Date:
January 12th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
022/09:06:27
407 1
5 3
3 3
3
N/A 2
7 0
0 185
5
000/00:00:54
813 1
2 -0
0 179
7
024/09:15:15
470 -0
4 8
2 8
2
N/A -7
6 0
0 185
6
000/00:02:16
939 3
1 0
0 184
8
Coasting Arc #1 (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 = -3213848
15 A = 6720961
83 meter
Y = 5519504
49 meter E =
0018659
Z = 2055881
36 I = 51
42196
XDOT = -5268
652837 Wp = 130
52472
YDOT = -994
254209 meter/sec RA = 315
08866 deg
ZDOT = -5546
034457 TA = 26
39998
MA = 26
30502
Ha = 186
587 n
mi
Hp = 177
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10544121
23 X = -3285316
37
Y = 18108610
53 feet Y = 5483165
47 meter
Z = 6745017
57 Z = 2040095
75
XDOT = -17285
606419 XDOT = -5230
201948
YDOT = -3261
988874 feet/sec YDOT = -1052
955683 meter/sec
ZDOT = -18195
651106 ZDOT = -5571
536077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20644122
95 X = -6292328
68
Y = -3709256
16 feet Y = -1130581
28 meter
Z = 6682599
49 Z = 2036856
32
XDOT = -3115
657204 XDOT = -949
652316
YDOT = -15747
224836 feet/sec YDOT = -4799
754130 meter/sec
ZDOT = -18296
629068 ZDOT = -5576
812540
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
53572171
00016717 00000-0 10270-3 0 9001
2 25544 51
6444 315
5024 0007191 172
6509 187
4762 15
77311535 38794
Satellite: ISS
Catalog Number: 25544
Epoch time: 10011
53572171 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 315
5024 deg
Eccentricity:
0007191
Arg of perigee: 172
6509 deg
Mean anomaly: 187
4762 deg
Mean motion: 15
77311535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3879
Checksum: 299
Coasting Arc #2 (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 = 3974901
06 A = 6710898
94 meter
Y = 1657885
63 meter E =
0009972
Z = 5145176
69 I = 51
36853
XDOT = -4157
771404 Wp = 159
50494
YDOT = 6389
135692 meter/sec RA = 309
93972 deg
ZDOT = 1143
480816 TA = 279
49168
MA = 279
60437
Ha = 186
243 n
mi
Hp = 177
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13041013
99 X = 3931072
87
Y = 5439257
31 feet Y = 1702089
58 meter
Z = 16880500
95 Z = 5164380
27
XDOT = -13640
982298 XDOT = -4234
461579
YDOT = 20961
731272 feet/sec YDOT = 6342
212084 meter/sec
ZDOT = 3751
577481 ZDOT = 1123
097206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -415162
29 X = -126541
47
Y = 14032378
16 feet Y = 4277068
86 meter
Z = 16956558
66 Z = 5168359
08
XDOT = -23452
001915 XDOT = -7148
170184
YDOT = -5168
821473 feet/sec YDOT = -1575
456785 meter/sec
ZDOT = 3670
968158 ZDOT = 1118
911094
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
54940546
00016717 00000-0 10270-3 0 9019
2 25544 51
6447 310
2720 0007199 178
1537 181
9655 15
77377835 38955
Satellite: ISS
Catalog Number: 25544
Epoch time: 10012
54940546 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 310
2720 deg
Eccentricity:
0007199
Arg of perigee: 178
1537 deg
Mean anomaly: 181
9655 deg
Mean motion: 15
77377835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3895
Checksum: 328
Coasting Arc #3 (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 = 3911413
16 A = 6722605
86 meter
Y = -5464704
90 meter E =
0009147
Z = 123698
63 I = 51
38922
XDOT = 3840
227562 Wp = 80
25869
YDOT = 2893
362009 meter/sec RA = 304
75129 deg
ZDOT = 6016
199205 TA = 281
09087
MA = 281
19372
Ha = 186
266 n
mi
Hp = 178
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12832720
34 X = 3971628
86
Y = -17928821
86 feet Y = -5420628
50 meter
Z = 405835
41 Z = 142845
50
XDOT = 12599
171792 XDOT = 3778
362976
YDOT = 9492
657510 feet/sec YDOT = 2935
