Date:
November 26th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
329/05:06:49
490 -2
5 3
3 3
3
N/A 0
6 0
1 190
2
000/00:07:38
981 2
0 0
1 189
6
Coasting Arc #1 (Orbit 868)
---------------------------------------
Vector Time (GMT): 2010/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4899823
37 A = 6725721
20 meter
Y = -295551
87 meter E =
0003450
Z = -4600819
52 I = 51
89321
XDOT = -2409
690138 Wp = 87
26305
YDOT = 6666
646977 meter/sec RA = 129
23290 deg
ZDOT = -2996
310367 TA = 153
08989
MA = 153
07199
Ha = 190
695 n
mi
Hp = 187
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16075536
00 X = 4925114
41
Y = -969658
38 feet Y = -240617
16 meter
Z = -15094552
22 Z = -4576954
41
XDOT = -7905
807539 XDOT = -2469
502976
YDOT = 21872
201368 feet/sec YDOT = 6639
366286 meter/sec
ZDOT = -9830
414590 ZDOT = -3008
161342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6588896
57 X = -2008295
68
Y = 14793101
77 feet Y = 4508937
42 meter
Z = -14998639
40 Z = -4571585
29
XDOT = -14715
285505 XDOT = -4485
219022
YDOT = -16563
709869 feet/sec YDOT = -5048
618768 meter/sec
ZDOT = -9878
109406 ZDOT = -3010
847747
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 10328
52117669
00016717 00000-0 10270-3 0 9008
2 25544 51
6411 130
0536 0007099 241
7606 118
2840 15
73079045 8697
Satellite: ISS
Catalog Number: 25544
Epoch time: 10328
52117669 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 130
0536 deg
Eccentricity:
0007099
Arg of perigee: 241
7606 deg
Mean anomaly: 118
2840 deg
Mean motion: 15
73079045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 869
Checksum: 299
Coasting Arc #2 (Orbit 879)
---------------------------------------
Vector Time (GMT): 2010/329/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2220542
40 A = 6734525
38 meter
Y = 5984786
86 meter E =
0005687
Z = -2134720
88 I = 51
93400
XDOT = -5337
573133 Wp = 315
75932
YDOT = -
379842 meter/sec RA = 125
53892 deg
ZDOT = 5546
264852 TA = 20
48529
MA = 20
46249
Ha = 190
223 n
mi
Hp = 189
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7285244
09 X = -2276930
15
Y = 19635127
50 feet Y = 5959640
37 meter
Z = -7003677
42 Z = -2145644
72
XDOT = -17511
722877 XDOT = -5364
115255
YDOT = -1
246202 feet/sec YDOT = -60
216802 meter/sec
ZDOT = 18196
406996 ZDOT = 5520
270136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17999891
19 X = 5486366
83
Y = -10677035
88 feet Y = -3254360
54 meter
Z = -7047647
32 Z = -2148122
90
XDOT = 12899
519292 XDOT = 3931
773480
YDOT = 9794
241374 feet/sec YDOT = 2985
284771 meter/sec
ZDOT = 18091
929089 ZDOT = 5514
419986
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 10329
21997259
00016717 00000-0 10270-3 0 9017
2 25544 51
6446 126
4744 0008198 265
5266 94
4960 15
72471238 8802
Satellite: ISS
Catalog Number: 25544
Epoch time: 10329
21997259 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 126
4744 deg
Eccentricity:
0008198
Arg of perigee: 265
5266 deg
Mean anomaly: 94
4960 deg
Mean motion: 15
72471238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 880
Checksum: 333
Coasting Arc #3 (Orbit 895)
---------------------------------------
Vector Time (GMT): 2010/330/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4784436
58 A = 6727237
56 meter
Y = -979322
91 meter E =
0003991
Z = -4629783
71 I = 51
92710
XDOT = -1424
544289 Wp = 24
53885
YDOT = 6965
875506 meter/sec RA = 120
47700 deg
ZDOT = -2942
950007 TA = 216
38163
MA = 216
40876
Ha = 189
436 n
mi
Hp = 189
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15696970
42 X = 4817522
80
Y = -3213001
68 feet Y = -925635
04 meter
Z = -15189579
09 Z = -4606460
44
XDOT = -4673
701735 XDOT = -1488
035690
YDOT = 22853
922264 feet/sec YDOT = 6949
590667 meter/sec
ZDOT = -9655
347792 ZDOT = -2950
024083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14407570
98 X = -4391427
64
Y = -7209701
84 feet Y = -2197517
12 meter
Z = -15095816
34 Z = -4601204
82
XDOT = 17205
639855 XDOT = 5244
279028
YDOT = -14088
470230 feet/sec YDOT = -4294
165726 meter/sec
ZDOT = -9683
863725 ZDOT = -2951
641663
