Date:
August 2nd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 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 3028)
---------------------------------------
Vector Time (GMT): 2010/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5886772
53 A = 6736192
33 meter
Y = 1453024
09 meter E =
0017697
Z = 2909467
41 I = 51
70110
XDOT = -3624
406982 Wp = 121
91121
YDOT = -4560
767225 meter/sec RA = 8
40280 deg
ZDOT = -5042
500272 TA = 24
63621
MA = 24
55178
Ha = 196
145 n
mi
Hp = 186
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19313558
18 X = -5916716
47
Y = 4767139
42 feet Y = 1387027
14 meter
Z = 9545496
75 Z = 2880797
19
XDOT = -11891
099021 XDOT = -3548
643054
YDOT = -14963
147063 feet/sec YDOT = -4600
873679 meter/sec
ZDOT = -16543
636064 ZDOT = -5059
923567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15517127
17 X = 4729620
36
Y = 12535298
83 feet Y = 3820759
08 meter
Z = 9430837
90 Z = 2874519
39
XDOT = -3861
988708 XDOT = -1177
134158
YDOT = 17312
292654 feet/sec YDOT = 5276
786801 meter/sec
ZDOT = -16613
263137 ZDOT = -5063
722604
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 10211
53766810
00016717 00000-0 10270-3 0 9008
2 25544 51
6422 8
7446 0007649 167
4000 192
7355 15
71333273 30296
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211
53766810 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 8
7446 deg
Eccentricity:
0007649
Arg of perigee: 167
4000 deg
Mean anomaly: 192
7355 deg
Mean motion: 15
71333273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 288
Coasting Arc #2 (Orbit 3044)
---------------------------------------
Vector Time (GMT): 2010/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4403939
30 A = 6733087
50 meter
Y = 3316504
31 meter E =
0015483
Z = 3862163
07 I = 51
66218
XDOT = -5817
533868 Wp = 127
13796
YDOT = 2915
774610 meter/sec RA = 3
33999 deg
ZDOT = 4109
325400 TA = 279
87419
MA = 280
04895
Ha = 195
851 n
mi
Hp = 186
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14448619
76 X = 4347764
73
Y = 10880919
65 feet Y = 3365437
54 meter
Z = 12671138
68 Z = 3883420
89
XDOT = -19086
397205 XDOT = -5869
668385
YDOT = 9566
189665 feet/sec YDOT = 2850
427797 meter/sec
ZDOT = 13482
038713 ZDOT = 4080
937582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -345548
62 X = -105323
22
Y = -18024347
84 feet Y = -5493821
22 meter
Z = 12756106
85 Z = 3888061
37
XDOT = 18060
093134 XDOT = 5504
716387
YDOT = 9162
037204 feet/sec YDOT = 2792
588940 meter/sec
ZDOT = 13368
499903 ZDOT = 4074
718770
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 10212
55521023
00016717 00000-0 10270-3 0 9017
2 25544 51
6431 3
5398 0007677 171
3351 188
7945 15
71382511 30456
Satellite: ISS
Catalog Number: 25544
Epoch time: 10212
55521023 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 3
5398 deg
Eccentricity:
0007677
Arg of perigee: 171
3351 deg
Mean anomaly: 188
7945 deg
Mean motion: 15
71382511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 287
Coasting Arc #3 (Orbit 3059)
---------------------------------------
Vector Time (GMT): 2010/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4034796
50 A = 6732241
50 meter
Y = -3431398
38 meter E =
0013066
Z = -4169465
53 I = 51
62973
XDOT = 6154
530716 Wp = 140
96198
YDOT = 2735
484062 meter/sec RA = 358
17491 deg
ZDOT = 3700
820262 TA = 166
95153
MA = 166
91770
Ha = 195
823 n
mi
Hp = 187
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13237521
32 X = 4093121
53
Y = -11257868
70 feet Y = -3385952
56 meter
Z = -13679348
84 Z = -4149723
10
XDOT = 20192
029908 XDOT = 6105
506814
YDOT = 8974
685243 feet/sec YDOT = 2804
033420 meter/sec