959028 meter/sec
ZDOT = 19738
186368 ZDOT = 6034
704808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21437565
42 X = 6534169
94
Y = 5146353
63 feet Y = 1568608
59 meter
Z = 481560
27 Z = 146779
57
XDOT = -3726
856132 XDOT = -1135
945749
YDOT = 13573
537806 feet/sec YDOT = 4137
214323 meter/sec
ZDOT = 19811
505965 ZDOT = 6038
547018
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
56307562
00016717 00000-0 10270-3 0 9028
2 25544 51
6445 305
0404 0007117 181
2214 178
8935 15
77365318 39119
Satellite: ISS
Catalog Number: 25544
Epoch time: 10013
56307562 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 305
0404 deg
Eccentricity:
0007117
Arg of perigee: 181
2214 deg
Mean anomaly: 178
8935 deg
Mean motion: 15
77365318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3911
Checksum: 291
Coasting Arc #4 (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 = -2745271
84 A = 6711177
88 meter
Y = -3420378
78 meter E =
0016319
Z = -5093151
49 I = 51
33529
XDOT = 4690
466256 Wp = 126
54747
YDOT = -5926
625798 meter/sec RA = 299
55638 deg
ZDOT = 1445
515054 TA = 157
40925
MA = 157
33733
Ha = 186
088 n
mi
Hp = 178
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9006797
39 X = -2682079
45
Y = -11221715
17 feet Y = -3450724
11 meter
Z = -16709814
61 Z = -5106334
65
XDOT = 15388
668819 XDOT = 4749
368325
YDOT = -19444
310362 feet/sec YDOT = -5873
845061 meter/sec
ZDOT = 4742
503457 ZDOT = 1468
443234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6832777
48 X = 2082630
58
Y = -12594171
59 feet Y = -3838703
50 meter
Z = -16762075
90 Z = -5109080
73
XDOT = 22990
438810 XDOT = 7007
485749
YDOT = 6012
680018 feet/sec YDOT = 1832
664869 meter/sec
ZDOT = 4833
189666 ZDOT = 1473
156210
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
51337470
00016717 00000-0 10270-3 0 9036
2 25544 51
6452 300
1361 0007077 184
9351 175
1746 15
77390015 39260
Satellite: ISS
Catalog Number: 25544
Epoch time: 10014
51337470 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 300
1361 deg
Eccentricity:
0007077
Arg of perigee: 184
9351 deg
Mean anomaly: 175
1746 deg
Mean motion: 15
77390015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3926
Checksum: 290
Coasting Arc #5 (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 = -4188323
58 A = 6720018
76 meter
Y = 4695859
58 meter E =
0011321
Z = -2342942
36 I = 51
35213
XDOT = -2502
367898 Wp = 164
63645
YDOT = -4911
756463 meter/sec RA = 294
40767 deg
ZDOT = -5387
793680 TA = 41
90170
MA = 41
81512
Ha = 185
862 n
mi
Hp = 178
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13741219
09 X = -4229140
91
Y = 15406363
45 feet Y = 4648795
28 meter
Z = -7686818
75 Z = -2363387
42
XDOT = -8209
868431 XDOT = -2421
085488
YDOT = -16114
686560 feet/sec YDOT = -4939
284403 meter/sec
ZDOT = -17676
488450 ZDOT = -5399
752960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19651401
65 X = -5989747
22
Y = -6224927
59 feet Y = -1897357
93 meter
Z = -7767690
07 Z = -2367591
93
XDOT = 10956
293703 XDOT = 3339
478321
YDOT = -12538
829029 feet/sec YDOT = -3821
835088 meter/sec
ZDOT = -17723
939778 ZDOT = -5402
256844
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
52701111
00016717 00000-0 10270-3 0 9046
2 25544 51
6457 294
9051 0007084 188
9599 171
1441 15
77416793 39425
Satellite: ISS
Catalog Number: 25544
Epoch time: 10015
52701111 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 294
9051 deg
Eccentricity:
0007084
Arg of perigee: 188
9599 deg
Mean anomaly: 171
1441 deg
Mean motion: 15
77416793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3942
