Date:
May 29th 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
156/03:21:58
281 -1
6 13
0 13
0
N/A -10
9 -0
0 191
1
000/00:03:52
562 -6
9 0
1 187
1
158/23:59:56
236 -0
7 2
6 2
6
N/A -2
2 0
0 191
3
000/00:09:52
471 -1
2 0
2 188
3
159/01:30:56
146 -0
8 2
7 2
7
N/A -2
2 0
0 191
3
000/00:09:52
292 -1
3 0
2 189
6
Coasting Arc #1 (Orbit 2037)
---------------------------------------
Vector Time (GMT): 2010/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3255218
05 A = 6718230
09 meter
Y = 2865798
61 meter E =
0007371
Z = 5127253
35 I = 51
46315
XDOT = -6072
741019 Wp = 20
82932
YDOT = 4557
874557 meter/sec RA = 331
03367 deg
ZDOT = 1314
150416 TA = 56
61290
MA = 56
54240
Ha = 190
641 n
mi
Hp = 181
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10679849
23 X = 3198022
67
Y = 9402226
40 feet Y = 2901879
73 meter
Z = 16821697
35 Z = 5142928
95
XDOT = -19923
691006 XDOT = -6129
640631
YDOT = 14953
656682 feet/sec YDOT = 4489
647187 meter/sec
ZDOT = 4311
517112 ZDOT = 1284
511245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12978860
56 X = 3955956
70
Y = -5648580
17 feet Y = -1721687
23 meter
Z = 16884112
75 Z = 5146277
57
XDOT = 4772
532241 XDOT = 1454
667827
YDOT = 23439
857313 feet/sec YDOT = 7144
468509 meter/sec
ZDOT = 4193
443221 ZDOT = 1278
161494
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
54977166
00016717 00000-0 10270-3 0 9006
2 25544 51
6445 331
3055 0009312 355
5318 4
5761 15
74840736 20383
Satellite: ISS
Catalog Number: 25544
Epoch time: 10148
54977166 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 331
3055 deg
Eccentricity:
0009312
Arg of perigee: 355
5318 deg
Mean anomaly: 4
5761 deg
Mean motion: 15
74840736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2038
Checksum: 303
Coasting Arc #2 (Orbit 2052)
---------------------------------------
Vector Time (GMT): 2010/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5110251
49 A = 6729306
89 meter
Y = -4278805
68 meter E =
0018353
Z = -845869
43 I = 51
47514
XDOT = 3681
067380 Wp = 19
81549
YDOT = 3230
291185 meter/sec RA = 325
85966 deg
ZDOT = 5953
059881 TA = 330
92365
MA = 331
02574
Ha = 190
679 n
mi
Hp = 181
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16765916
97 X = 5161827
17
Y = -14038076
39 feet Y = -4221371
29 meter
Z = -2775162
19 Z = -820919
12
XDOT = 12076
992718 XDOT = 3615
752999
YDOT = 10598
068193 feet/sec YDOT = 3271
088834 meter/sec
ZDOT = 19531
036355 ZDOT = 5970
784558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6047184
65 X = -1843181
88
Y = -21027052
69 feet Y = -6409045
66 meter
Z = -2675761
34 Z = -815572
06
XDOT = 12998
957415 XDOT = 3962
082220
YDOT = -6209
139745 feet/sec YDOT = -1892
545794 meter/sec
ZDOT = 19601
613669 ZDOT = 5974
571846
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
50157005
00016717 00000-0 10270-3 0 9016
2 25544 51
6446 326
4109 0009200 358
6856 1
4282 15
74907854 20532
Satellite: ISS
Catalog Number: 25544
Epoch time: 10149
50157005 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 326
4109 deg
Eccentricity:
0009200
Arg of perigee: 358
6856 deg
Mean anomaly: 1
4282 deg
Mean motion: 15
74907854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2053
Checksum: 292
Coasting Arc #3 (Orbit 2068)
---------------------------------------
Vector Time (GMT): 2010/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3158079
59 A = 6717513
02 meter
Y = -2812115
62 meter E =
0018533
Z = -5233611
93 I = 51
41161
XDOT = 5627
130191 Wp = 55
92992
YDOT = -5209
056971 meter/sec RA = 320
71681 deg
ZDOT = -587
883853 TA = 208
40717
MA = 208
50833
Ha = 190
724 n
mi
Hp = 181
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10361153
