Date:
January 27th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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
024/09:03:00
613 -4
8 9
2 9
2
N/A -7
6 0
0 187
9
000/00:02:31
227 -2
1 0
0 183
7
Coasting Arc #1 (Orbit 50)
---------------------------------------
Vector Time (GMT): 2010/022/09:31:16
822
Vector Time (MET): N/A
Weight (LBS) : 751555
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2548552
45 A = 6722348
18 meter
Y = 5989215
76 meter E =
0015106
Z = 1644218
55 I = 51
33025
XDOT = -4004
958386 Wp = 133
87201
YDOT = 3279
216970 meter/sec RA = 258
61243 deg
ZDOT = -5714
942560 TA = 27
84621
MA = 27
76543
Ha = 185
462 n
mi
Hp = 179
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8361392
57 X = 2473403
33
Y = 19649658
00 feet Y = 6017294
95 meter
Z = 5394417
80 Z = 1656416
94
XDOT = -13139
627251 XDOT = -4013
567619
YDOT = 10758
585858 feet/sec YDOT = 3234
383184 meter/sec
ZDOT = -18749
811548 ZDOT = -5734
419278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20447542
92 X = -6232411
08
Y = 6115099
34 feet Y = 1863882
28 meter
Z = 5442907
05 Z = 1658998
07
XDOT = -8811
979653 XDOT = -2685
891398
YDOT = -12643
763940 feet/sec YDOT = -3853
819249 meter/sec
ZDOT = -18826
855755 ZDOT = -5738
425634
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 10022
43166736
00016717 00000-0 10270-3 0 9008
2 25544 51
6440 259
2688 0004589 202
9860 157
1100 15
77037911 517
Satellite: ISS
Catalog Number: 25544
Epoch time: 10022
43166736 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 259
2688 deg
Eccentricity:
0004589
Arg of perigee: 202
9860 deg
Mean anomaly: 157
1100 deg
Mean motion: 15
77037911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 51
Checksum: 289
Coasting Arc #2 (Orbit 66)
---------------------------------------
Vector Time (GMT): 2010/023/09:31:16
822
Vector Time (MET): N/A
Weight (LBS) : 751555
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3755541
55 A = 6711437
47 meter
Y = -1980576
41 meter E =
0005579
Z = 5197889
22 I = 51
30137
XDOT = 2746
115251 Wp = 174
57312
YDOT = 7162
495067 meter/sec RA = 253
45248 deg
ZDOT = 739
507103 TA = 268
33226
MA = 268
39616
Ha = 185
153 n
mi
Hp = 179
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12321330
55 X = 3752159
37
Y = -6497954
09 feet Y = -1938598
85 meter
Z = 17053442
33 Z = 5216125
21
XDOT = 9009
564473 XDOT = 2662
226504
YDOT = 23498
999563 feet/sec YDOT = 7192
734675 meter/sec
ZDOT = 2426
204406 ZDOT = 752
644168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5332723
79 X = 1625414
21
Y = 12772389
28 feet Y = 3893024
25 meter
Z = 17125612
92 Z = 5219886
82
XDOT = -23302
440154 XDOT = -7102
583759
YDOT = 6381
734536 feet/sec YDOT = 1945
152686 meter/sec
ZDOT = 2478
452482 ZDOT = 755
432317
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 10023
44552147
00016717 00000-0 10270-3 0 9016
2 25544 51
6441 254
0387 0004605 208
8045 151
2866 15
77108235 675
Satellite: ISS
Catalog Number: 25544
Epoch time: 10023
44552147 = yrday
fracday
Element set: 901
Inclination: 51
6441 deg
RA of node: 254
0387 deg
Eccentricity:
0004605
Arg of perigee: 208
8045 deg
Mean anomaly: 151
2866 deg
Mean motion: 15
77108235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 67
Checksum: 285
Coasting Arc #3 (Orbit 81)
---------------------------------------
Vector Time (GMT): 2010/024/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3296393
36 A = 6716634
37 meter
Y = 2826575
40 meter E =
0005857
Z = -5127598
10 I = 51
31261
XDOT = -3717
200050 Wp = 126
63151
YDOT = -6624
084605 meter/sec RA = 248
37213 deg
ZDOT = -1266
269693 TA = 131
23249
MA = 131
18200
Ha = 187
916 n
mi
Hp = 183
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10814938
84 X = -3302846
86
Y = 9273541
34 feet Y = 2789677
40 meter
Z = -16822828
40 Z = -5143627
37
XDOT = -12195
538221 XDOT = -3636
700830
YDOT = -21732
561039 feet/sec YDOT = -6665
202366 meter/sec
ZDOT = -4154
428127 ZDOT = -1284