Checksum: 315
Coasting Arc #6 (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 = 1685430
94 A = 6715140
32 meter
Y = 5062680
67 meter E =
0009815
Z = 4066374
42 I = 51
32365
XDOT = -4835
222024 Wp = 116
30643
YDOT = 4658
725117 meter/sec RA = 289
17828 deg
ZDOT = -3793
305228 TA = 12
76063
MA = 12
73581
Ha = 185
720 n
mi
Hp = 178
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5529629
05 X = 1608940
66
Y = 16609844
73 feet Y = 5081100
15 meter
Z = 13341123
44 Z = 4074376
67
XDOT = -15863
589319 XDOT = -4868
530617
YDOT = 15284
531225 feet/sec YDOT = 4604
468878 meter/sec
ZDOT = -12445
227127 ZDOT = -3816
874675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12740570
51 X = -3883325
89
Y = 11970473
03 feet Y = 3648600
18 meter
Z = 13372918
63 Z = 4076065
60
XDOT = -19658
841422 XDOT = -5992
014865
YDOT = -6906
021610 feet/sec YDOT = -2104
955387 meter/sec
ZDOT = -12538
466713 ZDOT = -3821
724654
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
54063134
00016717 00000-0 10270-3 0 9056
2 25544 51
6449 289
6743 0007046 192
5465 167
5526 15
77437586 39589
Satellite: ISS
Catalog Number: 25544
Epoch time: 10016
54063134 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 289
6743 deg
Eccentricity:
0007046
Arg of perigee: 192
5465 deg
Mean anomaly: 167
5526 deg
Mean motion: 15
77437586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 339
Coasting Arc #7 (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 = 4204390
98 A = 6714866
67 meter
Y = -3240887
81 meter E =
0012373
Z = 4111496
98 I = 51
31447
XDOT = 1424
829210 Wp = 139
29025
YDOT = 6592
925256 meter/sec RA = 284
04453 deg
ZDOT = 3724
297887 TA = 272
37930
MA = 272
52095
Ha = 185
566 n
mi
Hp = 178
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13793933
65 X = 4220346
26
Y = -10632834
03 feet Y = -3193782
87 meter
Z = 13489163
31 Z = 4131959
96
XDOT = 4674
636515 XDOT = 1332
908538
YDOT = 21630
332205 feet/sec YDOT = 6608
344351 meter/sec
ZDOT = 12218
825088 ZDOT = 3730
996681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15572687
39 X = 4746555
12
Y = 7657045
56 feet Y = 2333867
49 meter
Z = 13570127
21 Z = 4136174
77
XDOT = -16857
896960 XDOT = -5138
286993
YDOT = 12493
244178 feet/sec YDOT = 3807
940825 meter/sec
ZDOT = 12245
503489 ZDOT = 3732
429463
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
55423438
00016717 00000-0 10270-3 0 9066
2 25544 51
6451 284
4424 0007008 196
7644 163
3290 15
77464883 39744
Satellite: ISS
Catalog Number: 25544
Epoch time: 10017
55423438 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 284
4424 deg
Eccentricity:
0007008
Arg of perigee: 196
7644 deg
Mean anomaly: 163
3290 deg
Mean motion: 15
77464883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3974
Checksum: 324
Coasting Arc #8 (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 = -851273
80 A = 6719976
73 meter
Y = -6275725
56 meter E =
0002736
Z = -2252333
23 I = 51
32622
XDOT = 4800
744980 Wp = 144
31622
YDOT = -2599
429678 meter/sec RA = 278
81337 deg
ZDOT = 5429
517760 TA = 190
26730
MA = 190
27289
Ha = 185
397 n
mi
Hp = 178
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2792893
04 X = -770093
08
Y = -20589650
80 feet Y = -6284791
01 meter
Z = -7389544
72 Z = -2256271
72
XDOT = 15750
475655 XDOT = 4803
080442
YDOT = -8528
312592 feet/sec YDOT = -2545
732089 meter/sec
ZDOT = 17813
378478 ZDOT = 5452
844810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17093931
16 X = 5210230
22
Y = -11802476
35 feet Y = -3597394
79 meter
Z = -7405296