50 X = -3100975
27
Y = -9226101
12 feet Y = -2847110
96 meter
Z = -17170642
82 Z = -5248815
71
XDOT = 18461
713226 XDOT = 5687
816425
YDOT = -17090
081926 feet/sec YDOT = -5145
791635 meter/sec
ZDOT = -1928
752798 ZDOT = -560
400660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12489904
58 X = -3806922
92
Y = 5864633
89 feet Y = 1787540
41 meter
Z = -17231186
02 Z = -5252065
50
XDOT = -8134
699336 XDOT = -2479
456358
YDOT = -22753
587854 feet/sec YDOT = -6935
293578 meter/sec
ZDOT = -1819
256587 ZDOT = -554
509408
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
51680642
00016717 00000-0 10270-3 0 9028
2 25544 51
6448 321
1908 0009183 3
5183 356
6044 15
74945469 20694
Satellite: ISS
Catalog Number: 25544
Epoch time: 10150
51680642 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 321
1908 deg
Eccentricity:
0009183
Arg of perigee: 3
5183 deg
Mean anomaly: 356
6044 deg
Mean motion: 15
74945469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2069
Checksum: 306
Coasting Arc #4 (Orbit 2084)
---------------------------------------
Vector Time (GMT): 2010/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4711619
03 A = 6729277
99 meter
Y = 4802337
19 meter E =
0010126
Z = 161612
11 I = 51
42918
XDOT = -3532
706046 Wp = 85
22393
YDOT = -3252
679371 meter/sec RA = 315
55134 deg
ZDOT = -6013
955851 TA = 93
01589
MA = 92
90001
Ha = 190
812 n
mi
Hp = 181
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15458067
68 X = -4765754
53
Y = 15755699
43 feet Y = 4749346
34 meter
Z = 530223
47 Z = 138592
35
XDOT = -11590
242933 XDOT = -3466
856742
YDOT = -10671
520246 feet/sec YDOT = -3291
815038 meter/sec
ZDOT = -19730
826283 ZDOT = -6030
958312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8853201
42 X = 2698455
79
Y = 20221364
76 feet Y = 6163471
98 meter
Z = 438508
78 Z = 133657
48
XDOT = -12706
553188 XDOT = -3872
957412
YDOT = 6020
328271 feet/sec YDOT = 1834
996057 meter/sec
ZDOT = -19798
536671 ZDOT = -6034
593977
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
53202284
00016717 00000-0 10270-3 0 9034
2 25544 51
6448 315
9695 0009453 6
1966 353
9313 15
75014115 20859
Satellite: ISS
Catalog Number: 25544
Epoch time: 10151
53202284 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 315
9695 deg
Eccentricity:
0009453
Arg of perigee: 6
1966 deg
Mean anomaly: 353
9313 deg
Mean motion: 15
75014115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2085
Checksum: 297
Coasting Arc #5 (Orbit 2100)
---------------------------------------
Vector Time (GMT): 2010/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3037451
80 A = 6717399
79 meter
Y = 2895270
79 meter E =
0010471
Z = 5242134
11 I = 51
36771
XDOT = -5116
308483 Wp = 23
56890
YDOT = 5758
908763 meter/sec RA = 310
39060 deg
ZDOT = -206
535082 TA = 68
45305
MA = 68
34148
Ha = 190
922 n
mi
Hp = 180
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9965393
05 X = 2979385
33
Y = 9498919
92 feet Y = 2928911
96 meter
Z = 17198602
72 Z = 5256749
40
XDOT = -16785
788987 XDOT = -5179
322077
YDOT = 18894
057621 feet/sec YDOT = 5701
342857 meter/sec
ZDOT = -677
608538 ZDOT = -231
542284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12394318
43 X = 3777788
26
Y = -5823557
23 feet Y = -1775020
24 meter
Z = 17256810
99 Z = 5259875
99
XDOT = 11235
350848 XDOT = 3424
534939
YDOT = 21515
989348 feet/sec YDOT = 6558
073553 meter/sec
ZDOT = -777
240094 ZDOT = -236
902781
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
54722609
00016717 00000-0 10270-3 0 9045
2 25544 51
6447 310
7486 0009269 11
5487 348
5888 15
74950762 21014
Satellite: ISS
Catalog Number: 25544
Epoch time: 10152