132584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7031856
22 X = -2143309
77
Y = -12303538
00 feet Y = -3750118
38 meter
Z = -16886236
33 Z = -5146924
83
XDOT = 22775
067291 XDOT = 6941
840510
YDOT = -7237
394812 feet/sec YDOT = -2205
957939 meter/sec
ZDOT = -4225
385890 ZDOT = -1287
897619
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 10024
39600206
00016717 00000-0 10270-3 0 9022
2 25544 51
6445 249
1354 0011012 237
6070 122
4029 15
75405810 821
Satellite: ISS
Catalog Number: 25544
Epoch time: 10024
39600206 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 249
1354 deg
Eccentricity:
0011012
Arg of perigee: 237
6070 deg
Mean anomaly: 122
4029 deg
Mean motion: 15
75405810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 82
Checksum: 257
Coasting Arc #4 (Orbit 97)
---------------------------------------
Vector Time (GMT): 2010/025/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3459386
19 A = 6728062
60 meter
Y = 5725140
32 meter E =
0013638
Z = 631774
39 I = 51
36307
XDOT = -3845
672391 Wp = 176
97897
YDOT = 2982
433515 meter/sec RA = 243
18749 deg
ZDOT = -5976
774146 TA = 356
10712
MA = 356
11772
Ha = 187
786 n
mi
Hp = 183
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11349692
22 X = 3392040
53
Y = 18783268
75 feet Y = 5763448
62 meter
Z = 2072750
61 Z = 648416
81
XDOT = -12617
035404 XDOT = -3849
702845
YDOT = 9784
886861 feet/sec YDOT = 2939
406870 meter/sec
ZDOT = -19608
839062 ZDOT = -5995
465808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20485421
02 X = -6243956
33
Y = 7854668
55 feet Y = 2394102
97 meter
Z = 2138855
13 Z = 651923
04
XDOT = -6858
704757 XDOT = -2090
533210
YDOT = -12534
755811 feet/sec YDOT = -3820
593571 meter/sec
ZDOT = -19682
793771 ZDOT = -5999
315541
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 10025
41093257
00016717 00000-0 10270-3 0 9039
2 25544 51
6443 243
9131 0011109 241
2304 118
7744 15
75383176 981
Satellite: ISS
Catalog Number: 25544
Epoch time: 10025
41093257 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 243
9131 deg
Eccentricity:
0011109
Arg of perigee: 241
2304 deg
Mean anomaly: 118
7744 deg
Mean motion: 15
75383176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 98
Checksum: 284
Coasting Arc #5 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2010/026/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3463656
83 A = 6715947
35 meter
Y = -2378029
53 meter E =
0009209
Z = 5246287
91 I = 51
33759
XDOT = 4183
906105 Wp = 237
86654
YDOT = 6459
591563 meter/sec RA = 238
02836 deg
ZDOT = 161
110690 TA = 210
57069
MA = 210
62439
Ha = 187
345 n
mi
Hp = 183
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11363703
50 X = 3464505
76
Y = -7801934
16 feet Y = -2339292
63 meter
Z = 17212230
69 Z = 5263115
97
XDOT = 13726
726065 XDOT = 4110
580217
YDOT = 21192
885705 feet/sec YDOT = 6505
968474 meter/sec
ZDOT = 528
578379 ZDOT = 181
258363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5911110
02 X = 1801706
33
Y = 12359842
61 feet Y = 3767280
03 meter
Z = 17278827
74 Z = 5266586
69
XDOT = -22204
359015 XDOT = -6767
888628
YDOT = 9747
324750 feet/sec YDOT = 2970
984584 meter/sec
ZDOT = 608
604276 ZDOT = 185
502583
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 10026
42584443
00016717 00000-0 10270-3 0 9044
2 25544 51
6443 238
6903 0011142 246
1126 113
8871 15
75461530 1149
Satellite: ISS
Catalog Number: 25544
Epoch time: 10026
42584443 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 238
6903 deg
Eccentricity:
0011142
Arg of perigee: 246
1126 deg
Mean anomaly: 113
8871 deg
Mean motion: 15
75461530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 114
Checksum: 277
Coasting Arc #6 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2010/027/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3817811
91 A = 6727954
57 meter
Y = -5523933
55 meter E =
0004851
Z = 364817
01 I = 51
39502
XDOT = 4143
463915 Wp = 350
79818