23 Z = -2257134
29
XDOT = 13843
720138 XDOT = 4219
565898
YDOT = 8817
961619 feet/sec YDOT = 2687
714702 meter/sec
ZDOT = 17905
696693 ZDOT = 5457
656352
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
50447197
00016717 00000-0 10270-3 0 9071
2 25544 51
6453 279
5375 0007020 201
0111 159
0766 15
77510077 39892
Satellite: ISS
Catalog Number: 25544
Epoch time: 10018
50447197 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 279
5375 deg
Eccentricity:
0007020
Arg of perigee: 201
0111 deg
Mean anomaly: 159
0766 deg
Mean motion: 15
77510077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 307
Coasting Arc #9 (Orbit 4004)
---------------------------------------
Vector Time (GMT): 2010/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4186343
93 A = 6710569
56 meter
Y = 1178317
74 meter E =
0011656
Z = -5119315
43 I = 51
29132
XDOT = -555
345559 Wp = 109
05723
YDOT = -7569
502455 meter/sec RA = 273
65872 deg
ZDOT = -1294
295575 TA = 148
53725
MA = 148
46748
Ha = 185
097 n
mi
Hp = 178
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13734724
18 X = -4174340
73
Y = 3865871
85 feet Y = 1131570
83 meter
Z = -16795654
31 Z = -5139623
10
XDOT = -1821
999866 XDOT = -464
373442
YDOT = -24834
325640 feet/sec YDOT = -7575
203967 meter/sec
ZDOT = -4246
376557 ZDOT = -1296
772653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9815150
16 X = -2991657
77
Y = -10224646
74 feet Y = -3116472
33 meter
Z = -16876049
41 Z = -5143819
86
XDOT = 20337
635338 XDOT = 6198
911251
YDOT = -12530
995832 feet/sec YDOT = -3819
447529 meter/sec
ZDOT = -4256
384620 ZDOT = -1297
346032
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 10019
51804292
00016717 00000-0 10270-3 0 9087
2 25544 51
6453 274
3056 0006935 205
5858 154
4965 15
77542852 40058
Satellite: ISS
Catalog Number: 25544
Epoch time: 10019
51804292 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 274
3056 deg
Eccentricity:
0006935
Arg of perigee: 205
5858 deg
Mean anomaly: 154
4965 deg
Mean motion: 15
77542852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4005
Checksum: 319
Coasting Arc #10 (Orbit 4020)
---------------------------------------
Vector Time (GMT): 2010/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 138102
77 A = 6722221
09 meter
Y = 6710633
48 meter E =
0015725
Z = -52537
34 I = 51
32940
XDOT = -4818
675119 Wp = 160
99491
YDOT = 56
089484 meter/sec RA = 268
46212 deg
ZDOT = -6020
729966 TA = 19
57949
MA = 19
51917
Ha = 185
097 n
mi
Hp = 179
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 453093
07 X = 63308
23
Y = 22016514
03 feet Y = 6711759
63 meter
Z = -172366
61 Z = -52047
97
XDOT = -15809
301572 XDOT = -4789
697041
YDOT = 184
020616 feet/sec YDOT = 2
366368 meter/sec
ZDOT = -19753
051070 ZDOT = -6044
068325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19038195
47 X = -5802841
98
Y = 11067069
35 feet Y = 3373242
74 meter
Z = -170243
79 Z = -51890
31
XDOT = -6958
877853 XDOT = -2121
065970
YDOT = -12249
843940 feet/sec YDOT = -3733
752433 meter/sec
ZDOT = -19845
479692 ZDOT = -6048
902210
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 10020
53159900
00016717 00000-0 10270-3 0 9091
2 25544 51
6451 269
0736 0007119 209
2357 150
8411 15
77506462 40213
Satellite: ISS
Catalog Number: 25544
Epoch time: 10020
53159900 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 269
0736 deg
Eccentricity:
0007119
Arg of perigee: 209
2357 deg
Mean anomaly: 150
8411 deg
Mean motion: 15
77506462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4021
Checksum: 288
Coasting Arc #11 (Orbit 4036)
