Date:
May 11th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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
There are no maneuvers
Coasting Arc #1 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2010/130/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4762138
62 A = 6725606
59 meter
Y = -2480391
75 meter E =
0007306
Z = 4054029
51 I = 51
94271
XDOT = 130
489278 Wp = 11
39960
YDOT = -6634
425352 meter/sec RA = 63
74874 deg
ZDOT = -3897
693345 TA = 118
66997
MA = 118
59650
Ha = 190
059 n
mi
Hp = 186
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15623814
35 X = -4753742
56
Y = -8137768
21 feet Y = -2533597
96 meter
Z = 13300621
77 Z = 4030915
00
XDOT = 428
114430 XDOT = 223
601522
YDOT = -21766
487375 feet/sec YDOT = -6632
445439 meter/sec
ZDOT = -12787
707826 ZDOT = -3896
833391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17412711
67 X = -5307394
52
Y = -3092780
01 feet Y = -942679
35 meter
Z = 13208541
55 Z = 4025963
46
XDOT = -6226
316368 XDOT = -1897
781229
YDOT = -19659
642395 feet/sec YDOT = -5992
259002 meter/sec
ZDOT = -12784
349935 ZDOT = -3896
669860
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 10130
45719941
00016717 00000-0 10270-3 0 9002
2 25544 51
6425 64
2228 0010292 298
2222 61
7902 15
73835137 17534
Satellite: ISS
Catalog Number: 25544
Epoch time: 10130
45719941 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 64
2228 deg
Eccentricity:
0010292
Arg of perigee: 298
2222 deg
Mean anomaly: 61
7902 deg
Mean motion: 15
73835137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 290
Coasting Arc #2 (Orbit 1768)
---------------------------------------
Vector Time (GMT): 2010/131/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 428998
61 A = 6727534
63 meter
Y = 5796498
48 meter E =
0006493
Z = 3379009
93 I = 51
93640
XDOT = -5678
206611 Wp = 35
20104
YDOT = -2300
540237 meter/sec RA = 58
68685 deg
ZDOT = 4668
124332 TA = 4
46794
MA = 4
46215
Ha = 190
152 n
mi
Hp = 186
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1407475
75 X = 347734
29
Y = 19017383
47 feet Y = 5800841
30 meter
Z = 11085990
58 Z = 3380896
86
XDOT = -18629
286782 XDOT = -5674
736894
YDOT = -7547
704190 feet/sec YDOT = -2364
018096 meter/sec
ZDOT = 15315
368542 ZDOT = 4640
547393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7248442
55 X = 2209325
29
Y = 17633326
59 feet Y = 5374637
95 meter
Z = 11093553
22 Z = 3381315
02
XDOT = -18856
657382 XDOT = -5747
509170
YDOT = -1813
254623 feet/sec YDOT = -552
680009 meter/sec
ZDOT = 15205
523649 ZDOT = 4634
643608
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 10131
47313299
00016717 00000-0 10270-3 0 9012
2 25544 51
6435 59
0072 0010262 301
2610 58
7547 15
73883303 17693
Satellite: ISS
Catalog Number: 25544
Epoch time: 10131
47313299 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 59
0072 deg
Eccentricity:
0010262
Arg of perigee: 301
2610 deg
Mean anomaly: 58
7547 deg
Mean motion: 15
73883303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1769
Checksum: 289
Coasting Arc #3 (Orbit 1783)
---------------------------------------
Vector Time (GMT): 2010/132/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5112384
37 A = 6725377
96 meter
Y = 1517116
82 meter E =
0003866
Z = -4094172
89 I = 51
91222
XDOT = 1121
326758 Wp = 339
12780
YDOT = 6580
110839 meter/sec RA = 53
52182 deg
ZDOT = 3840
922151 TA = 330
18309
MA = 330
20511
Ha = 190
553 n
mi
Hp = 186
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16772914
60 X = 5114928
92
Y = 4977417
40 feet Y = 1574301
02 meter
Z = -13432325
75 Z = -4069330
10
XDOT = 3678
893564 XDOT = 1029
004511
YDOT = 21588
290154 feet/sec YDOT = 6592
133757 meter/sec