YDOT = -2468
268367 meter/sec RA = 232
86391 deg
ZDOT = 6003
398598 TA = 13
18252
MA = 13
16984
Ha = 187
072 n
mi
Hp = 184
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12525629
62 X = -3757530
74
Y = -18123141
56 feet Y = -5566289
57 meter
Z = 1196906
20 Z = 346416
27
XDOT = 13594
041717 XDOT = 4141
593703
YDOT = -8097
993330 feet/sec YDOT = -2421
944785 meter/sec
ZDOT = 19696
189626 ZDOT = 6023
522369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19719337
81 X = 6010454
17
Y = -9831428
94 feet Y = -2996619
54 meter
Z = 1123816
25 Z = 342539
19
XDOT = 5384
227939 XDOT = 1641
112676
YDOT = 13053
666144 feet/sec YDOT = 3978
757441 meter/sec
ZDOT = 19775
849424 ZDOT = 6027
678904
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 10027
44074212
00016717 00000-0 10270-3 0 9056
2 25544 51
6441 233
4670 0011113 250
5739 109
4224 15
75466942 1301
Satellite: ISS
Catalog Number: 25544
Epoch time: 10027
44074212 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 233
4670 deg
Eccentricity:
0011113
Arg of perigee: 250
5739 deg
Mean anomaly: 109
4224 deg
Mean motion: 15
75466942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 271
Coasting Arc #7 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2010/028/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3810502
30 A = 6716120
04 meter
Y = 1958007
03 meter E =
0006124
Z = -5176166
41 I = 51
37436
XDOT = -4522
423248 Wp = 142
95192
YDOT = -6152
158916 meter/sec RA = 227
68689 deg
ZDOT = 997
834905 TA = 136
61973
MA = 136
57151
Ha = 186
602 n
mi
Hp = 184
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12501647
96 X = -3806969
63
Y = 6423907
56 feet Y = 1915415
99 meter
Z = -16982173
26 Z = -5194668
59
XDOT = -14837
346615 XDOT = -4458
139783
YDOT = -20184
248412 feet/sec YDOT = -6202
371998 meter/sec
ZDOT = 3273
736566 ZDOT = 976
021075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4823163
37 X = -1470100
20
Y = -13107301
14 feet Y = -3995105
39 meter
Z = -17055431
70 Z = -5198495
58
XDOT = 20926
837095 XDOT = 6378
499947
YDOT = -11865
523648 feet/sec YDOT = -3616
611608 meter/sec
ZDOT = 3187
082102 ZDOT = 971
422625
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 10028
39219308
00016717 00000-0 10270-3 0 9069
2 25544 51
6437 228
5704 0011143 254
6000 105
3933 15
75505241 1452
Satellite: ISS
Catalog Number: 25544
Epoch time: 10028
39219308 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 228
5704 deg
Eccentricity:
0011143
Arg of perigee: 254
6000 deg
Mean anomaly: 105
3933 deg
Mean motion: 15
75505241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 275
Coasting Arc #8 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2010/029/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4037928
12 A = 6727189
90 meter
Y = 5192987
55 meter E =
0010972
Z = -1374007
65 I = 51
43229
XDOT = -4621
304975 Wp = 211
60044
YDOT = 2051
805605 meter/sec RA = 222
54504 deg
ZDOT = -5814
693175 TA = 343
55884
MA = 343
59440
Ha = 186
420 n
mi
Hp = 184
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13247795
69 X = 3986233
59
Y = 17037360
72 feet Y = 5237853
11 meter
Z = -4507899
12 Z = -1354517
19
XDOT = -15161
761729 XDOT = -4615
659308
YDOT = 6731
645685 feet/sec YDOT = 2000
159425 meter/sec
ZDOT = -19077
077347 ZDOT = -5837
128923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18369981
12 X = -5599170
25
Y = 11358330
67 feet Y = 3462019
19 meter
Z = -4430465
36 Z = -1350405
84
XDOT = -4239
867086 XDOT = -1292
311488
YDOT = -14348
338298 feet/sec YDOT = -4373
373513 meter/sec
ZDOT = -19165
929560 ZDOT = -5841
775330
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 10029
40705905
00016717 00000-0 10270-3 0 9076
2 25544 51
6435 223
3476 0011274 258
0099 101
9802 15
75474994 1615
Satellite: ISS
Catalog Number: 25544
Epoch time: 10029
40705905 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 223
3476 deg
Eccentricity:
0011274
Arg of perigee: 258
0099 deg
Mean anomaly: 101