---------------------------------------
Vector Time (GMT): 2010/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4235610
79 A = 6710482
82 meter
Y = 1083661
61 meter E =
0003111
Z = 5090419
02 I = 51
29283
XDOT = -244
618638 Wp = 186
41480
YDOT = 7573
068817 meter/sec RA = 263
26309 deg
ZDOT = -1411
769801 TA = 277
14308
MA = 277
17846
Ha = 184
614 n
mi
Hp = 179
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13896360
86 X = 4198450
26
Y = 3555320
24 feet Y = 1130818
83 meter
Z = 16700849
79 Z = 5110905
12
XDOT = -802
554587 XDOT = -322
425813
YDOT = 24846
026302 feet/sec YDOT = 7569
898336 meter/sec
ZDOT = -4631
790687 ZDOT = -1413
146961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3813442
81 X = 1162337
37
Y = 13729133
26 feet Y = 4184639
82 meter
Z = 16782016
71 Z = 5115158
69
XDOT = -20909
089837 XDOT = -6373
090582
YDOT = 11463
393475 feet/sec YDOT = 3494
042331 meter/sec
ZDOT = -4637
028320 ZDOT = -1413
366232
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 10021
54513552
00016717 00000-0 10270-3 0 9102
2 25544 51
6451 263
8412 0006973 215
1688 144
9018 15
77608620 40379
Satellite: ISS
Catalog Number: 25544
Epoch time: 10021
54513552 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 263
8412 deg
Eccentricity:
0006973
Arg of perigee: 215
1688 deg
Mean anomaly: 144
9018 deg
Mean motion: 15
77608620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4037
Checksum: 295
Coasting Arc #12 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2010/022/09:06:54
813
Vector Time (MET): N/A
Weight (LBS) : 751525
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3102502
99 A = 6714008
82 meter
Y = -3664798
98 meter E =
0009340
Z = 4691922
18 I = 51
30118
XDOT = 3447
929360 Wp = 148
51233
YDOT = 6352
384817 meter/sec RA = 258
73228 deg
ZDOT = 2671
586781 TA = 275
05990
MA = 275
16650
Ha = 185
541 n
mi
Hp = 179
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10178815
59 X = 3120460
55
Y = -12023618
72 feet Y = -3630004
69 meter
Z = 15393445
46 Z = 4707037
50
XDOT = 11312
104200 XDOT = 3363
661652
YDOT = 20841
157537 feet/sec YDOT = 6390
470361 meter/sec
ZDOT = 8765
048495 ZDOT = 2688
132162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9569800
83 X = 2916875
29
Y = 12439905
14 feet Y = 3791683
09 meter
Z = 15453204
49 Z = 4710136
73
XDOT = -21869
564874 XDOT = -6665
843374
YDOT = 5812
403409 feet/sec YDOT = 1771
620559 meter/sec
ZDOT = 8830
765154 ZDOT = 2691
617219
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
43199557
00016717 00000-0 10270-3 0 9117
2 25544 51
6435 259
2624 0004704 203
8713 156
2234 15
76984436 40511
Satellite: ISS
Catalog Number: 25544
Epoch time: 10022
43199557 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 259
2624 deg
Eccentricity:
0004704
Arg of perigee: 203
8713 deg
Mean anomaly: 156
2234 deg
Mean motion: 15
76984436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 302
Coasting Arc #13 (Orbit 4065)
---------------------------------------
Vector Time (GMT): 2010/023/09:06:54
813
Vector Time (MET): N/A
Weight (LBS) : 751525
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2906498
22 A = 6722802
98 meter
Y = -5898679
26 meter E =
0004143
Z = -1391583
71 I = 51
33841
XDOT = 3870
261575 Wp = 46
91202
YDOT = -3271
893596 meter/sec RA = 253
51631 deg
ZDOT = 5799
094329 TA = 297
71270
MA = 297
75472
Ha = 185
429 n
mi
Hp = 179
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9535755
32 X = -2833562
12
Y = -19352622
23 feet Y = -5930773
57 meter
Z = -4565563
36 Z = -1405526
46
XDOT = 12697