ZDOT = 12601
450626 ZDOT = 3846
145807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17549798
20 X = 5349178
49
Y = -870799
09 feet Y = -265419
56 meter
Z = -13333379
74 Z = -4064014
14
XDOT = 10472
065858 XDOT = 3191
885673
YDOT = 17905
258767 feet/sec YDOT = 5457
522872 meter/sec
ZDOT = 12622
294871 ZDOT = 3847
275477
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 10132
42555783
00016717 00000-0 10270-3 0 9025
2 25544 51
6437 54
1175 0010375 305
7679 54
2518 15
73862397 17840
Satellite: ISS
Catalog Number: 25544
Epoch time: 10132
42555783 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 54
1175 deg
Eccentricity:
0010375
Arg of perigee: 305
7679 deg
Mean anomaly: 54
2518 deg
Mean motion: 15
73862397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1784
Checksum: 319
Coasting Arc #4 (Orbit 1799)
---------------------------------------
Vector Time (GMT): 2010/133/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1502710
79 A = 6727547
21 meter
Y = -5645309
41 meter E =
0007249
Z = -3340581
01 I = 51
90229
XDOT = 5977
578275 Wp = 333
67697
YDOT = 1193
973596 meter/sec RA = 48
45718 deg
ZDOT = -4696
419921 TA = 245
43117
MA = 245
50674
Ha = 190
567 n
mi
Hp = 185
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4930153
51 X = -1423243
93
Y = -18521356
34 feet Y = -5661669
02 meter
Z = -10959911
45 Z = -3347688
79
XDOT = 19611
477280 XDOT = 5986
597653
YDOT = 3917
236206 feet/sec YDOT = 1260
869259 meter/sec
ZDOT = -15408
201840 ZDOT = -4667
358172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10983704
40 X = -3347833
10
Y = -15687048
50 feet Y = -4781412
38 meter
Z = -10988241
91 Z = -3349216
13
XDOT = 18694
287346 XDOT = 5698
018783
YDOT = -2354
025468 feet/sec YDOT = -717
506963 meter/sec
ZDOT = -15292
457383 ZDOT = -4661
141010
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 10133
44146056
00016717 00000-0 10270-3 0 9038
2 25544 51
6447 48
9019 0010391 309
8849 50
1400 15
73914656 18001
Satellite: ISS
Catalog Number: 25544
Epoch time: 10133
44146056 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 48
9019 deg
Eccentricity:
0010391
Arg of perigee: 309
8849 deg
Mean anomaly: 50
1400 deg
Mean motion: 15
73914656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1800
Checksum: 293
Coasting Arc #5 (Orbit 1815)
---------------------------------------
Vector Time (GMT): 2010/134/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5300348
07 A = 6725160
35 meter
Y = -567254
19 meter E =
0009998
Z = 4104649
81 I = 51
87368
XDOT = -2293
380417 Wp = 15
75219
YDOT = -6276
318334 meter/sec RA = 43
28999 deg
ZDOT = -3817
244870 TA = 113
39138
MA = 113
28620
Ha = 190
759 n
mi
Hp = 185
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17389593
39 X = -5313551
05
Y = -1861070
17 feet Y = -626600
10 meter
Z = 13466698
85 Z = 4078868
04
XDOT = -7524
213966 XDOT = -2204
483169
YDOT = -20591
595584 feet/sec YDOT = -6301
466811 meter/sec
ZDOT = -12523
769258 ZDOT = -3828
171097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16954040
94 X = -5167591
68
Y = 4601849
80 feet Y = 1402643
82 meter
Z = 13364018
57 Z = 4073352
86
XDOT = -14076
020054 XDOT = -4290
370912
YDOT = -15251
306372 feet/sec YDOT = -4648
598182 meter/sec
ZDOT = -12567
297887 ZDOT = -3830
512396
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 10134
45734708
00016717 00000-0 10270-3 0 9048
2 25544 51
6451 43
6866 0010420 313
4656 46
5640 15
73933597 18165
Satellite: ISS
Catalog Number: 25544
Epoch time: 10134
45734708 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 43
6866 deg
Eccentricity:
0010420
Arg of perigee: 313
4656 deg
Mean anomaly: 46
5640 deg
Mean motion: 15