9802 deg
Mean motion: 15
75474994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 161
Checksum: 305
Coasting Arc #9 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2010/030/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4282405
58 A = 6717106
02 meter
Y = -1656816
18 meter E =
0006339
Z = 4908429
05 I = 51
42239
XDOT = 4676
992390 Wp = 289
37985
YDOT = 5725
123944 meter/sec RA = 217
35169 deg
ZDOT = -2148
177627 TA = 181
53139
MA = 181
53333
Ha = 185
730 n
mi
Hp = 183
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14049887
07 X = 4276770
65
Y = -5435748
61 feet Y = -1608959
48 meter
Z = 16103769
85 Z = 4929218
54
XDOT = 15344
463222 XDOT = 4623
060551
YDOT = 18783
215041 feet/sec YDOT = 5777
123376 meter/sec
ZDOT = -7047
826861 ZDOT = -2125
588330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4146111
01 X = 1263734
64
Y = 14390881
14 feet Y = 4386340
57 meter
Z = 16186117
40 Z = 4933528
58
XDOT = -19052
750843 XDOT = -5807
278457
YDOT = 13314
649276 feet/sec YDOT = 4058
305099 meter/sec
ZDOT = -6958
071146 ZDOT = -2120
820085
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 10030
42190584
00016717 00000-0 10270-3 0 9082
2 25544 51
6434 218
1236 0011273 263
2440 96
7442 15
75573218 1774
Satellite: ISS
Catalog Number: 25544
Epoch time: 10030
42190584 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 218
1236 deg
Eccentricity:
0011273
Arg of perigee: 263
2440 deg
Mean anomaly: 96
7442 deg
Mean motion: 15
75573218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 177
Checksum: 290
Coasting Arc #10 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2010/031/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4071127
36 A = 6725318
96 meter
Y = -4796428
05 meter E =
0004057
Z = 2369292
80 I = 51
47397
XDOT = 5219
196102 Wp = 31
49984
YDOT = -1772
481044 meter/sec RA = 212
22787 deg
ZDOT = 5379
117787 TA = 355
27589
MA = 355
27972
Ha = 185
530 n
mi
Hp = 183
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13356717
06 X = -4028699
51
Y = -15736312
50 feet Y = -4841716
59 meter
Z = 7773270
34 Z = 2349618
92
XDOT = 17123
346790 XDOT = 5212
498448
YDOT = -5815
226521 feet/sec YDOT = -1714
154374 meter/sec
ZDOT = 17648
024236 ZDOT = 5404
455558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16680251
02 X = 5084140
51
Y = -12207045
74 feet Y = -3720707
54 meter
Z = 7695090
22 Z = 2345463
50
XDOT = 3655
666140 XDOT = 1114
247040
YDOT = 16185
046500 feet/sec YDOT = 4933
202173 meter/sec
ZDOT = 17748
402824 ZDOT = 5409
713181
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 10031
43673841
00016717 00000-0 10270-3 0 9097
2 25544 51
6428 212
8990 0011298 267
4974 92
4896 15
75569351 1937
Satellite: ISS
Catalog Number: 25544
Epoch time: 10031
43673841 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 212
8990 deg
Eccentricity:
0011298
Arg of perigee: 267
4974 deg
Mean anomaly: 92
4896 deg
Mean motion: 15
75569351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 338
Coasting Arc #11 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2010/032/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4834171
91 A = 6718986
50 meter
Y = 1486773
91 meter E =
0003916
Z = -4423003
50 I = 51
47896
XDOT = -4597
627463 Wp = 216
10166
YDOT = -5253
257583 meter/sec RA = 207
02328 deg
ZDOT = 3254
595394 TA = 86
60933
MA = 86
56454
Ha = 185
304 n
mi
Hp = 183
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15860144
07 X = -4828952
44
Y = 4877867
14 feet Y = 1432744
43 meter
Z = -14511166
35 Z = -4446474
61
XDOT = -15084
079602 XDOT = -4554
352704
YDOT = -17235
097057 feet/sec YDOT = -5304
428956 meter/sec
ZDOT = 10677
806411 ZDOT = 3232
365944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3978976
61 X = -1212792
07
Y = -16024916
23 feet Y = -4884394
47 meter
Z = -14604160
77 Z = -4451348
20
XDOT = 16894
077574 XDOT = 5149
314845
YDOT = -13858
987157 feet/sec YDOT = -4224
219286 meter/sec
ZDOT = 10589