ZDOT = 12141
798759 ZDOT = 3730
599834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17142740
47 X = -5225107
29
Y = -3201932
10 feet Y = -975948
90 meter
Z = -13600376
58 Z = -4145394
78
XDOT = -5998
832653 XDOT = -1828
444193
YDOT = -20013
019266 feet/sec YDOT = -6099
968272 meter/sec
ZDOT = 12260
841561 ZDOT = 3737
104508
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 10213
50914917
00016717 00000-0 10270-3 0 9022
2 25544 51
6442 358
6609 0007609 174
0799 186
0454 15
71370390 30603
Satellite: ISS
Catalog Number: 25544
Epoch time: 10213
50914917 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 358
6609 deg
Eccentricity:
0007609
Arg of perigee: 174
0799 deg
Mean anomaly: 186
0454 deg
Mean motion: 15
71370390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 309
Coasting Arc #4 (Orbit 3075)
---------------------------------------
Vector Time (GMT): 2010/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6097573
56 A = 6736715
92 meter
Y = -1291998
91 meter E =
0011505
Z = -2543244
12 I = 51
61493
XDOT = 3174
176473 Wp = 157
68464
YDOT = -4604
441598 meter/sec RA = 353
10498 deg
ZDOT = -5289
396247 TA = 51
12935
MA = 51
02676
Ha = 195
573 n
mi
Hp = 187
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20005162
59 X = -6070318
44
Y = -4238841
58 feet Y = -1360033
08 meter
Z = -8343976
77 Z = -2572799
88
XDOT = 10413
964808 XDOT = 3251
123090
YDOT = -15106
435690 feet/sec YDOT = -4568
515509 meter/sec
ZDOT = -17353
662229 ZDOT = -5273
789536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9641619
94 X = 2938765
76
Y = 17978534
22 feet Y = 5479857
23 meter
Z = -8462135
01 Z = -2579258
75
XDOT = -17015
707449 XDOT = -5186
387631
YDOT = 1014
413853 feet/sec YDOT = 309
193342 meter/sec
ZDOT = -17291
214696 ZDOT = -5270
362239
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 10214
52667404
00016717 00000-0 10270-3 0 9032
2 25544 51
6440 353
4557 0007532 178
1212 181
9980 15
71393501 30760
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214
52667404 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 353
4557 deg
Eccentricity:
0007532
Arg of perigee: 178
1212 deg
Mean anomaly: 181
9980 deg
Mean motion: 15
71393501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 296
Coasting Arc #5 (Orbit 3091)
---------------------------------------
Vector Time (GMT): 2010/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1371872
07 A = 6729001
25 meter
Y = 4322991
60 meter E =
0006436
Z = 4965333
78 I = 51
55905
XDOT = -7432
911066 Wp = 129
85057
YDOT = -47
895012 meter/sec RA = 347
94790 deg
ZDOT = -2014
273460 TA = 339
64444
MA = 339
67008
Ha = 195
625 n
mi
Hp = 187
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4500892
63 X = -1444231
20
Y = 14183043
29 feet Y = 4307245
54 meter
Z = 16290465
16 Z = 4958493
82
XDOT = -24386
191162 XDOT = -7422
038122
YDOT = -157
135866 feet/sec YDOT = -130
953320 meter/sec
ZDOT = -6608
508727 ZDOT = -2050
356009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13701883
08 X = 4176333
96
Y = -5879363
79 feet Y = -1792030
08 meter
Z = 16263071
30 Z = 4956984
13
XDOT = 15484
161929 XDOT = 4719
572556
YDOT = 17428
087009 feet/sec YDOT = 5312
080920 meter/sec
ZDOT = -6752
773111 ZDOT = -2058
245244
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 10215
54419145
00016717 00000-0 10270-3 0 9043
2 25544 51
6444 348
2512 0007526 181
0944 179
0203 15
71367854 30921
Satellite: ISS
Catalog Number: 25544
Epoch time: 10215
54419145 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 348
2512 deg
Eccentricity:
0007526
Arg of perigee: 181
0944 deg
Mean anomaly: 179
0203 deg
Mean motion: 15
