Date:
January 6th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 3767)
---------------------------------------
Vector Time (GMT): 2010/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6195935
42 A = 6722267
64 meter
Y = -2144505
79 meter E =
0009442
Z = -1489763
63 I = 51
60985
XDOT = 2839
921502 Wp = 86
51886
YDOT = 4205
306728 meter/sec RA = 351
27980 deg
ZDOT = 5789
718064 TA = 257
06055
MA = 257
16602
Ha = 187
540 n
mi
Hp = 177
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20327872
10 X = 6226692
05
Y = -7035780
14 feet Y = -2075047
10 meter
Z = -4887675
95 Z = -1459589
71
XDOT = 9317
327762 XDOT = 2764
561007
YDOT = 13796
938084 feet/sec YDOT = 4236
642643 meter/sec
ZDOT = 18995
138004 ZDOT = 5803
331424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11504214
64 X = 3506484
62
Y = 18207989
94 feet Y = 5549795
33 meter
Z = -4768239
77 Z = -1453359
48
XDOT = -9999
070266 XDOT = -3047
716617
YDOT = 11277
973865 feet/sec YDOT = 3437
526434 meter/sec
ZDOT = 19049
092258 ZDOT = 5806
163320
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 10004
50282405
00016717 00000-0 10270-3 0 9008
2 25544 51
6428 351
7849 0007599 145
6176 214
5482 15
77159841 37683
Satellite: ISS
Catalog Number: 25544
Epoch time: 10004
50282405 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 351
7849 deg
Eccentricity:
0007599
Arg of perigee: 145
6176 deg
Mean anomaly: 214
5482 deg
Mean motion: 15
77159841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3768
Checksum: 325
Coasting Arc #2 (Orbit 3783)
---------------------------------------
Vector Time (GMT): 2010/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1525816
41 A = 6711219
07 meter
Y = -3916321
27 meter E =
0019487
Z = -5247785
82 I = 51
54289
XDOT = 7350
323394 Wp = 105
91539
YDOT = -2215
657986 meter/sec RA = 346
13326 deg
ZDOT = -490
388214 TA = 159
45443
MA = 159
37595
Ha = 187
407 n
mi
Hp = 177
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5005959
34 X = -1456417
52
Y = -12848823
07 feet Y = -3932995
52 meter
Z = -17217145
07 Z = -5255029
80
XDOT = 24115
234231 XDOT = 7376
935167
YDOT = -7269
219115 feet/sec YDOT = -2133
313501 meter/sec
ZDOT = -1608
885217 ZDOT = -454
616262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11252872
09 X = 3429875
41
Y = -7907874
60 feet Y = -2410320
18 meter
Z = -17245879
40 Z = -5256544
04
XDOT = 12389
880130 XDOT = 3776
435464
YDOT = 20782
452812 feet/sec YDOT = 6334
491617 meter/sec
ZDOT = -1467
291536 ZDOT = -447
230460
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 10005
51662480
00016717 00000-0 10270-3 0 9016
2 25544 51
6429 346
5537 0007402 149
6581 210
5013 15
77144707 37846
Satellite: ISS
Catalog Number: 25544
Epoch time: 10005
51662480 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 346
5537 deg
Eccentricity:
0007402
Arg of perigee: 149
6581 deg
Mean anomaly: 210
5013 deg
Mean motion: 15
77144707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3784
Checksum: 296
Coasting Arc #3 (Orbit 3799)
---------------------------------------
Vector Time (GMT): 2010/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6466613
65 A = 6722933
41 meter
Y = 1684925
22 meter E =
0017861
Z = -649569
47 I = 51
55415
XDOT = -659
673836 Wp = 144
98560
YDOT = -4805
531447 meter/sec RA = 340
96995 deg
ZDOT = -5993
236994 TA = 42
11028
MA = 41
97317
Ha = 187
192 n
mi
Hp = 177
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21215924
06 X = -6481818
70
Y = 5527969
90 feet Y = 1612526
75 meter
Z = -2131133
43 Z = -681020
87
XDOT = -2164
284239 XDOT = -576
774675
YDOT = -15766
179288 feet/sec YDOT = -4812
444439 meter/sec
ZDOT = -19662
851031 ZDOT = -5996
