270-3 0 9073
2 25544 51
6482 322
1713 0010103
2141 359
9025 15
74890314 20669
Satellite: ISS
Catalog Number: 25544
Epoch time: 10150
32661842 = yrday
fracday
Element set: 907
Inclination: 51
6482 deg
RA of node: 322
1713 deg
Eccentricity:
0010103
Arg of perigee:
2141 deg
Mean anomaly: 359
9025 deg
Mean motion: 15
74890314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 266
Coasting Arc #9 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2010/151/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4634435
02 A = 6729526
86 meter
Y = -4843238
03 meter E =
0020404
Z = -434479
47 I = 51
43774
XDOT = 3743
907696 Wp = 23
44641
YDOT = 3053
769768 meter/sec RA = 316
69979 deg
ZDOT = 6008
558373 TA = 331
80880
MA = 331
91910
Ha = 191
135 n
mi
Hp = 181
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15204839
31 X = 4690359
17
Y = -15889888
55 feet Y = -4791100
26 meter
Z = -1425457
59 Z = -411830
33
XDOT = 12283
161733 XDOT = 3680
293140
YDOT = 10018
929685 feet/sec YDOT = 3095
279695 meter/sec
ZDOT = 19713
118023 ZDOT = 6026
592269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18219483
56 X = 5553298
59
Y = -12327823
67 feet Y = -3757520
65 meter
Z = -1335218
56 Z = -406974
62
XDOT = 8883
412133 XDOT = 2707
664018
YDOT = 11029
550699 feet/sec YDOT = 3361
807053 meter/sec
ZDOT = 19784
936537 ZDOT = 6030
448656
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
27842767
00016717 00000-0 10270-3 0 9086
2 25544 51
6486 317
2775 0010213 3
4474 356
6758 15
74907857 20817
Satellite: ISS
Catalog Number: 25544
Epoch time: 10151
27842767 = yrday
fracday
Element set: 908
Inclination: 51
6486 deg
RA of node: 317
2775 deg
Eccentricity:
0010213
Arg of perigee: 3
4474 deg
Mean anomaly: 356
6758 deg
Mean motion: 15
74907857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2081
Checksum: 327
Coasting Arc #10 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2010/152/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3236679
36 A = 6717406
99 meter
Y = -2678774
46 meter E =
0019336
Z = -5255490
69 I = 51
37588
XDOT = 5027
413738 Wp = 57
12475
YDOT = -5818
435670 meter/sec RA = 311
54596 deg
ZDOT = -120
489917 TA = 211
66790
MA = 211
78437
Ha = 191
181 n
mi
Hp = 180
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10619026
76 X = -3180954
09
Y = -8788630
12 feet Y = -2714656
58 meter
Z = -17242423
53 Z = -5271079
50
XDOT = 16494
139562 XDOT = 5092
688204
YDOT = -19089
355874 feet/sec YDOT = -5761
851149 meter/sec
ZDOT = -395
308126 ZDOT = -95
909099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8613771
02 X = -2625477
41
Y = -10661229
95 feet Y = -3249542
89 meter
Z = -17304509
32 Z = -5274414
44
XDOT = 19106
385980 XDOT = 5823
626447
YDOT = -14901
261532 feet/sec YDOT = -4541
904515 meter/sec
ZDOT = -297
373743 ZDOT = -90
639517
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
29367279
00016717 00000-0 10270-3 0 9090
2 25544 51
6484 312
0573 0010293 6
9199 353
2105 15
74946739 20972
Satellite: ISS
Catalog Number: 25544
Epoch time: 10152
29367279 = yrday
fracday
Element set: 909
Inclination: 51
6484 deg
RA of node: 312
0573 deg
Eccentricity:
0010293
Arg of perigee: 6
9199 deg
Mean anomaly: 353
2105 deg
Mean motion: 15
74946739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2097
Checksum: 326
Coasting Arc #11 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2010/153/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4145642
89 A = 6729527
97 meter
Y = 5296954
38 meter E =
0009944
Z = -244229
08 I = 51
39730
XDOT = -3653
338474 Wp = 81
60892
YDOT = -3126
702923 meter/sec RA = 306
38726 deg
ZDOT = -6007
159929 TA = 101
05233
MA = 100
94047
Ha = 191
315 n
mi
Hp = 180
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13601190
59 X = -4203379
86
Y = 17378459
25 feet Y = 5250272
54 meter
Z = -801276
52 Z = -264508
12
XDOT = -11986
018614 XDOT = -3588
921965
YDOT = -10258
211691 feet/sec YDOT = -3167
195769 meter/sec
ZDOT = -19708
529952 ZDOT = -6024
751753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16456798
65 X = -5016032