708579 XDOT = 3878
390081
YDOT = -10734
559042 feet/sec YDOT = -3228
568834 meter/sec
ZDOT = 19025
900030 ZDOT = 5817
915525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20854724
43 X = 6356520
01
Y = -5479611
25 feet Y = -1670185
51 meter
Z = -4620964
73 Z = -1408470
05
XDOT = 7623
692294 XDOT = 2323
701411
YDOT = 12944
766390 feet/sec YDOT = 3945
564796 meter/sec
ZDOT = 19100
349793 ZDOT = 5821
786617
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
38253523
00016717 00000-0 10270-3 0 9127
2 25544 51
6437 254
3593 0004606 208
5314 151
5599 15
76992058 40661
Satellite: ISS
Catalog Number: 25544
Epoch time: 10023
38253523 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 254
3593 deg
Eccentricity:
0004606
Arg of perigee: 208
5314 deg
Mean anomaly: 151
5599 deg
Mean motion: 15
76992058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4066
Checksum: 312
Coasting Arc #14 (Orbit 4081)
---------------------------------------
Vector Time (GMT): 2010/024/09:06:54
813
Vector Time (MET): N/A
Weight (LBS) : 751525
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3713618
48 A = 6711529
94 meter
Y = 1999597
36 meter E =
0012859
Z = -5231238
81 I = 51
31115
XDOT = -3158
719373 Wp = 103
27308
YDOT = -7005
319955 meter/sec RA = 248
35256 deg
ZDOT = -439
189043 TA = 162
55691
MA = 162
51270
Ha = 185
213 n
mi
Hp = 179
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12183787
68 X = -3710290
10
Y = 6560358
78 feet Y = 1958088
40 meter
Z = -17162856
98 Z = -5249271
23
XDOT = -10363
252536 XDOT = -3078
016399
YDOT = -22983
333187 feet/sec YDOT = -7040
191365 meter/sec
ZDOT = -1440
908934 ZDOT = -454
338383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4257423
56 X = -1297662
70
Y = -13072968
00 feet Y = -3984640
65 meter
Z = -17234224
72 Z = -5252991
69
XDOT = 23527
942085 XDOT = 7171
316747
YDOT = -5699
737084 feet/sec YDOT = -1737
279863 meter/sec
ZDOT = -1501
129622 ZDOT = -457
544309
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
39642844
00016717 00000-0 10270-3 0 9138
2 25544 51
6444 249
1295 0004546 212
3123 147
7764 15
77034783 40826
Satellite: ISS
Catalog Number: 25544
Epoch time: 10024
39642844 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 249
1295 deg
Eccentricity:
0004546
Arg of perigee: 212
3123 deg
Mean anomaly: 147
7764 deg
Mean motion: 15
77034783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4082
Checksum: 308
Coasting Arc #15 (Orbit 4081)
---------------------------------------
Vector Time (GMT): 2010/024/09:16:23
939
Vector Time (MET): N/A
Weight (LBS) : 750815
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4626724
19 A = 6719441
60 meter
Y = -2120834
66 meter E =
0004109
Z = -4389917
09 I = 51
32318
XDOT = 64
466536 Wp = 170
86526
YDOT = -6960
674728 meter/sec RA = 248
29072 deg
ZDOT = 3291
280782 TA = 132
34986
MA = 132
31505
Ha = 185
606 n
mi
Hp = 184
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15179541
30 X = -4581339
50
Y = -6958118
96 feet Y = -2172319
41 meter
Z = -14402615
13 Z = -4412283
44
XDOT = 211
504384 XDOT = 126
308909
YDOT = -22836
859343 feet/sec YDOT = -6959
608242 meter/sec
ZDOT = 10798
165296 ZDOT = 3291
743757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9011430
76 X = 2746684
10
Y = -13966612
99 feet Y = -4257023
64 meter
Z = -14491275
07 Z = -4416940
64
XDOT = 21570
514377 XDOT = 6574
692782
YDOT = 2699
958340 feet/sec YDOT = 822
947302 meter/sec
ZDOT = 10799
787963 ZDOT = 3291
775371
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
39642748
00016717 00000-0 10270-3 0 9142