240591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10890312
55 X = -3319367
27
Y = -19013912
40 feet Y = -5795440
50 meter
Z = -2255624
66 Z = -687514
40
XDOT = 13292
464979 XDOT = 4051
543325
YDOT = -5314
350524 feet/sec YDOT = -1619
814040 meter/sec
ZDOT = -19674
810485 ZDOT = -5996
882236
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 10006
53041267
00016717 00000-0 10270-3 0 9024
2 25544 51
6433 341
3232 0007265 153
3041 206
8499 15
77181864 38006
Satellite: ISS
Catalog Number: 25544
Epoch time: 10006
53041267 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 341
3232 deg
Eccentricity:
0007265
Arg of perigee: 153
3041 deg
Mean anomaly: 206
8499 deg
Mean motion: 15
77181864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3800
Checksum: 284
Coasting Arc #4 (Orbit 3815)
---------------------------------------
Vector Time (GMT): 2010/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -334778
54 A = 6712280
64 meter
Y = 4488714
33 meter E =
0008289
Z = 4971890
13 I = 51
48984
XDOT = -7294
087420 Wp = 113
54380
YDOT = 1595
313794 meter/sec RA = 335
77987 deg
ZDOT = -1932
153009 TA = 355
12471
MA = 355
13277
Ha = 187
104 n
mi
Hp = 177
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1098354
80 X = -409099
69
Y = 14726753
07 feet Y = 4484554
74 meter
Z = 16311975
50 Z = 4970083
58
XDOT = -23930
733006 XDOT = -7301
998378
YDOT = 5233
969141 feet/sec YDOT = 1513
702900 meter/sec
ZDOT = -6339
084674 ZDOT = -1967
606632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14476784
82 X = -4412524
01
Y = 2955931
63 feet Y = 900967
96 meter
Z = 16304887
41 Z = 4969729
68
XDOT = -11467
148301 XDOT = -3495
186802
YDOT = -20433
638369 feet/sec YDOT = -6228
172975 meter/sec
ZDOT = -6479
418417 ZDOT = -1974
926734
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 10007
54418816
00016717 00000-0 10270-3 0 9035
2 25544 51
6431 336
0932 0007211 157
7699 202
3780 15
77195782 38165
Satellite: ISS
Catalog Number: 25544
Epoch time: 10007
54418816 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 336
0932 deg
Eccentricity:
0007211
Arg of perigee: 157
7699 deg
Mean anomaly: 202
3780 deg
Mean motion: 15
77195782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3816
Checksum: 314
Coasting Arc #5 (Orbit 3831)
---------------------------------------
Vector Time (GMT): 2010/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6088247
74 A = 6719789
23 meter
Y = -999782
19 meter E =
0016234
Z = 2655118
51 I = 51
48922
XDOT = -1374
152353 Wp = 104
76329
YDOT = 5518
709361 meter/sec RA = 330
64871 deg
ZDOT = 5198
559621 TA = 285
57949
MA = 285
75862
Ha = 186
940 n
mi
Hp = 177
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19974566
09 X = 6086076
94
Y = -3280125
31 feet Y = -931712
18 meter
Z = 8711018
74 Z = 2684689
78
XDOT = -4508
373863 XDOT = -1461
014994
YDOT = 18106
001841 feet/sec YDOT = 5502
856648 meter/sec
ZDOT = 17055
641800 ZDOT = 5191
673500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9012323
71 X = 2746956
27
Y = 18068412
19 feet Y = 5507252
03 meter
Z = 8828072
40 Z = 2690796
47
XDOT = -17342
469022 XDOT = -5285
984558
YDOT = 282
079586 feet/sec YDOT = 85
977858 meter/sec
ZDOT = 17028
458372 ZDOT = 5190
274112
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 10008
55794954
00016717 00000-0 10270-3 0 9048
2 25544 51
6435 330
8629 0007312 162
2636 197
8786 15
77249994 38325
Satellite: ISS
Catalog Number: 25544
Epoch time: 10008
55794954 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 330
8629 deg
Eccentricity:
0007312
Arg of perigee: 162
2636 deg
Mean anomaly: 197
8786 deg
Mean motion: 15
77249994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3832
Checksum: 347