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 10330
23679158
00016717 00000-0 10270-3 0 9027
2 25544 51
6452 121
2651 0008227 270
5026 89
5194 15
72508314 8969
Satellite: ISS
Catalog Number: 25544
Epoch time: 10330
23679158 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 121
2651 deg
Eccentricity:
0008227
Arg of perigee: 270
5026 deg
Mean anomaly: 89
5194 deg
Mean motion: 15
72508314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 896
Checksum: 300
Coasting Arc #4 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2010/331/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 269276
42 A = 6732558
20 meter
Y = -6026402
26 meter E =
0005132
Z = 2983988
67 I = 51
95935
XDOT = 5397
271368 Wp = 101
10992
YDOT = -2242
166319 meter/sec RA = 115
32860 deg
ZDOT = -5009
028152 TA = 44
62871
MA = 44
58740
Ha = 190
045 n
mi
Hp = 189
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 883452
82 X = 322148
98
Y = -19771660
96 feet Y = -6023095
64 meter
Z = 9789989
08 Z = 2985424
83
XDOT = 17707
583228 XDOT = 5446
275676
YDOT = -7356
188709 feet/sec YDOT = -2181
536431 meter/sec
ZDOT = -16433
819397 ZDOT = -4982
689144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12585454
98 X = -3836046
68
Y = 15270588
36 feet Y = 4654475
33 meter
Z = 9795836
18 Z = 2985770
87
XDOT = -17524
799591 XDOT = -5341
558915
YDOT = -3956
042013 feet/sec YDOT = -1205
801606 meter/sec
ZDOT = -16327
908433 ZDOT = -4976
746490
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 10331
25359292
00016717 00000-0 10270-3 0 9035
2 25544 51
6450 116
0555 0008158 274
3846 85
6384 15
72507583 9121
Satellite: ISS
Catalog Number: 25544
Epoch time: 10331
25359292 = yrday
fracday
Element set: 903
Inclination: 51
6450 deg
RA of node: 116
0555 deg
Eccentricity:
0008158
Arg of perigee: 274
3846 deg
Mean anomaly: 85
6384 deg
Mean motion: 15
72507583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 310
Coasting Arc #5 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2010/332/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4485455
18 A = 6729164
69 meter
Y = 2894615
63 meter E =
0002508
Z = 4095664
99 I = 51
96044
XDOT = -760
551016 Wp = 117
07166
YDOT = -6624
086368 meter/sec RA = 110
27549 deg
ZDOT = 3845
738718 TA = 293
54108
MA = 293
56743
Ha = 190
716 n
mi
Hp = 189
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14716060
30 X = -4537386
10
Y = 9496770
44 feet Y = 2844166
01 meter
Z = 13437221
10 Z = 4073748
47
XDOT = -2495
246114 XDOT = -705
104776
YDOT = -21732
566823 feet/sec YDOT = -6632
281481 meter/sec
ZDOT = 12617
253011 ZDOT = 3842
178281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17550233
81 X = 5349311
26
Y = 1049546
71 feet Y = 319901
84 meter
Z = 13349072
46 Z = 4068797
28
XDOT = -10657
338383 XDOT = -3248
356739
YDOT = 17790
443078 feet/sec YDOT = 5422
527050 meter/sec
ZDOT = 12603
024847 ZDOT = 3841
401973
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 10332
27037379
00016717 00000-0 10270-3 0 9048
2 25544 51
6454 110
8450 0008231 279
3579 80
6652 15
72534430 9282
Satellite: ISS
Catalog Number: 25544
Epoch time: 10332
27037379 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 110
8450 deg
Eccentricity:
0008231
Arg of perigee: 279
3579 deg
Mean anomaly: 80
6652 deg
Mean motion: 15
72534430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 304
Coasting Arc #6 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2010/333/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1544716
03 A = 6730284
77 meter
Y = 5398322
09 meter E =
0002638
Z = -3707810
75 I = 51
97393
XDOT = -4675
751167 Wp = 286
33116
YDOT = 4314
957810 meter/sec RA = 105
12274 deg
ZDOT = 4332
514468 TA = 29
27953
MA = 29
26475
Ha = 190
945 n
mi
Hp = 189
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5067965
98 X = 1502248
26
Y = 17711030
47 feet Y = 5415358
71 meter
Z = -12164733
42 Z = -3700409
39
XDOT = -15340
390967 XDOT = -4744
701124
YDOT = 14156
685727 feet/sec YDOT = 4262
285072 meter/sec
ZDOT = 14214
286311 ZDOT = 4309
632084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5988185