71367854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3092
Checksum: 298
Coasting Arc #6 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2010/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6555126
59 A = 6739080
95 meter
Y = -1237044
90 meter E =
0010593
Z = 945855
02 I = 51
56530
XDOT = 61
906571 Wp = 88
01616
YDOT = 4903
216536 meter/sec RA = 342
85250 deg
ZDOT = 5926
981240 TA = 282
30813
MA = 282
42671
Ha = 195
373 n
mi
Hp = 187
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21506320
83 X = 6563877
49
Y = -4058546
25 feet Y = -1163692
71 meter
Z = 3103198
89 Z = 977720
82
XDOT = 203
105548 XDOT = -21
718756
YDOT = 16086
668426 feet/sec YDOT = 4903
440688 meter/sec
ZDOT = 19445
476510 ZDOT = 5927
079311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17432840
66 X = -5313529
83
Y = -13201615
44 feet Y = -4023852
39 meter
Z = 3230618
03 Z = 984692
37
XDOT = 10901
806470 XDOT = 3322
870612
YDOT = -9593
538187 feet/sec YDOT = -2924
110439 meter/sec
ZDOT = 19445
814717 ZDOT = 5927
084326
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 10216
56169618
00016717 00000-0 10270-3 0 9054
2 25544 51
6454 343
0463 0007480 185
6533 174
4545 15
71429694 31080
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216
56169618 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 343
0463 deg
Eccentricity:
0007480
Arg of perigee: 185
6533 deg
Mean anomaly: 174
4545 deg
Mean motion: 15
71429694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 318
Coasting Arc #7 (Orbit 3122)
---------------------------------------
Vector Time (GMT): 2010/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1430093
20 A = 6727390
25 meter
Y = -3944958
80 meter E =
0015772
Z = -5270397
92 I = 51
49756
XDOT = 7155
643262 Wp = 118
52036
YDOT = -2803
326845 meter/sec RA = 337
71910 deg
ZDOT = 149
623062 TA = 152
94608
MA = 152
86379
Ha = 195
163 n
mi
Hp = 187
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4691906
82 X = -1360271
22
Y = -12942778
21 feet Y = -3960560
00 meter
Z = -17291331
76 Z = -5277176
08
XDOT = 23476
519890 XDOT = 7185
731915
YDOT = -9197
266551 feet/sec YDOT = -2723
139946 meter/sec
ZDOT = 490
889312 ZDOT = 184
457695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6303435
90 X = -1921287
26
Y = 12200808
82 feet Y = 3718806
53 meter
Z = -17318389
39 Z = -5278645
09
XDOT = -21874
601567 XDOT = -6667
378558
YDOT = -10373
961954 feet/sec YDOT = -3161
983604 meter/sec
ZDOT = 630
198039 ZDOT = 192
084362
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 10217
51560057
00016717 00000-0 10270-3 0 9063
2 25544 51
6455 338
1675 0007331 189
5309 170
5715 15
71451001 31230
Satellite: ISS
Catalog Number: 25544
Epoch time: 10217
51560057 = yrday
fracday
Element set: 906
Inclination: 51
6455 deg
RA of node: 338
1675 deg
Eccentricity:
0007331
Arg of perigee: 189
5309 deg
Mean anomaly: 170
5715 deg
Mean motion: 15
71451001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 287
Coasting Arc #8 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2010/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5668315
21 A = 6739293
94 meter
Y = 3558442
54 meter E =
0017708
Z = 690817
10 I = 51
51017
XDOT = -3089
554469 Wp = 149
97622
YDOT = -3751
257183 meter/sec RA = 332
58813 deg
ZDOT = -5976
821625 TA = 22
48622
MA = 22
40871
Ha = 195
060 n
mi
Hp = 187
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18596834
68 X = -5711040
91
Y = 11674680
26 feet Y = 3494817
08 meter
Z = 2266460
30 Z = 663177
38
XDOT = -10136
333561 XDOT = -3018
343645
YDOT = -12307
274222 feet/sec YDOT = -3785
407593 meter/sec
ZDOT = -19608
994833 ZDOT = -5991