Coasting Arc #6 (Orbit 3846)
---------------------------------------
Vector Time (GMT): 2010/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1975075
27 A = 6716497
32 meter
Y = -5120808
81 meter E =
0011867
Z = -3885172
98 I = 51
45183
XDOT = 6514
613927 Wp = 136
63730
YDOT = -565
112391 meter/sec RA = 325
42721 deg
ZDOT = 4055
447688 TA = 175
73728
MA = 175
72716
Ha = 186
872 n
mi
Hp = 177
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6479905
73 X = 2051063
67
Y = -16800553
82 feet Y = -5098297
06 meter
Z = -12746630
50 Z = -3875394
05
XDOT = 21373
405272 XDOT = 6500
748363
YDOT = -1854
043277 feet/sec YDOT = -492
340080 meter/sec
ZDOT = 13305
274568 ZDOT = 4087
061849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18006651
69 X = 5488427
44
Y = 995941
57 feet Y = 303562
99 meter
Z = -12707988
49 Z = -3873394
89
XDOT = 8466
416985 XDOT = 2580
563897
YDOT = 18345
476026 feet/sec YDOT = 5591
701093 meter/sec
ZDOT = 13430
422724 ZDOT = 4093
592846
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 10009
50834173
00016717 00000-0 10270-3 0 9053
2 25544 51
6435 325
9589 0007081 165
3371 194
8000 15
77218075 38476
Satellite: ISS
Catalog Number: 25544
Epoch time: 10009
50834173 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 325
9589 deg
Eccentricity:
0007081
Arg of perigee: 165
3371 deg
Mean anomaly: 194
8000 deg
Mean motion: 15
77218075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3847
Checksum: 313
Coasting Arc #7 (Orbit 3862)
---------------------------------------
Vector Time (GMT): 2010/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5182125
40 A = 6714813
59 meter
Y = -128924
85 meter E =
0010303
Z = -4274144
52 I = 51
42341
XDOT = 3033
695647 Wp = 111
40025
YDOT = -6149
767378 meter/sec RA = 320
30327 deg
ZDOT = -3503
117248 TA = 123
06344
MA = 122
96445
Ha = 186
631 n
mi
Hp = 177
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17001723
74 X = -5159535
68
Y = -422981
79 feet Y = -186747
62 meter
Z = -14022783
85 Z = -4299264
29
XDOT = 9953
069709 XDOT = 3119
255374
YDOT = -20176
402160 feet/sec YDOT = -6115
363987 meter/sec
ZDOT = -11493
166823 ZDOT = -3488
172552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5145265
89 X = -1568277
04
Y = -16123422
13 feet Y = -4914419
07 meter
Z = -14122233
82 Z = -4304456
87
XDOT = 21170
630198 XDOT = 6452
808084
YDOT = 3229
167436 feet/sec YDOT = 984
250235 meter/sec
ZDOT = -11434
087309 ZDOT = -3485
109812
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 10010
52207984
00016717 00000-0 10270-3 0 9062
2 25544 51
6442 320
7278 0007052 169
0839 191
0480 15
77265167 38633
Satellite: ISS
Catalog Number: 25544
Epoch time: 10010
52207984 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 320
7278 deg
Eccentricity:
0007052
Arg of perigee: 169
0839 deg
Mean anomaly: 191
0480 deg
Mean motion: 15
77265167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3863
Checksum: 309
Coasting Arc #8 (Orbit 3878)
---------------------------------------
Vector Time (GMT): 2010/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3175468
23 A = 6720999
46 meter
Y = 5526906
52 meter E =
0018465
Z = 2095799
71 I = 51
42215
XDOT = -5298
940809 Wp = 129
89703
YDOT = -941
260874 meter/sec RA = 315
08392 deg
ZDOT = -5526
149640 TA = 26
55357
MA = 26
45909
Ha = 186
592 n
mi
Hp = 177
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10418202
84 X = -3247215
98
Y = 18132895
41 feet Y = 5490995
12 meter
Z = 6875983
31 Z = 2080199
88
XDOT = -17384
976407 XDOT = -5261
176846
YDOT = -3088
126227 feet/sec YDOT = -1000
304889 meter/sec
ZDOT = -18130
412206 ZDOT = -5551
800060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20623884