54722609 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 310
7486 deg
Eccentricity:
0009269
Arg of perigee: 11
5487 deg
Mean anomaly: 348
5888 deg
Mean motion: 15
74950762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2101
Checksum: 323
Coasting Arc #6 (Orbit 2116)
---------------------------------------
Vector Time (GMT): 2010/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4195262
46 A = 6729119
38 meter
Y = -5219555
04 meter E =
0021310
Z = 519862
86 I = 51
39044
XDOT = 3464
820775 Wp = 35
84431
YDOT = 3392
574915 meter/sec RA = 305
23664 deg
ZDOT = 5994
952608 TA = 329
84009
MA = 329
96261
Ha = 190
880 n
mi
Hp = 180
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13763984
44 X = 4250791
27
Y = -17124524
40 feet Y = -5172330
70 meter
Z = 1705586
83 Z = 540377
62
XDOT = 11367
522227 XDOT = 3397
504545
YDOT = 11130
495129 feet/sec YDOT = 3430
943455 meter/sec
ZDOT = 19668
479684 ZDOT = 6011
621594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11412168
32 X = -3478428
90
Y = -18766287
43 feet Y = -5719964
41 meter
Z = 1787316
44 Z = 544774
05
XDOT = 12930
690319 XDOT = 3941
274409
YDOT = -5952
110480 feet/sec YDOT = -1814
203274 meter/sec
ZDOT = 19734
872306 ZDOT = 6015
189079
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
56240643
00016717 00000-0 10270-3 0 9052
2 25544 51
6459 305
5283 0009160 15
0209 345
1225 15
75033613 21178
Satellite: ISS
Catalog Number: 25544
Epoch time: 10153
56240643 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 305
5283 deg
Eccentricity:
0009160
Arg of perigee: 15
0209 deg
Mean anomaly: 345
1225 deg
Mean motion: 15
75033613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2117
Checksum: 274
Coasting Arc #7 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2010/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3019919
60 A = 6717436
96 meter
Y = -3054355
19 meter E =
0018594
Z = -5178670
84 I = 51
33500
XDOT = 4499
977370 Wp = 68
54367
YDOT = -6153
839116 meter/sec RA = 300
06076 deg
ZDOT = 1014
983402 TA = 211
13196
MA = 211
24225
Ha = 190
962 n
mi
Hp = 180
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9907872
70 X = -2960383
77
Y = -10020850
36 feet Y = -3087792
26 meter
Z = -16990389
89 Z = -5193197
33
XDOT = 14763
705283 XDOT = 4563
525660
YDOT = -20189
760880 feet/sec YDOT = -6103
162485 meter/sec
ZDOT = 3329
998037 ZDOT = 1036
997946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12662058
58 X = -3859395
46
Y = 6023791
63 feet Y = 1836051
69 meter
Z = -17048253
25 Z = -5196307
59
XDOT = -13871
896427 XDOT = -4228
154031
YDOT = -19575
263749 feet/sec YDOT = -5966
540391 meter/sec
ZDOT = 3417
696787 ZDOT = 1041
713981
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
51412376
00016717 00000-0 10270-3 0 9063
2 25544 51
6461 300
6350 0009241 18
7744 341
3759 15
75059575 21328
Satellite: ISS
Catalog Number: 25544
Epoch time: 10154
51412376 = yrday
fracday
Element set: 906
Inclination: 51
6461 deg
RA of node: 300
6350 deg
Eccentricity:
0009241
Arg of perigee: 18
7744 deg
Mean anomaly: 341
3759 deg
Mean motion: 15
75059575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2132
Checksum: 295
Coasting Arc #8 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2010/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3673251
62 A = 6728318
34 meter
Y = 5494982
67 meter E =
0009067
Z = -1271254
64 I = 51
35750
XDOT = -3447
764505 Wp = 79
91717
YDOT = -3646
240862 meter/sec RA = 294
91616 deg
ZDOT = -5832
354504 TA = 114
07650
MA = 113
98162
Ha = 191
054 n
mi
Hp = 180
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12051350
47 X = -3728248
97
Y = 18028158
36 feet Y = 5453598
80 meter
Z = -4170782
94 Z = -1289232