23
Y = 14698333
52 feet Y = 4480052
06 meter
Z = -882068
59 Z = -268854
51
XDOT = -8795
075559 XDOT = -2680
739030
YDOT = -10997
211045 feet/sec YDOT = -3351
949927 meter/sec
ZDOT = -19778
598041 ZDOT = -6028
516683
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
30890151
00016717 00000-0 10270-3 0 9105
2 25544 51
6484 306
8374 0010140 10
6957 349
4420 15
74917254 21133
Satellite: ISS
Catalog Number: 25544
Epoch time: 10153
30890151 = yrday
fracday
Element set: 910
Inclination: 51
6484 deg
RA of node: 306
8374 deg
Eccentricity:
0010140
Arg of perigee: 10
6957 deg
Mean anomaly: 349
4420 deg
Mean motion: 15
74917254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 282
Coasting Arc #12 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2010/154/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3175783
55 A = 6717406
08 meter
Y = 2802527
50 meter E =
0012533
Z = 5210519
38 I = 51
33995
XDOT = -4424
789730 Wp = 23
99295
YDOT = 6273
883879 meter/sec RA = 301
21634 deg
ZDOT = -665
721722 TA = 72
42726
MA = 72
29039
Ha = 191
268 n
mi
Hp = 180
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10419237
36 X = 3118897
42
Y = 9194644
04 feet Y = 2837722
34 meter
Z = 17094879
84 Z = 5225809
46
XDOT = -14517
026674 XDOT = -4491
382620
YDOT = 20583
608528 feet/sec YDOT = 6224
030981 meter/sec
ZDOT = -2184
126383 ZDOT = -687
378358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8714072
28 X = 2656049
23
Y = 10727577
22 feet Y = 3269765
54 meter
Z = 17155784
28 Z = 5229083
05
XDOT = -16828
031908 XDOT = -5129
184126
YDOT = 17362
394478 feet/sec YDOT = 5292
057837 meter/sec
ZDOT = -2270
401152 ZDOT = -692
018271
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
32410969
00016717 00000-0 10270-3 0 9114
2 25544 51
6482 301
6167 0010336 13
9105 346
2342 15
74998389 21295
Satellite: ISS
Catalog Number: 25544
Epoch time: 10154
32410969 = yrday
fracday
Element set: 911
Inclination: 51
6482 deg
RA of node: 301
6167 deg
Eccentricity:
0010336
Arg of perigee: 13
9105 deg
Mean anomaly: 346
2342 deg
Mean motion: 15
74998389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 303
Coasting Arc #13 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2010/155/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3560881
59 A = 6728883
97 meter
Y = -5620072
54 meter E =
0022752
Z = 912068
21 I = 51
36337
XDOT = 3665
831708 Wp = 38
55568
YDOT = 3295
214733 meter/sec RA = 296
06734 deg
ZDOT = 5931
096354 TA = 331
45747
MA = 331
58185
Ha = 191
338 n
mi
Hp = 180
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11682682
39 X = 3619030
94
Y = -18438558
19 feet Y = -5579927
60 meter
Z = 2992349
78 Z = 929507
66
XDOT = 12027
006917 XDOT = 3599
899338
YDOT = 10811
071960 feet/sec YDOT = 3335
838982 meter/sec
ZDOT = 19458
977540 ZDOT = 5948
745184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14181489
22 X = 4322517
91
Y = -16581021
83 feet Y = -5053895
45 meter
Z = 3061818
41 Z = 933242
25
XDOT = 9034
467120 XDOT = 2753
705578
YDOT = 11369
752966 feet/sec YDOT = 3465
500704 meter/sec
ZDOT = 19529
281570 ZDOT = 5952
525023
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
33930103
00016717 00000-0 10270-3 0 9124
2 25544 51
6473 296
3957 0010354 17
3005 342
8510 15
75028766 21450
Satellite: ISS
Catalog Number: 25544
Epoch time: 10155
33930103 = yrday
fracday
Element set: 912
Inclination: 51
6473 deg
RA of node: 296
3957 deg
Eccentricity:
0010354
Arg of perigee: 17
3005 deg
Mean anomaly: 342
8510 deg
Mean motion: 15
75028766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2145
Checksum: 288
Coasting Arc #14 (Orbit 2159)
---------------------------------------
Vector Time (GMT): 2010/156/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3236152
49 A = 6717828
54 meter
Y = -2968558
98 meter E =
0018721
Z = -5097115
44 I = 51
31292
XDOT = 3746
424951 Wp = 67
76150
YDOT = -6558
298845 meter/sec RA = 290
88042 deg
ZDOT = 1452
185627 TA = 216
17298
MA = 216
29974
Ha = 191
421 n
mi
Hp = 179
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10617298
19 X = -3177956