60 X = -6286160
03
Y = -3583389
62 feet Y = -1092217
16 meter
Z = 6814300
82 Z = 2076998
89
XDOT = -3304
044684 XDOT = -1007
072820
YDOT = -15782
564845 feet/sec YDOT = -4810
525765 meter/sec
ZDOT = -18231
978520 ZDOT = -5557
107053
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 10011
53580582
00016717 00000-0 10270-3 0 9073
2 25544 51
6447 315
4973 0007038 172
9253 187
2012 15
77272768 38798
Satellite: ISS
Catalog Number: 25544
Epoch time: 10011
53580582 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 315
4973 deg
Eccentricity:
0007038
Arg of perigee: 172
9253 deg
Mean anomaly: 187
2012 deg
Mean motion: 15
77272768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3879
Checksum: 325
Coasting Arc #9 (Orbit 3894)
---------------------------------------
Vector Time (GMT): 2010/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4014344
05 A = 6711077
65 meter
Y = 1596772
72 meter E =
0009952
Z = 5134144
32 I = 51
36915
XDOT = -4107
213169 Wp = 159
12805
YDOT = 6409
764326 meter/sec RA = 309
93617 deg
ZDOT = 1207
997494 TA = 279
24258
MA = 279
35513
Ha = 186
258 n
mi
Hp = 178
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13170420
11 X = 3971249
89
Y = 5238755
65 feet Y = 1641421
85 meter
Z = 16844305
50 Z = 5153541
28
XDOT = -13475
108822 XDOT = -4184
451180
YDOT = 21029
410519 feet/sec YDOT = 6363
403019 meter/sec
ZDOT = 3963
246370 ZDOT = 1187
858164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -181438
46 X = -55302
44
Y = 14081110
14 feet Y = 4291922
37 meter
Z = 16921127
97 Z = 5157559
81
XDOT = -23452
318671 XDOT = -7148
266731
YDOT = -5007
907033 feet/sec YDOT = -1526
410064 meter/sec
ZDOT = 3883
604544 ZDOT = 1183
722665
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 10012
54951709
00016717 00000-0 10270-3 0 9089
2 25544 51
6450 310
2672 0007048 178
4518 181
6670 15
77332410 38954
Satellite: ISS
Catalog Number: 25544
Epoch time: 10012
54951709 = yrday
fracday
Element set: 908
Inclination: 51
6450 deg
RA of node: 310
2672 deg
Eccentricity:
0007048
Arg of perigee: 178
4518 deg
Mean anomaly: 181
6670 deg
Mean motion: 15
77332410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3895
Checksum: 307
Coasting Arc #10 (Orbit 3910)
---------------------------------------
Vector Time (GMT): 2010/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3863765
35 A = 6722761
41 meter
Y = -5499811
40 meter E =
0008947
Z = 50262
07 I = 51
38970
XDOT = 3902
813533 Wp = 78
90752
YDOT = 2805
072903 meter/sec RA = 304
74691 deg
ZDOT = 6017
667570 TA = 281
64078
MA = 281
74119
Ha = 186
291 n
mi
Hp = 178
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12676395
49 X = 3924733
88
Y = -18044000
65 feet Y = -5456263
60 meter
Z = 164901
82 Z = 69179
30
XDOT = 12804
506343 XDOT = 3841
924427
YDOT = 9202
995088 feet/sec YDOT = 2848
375250 meter/sec
ZDOT = 19743
003839 ZDOT = 6036
479569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21486043
15 X = 6548945
95
Y = 4959500
03 feet Y = 1511655
61 meter
Z = 239716
83 Z = 73065
69
XDOT = -3394
877120 XDOT = -1034
758546
YDOT = 13651
310314 feet/sec YDOT = 4160
919384 meter/sec
ZDOT = 19817
535199 ZDOT = 6040
384729
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 10013
56321901
00016717 00000-0 10270-3 0 9098
2 25544 51
6448 305
0359 0006958 181
4870 178
6275 15
77312933 39113
Satellite: ISS
Catalog Number: 25544
Epoch time: 10013
56321901 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 305
0359 deg
Eccentricity:
0006958
Arg of perigee: 181
4870 deg
Mean anomaly: 178
6275 deg
Mean motion: 15
77312933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3911
Checksum: 315
Coasting Arc #11 (Orbit 3925)