36
XDOT = -11311
563336 XDOT = -3378
402755
YDOT = -11962
732487 feet/sec YDOT = -3684
407399 meter/sec
ZDOT = -19135
021337 ZDOT = -5848
935673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13442891
47 X = 4097393
32
Y = 16998109
62 feet Y = 5181023
81 meter
Z = -4242394
44 Z = -1293081
82
XDOT = -13593
213695 XDOT = -4143
211534
YDOT = 5985
087222 feet/sec YDOT = 1824
254585 meter/sec
ZDOT = -19201
073362 ZDOT = -5852
487161
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
52927026
00016717 00000-0 10270-3 0 9079
2 25544 51
6456 295
4128 0009373 21
9149 338
2414 15
75097693 21480
Satellite: ISS
Catalog Number: 25544
Epoch time: 10155
52927026 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 295
4128 deg
Eccentricity:
0009373
Arg of perigee: 21
9149 deg
Mean anomaly: 338
2414 deg
Mean motion: 15
75097693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2148
Checksum: 323
Coasting Arc #9 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2010/156/03:23:54
562
Vector Time (MET): N/A
Weight (LBS) : 815047
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4624113
45 A = 6728009
02 meter
Y = 2377747
66 meter E =
0006668
Z = -4276516
84 I = 51
32791
XDOT = -291
159643 Wp = 40
47703
YDOT = -6848
190363 meter/sec RA = 291
62002 deg
ZDOT = -3490
824376 TA = 193
97365
MA = 193
99211
Ha = 191
104 n
mi
Hp = 187
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15170975
88 X = -4629583
55
Y = 7801009
39 feet Y = 2326007
91 meter
Z = -14030567
06 Z = -4298993
93
XDOT = -955
248172 XDOT = -197
602437
YDOT = -22467
816152 feet/sec YDOT = -6850
922830 meter/sec
ZDOT = -11452
835878 ZDOT = -3492
012265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14854780
79 X = -4527737
19
Y = -8235854
07 feet Y = -2510288
32 meter
Z = -14120101
41 Z = -4303806
91
XDOT = 17609
644177 XDOT = 5367
419545
YDOT = -12107
483364 feet/sec YDOT = -3690
360929 meter/sec
ZDOT = -11457
575062 ZDOT = -3492
268879
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
16374960
00016717 00000-0 10270-3 0 9084
2 25544 51
6484 292
1557 0004304 297
5894 62
4832 15
72643095 21589
Satellite: ISS
Catalog Number: 25544
Epoch time: 10156
16374960 = yrday
fracday
Element set: 908
Inclination: 51
6484 deg
RA of node: 292
1557 deg
Eccentricity:
0004304
Arg of perigee: 297
5894 deg
Mean anomaly: 62
4832 deg
Mean motion: 15
72643095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 327
Coasting Arc #10 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2010/157/03:23:54
562
Vector Time (MET): N/A
Weight (LBS) : 815047
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1145078
47 A = 6731055
27 meter
Y = 5700463
20 meter E =
0009165
Z = 3385944
68 I = 51
32737
XDOT = -4929
612406 Wp = 75
51379
YDOT = 3725
279638 meter/sec RA = 286
42263 deg
ZDOT = -4591
997644 TA = 64
35288
MA = 64
25824
Ha = 191
213 n
mi
Hp = 187
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3756819
11 X = 1064801
32
Y = 18702307
07 feet Y = 5712818
95 meter
Z = 11108742
39 Z = 3391313
09
XDOT = -16173
269049 XDOT = -4948
595508
YDOT = 12222
046055 feet/sec YDOT = 3670
048093 meter/sec
ZDOT = -15065
609068 ZDOT = -4615
991629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13288985
09 X = -4050482
66
Y = 13668102
84 feet Y = 4166037
75 meter
Z = 11130138
23 Z = 3392466
13
XDOT = -18201
094021 XDOT = -5547
693458
YDOT = -5316
581240 feet/sec YDOT = -1620
493962 meter/sec
ZDOT = -15161
181512 ZDOT = -4621
128125
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
18046410
00016717 00000-0 10270-3 0 9094
2 25544 51
6478 286
9456 0004284 301
6799 58
3946 15
72639765 21746
Satellite: ISS
Catalog Number: 25544
Epoch time: 10157