60 X = 1825198
97
Y = -17442126
32 feet Y = -5316360
10 meter
Z = -12135051
76 Z = -3698763
78
XDOT = 19489
834458 XDOT = 5940
501543
YDOT = -3138
213800 feet/sec YDOT = -956
527566 meter/sec
ZDOT = 14122
227243 ZDOT = 4304
454864
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 10333
22358755
00016717 00000-0 10270-3 0 9059
2 25544 51
6451 105
9604 0008454 283
2372 76
7847 15
72577697 9438
Satellite: ISS
Catalog Number: 25544
Epoch time: 10333
22358755 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 105
9604 deg
Eccentricity:
0008454
Arg of perigee: 283
2372 deg
Mean anomaly: 76
7847 deg
Mean motion: 15
72577697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 331
Coasting Arc #7 (Orbit 958)
---------------------------------------
Vector Time (GMT): 2010/334/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3554238
01 A = 6731071
41 meter
Y = -4551473
00 meter E =
0004155
Z = -3458064
22 I = 51
98306
XDOT = 2658
386083 Wp = 309
81160
YDOT = 5571
486076 meter/sec RA = 100
07304 deg
ZDOT = -4594
596654 TA = 270
88918
MA = 270
93679
Ha = 191
073 n
mi
Hp = 189
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11660885
86 X = 3621668
18
Y = -14932654
19 feet Y = -4511350
23 meter
Z = -11345355
04 Z = -3440633
82
XDOT = 8721
739117 XDOT = 2618
207176
YDOT = 18279
153794 feet/sec YDOT = 5600
989253 meter/sec
ZDOT = -15074
136004 ZDOT = -4581
779419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18088480
06 X = -5513368
72
Y = 5775307
21 feet Y = 1760313
64 meter
Z = -11275203
63 Z = -3436682
07
XDOT = 3389
124379 XDOT = 1033
005111
YDOT = -18754
225370 feet/sec YDOT = -5716
287893 meter/sec
ZDOT = -15022
688191 ZDOT = -4578
915361
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 10334
24033122
00016717 00000-0 10270-3 0 9061
2 25544 51
6447 100
7503 0008545 286
7874 73
2350 15
72588431 9596
Satellite: ISS
Catalog Number: 25544
Epoch time: 10334
24033122 = yrday
fracday
Element set: 906
Inclination: 51
6447 deg
RA of node: 100
7503 deg
Eccentricity:
0008545
Arg of perigee: 286
7874 deg
Mean anomaly: 73
2350 deg
Mean motion: 15
72588431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 959
Checksum: 301
Coasting Arc #8 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2010/335/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3002655
47 A = 6728014
08 meter
Y = -4227244
41 meter E =
0006368
Z = 4289873
47 I = 51
97818
XDOT = 3306
895165 Wp = 13
11590
YDOT = -5967
760619 meter/sec RA = 94
92156 deg
ZDOT = -3558
921168 TA = 112
86780
MA = 112
80055
Ha = 191
201 n
mi
Hp = 188
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9851231
86 X = -2976002
31
Y = -13868912
11 feet Y = -4260673
08 meter
Z = 14074388
03 Z = 4275350
83
XDOT = 10849
393587 XDOT = 3390
670939
YDOT = -19579
267123 feet/sec YDOT = -5930
312348 meter/sec
ZDOT = -11676
250550 ZDOT = -3542
652729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 730678
36 X = 222710
76
Y = 17043996
45 feet Y = 5195010
12 meter
Z = 14016068
80 Z = 4272097
77
XDOT = -18607
649199 XDOT = -5671
611476
YDOT = 10364
954393 feet/sec YDOT = 3159
238099 meter/sec
ZDOT = -11610
736178 ZDOT = -3538
952387
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 10335
25705430
00016717 00000-0 10270-3 0 9072
2 25544 51
6451 95
5394 0008596 292
0539 67
9711 15
72681159 9754
Satellite: ISS
Catalog Number: 25544
Epoch time: 10335
25705430 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 95
5394 deg
Eccentricity:
0008596
Arg of perigee: 292
0539 deg
Mean anomaly: 67
9711 deg
Mean motion: 15
72681159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 330
Coasting Arc #9 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2010/336/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2136075
64 A = 6732717
24 meter
Y = 5755509
38 meter E =
0008415
Z = 2750597
79 I = 51
99456
XDOT = -4062
155737 Wp = 41
75344
YDOT = -3987
630984 meter/sec RA = 89
86707 deg
ZDOT = 5186
451619 TA = 349
50607
MA = 349
52362
Ha = 191
479 n
mi
Hp = 188
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7008122