657951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21338438
78 X = 6503956
14
Y = 5224973
79 feet Y = 1592572
01 meter
Z = 2155908
42 Z = 657120
89
XDOT = -1473
701921 XDOT = -449
184346
YDOT = 14206
142288 feet/sec YDOT = 4330
032169 meter/sec
ZDOT = -19668
276580 ZDOT = -5994
890702
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 10218
53308976
00016717 00000-0 10270-3 0 9077
2 25544 51
6457 332
9620 0007380 193
6676 166
4287 15
71439190 31391
Satellite: ISS
Catalog Number: 25544
Epoch time: 10218
53308976 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 332
9620 deg
Eccentricity:
0007380
Arg of perigee: 193
6676 deg
Mean anomaly: 166
4287 deg
Mean motion: 15
71439190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 332
Coasting Arc #9 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2010/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3785930
69 A = 6728196
49 meter
Y = 2351004
55 meter E =
0010105
Z = 5041444
49 I = 51
44802
XDOT = -5482
734137 Wp = 168
43646
YDOT = 5120
218712 meter/sec RA = 327
48149 deg
ZDOT = 1719
241985 TA = 264
90851
MA = 265
02386
Ha = 194
735 n
mi
Hp = 187
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12421032
46 X = 3734869
96
Y = 7713269
53 feet Y = 2393055
06 meter
Z = 16540172
23 Z = 5059712
45
XDOT = -17987
972890 XDOT = -5547
933489
YDOT = 16798
617821 feet/sec YDOT = 5058
542769 meter/sec
ZDOT = 5640
557693 ZDOT = 1692
449509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3290009
02 X = -1002794
75
Y = -14160913
50 feet Y = -4316246
43 meter
Z = 16613194
79 Z = 5063701
77
XDOT = 23590
558399 XDOT = 7190
402200
YDOT = 1050
430793 feet/sec YDOT = 320
171306 meter/sec
ZDOT = 5533
377431 ZDOT = 1686
573441
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 10219
55056819
00016717 00000-0 10270-3 0 9087
2 25544 51
6466 327
7571 0007280 198
1513 161
9390 15
71494074 31552
Satellite: ISS
Catalog Number: 25544
Epoch time: 10219
55056819 = yrday
fracday
Element set: 908
Inclination: 51
6466 deg
RA of node: 327
7571 deg
Eccentricity:
0007280
Arg of perigee: 198
1513 deg
Mean anomaly: 161
9390 deg
Mean motion: 15
71494074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 323
Coasting Arc #10 (Orbit 3169)
---------------------------------------
Vector Time (GMT): 2010/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3711722
68 A = 6737266
64 meter
Y = -5148078
37 meter E =
0002595
Z = -2265936
53 I = 51
45323
XDOT = 5260
943075 Wp = 146
10152
YDOT = 1403
406083 meter/sec RA = 322
31852 deg
ZDOT = 5430
112501 TA = 188
43582
MA = 188
44018
Ha = 194
686 n
mi
Hp = 188
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12177567
86 X = 3780020
84
Y = -16890020
90 feet Y = -5106189
59 meter
Z = -7434174
98 Z = -2247739
94
XDOT = 17260
311926 XDOT = 5218
481016
YDOT = 4604
350667 feet/sec YDOT = 1461
999206 meter/sec
ZDOT = 17815
329729 ZDOT = 5455
566575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20517180
26 X = -6253636
54
Y = 3699792
73 feet Y = 1127696
83 meter
Z = -7361370
16 Z = -2243745
62
XDOT = -8900
665088 XDOT = -2712
922719
YDOT = -13715
194095 feet/sec YDOT = -4180
391160 meter/sec
ZDOT = 17917
100945 ZDOT = 5461
132368
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 10220
50444842
00016717 00000-0 10270-3 0 9092
2 25544 51
6467 322
8780 0007067 202
3646 157
7209 15
71446669 31705
Satellite: ISS
Catalog Number: 25544
Epoch time: 10220
50444842 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 322
8780 deg
Eccentricity:
0007067
Arg of perigee: 202
3646 deg
Mean anomaly: 157
7209 deg
Mean motion: 15
71446669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 311
Coasting Arc #11 (Orbit 3185)