18046410 = yrday
fracday
Element set: 909
Inclination: 51
6478 deg
RA of node: 286
9456 deg
Eccentricity:
0004284
Arg of perigee: 301
6799 deg
Mean anomaly: 58
3946 deg
Mean motion: 15
72639765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2174
Checksum: 344
Coasting Arc #11 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2010/158/03:23:54
562
Vector Time (MET): N/A
Weight (LBS) : 815047
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3855118
86 A = 6729881
53 meter
Y = -4061355
85 meter E =
0008122
Z = 3724949
96 I = 51
31686
XDOT = 2250
635223 Wp = 81
22508
YDOT = 6025
956668 meter/sec RA = 281
32576 deg
ZDOT = 4234
247536 TA = 323
97044
MA = 324
02516
Ha = 191
212 n
mi
Hp = 187
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12648027
75 X = 3882151
81
Y = -13324658
30 feet Y = -4018094
86 meter
Z = 12220964
43 Z = 3743743
57
XDOT = 7383
973830 XDOT = 2162
515173
YDOT = 19770
199043 feet/sec YDOT = 6050
631452 meter/sec
ZDOT = 13891
888240 ZDOT = 4244
967848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18155722
00 X = 5533864
07
Y = 2460425
03 feet Y = 749937
55 meter
Z = 12295818
95 Z = 3747765
61
XDOT = -11637
352751 XDOT = -3547
065118
YDOT = 16127
684297 feet/sec YDOT = 4915
718174 meter/sec
ZDOT = 13934
607791 ZDOT = 4247
268455
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
19716224
00016717 00000-0 10270-3 0 9105
2 25544 51
6483 281
7348 0004396 306
5880 53
4878 15
72663287 21908
Satellite: ISS
Catalog Number: 25544
Epoch time: 10158
19716224 = yrday
fracday
Element set: 910
Inclination: 51
6483 deg
RA of node: 281
7348 deg
Eccentricity:
0004396
Arg of perigee: 306
5880 deg
Mean anomaly: 53
4878 deg
Mean motion: 15
72663287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 327
Coasting Arc #12 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2010/159/00:04:52
471
Vector Time (MET): N/A
Weight (LBS) : 814792
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4172039
55 A = 6726986
33 meter
Y = 2076007
18 meter E =
0008408
Z = -4859043
42 I = 51
29659
XDOT = -963
034557 Wp = 53
07437
YDOT = -7281
684088 meter/sec RA = 276
88022 deg
ZDOT = -2281
940753 TA = 194
56887
MA = 194
59312
Ha = 191
316 n
mi
Hp = 188
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13687793
79 X = -4171339
08
Y = 6811047
19 feet Y = 2029357
45 meter
Z = -15941743
49 Z = -4879309
51
XDOT = -3159
562194 XDOT = -870
452466
YDOT = -23890
039659 feet/sec YDOT = -7291
935386 meter/sec
ZDOT = -7486
682260 ZDOT = -2286
395228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3505223
28 X = -1068392
05
Y = -14794564
27 feet Y = -4509383
19 meter
Z = -16022469
41 Z = -4883648
67
XDOT = 22888
105356 XDOT = 6976
294512
YDOT = 2712
472241 feet/sec YDOT = 826
761539 meter/sec
ZDOT = -7504
447528 ZDOT = -2287
355606
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 10159
02322238
00016717 00000-0 10270-3 0 9117
2 25544 51
6466 277
5007 0005282 286
7431 73
3151 15
72193611 22039
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
02322238 = yrday
fracday
Element set: 911
Inclination: 51
6466 deg
RA of node: 277
5007 deg
Eccentricity:
0005282
Arg of perigee: 286
7431 deg
Mean anomaly: 73
3151 deg
Mean motion: 15
72193611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 280
Coasting Arc #13 (Orbit 2203)
---------------------------------------
Vector Time (GMT): 2010/159/01:35:52
292
Vector Time (MET): N/A
Weight (LBS) : 814538
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4125282
51 A = 6728769
27 meter
Y = 2330793
64 meter E =
0005918
Z = -4783064
58 I = 51
29865
XDOT = -1177
374774 Wp = 51
19119
YDOT = -7184
323752 meter/sec RA = 276
55698 deg