73933597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1816
Checksum: 307
Coasting Arc #6 (Orbit 1831)
---------------------------------------
Vector Time (GMT): 2010/135/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2479544
90 A = 6727431
86 meter
Y = 5283755
20 meter E =
0009543
Z = 3332565
20 I = 51
85905
XDOT = -6101
198249 Wp = 35
17396
YDOT = -103
120283 meter/sec RA = 38
22186 deg
ZDOT = 4704
010885 TA = 3
90906
MA = 3
90161
Ha = 190
871 n
mi
Hp = 185
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8134989
82 X = 2404087
43
Y = 17335154
84 feet Y = 5311060
61 meter
Z = 10933612
85 Z = 3344428
43
XDOT = -20017
054623 XDOT = -6122
443310
YDOT = -338
321139 feet/sec YDOT = -171
466906 meter/sec
ZDOT = 15433
106578 ZDOT = 4674
319125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14033878
17 X = 4277526
07
Y = 12988473
26 feet Y = 3958886
65 meter
Z = 10980863
75 Z = 3346967
27
XDOT = -17791
079996 XDOT = -5422
721183
YDOT = 6278
165287 feet/sec YDOT = 1913
584779 meter/sec
ZDOT = 15314
851244 ZDOT = 4667
966659
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 10135
47321728
00016717 00000-0 10270-3 0 9056
2 25544 51
6452 38
4706 0010416 317
3796 42
6558 15
73953740 18329
Satellite: ISS
Catalog Number: 25544
Epoch time: 10135
47321728 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 38
4706 deg
Eccentricity:
0010416
Arg of perigee: 317
3796 deg
Mean anomaly: 42
6558 deg
Mean motion: 15
73953740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1832
Checksum: 309
Coasting Arc #7 (Orbit 1846)
---------------------------------------
Vector Time (GMT): 2010/136/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5310442
55 A = 6725002
51 meter
Y = -393767
38 meter E =
0005690
Z = -4103741
26 I = 51
82653
XDOT = 3373
593798 Wp = 4
63125
YDOT = 5775
502450 meter/sec RA = 33
05049 deg
ZDOT = 3817
336586 TA = 304
43008
MA = 304
48385
Ha = 191
141 n
mi
Hp = 184
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17422711
79 X = 5334386
52
Y = -1291887
74 feet Y = -334248
40 meter
Z = -13463718
06 Z = -4077884
71
XDOT = 11068
221123 XDOT = 3290
216196
YDOT = 18948
498852 feet/sec YDOT = 5812
761261 meter/sec
ZDOT = 12524
070163 ZDOT = 3833
523991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15572180
20 X = 4746400
52
Y = -8092563
75 feet Y = -2466613
43 meter
Z = -13360732
76 Z = -4072351
34
XDOT = 16988
265612 XDOT = 5178
023359
YDOT = 11938
576102 feet/sec YDOT = 3638
877996 meter/sec
ZDOT = 12588
538715 ZDOT = 3836
986600
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 10136
42558063
00016717 00000-0 10270-3 0 9067
2 25544 51
6454 33
5806 0010479 320
9705 39
0701 15
73983219 18477
Satellite: ISS
Catalog Number: 25544
Epoch time: 10136
42558063 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 33
5806 deg
Eccentricity:
0010479
Arg of perigee: 320
9705 deg
Mean anomaly: 39
0701 deg
Mean motion: 15
73983219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1847
Checksum: 308
Coasting Arc #8 (Orbit 1862)
---------------------------------------
Vector Time (GMT): 2010/137/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3366707
16 A = 6727200
72 meter
Y = -4771027
41 meter E =
0008640
Z = -3348220
65 I = 51
80913
XDOT = 6029
950238 Wp = 351
72808
YDOT = -964
566643 meter/sec RA = 27
97876 deg
ZDOT = -4678
927144 TA = 227
53564
MA = 227
60871
Ha = 191
175 n
mi
Hp = 184
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11045627
16 X = -3296841
28
Y = -15652977
07 feet Y = -4808284
83 meter
Z = -10984975
87 Z = -3364407
19
XDOT = 19783
301307 XDOT = 6063
017576
YDOT = -3164
588724 feet/sec YDOT = -896
950611 meter/sec
ZDOT = -15350
810839 ZDOT = -4649