---------------------------------------
Vector Time (GMT): 2010/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5136470
09 A = 6731045
96 meter
Y = 19200
35 meter E =
0006339
Z = -4352924
83 I = 51
40944
XDOT = 2836
922562 Wp = 120
34210
YDOT = -6300
690623 meter/sec RA = 317
23213 deg
ZDOT = -3382
184244 TA = 115
46472
MA = 115
39913
Ha = 194
460 n
mi
Hp = 188
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16851935
99 X = -5115157
85
Y = 62993
27 feet Y = -38119
32 meter
Z = -14281249
43 Z = -4377825
41
XDOT = 9307
488719 XDOT = 2923
596817
YDOT = -20671
557161 feet/sec YDOT = -6268
481645 meter/sec
ZDOT = -11096
405000 ZDOT = -3368
192649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12324415
10 X = 3756481
72
Y = 11368666
12 feet Y = 3465169
43 meter
Z = -14380821
37 Z = -4383274
35
XDOT = -20109
514053 XDOT = -6129
379883
YDOT = 7862
568548 feet/sec YDOT = 2396
510893 meter/sec
ZDOT = -11040
415039 ZDOT = -3365
118504
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 10221
52191099
00016717 00000-0 10270-3 0 9100
2 25544 51
6466 317
6735 0007190 205
8403 154
2401 15
71473815 31868
Satellite: ISS
Catalog Number: 25544
Epoch time: 10221
52191099 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 317
6735 deg
Eccentricity:
0007190
Arg of perigee: 205
8403 deg
Mean anomaly: 154
2401 deg
Mean motion: 15
71473815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 292
Coasting Arc #12 (Orbit 3201)
---------------------------------------
Vector Time (GMT): 2010/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1164305
44 A = 6733743
18 meter
Y = 5569201
58 meter E =
0010216
Z = 3589218
91 I = 51
39680
XDOT = -6129
108029 Wp = 121
32462
YDOT = 1554
579537 meter/sec RA = 312
04998 deg
ZDOT = -4396
411965 TA = 15
61791
MA = 15
58642
Ha = 194
351 n
mi
Hp = 188
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3819899
73 X = -1243930
08
Y = 18271658
73 feet Y = 5555736
33 meter
Z = 11775652
59 Z = 3583369
59
XDOT = -20108
622144 XDOT = -6124
679645
YDOT = 5100
326564 feet/sec YDOT = 1486
065050 meter/sec
ZDOT = -14423
923771 ZDOT = -4426
175647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15101194
47 X = 4602844
08
Y = -10997726
66 feet Y = -3352107
09 meter
Z = 11752237
00 Z = 3582081
84
XDOT = 17504
086811 XDOT = 5335
245660
YDOT = 8480
588989 feet/sec YDOT = 2584
883524 meter/sec
ZDOT = -14542
949406 ZDOT = -4432
690979
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 10222
53936499
00016717 00000-0 10270-3 0 9114
2 25544 51
6463 312
4690 0006979 208
8906 151
1870 15
71495421 32025
Satellite: ISS
Catalog Number: 25544
Epoch time: 10222
53936499 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 312
4690 deg
Eccentricity:
0006979
Arg of perigee: 208
8906 deg
Mean anomaly: 151
1870 deg
Mean motion: 15
71495421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3202
Checksum: 313
Coasting Arc #13 (Orbit 3217)
---------------------------------------
Vector Time (GMT): 2010/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5258542
94 A = 6734559
54 meter
Y = -2674023
07 meter E =
0010418
Z = 3246535
46 I = 51
38045
XDOT = 157
914461 Wp = 121
09529
YDOT = 6069
261879 meter/sec RA = 306
96651 deg
ZDOT = 4726
693877 TA = 277
00825
MA = 277
12673
Ha = 194
122 n
mi
Hp = 188
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17252437
46 X = 5272282
77
Y = -8773041
57 feet Y = -2615142
07 meter
Z = 10651363
05 Z = 3272114
30
XDOT = 518
092064 XDOT = 67
074181
YDOT = 19912
276505 feet/sec YDOT = 6070
519859 meter/sec
ZDOT = 15507
525842 ZDOT = 4727
240360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18733617