463797 ZDOT = 3227
668565
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 10032
38812798
00016717 00000-0 10270-3 0 9100
2 25544 51
6424 208
0010 0011314 271
1235 88
8633 15
75600552 2088
Satellite: ISS
Catalog Number: 25544
Epoch time: 10032
38812798 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 208
0010 deg
Eccentricity:
0011314
Arg of perigee: 271
1235 deg
Mean anomaly: 88
8633 deg
Mean motion: 15
75600552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 272
Coasting Arc #12 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2010/033/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3893660
16 A = 6722965
28 meter
Y = 4382234
90 meter E =
0006700
Z = -3286368
49 I = 51
51918
XDOT = -5863
519006 Wp = 275
13126
YDOT = 1673
633105 meter/sec RA = 201
91539 deg
ZDOT = -4706
531445 TA = 303
52730
MA = 303
59128
Ha = 185
649 n
mi
Hp = 183
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12774475
59 X = 3860332
08
Y = 14377411
10 feet Y = 4425589
69 meter
Z = -10782048
86 Z = -3267534
58
XDOT = -19237
267081 XDOT = -5858
935105
YDOT = 5490
922260 feet/sec YDOT = 1608
089267 meter/sec
ZDOT = -15441
376132 ZDOT = -4735
004698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14870386
59 X = -4532493
83
Y = 12262843
53 feet Y = 3737714
71 meter
Z = -10707195
03 Z = -3263553
04
XDOT = -3839
922898 XDOT = -1170
408499
YDOT = -18262
817642 feet/sec YDOT = -5566
506817 meter/sec
ZDOT = -15554
200390 ZDOT = -4740
920279
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 10033
40292734
00016717 00000-0 10270-3 0 9117
2 25544 51
6420 202
7779 0011369 275
1978 84
7888 15
75607201 2248
Satellite: ISS
Catalog Number: 25544
Epoch time: 10033
40292734 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 202
7779 deg
Eccentricity:
0011369
Arg of perigee: 275
1978 deg
Mean anomaly: 84
7888 deg
Mean motion: 15
75607201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 309
Coasting Arc #13 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2010/034/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5390873
67 A = 6721224
87 meter
Y = -1478598
65 meter E =
0003356
Z = 3734573
09 I = 51
54344
XDOT = 4262
598957 Wp = 3
66885
YDOT = 4802
168519 meter/sec RA = 196
70767 deg
ZDOT = -4248
295444 TA = 131
14511
MA = 131
11614
Ha = 185
908 n
mi
Hp = 183
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17686593
42 X = 5388865
40
Y = -4851045
45 feet Y = -1418325
86 meter
Z = 12252536
38 Z = 3760756
65
XDOT = 13984
904716 XDOT = 4229
220546
YDOT = 15755
146059 feet/sec YDOT = 4849
648714 meter/sec
ZDOT = -13937
977178 ZDOT = -4227
669269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4460438
23 X = 1359541
57
Y = 17717203
41 feet Y = 5400203
60 meter
Z = 12356296
80 Z = 3766199
26
XDOT = -14769
762875 XDOT = -4501
823724
YDOT = 13389
765708 feet/sec YDOT = 4081
200588 meter/sec
ZDOT = -13855
993337 ZDOT = -4223
306769
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 10034
41770811
00016717 00000-0 10270-3 0 9127
2 25544 51
6426 197
5534 0011487 279
6530 80
3336 15
75679436 2405
Satellite: ISS
Catalog Number: 25544
Epoch time: 10034
41770811 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 197
5534 deg
Eccentricity:
0011487
Arg of perigee: 279
6530 deg
Mean anomaly: 80
3336 deg
Mean motion: 15
75679436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 306
Coasting Arc #14 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2010/035/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3486475
79 A = 6720242
86 meter
Y = -4031805
87 meter E =
0000784
Z = 4093294
71 I = 51
56757
XDOT = 6470
742314 Wp = 282
94731
YDOT = -1744
557353 meter/sec RA = 191
60440 deg
ZDOT = 3793
903412 TA = 128
08744
MA = 128
08037
Ha = 186
345 n
mi
Hp = 183
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11438568
85 X = -3461016
50
Y = -13227709
54 feet Y = -4070651
34 meter
Z = 13429444
60 Z = 4076419
52
XDOT = 21229
469533 XDOT = 6471
339512
YDOT = -5723