03
Y = -9739366
73 feet Y = -3004421
67 meter
Z = -16722819
68 Z = -5112695
68
XDOT = 12291
420443 XDOT = 3812
428103
YDOT = -21516
728493 feet/sec YDOT = -6516
035189 meter/sec
ZDOT = 4764
388541 ZDOT = 1470
545519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9207966
70 X = -2806588
25
Y = -10987079
26 feet Y = -3348861
76 meter
Z = -16784886
71 Z = -5116033
47
XDOT = 14074
164388 XDOT = 4289
805306
YDOT = -19129
308807 feet/sec YDOT = -5830
613324 meter/sec
ZDOT = 4837
516827 ZDOT = 1474
475129
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
29102748
00016717 00000-0 10270-3 0 9137
2 25544 51
6462 291
5005 0010413 20
7082 339
4501 15
75047427 21602
Satellite: ISS
Catalog Number: 25544
Epoch time: 10156
29102748 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 291
5005 deg
Eccentricity:
0010413
Arg of perigee: 20
7082 deg
Mean anomaly: 339
4501 deg
Mean motion: 15
75047427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2160
Checksum: 273
Coasting Arc #15 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2010/157/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3000196
39 A = 6727992
90 meter
Y = 5798185
47 meter E =
0009584
Z = -1642932
05 I = 51
33719
XDOT = -3744
056168 Wp = 70
14093
YDOT = -3547
695754 meter/sec RA = 285
74288 deg
ZDOT = -5707
107940 TA = 128
07197
MA = 127
98547
Ha = 191
529 n
mi
Hp = 179
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9843164
00 X = -3056828
63
Y = 19022918
20 feet Y = 5764319
00 meter
Z = -5390197
03 Z = -1657644
11
XDOT = -12283
648844 XDOT = -3676
382597
YDOT = -11639
421764 feet/sec YDOT = -3589
185064 meter/sec
ZDOT = -18724
107415 ZDOT = -5725
132694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11823734
08 X = -3603874
15
Y = 17841623
01 feet Y = 5438126
69 meter
Z = -5448790
64 Z = -1660791
39
XDOT = -9532
387929 XDOT = -2905
471841
YDOT = -12033
804317 feet/sec YDOT = -3667
903556 meter/sec
ZDOT = -18795
915794 ZDOT = -5728
995134
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 10157
30618477
00016717 00000-0 10270-3 0 9142
2 25544 51
6458 286
2801 0010364 24
2864 335
8786 15
75045990 21769
Satellite: ISS
Catalog Number: 25544
Epoch time: 10157
30618477 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 286
2801 deg
Eccentricity:
0010364
Arg of perigee: 24
2864 deg
Mean anomaly: 335
8786 deg
Mean motion: 15
75045990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2176
Checksum: 325
Coasting Arc #16 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2010/158/06:39:48
549
Vector Time (MET): N/A
Weight (LBS) : 816271
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3347420
70 A = 6718735
06 meter
Y = 3228138
32 meter E =
0016515
Z = 4844748
18 I = 51
29918
XDOT = -3103
808960 Wp = 39
38241
YDOT = 6673
047121 meter/sec RA = 280
54113 deg
ZDOT = -2284
960111 TA = 73
03796
MA = 72
85701
Ha = 191
466 n
mi
Hp = 179
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10982351
37 X = 3287539
10
Y = 10591005
00 feet Y = 3265235
83 meter
Z = 15894843
12 Z = 4860865
04
XDOT = -10183
100263 XDOT = -3167
097444
YDOT = 21893
199217 feet/sec YDOT = 6637
984865 meter/sec
ZDOT = -7496
588292 ZDOT = -2300
191596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9870681
32 X = 3008583
67
Y = 11545810
20 feet Y = 3519162
95 meter
Z = 15959053
34 Z = 4864319
46
XDOT = -11262
601655 XDOT = -3432
840984
YDOT = 20150
647205 feet/sec YDOT = 6141
917268 meter/sec
ZDOT = -7557
246117 ZDOT = -2303
448616
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 10158
32132300
00016717 00000-0 10270-3 0 9152
2 25544 51
6456 281
0580 0010389 27
7488 332
4228 15
75097492 21927
Satellite: ISS
Catalog Number: 25544
Epoch time: 10158
32132300 = yrday
fracday
Element set: 915
Inclination: 51
6456 deg
RA of node: 281
0580 deg
Eccentricity:
0010389
Arg of perigee: 27
7488 deg
Mean anomaly: 332
4228 deg
Mean motion: 15
75097492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 303
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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