553246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16436219
42 X = -5009759
68
Y = -9769944
44 feet Y = -2977879
07 meter
Z = -11049440
81 Z = -3367869
56
XDOT = 16112
745625 XDOT = 4911
164867
YDOT = -9841
621276 feet/sec YDOT = -2999
726165 meter/sec
ZDOT = -15233
809896 ZDOT = -4643
265256
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 10137
44141910
00016717 00000-0 10270-3 0 9070
2 25544 51
6460 28
3644 0010520 325
1542 34
8932 15
74017846 18631
Satellite: ISS
Catalog Number: 25544
Epoch time: 10137
44141910 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 28
3644 deg
Eccentricity:
0010520
Arg of perigee: 325
1542 deg
Mean anomaly: 34
8932 deg
Mean motion: 15
74017846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1863
Checksum: 285
Coasting Arc #9 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2010/138/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5202506
71 A = 6725039
25 meter
Y = 1287105
68 meter E =
0012396
Z = 4066245
67 I = 51
77383
XDOT = -4286
936894 Wp = 23
62646
YDOT = -5097
281215 meter/sec RA = 22
80321 deg
ZDOT = -3856
231595 TA = 106
07177
MA = 105
93523
Ha = 191
369 n
mi
Hp = 184
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17068591
56 X = -5236265
83
Y = 4222787
66 feet Y = 1228738
88 meter
Z = 13340701
03 Z = 4040889
98
XDOT = -14064
753589 XDOT = -4210
886635
YDOT = -16723
363567 feet/sec YDOT = -5144
794586 meter/sec
ZDOT = -12651
678461 ZDOT = -3876
873515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13715264
54 X = -4180412
63
Y = 11124068
41 feet Y = 3390616
05 meter
Z = 13239700
83 Z = 4035460
81
XDOT = -18969
230662 XDOT = -5781
821506
YDOT = -8172
465098 feet/sec YDOT = -2490
967362 meter/sec
ZDOT = -12733
890042 ZDOT = -3881
289685
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 10138
45724190
00016717 00000-0 10270-3 0 9080
2 25544 51
6455 23
1481 0010509 328
8299 31
2240 15
74022901 18791
Satellite: ISS
Catalog Number: 25544
Epoch time: 10138
45724190 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 23
1481 deg
Eccentricity:
0010509
Arg of perigee: 328
8299 deg
Mean anomaly: 31
2240 deg
Mean motion: 15
74022901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 295
Coasting Arc #10 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2010/139/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4091155
76 A = 6726973
29 meter
Y = 4112906
42 meter E =
0011983
Z = 3389726
34 I = 51
75298
XDOT = -5828
991137 Wp = 39
01951
YDOT = 1975
405256 meter/sec RA = 17
72673 deg
ZDOT = 4638
628895 TA =
95121
MA =
94893
Ha = 191
431 n
mi
Hp = 184
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13422427
02 X = 4028393
75
Y = 13493787
45 feet Y = 4158304
88 meter
Z = 11121149
41 Z = 3409449
17
XDOT = -19123
986669 XDOT = -5873
180877
YDOT = 6480
988372 feet/sec YDOT = 1909
974438 meter/sec
ZDOT = 15218
598737 ZDOT = 4610
204513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17941413
64 X = 5468542
88
Y = 6212578
84 feet Y = 1893594
03 meter
Z = 11199703
22 Z = 3413669
54
XDOT = -13926
263803 XDOT = -4244
725207
YDOT = 12988
527276 feet/sec YDOT = 3958
903114 meter/sec
ZDOT = 15105
372063 ZDOT = 4604
117405
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 10139
47304825
00016717 00000-0 10270-3 0 9093
2 25544 51
6460 17
9309 0010579 332
8056 27
2552 15
74044836 18950
Satellite: ISS
Catalog Number: 25544
Epoch time: 10139
47304825 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 17
9309 deg
Eccentricity:
0010579
Arg of perigee: 332
8056 deg
Mean anomaly: 27
2552 deg
Mean motion: 15
74044836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 317
Coasting Arc #11 (Orbit 1909)
---------------------------------------