04 X = -5710006
47
Y = -4634104
42 feet Y = -1412475
03 meter
Z = 10753653
35 Z = 3277713
54
XDOT = 12386
302565 XDOT = 3775
345022
YDOT = -13956
911682 feet/sec YDOT = -4254
066681 meter/sec
ZDOT = 15509
693915 ZDOT = 4727
354705
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 10223
55680824
00016717 00000-0 10270-3 0 9126
2 25544 51
6461 307
2636 0007007 213
6571 146
4147 15
71531311 32180
Satellite: ISS
Catalog Number: 25544
Epoch time: 10223
55680824 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 307
2636 deg
Eccentricity:
0007007
Arg of perigee: 213
6571 deg
Mean anomaly: 146
4147 deg
Mean motion: 15
71531311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 280
Coasting Arc #14 (Orbit 3232)
---------------------------------------
Vector Time (GMT): 2010/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1361085
73 A = 6730051
23 meter
Y = -4752248
11 meter E =
0010606
Z = -4576215
72 I = 51
34718
XDOT = 5535
616561 Wp = 147
89623
YDOT = -4440
417348 meter/sec RA = 301
78372 deg
ZDOT = 2959
085518 TA = 151
65831
MA = 151
60058
Ha = 193
927 n
mi
Hp = 188
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4465504
37 X = -1285613
98
Y = -15591365
17 feet Y = -4767046
65 meter
Z = -15013831
09 Z = -4582644
40
XDOT = 18161
471658 XDOT = 5570
484220
YDOT = -14568
298385 feet/sec YDOT = -4378
319781 meter/sec
ZDOT = 9708
285819 ZDOT = 2986
061870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6655967
34 X = -2028738
84
Y = 14763372
02 feet Y = 4499875
79 meter
Z = -15039530
14 Z = -4584048
79
XDOT = -22156
188064 XDOT = -6753
206122
YDOT = 29
840209 feet/sec YDOT = 9
095296 meter/sec
ZDOT = 9816
160431 ZDOT = 2991
965699
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 10224
51065509
00016717 00000-0 10270-3 0 9131
2 25544 51
6452 302
3844 0006843 217
1411 142
9279 15
71554390 32332
Satellite: ISS
Catalog Number: 25544
Epoch time: 10224
51065509 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 302
3844 deg
Eccentricity:
0006843
Arg of perigee: 217
1411 deg
Mean anomaly: 142
9279 deg
Mean motion: 15
71554390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3233
Checksum: 287
Coasting Arc #15 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2010/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4165371
74 A = 6737637
36 meter
Y = 4942250
42 meter E =
0010604
Z = -1878727
23 I = 51
35679
XDOT = -2778
228543 Wp = 180
16326
YDOT = -4472
865737 meter/sec RA = 296
68621 deg
ZDOT = -5617
175003 TA = 20
77501
MA = 20
73194
Ha = 193
709 n
mi
Hp = 188
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13665917
80 X = -4211200
89
Y = 16214732
35 feet Y = 4895414
48 meter
Z = -6163803
25 Z = -1899073
76
XDOT = -9114
923042 XDOT = -2700
718710
YDOT = -14674
756356 feet/sec YDOT = -4503
500214 meter/sec
ZDOT = -18429
051846 ZDOT = -5630
483197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20793261
04 X = 6337785
97
Y = -4038016
06 feet Y = -1230787
30 meter
Z = -6245161
86 Z = -1903525
33
XDOT = -2519
739768 XDOT = -768
016681
YDOT = 15557
522047 feet/sec YDOT = 4741
932720 meter/sec
ZDOT = -18482
262817 ZDOT = -5633
393706
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 10225
52808320
00016717 00000-0 10270-3 0 9140
2 25544 51
6443 297
1789 0006813 221
4446 138
6200 15
71532026 32499
Satellite: ISS
Catalog Number: 25544
Epoch time: 10225
52808320 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 297
1789 deg
Eccentricity:
0006813
Arg of perigee: 221
4446 deg
Mean anomaly: 138
6200 deg
Mean motion: 15
71532026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 293
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list