---------------------------------------
Vector Time (GMT): 2010/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2816740
29 A = 6711246
85 meter
Y = -3329188
18 meter E =
0016271
Z = -5114580
64 I = 51
33545
XDOT = 4634
443384 Wp = 125
30814
YDOT = -5994
338394 meter/sec RA = 299
55403 deg
ZDOT = 1343
258211 TA = 157
64565
MA = 157
57465
Ha = 186
122 n
mi
Hp = 178
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9241273
92 X = -2754458
20
Y = -10922533
41 feet Y = -3360337
80 meter
Z = -16780120
22 Z = -5128113
19
XDOT = 15204
866747 XDOT = 4694
603526
YDOT = -19666
464547 feet/sec YDOT = -5942
177092 meter/sec
ZDOT = 4407
015127 ZDOT = 1365
917286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6465798
41 X = 1970775
36
Y = -12692248
62 feet Y = -3868597
38 meter
Z = -16833763
40 Z = -5130931
08
XDOT = 23116
410938 XDOT = 7045
882054
YDOT = 5785
084966 feet/sec YDOT = 1763
293898 meter/sec
ZDOT = 4496
634568 ZDOT = 1370
574216
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 10014
51355164
00016717 00000-0 10270-3 0 9104
2 25544 51
6455 300
1318 0006917 185
1884 174
9210 15
77331533 39264
Satellite: ISS
Catalog Number: 25544
Epoch time: 10014
51355164 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 300
1318 deg
Eccentricity:
0006917
Arg of perigee: 185
1884 deg
Mean anomaly: 174
9210 deg
Mean motion: 15
77331533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3926
Checksum: 292
Coasting Arc #12 (Orbit 3941)
---------------------------------------
Vector Time (GMT): 2010/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4140555
60 A = 6720411
88 meter
Y = 4786839
96 meter E =
0011524
Z = -2242066
85 I = 51
35330
XDOT = -2604
846931 Wp = 164
69654
YDOT = -4794
990945 meter/sec RA = 294
40433 deg
ZDOT = -5444
143623 TA = 40
61492
MA = 40
52902
Ha = 185
911 n
mi
Hp = 178
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13584499
99 X = -4182883
85
Y = 15704855
50 feet Y = 4740301
37 meter
Z = -7355862
37 Z = -2262283
52
XDOT = -8546
085733 XDOT = -2524
588866
YDOT = -15731
597589 feet/sec YDOT = -4823
670588 meter/sec
ZDOT = -17861
363591 ZDOT = -5456
603211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19860866
66 X = -6053592
16
Y = -5961902
53 feet Y = -1817187
89 meter
Z = -7435827
54 Z = -2266440
23
XDOT = 10489
042893 XDOT = 3197
060274
YDOT = -12673
383096 feet/sec YDOT = -3862
847168 meter/sec
ZDOT = -17910
793872 ZDOT = -5459
209972
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 10015
52722790
00016717 00000-0 10270-3 0 9110
2 25544 51
6460 294
9012 0006924 189
2126 170
8913 15
77350568 39425
Satellite: ISS
Catalog Number: 25544
Epoch time: 10015
52722790 = yrday
fracday
Element set: 911
Inclination: 51
6460 deg
RA of node: 294
9012 deg
Eccentricity:
0006924
Arg of perigee: 189
2126 deg
Mean anomaly: 170
8913 deg
Mean motion: 15
77350568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3942
Checksum: 309
Coasting Arc #13 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2010/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1793234
81 A = 6715035
36 meter
Y = 4957010
20 meter E =
0009294
Z = 4149974
41 I = 51
32312
XDOT = -4783
517842 Wp = 115
02820
YDOT = 4806
574766 meter/sec RA = 289
17653 deg
ZDOT = -3671
786032 TA = 12
56619
MA = 12
54304
Ha = 185
767 n
mi
Hp = 178
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5883316
30 X = 1717512
05
Y = 16263156
84 feet Y = 4976639
49 meter
Z = 13615401
62 Z = 4158502
21
XDOT = -15693
956174 XDOT = -4819
073861
YDOT = 15769
602250 feet/sec YDOT = 4752
884137 meter/sec
ZDOT = -12046
542101 ZDOT = -3695
109753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12277441
04 X = -3742164
03