613363 feet/sec YDOT = -1672
194321 meter/sec
ZDOT = 12447
189671 ZDOT = 3825
339282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13283563
57 X = 4048830
18
Y = -11452396
26 feet Y = -3490690
38 meter
Z = 13362361
25 Z = 4072847
71
XDOT = 4784
643744 XDOT = 1458
359413
YDOT = 20215
099530 feet/sec YDOT = 6161
562337 meter/sec
ZDOT = 12571
775150 ZDOT = 3831
877066
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 10035
43247463
00016717 00000-0 10270-3 0 9133
2 25544 51
6413 192
3285 0011416 283
6193 76
3700 15
75655295 2563
Satellite: ISS
Catalog Number: 25544
Epoch time: 10035
43247463 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 192
3285 deg
Eccentricity:
0011416
Arg of perigee: 283
6193 deg
Mean anomaly: 76
3700 deg
Mean motion: 15
75655295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 300
Coasting Arc #15 (Orbit 270)
---------------------------------------
Vector Time (GMT): 2010/036/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5870186
52 A = 6723737
23 meter
Y = 1608866
10 meter E =
0008493
Z = -2844019
27 I = 51
60899
XDOT = -3688
613266 Wp = 308
46698
YDOT = -4465
901506 meter/sec RA = 186
40235 deg
ZDOT = 5082
110672 TA = 18
84286
MA = 18
81144
Ha = 186
409 n
mi
Hp = 183
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19259142
13 X = -5873925
32
Y = 5278432
07 feet Y = 1543201
32 meter
Z = -9330771
88 Z = -2872545
31
XDOT = -12101
749562 XDOT = -3663
088261
YDOT = -14651
907828 feet/sec YDOT = -4507
007115 meter/sec
ZDOT = 16673
591445 ZDOT = 5064
253571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5514218
47 X = -1680733
79
Y = -19137582
68 feet Y = -5833135
20 meter
Z = -9443835
46 Z = -2878481
05
XDOT = 13104
678500 XDOT = 3994
306007
YDOT = -11976
796910 feet/sec YDOT = -3650
527698 meter/sec
ZDOT = 16602
591703 ZDOT = 5060
469951
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 10036
38380020
00016717 00000-0 10270-3 0 9146
2 25544 51
6405 187
4301 0011321 286
7013 73
2908 15
75696793 2719
Satellite: ISS
Catalog Number: 25544
Epoch time: 10036
38380020 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 187
4301 deg
Eccentricity:
0011321
Arg of perigee: 286
7013 deg
Mean anomaly: 73
2908 deg
Mean motion: 15
75696793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 271
Checksum: 289
Coasting Arc #16 (Orbit 285)
---------------------------------------
Vector Time (GMT): 2010/037/09:04:16
227
Vector Time (MET): N/A
Weight (LBS) : 750815
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2899747
46 A = 6717622
35 meter
Y = 3804838
35 meter E =
0007670
Z = -4719466
25 I = 51
61784
XDOT = -6947
392695 Wp = 1
41981
YDOT = 1964
159468 meter/sec RA = 181
29734 deg
ZDOT = -2677
686708 TA = 242
20693
MA = 242
28470
Ha = 186
819 n
mi
Hp = 183
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9513607
14 X = 2879911
54
Y = 12483065
46 feet Y = 3837154
28 meter
Z = -15483813
16 Z = -4705427
55
XDOT = -22793
283119 XDOT = -6955
832400
YDOT = 6444
092744 feet/sec YDOT = 1886
422498 meter/sec
ZDOT = -8785
061377 ZDOT = -2711
457093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12193840
13 X = -3716682
47
Y = 9968542
31 feet Y = 3038411
69 meter
Z = -15427979
17 Z = -4702448
05
XDOT = -6385
222508 XDOT = -1946
215820
YDOT = -21652
054327 feet/sec YDOT = -6599
546159 meter/sec
ZDOT = -8918
924195 ZDOT = -2718
488095
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 10037
39853108
00016717 00000-0 10270-3 0 9151
2 25544 51
6398 182
2063 0011202 291
1387 68
8580 15
75730444 2864
Satellite: ISS
Catalog Number: 25544
Epoch time: 10037
39853108 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 182
2063 deg
Eccentricity:
0011202
Arg of perigee: 291
1387 deg
Mean anomaly: 68
8580 deg
Mean motion: 15
75730444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 286
Checksum: 309
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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