2 25544 51
6444 249
1296 0008188 264
9536 95
0694 15
75489735 40820
Satellite: ISS
Catalog Number: 25544
Epoch time: 10024
39642748 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 249
1296 deg
Eccentricity:
0008188
Arg of perigee: 264
9536 deg
Mean anomaly: 95
0694 deg
Mean motion: 15
75489735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4082
Checksum: 346
Coasting Arc #16 (Orbit 4097)
---------------------------------------
Vector Time (GMT): 2010/025/09:20:23
939
Vector Time (MET): N/A
Weight (LBS) : 750815
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1297055
21 A = 6719842
78 meter
Y = 5018156
21 meter E =
0002960
Z = -4278623
46 I = 51
33736
XDOT = -5320
042708 Wp = 357
67025
YDOT = -4345
227390 meter/sec RA = 243
15676 deg
ZDOT = -3480
511721 TA = 236
94614
MA = 236
97457
Ha = 184
764 n
mi
Hp = 184
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4255430
47 X = -1332288
13
Y = 16463767
09 feet Y = 5003455
11 meter
Z = -14037478
56 Z = -4285009
68
XDOT = -17454
208358 XDOT = -5254
150667
YDOT = -14255
995374 feet/sec YDOT = -4404
350557 meter/sec
ZDOT = -11419
001708 ZDOT = -3506
196552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15927462
06 X = -4854690
44
Y = -5896923
25 feet Y = -1797382
21 meter
Z = -14062623
08 Z = -4286287
52
XDOT = 15591
281460 XDOT = 4752
222589
YDOT = -14613
968870 feet/sec YDOT = -4454
337712 meter/sec
ZDOT = -11520
885149 ZDOT = -3511
565793
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
41129365
00016717 00000-0 10270-3 0 9152
2 25544 51
6447 243
9069 0008248 269
4050 90
6169 15
75522581 40983
Satellite: ISS
Catalog Number: 25544
Epoch time: 10025
41129365 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 243
9069 deg
Eccentricity:
0008248
Arg of perigee: 269
4050 deg
Mean anomaly: 90
6169 deg
Mean motion: 15
75522581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4098
Checksum: 319
Coasting Arc #17 (Orbit 4113)
---------------------------------------
Vector Time (GMT): 2010/026/09:20:23
939
Vector Time (MET): N/A
Weight (LBS) : 750815
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4859390
65 A = 6724878
29 meter
Y = 3850771
76 meter E =
0005866
Z = 2595746
02 I = 51
36847
XDOT = -1519
761358 Wp = 116
34025
YDOT = 5447
330063 meter/sec RA = 237
94211 deg
ZDOT = -5229
448828 TA = 34
03248
MA = 33
99487
Ha = 185
353 n
mi
Hp = 184
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15942882
70 X = 4803359
98
Y = 12633765
63 feet Y = 3904798
81 meter
Z = 8516227
09 Z = 2619216
91
XDOT = -4986
093695 XDOT = -1555
158029
YDOT = 17871
817791 feet/sec YDOT = 5430
137785 meter/sec
ZDOT = -17156
984344 ZDOT = -5236
917183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13998674
45 X = -4266795
97
Y = 14704763
96 feet Y = 4482012
06 meter
Z = 8609337
79 Z = 2624126
16
XDOT = -16293
215998 XDOT = -4966
172236
YDOT = -5436
129715 feet/sec YDOT = -1656
932337 meter/sec
ZDOT = -17186
402727 ZDOT = -5238
415551
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
42614741
00016717 00000-0 10270-3 0 9162
2 25544 51
6441 238
6839 0008157 272
9099 87
1132 15
75511736 41144
Satellite: ISS
Catalog Number: 25544
Epoch time: 10026
42614741 = yrday
fracday
Element set: 916
Inclination: 51
6441 deg
RA of node: 238
6839 deg
Eccentricity:
0008157
Arg of perigee: 272
9099 deg
Mean anomaly: 87
1132 deg
Mean motion: 15
75511736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4114
Checksum: 310
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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