Y = 12142674
87 feet Y = 3701087
30 meter
Z = 13649275
84 Z = 4160299
28
XDOT = -20014
931586 XDOT = -6100
551148
YDOT = -6582
877412 feet/sec YDOT = -2006
461035 meter/sec
ZDOT = -12138
805506 ZDOT = -3699
907918
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 10016
54089207
00016717 00000-0 10270-3 0 9123
2 25544 51
6452 289
6707 0006871 192
8054 167
2938 15
77367752 39586
Satellite: ISS
Catalog Number: 25544
Epoch time: 10016
54089207 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 289
6707 deg
Eccentricity:
0006871
Arg of perigee: 192
8054 deg
Mean anomaly: 167
2938 deg
Mean motion: 15
77367752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 343
Coasting Arc #14 (Orbit 3973)
---------------------------------------
Vector Time (GMT): 2010/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4164668
71 A = 6715448
09 meter
Y = -3413948
20 meter E =
0012337
Z = 4011277
33 I = 51
31619
XDOT = 1570
665919 Wp = 136
19296
YDOT = 6477
096556 meter/sec RA = 284
04340 deg
ZDOT = 3865
971153 TA = 273
73745
MA = 273
87851
Ha = 185
634 n
mi
Hp = 178
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13663611
24 X = 4183048
97
Y = -11200617
45 feet Y = -3367273
89 meter
Z = 13160358
68 Z = 4031553
22
XDOT = 5153
103410 XDOT = 1479
341420
YDOT = 21250
316785 feet/sec YDOT = 6494
149808 meter/sec
ZDOT = 12683
632391 ZDOT = 3873
379845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16026532
48 X = 4884887
10
Y = 7292496
24 feet Y = 2222752
85 meter
Z = 13240577
75 Z = 4035728
10
XDOT = -16334
245235 XDOT = -4978
677948
YDOT = 12720
849751 feet/sec YDOT = 3877
315004 meter/sec
ZDOT = 12713
119499 ZDOT = 3874
958823
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 10017
55454333
00016717 00000-0 10270-3 0 9132
2 25544 51
6454 284
4392 0006832 196
9870 163
1067 15
77386623 39743
Satellite: ISS
Catalog Number: 25544
Epoch time: 10017
55454333 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 284
4392 deg
Eccentricity:
0006832
Arg of perigee: 196
9870 deg
Mean anomaly: 163
1067 deg
Mean motion: 15
77386623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3974
Checksum: 329
Coasting Arc #15 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2010/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -999375
67 A = 6719874
29 meter
Y = -6191548
82 meter E =
0003078
Z = -2418769
63 I = 51
32559
XDOT = 4763
002337 Wp = 149
38172
YDOT = -2852
602656 meter/sec RA = 278
81149 deg
ZDOT = 5334
481603 TA = 183
17283
MA = 183
17478
Ha = 185
472 n
mi
Hp = 178
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3278791
56 X = -918316
72
Y = -20313480
37 feet Y = -6202271
10 meter
Z = -7935595
88 Z = -2423427
87
XDOT = 15626
648087 XDOT = 4768
633287
YDOT = -9358
932600 feet/sec YDOT = -2799
308698 meter/sec
ZDOT = 17501
580061 ZDOT = 5357
633296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16628648
15 X = 5068411
96
Y = -12107042
22 feet Y = -3690226
47 meter
Z = -7954195
77 Z = -2424438
87
XDOT = 14506
076268 XDOT = 4421
452047
YDOT = 8365
890987 feet/sec YDOT = 2549
923573 meter/sec
ZDOT = 17593
197604 ZDOT = 5362
406630
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 10018
50482981
00016717 00000-0 10270-3 0 9149
2 25544 51
6457 279
5347 0006842 201
2097 158
8786 15
77425984 39892
Satellite: ISS
Catalog Number: 25544
Epoch time: 10018
50482981 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 279
5347 deg
Eccentricity:
0006842
Arg of perigee: 201
2097 deg
Mean anomaly: 158
8786 deg
Mean motion: 15
77425984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 355
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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