ZDOT = -2483
881960 TA = 194
35889
MA = 194
37572
Ha = 191
271 n
mi
Hp = 189
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13534391
44 X = -4127803
68
Y = 7646960
77 feet Y = 2284648
76 meter
Z = -15692469
09 Z = -4803111
32
XDOT = -3862
778129 XDOT = -1084
884445
YDOT = -23570
615984 feet/sec YDOT = -7196
972416 meter/sec
ZDOT = -8149
219030 ZDOT = -2489
377935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9766168
67 X = -2976728
21
Y = -11990212
67 feet Y = -3654616
82 meter
Z = -15772320
57 Z = -4807403
31
XDOT = 21739
798790 XDOT = 6626
290671
YDOT = -6951
916281 feet/sec YDOT = -2118
944082 meter/sec
ZDOT = -8171
133082 ZDOT = -2490
561363
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 10159
08678970
00016717 00000-0 10270-3 0 9121
2 25544 51
6478 277
1759 0006616 270
8818 89
1586 15
71681060 22044
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
08678970 = yrday
fracday
Element set: 912
Inclination: 51
6478 deg
RA of node: 277
1759 deg
Eccentricity:
0006616
Arg of perigee: 270
8818 deg
Mean anomaly: 89
1586 deg
Mean motion: 15
71681060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2204
Checksum: 339
Coasting Arc #14 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2010/160/01:35:52
292
Vector Time (MET): N/A
Weight (LBS) : 814538
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2126816
98 A = 6735319
97 meter
Y = 5727470
34 meter E =
0006869
Z = 2827043
28 I = 51
31806
XDOT = -4151
940833 Wp = 103
79420
YDOT = 4045
257143 meter/sec RA = 271
37283 deg
ZDOT = -5063
280358 TA = 43
66123
MA = 43
60691
Ha = 191
363 n
mi
Hp = 189
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6977746
00 X = 2048879
83
Y = 18790913
20 feet Y = 5750817
51 meter
Z = 9275076
37 Z = 2837187
02
XDOT = -13621
853127 XDOT = -4172
270171
YDOT = 13271
841019 feet/sec YDOT = 3998
714720 meter/sec
ZDOT = -16611
812198 ZDOT = -5083
499604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17212337
21 X = -5246320
38
Y = 10235782
26 feet Y = 3119866
43 meter
Z = 9315503
70 Z = 2839365
53
XDOT = -14769
931553 XDOT = -4501
875137
YDOT = -9619
494961 feet/sec YDOT = -2932
022064 meter/sec
ZDOT = -16692
348238 ZDOT = -5087
827743
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 10160
10412833
00016717 00000-0 10270-3 0 9131
2 25544 51
6475 271
9702 0006645 274
5714 85
4689 15
71670195 22207
Satellite: ISS
Catalog Number: 25544
Epoch time: 10160
10412833 = yrday
fracday
Element set: 913
Inclination: 51
6475 deg
RA of node: 271
9702 deg
Eccentricity:
0006645
Arg of perigee: 274
5714 deg
Mean anomaly: 85
4689 deg
Mean motion: 15
71670195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 302
Coasting Arc #15 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2010/161/01:35:52
292
Vector Time (MET): N/A
Weight (LBS) : 814538
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2901128
11 A = 6731785
10 meter
Y = -4581908
44 meter E =
0004211
Z = 3985655
32 I = 51
30747
XDOT = 3505
292538 Wp = 105
89357
YDOT = 5625
981413 meter/sec RA = 266
28044 deg
ZDOT = 3911
585983 TA = 303
45935
MA = 303
49960
Ha = 191
463 n
mi
Hp = 189
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9518136
84 X = 2932786
34
Y = -15032508
00 feet Y = -4549289
95 meter
Z = 13076296
98 Z = 3999825
35
XDOT = 11500
303602 XDOT = 3423
119215
YDOT = 18457
944269 feet/sec YDOT = 5664
719574 meter/sec
ZDOT = 12833
287345 ZDOT = 3928
416288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16612531
62 X = 5063499
64
Y = 6254263
43 feet Y = 1906299
49 meter
Z = 13132735
84 Z = 4002857
88
XDOT = -15354
014891 XDOT = -4679
903739
YDOT = 13663
675985 feet/sec YDOT = 4164
688440 meter/sec
ZDOT = 12900