Vector Time (GMT): 2010/140/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4934049
83 A = 6724984
74 meter
Y = -2156551
82 meter E =
0007889
Z = -4025213
96 I = 51
71787
XDOT = 5059
324092 Wp = 17
65722
YDOT = 4289
635662 meter/sec RA = 12
54647 deg
ZDOT = 3912
791818 TA = 292
63637
MA = 292
71979
Ha = 191
673 n
mi
Hp = 183
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16187827
53 X = 4977351
85
Y = -7075301
24 feet Y = -2101133
89 meter
Z = -13206082
55 Z = -4001139
33
XDOT = 16598
832323 XDOT = 4991
972944
YDOT = 14073
607814 feet/sec YDOT = 4345
835136 meter/sec
ZDOT = 12837
243496 ZDOT = 3937
206787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11237342
89 X = 3425142
11
Y = -13724120
95 feet Y = -4183112
07 meter
Z = -13110182
80 Z = -3995983
72
XDOT = 20126
328544 XDOT = 6134
504940
YDOT = 4153
172542 feet/sec YDOT = 1265
886991 meter/sec
ZDOT = 12934
487079 ZDOT = 3942
431662
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 10140
42535149
00016717 00000-0 10270-3 0 9107
2 25544 51
6466 13
0404 0010652 336
0539 24
0128 15
74083254 19102
Satellite: ISS
Catalog Number: 25544
Epoch time: 10140
42535149 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 13
0404 deg
Eccentricity:
0010652
Arg of perigee: 336
0539 deg
Mean anomaly: 24
0128 deg
Mean motion: 15
74083254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1910
Checksum: 263
Coasting Arc #12 (Orbit 1925)
---------------------------------------
Vector Time (GMT): 2010/141/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4690647
74 A = 6726609
55 meter
Y = -3370367
70 meter E =
0010495
Z = -3458946
14 I = 51
69453
XDOT = 5464
339347 Wp = 6
73731
YDOT = -2916
348009 meter/sec RA = 7
46661 deg
ZDOT = -4559
650386 TA = 214
16134
MA = 214
22892
Ha = 191
704 n
mi
Hp = 183
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15389264
25 X = -4635808
07
Y = -11057636
80 feet Y = -3422514
47 meter
Z = -11348248
49 Z = -3481600
39
XDOT = 17927
622529 XDOT = 5518
694386
YDOT = -9568
070896 feet/sec YDOT = -2854
938309 meter/sec
ZDOT = -14959
482894 ZDOT = -4532
972687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18727325
29 X = -5708088
75
Y = -2516352
81 feet Y = -766984
34 meter
Z = -11438478
29 Z = -3486448
18
XDOT = 11182
340664 XDOT = 3408
377434
YDOT = -15573
493625 feet/sec YDOT = -4746
800857 meter/sec
ZDOT = -14853
215936 ZDOT = -4527
260217
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
44112660
00016717 00000-0 10270-3 0 9110
2 25544 51
6471 7
8238 0010715 339
3468 20
7261 15
74102291 19262
Satellite: ISS
Catalog Number: 25544
Epoch time: 10141
44112660 = yrday
fracday
Element set: 911
Inclination: 51
6471 deg
RA of node: 7
8238 deg
Eccentricity:
0010715
Arg of perigee: 339
3468 deg
Mean anomaly: 20
7261 deg
Mean motion: 15
74102291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 276
Coasting Arc #13 (Orbit 1941)
---------------------------------------
Vector Time (GMT): 2010/142/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4597026
98 A = 6725127
93 meter
Y = 2933925
57 meter E =
0014636
Z = 3938010
08 I = 51
65923
XDOT = -5621
546329 Wp = 32
44441
YDOT = -3398
863530 meter/sec RA = 2
28152 deg
ZDOT = -4011
056487 TA = 99
27589
MA = 99
11033
Ha = 191
877 n
mi
Hp = 183
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15082109
51 X = -4648623
29
Y = 9625740
07 feet Y = 2882230
17 meter
Z = 12919980
58 Z = 3915552
38
XDOT = -18443
393467 XDOT = -5563
636672
YDOT = -11151
127067 feet/sec YDOT = -3461
402994 meter/sec
ZDOT = -13159
634145 ZDOT = -4038
225707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8549155
34 X = -2605782
55
Y = 15790514
61 feet Y = 4812948
85 meter
Z = 12830525