356484 ZDOT = 3932
028656
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 10161
12145203
00016717 00000-0 10270-3 0 9149
2 25544 51
6481 266
7639 0006677 279
5562 80
4845 15
71698665 22364
Satellite: ISS
Catalog Number: 25544
Epoch time: 10161
12145203 = yrday
fracday
Element set: 914
Inclination: 51
6481 deg
RA of node: 266
7639 deg
Eccentricity:
0006677
Arg of perigee: 279
5562 deg
Mean anomaly: 80
4845 deg
Mean motion: 15
71698665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 327
Coasting Arc #16 (Orbit 2250)
---------------------------------------
Vector Time (GMT): 2010/162/01:35:52
292
Vector Time (MET): N/A
Weight (LBS) : 814538
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3808852
21 A = 6731823
66 meter
Y = -3907284
90 meter E =
0000500
Z = -3942884
97 I = 51
31158
XDOT = 2246
476177 Wp = 177
82839
YDOT = -6196
668616 meter/sec RA = 261
08768 deg
ZDOT = 3970
132715 TA = 133
55119
MA = 133
54704
Ha = 191
683 n
mi
Hp = 189
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12496234
28 X = -3745723
10
Y = -12819176
17 feet Y = -3949524
03 meter
Z = -12935974
31 Z = -3961236
00
XDOT = 7370
328666 XDOT = 2296
315062
YDOT = -20330
277611 feet/sec YDOT = -6171
269272 meter/sec
ZDOT = 13025
369801 ZDOT = 3981
166115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9831288
83 X = 2996576
84
Y = -14897502
01 feet Y = -4540758
61 meter
Z = -13009103
51 Z = -3965174
75
XDOT = 20339
502651 XDOT = 6199
480408
YDOT = 2008
612768 feet/sec YDOT = 612
225172 meter/sec
ZDOT = 13069
309874 ZDOT = 3983
525650
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 10162
07517990
00016717 00000-0 10270-3 0 9151
2 25544 51
6485 261
8834 0006800 283
7418 76
2987 15
71730452 22514
Satellite: ISS
Catalog Number: 25544
Epoch time: 10162
07517990 = yrday
fracday
Element set: 915
Inclination: 51
6485 deg
RA of node: 261
8834 deg
Eccentricity:
0006800
Arg of perigee: 283
7418 deg
Mean anomaly: 76
2987 deg
Mean motion: 15
71730452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2251
Checksum: 319
Coasting Arc #17 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2010/163/01:35:52
292
Vector Time (MET): N/A
Weight (LBS) : 814538
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -894338
14 A = 6734982
09 meter
Y = 6010812
62 meter E =
0002455
Z = -2901546
32 I = 51
32806
XDOT = -4917
382076 Wp = 273
00264
YDOT = -3151
280895 meter/sec RA = 255
99669 deg
ZDOT = -5008
708052 TA = 300
49327
MA = 300
51750
Ha = 192
024 n
mi
Hp = 189
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2934180
25 X = -947390
37
Y = 19720513
85 feet Y = 6000515
57 meter
Z = -9519508
93 Z = -2906018
68
XDOT = -16133
143295 XDOT = -4857
446832
YDOT = -10338
848081 feet/sec YDOT = -3205
933842 meter/sec
ZDOT = -16432
769198 ZDOT = -5032
451945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19848067
25 X = -6049690
90
Y = 1795304
31 feet Y = 547208
75 meter
Z = -9537307
76 Z = -2906971
41
XDOT = 6450
088595 XDOT = 1965
987004
YDOT = -16555
969624 feet/sec YDOT = -5046
259541 meter/sec
ZDOT = -16527
393945 ZDOT = -5037
549675
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 10163
09247680
00016717 00000-0 10270-3 0 9161
2 25544 51
6486 256
6778 0006923 287
0088 73
0315 15
71729344 22675
Satellite: ISS
Catalog Number: 25544
Epoch time: 10163
09247680 = yrday
fracday
Element set: 916
Inclination: 51
6486 deg
RA of node: 256
6778 deg
Eccentricity:
0006923
Arg of perigee: 287
0088 deg
Mean anomaly: 73
0315 deg
Mean motion: 15
71729344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 330
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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