66 Z = 3910744
22
XDOT = -20319
861266 XDOT = -6193
493714
YDOT = -169
661351 feet/sec YDOT = -51
712780 meter/sec
ZDOT = -13267
842884 ZDOT = -4044
038511
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
45688616
00016717 00000-0 10270-3 0 9122
2 25544 51
6469 2
6070 0010792 343
6632 16
4182 15
74142691 19422
Satellite: ISS
Catalog Number: 25544
Epoch time: 10142
45688616 = yrday
fracday
Element set: 912
Inclination: 51
6469 deg
RA of node: 2
6070 deg
Eccentricity:
0010792
Arg of perigee: 343
6632 deg
Mean anomaly: 16
4182 deg
Mean motion: 15
74142691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1942
Checksum: 298
Coasting Arc #14 (Orbit 1957)
---------------------------------------
Vector Time (GMT): 2010/143/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5097631
34 A = 6726216
19 meter
Y = 2560865
84 meter E =
0013801
Z = 3545895
77 I = 51
63322
XDOT = -5011
336014 Wp = 44
20094
YDOT = 3787
159665 meter/sec RA = 357
19689 deg
ZDOT = 4468
601800 TA = 358
12137
MA = 358
12655
Ha = 191
920 n
mi
Hp = 183
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16724512
27 X = 5051390
86
Y = 8401790
81 feet Y = 2617611
82 meter
Z = 11633516
31 Z = 3570548
23
XDOT = -16441
391122 XDOT = -5075
020201
YDOT = 12425
064517 feet/sec YDOT = 3730
763559 meter/sec
ZDOT = 14660
767061 ZDOT = 4444
101961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18622697
73 X = 5676198
27
Y = -1095680
99 feet Y = -333963
57 meter
Z = 11731696
96 Z = 3575821
23
XDOT = -8135
124422 XDOT = -2479
585924
YDOT = 17685
824380 feet/sec YDOT = 5390
639271 meter/sec
ZDOT = 14563
178985 ZDOT = 4438
856955
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
47263040
00016717 00000-0 10270-3 0 9136
2 25544 51
6472 357
3897 0010849 347
5434 12
5460 15
74136118 19589
Satellite: ISS
Catalog Number: 25544
Epoch time: 10143
47263040 = yrday
fracday
Element set: 913
Inclination: 51
6472 deg
RA of node: 357
3897 deg
Eccentricity:
0010849
Arg of perigee: 347
5434 deg
Mean anomaly: 12
5460 deg
Mean motion: 15
74136118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1958
Checksum: 309
Coasting Arc #15 (Orbit 1972)
---------------------------------------
Vector Time (GMT): 2010/144/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4115066
14 A = 6725285
16 meter
Y = -3662454
80 meter E =
0010016
Z = -3854012
98 I = 51
59986
XDOT = 6027
434983 Wp = 24
57430
YDOT = 2450
778858 meter/sec RA = 352
00704 deg
ZDOT = 4119
501722 TA = 288
41615
MA = 288
52502
Ha = 192
118 n
mi
Hp = 182
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13500873
16 X = 4174436
94
Y = -12015927
83 feet Y = -3616105
40 meter
Z = -12644399
54 Z = -3833877
73
XDOT = 19775
049157 XDOT = 5979
569821
YDOT = 8040
613051 feet/sec YDOT = 2517
913257 meter/sec
ZDOT = 13515
425597 ZDOT = 4148
667438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5410532
71 X = 1649130
37
Y = -17303296
37 feet Y = -5274044
73 meter
Z = -12564195
47 Z = -3829566
78
XDOT = 19754
590721 XDOT = 6021
199252
YDOT = -3690
481079 feet/sec YDOT = -1124
858633 meter/sec
ZDOT = 13631
575892 ZDOT = 4154
904332
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
42487455
00016717 00000-0 10270-3 0 9141
2 25544 51
6470 352
4990 0010923 349
9536 10
1407 15
74176502 19732
Satellite: ISS
Catalog Number: 25544
Epoch time: 10144
42487455 = yrday
fracday
Element set: 914
Inclination: 51
6470 deg
RA of node: 352
4990 deg
Eccentricity:
0010923
Arg of perigee: 349
9536 deg
Mean anomaly: 10
1407 deg
Mean motion: 15
74176502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1973
Checksum: 307
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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