16 X = -2213638
27
Y = 18882904
79 feet Y = 5731188
63 meter
Z = 9024270
98 Z = 2740032
49
XDOT = -13327
282603 XDOT = -4042
458809
YDOT = -13082
778819 feet/sec YDOT = -4032
946676 meter/sec
ZDOT = 17015
917386 ZDOT = 5166
764789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16032882
29 X = 4886822
52
Y = -12222581
44 feet Y = -3725442
82 meter
Z = 8981677
16 Z = 2737615
20
XDOT = 3508
109533 XDOT = 1069
271786
YDOT = 17054
637315 feet/sec YDOT = 5198
253454 meter/sec
ZDOT = 16936
836052 ZDOT = 5162
347629
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 10336
27376039
00016717 00000-0 10270-3 0 9085
2 25544 51
6443 90
3279 0008609 295
9449 64
0826 15
72667787 9911
Satellite: ISS
Catalog Number: 25544
Epoch time: 10336
27376039 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 90
3279 deg
Eccentricity:
0008609
Arg of perigee: 295
9449 deg
Mean anomaly: 64
0826 deg
Mean motion: 15
72667787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 350
Coasting Arc #10 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2010/337/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3966560
64 A = 6726215
72 meter
Y = 2663220
48 meter E =
0003195
Z = -4736944
75 I = 51
97129
XDOT = -1485
015660 Wp = 79
39790
YDOT = 7044
870991 meter/sec RA = 84
72150 deg
ZDOT = 2719
401572 TA = 217
24352
MA = 217
26568
Ha = 191
637 n
mi
Hp = 188
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13013650
39 X = 3959496
96
Y = 8737599
99 feet Y = 2707537
90 meter
Z = -15541157
30 Z = -4717691
65
XDOT = -4872
098623 XDOT = -1576
893019
YDOT = 23113
093802 feet/sec YDOT = 7027
750681 meter/sec
ZDOT = 8921
921167 ZDOT = 2711
964687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6686694
10 X = -2038104
36
Y = -14261396
16 feet Y = -4346873
55 meter
Z = -15463797
14 Z = -4713365
37
XDOT = 15143
306017 XDOT = 4615
679674
YDOT = -16734
183657 feet/sec YDOT = -5100
579179 meter/sec
ZDOT = 8891
863131 ZDOT = 2710
239882
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 10337
22690383
00016717 00000-0 10270-3 0 9093
2 25544 51
6438 85
4422 0008579 299
5220 60
5086 15
72705231 10067
Satellite: ISS
Catalog Number: 25544
Epoch time: 10337
22690383 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 85
4422 deg
Eccentricity:
0008579
Arg of perigee: 299
5220 deg
Mean anomaly: 60
5086 deg
Mean motion: 15
72705231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 304
Coasting Arc #11 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2010/338/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 421890
71 A = 6734112
63 meter
Y = -6413972
58 meter E =
0002927
Z = -2004354
73 I = 51
99398
XDOT = 4837
292428 Wp = 260
88664
YDOT = 2074
292956 meter/sec RA = 79
65967 deg
ZDOT = -5613
126606 TA = 301
31094
MA = 301
33958
Ha = 191
710 n
mi
Hp = 188
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1384155
86 X = 503318
59
Y = -21043217
12 feet Y = -6408799
22 meter
Z = -6575966
95 Z = -2002108
10
XDOT = 15870
381983 XDOT = 4841
005910
YDOT = 6805
423084 feet/sec YDOT = 2128
407898 meter/sec
ZDOT = -18415
769706 ZDOT = -5589
617268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11816845
69 X = -3601774
57
Y = 17470426
64 feet Y = 5324986
04 meter
Z = -6566777
49 Z = -2001553
78
XDOT = -9112
804088 XDOT = -2777
582686
YDOT = -13058
398733 feet/sec YDOT = -3980
199934 meter/sec
ZDOT = -18321
281206 ZDOT = -5584
326512
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 10338
24357225
00016717 00000-0 10270-3 0 9103
2 25544 51
6438 80
2325 0008620 303
3403 56
6934 15
72708890 10226
Satellite: ISS
Catalog Number: 25544
Epoch time: 10338
24357225 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 80
2325 deg
Eccentricity:
0008620
Arg of perigee: 303
3403 deg
Mean anomaly: 56
6934 deg
Mean motion: 15
72708890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 283
Coasting Arc #12 (Orbit 1037)
---------------------------------------
Vector Time (GMT): 2010/339/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4354366
01 A = 6724821
05 meter
Y = -941852
31 meter E =
0008710
Z = 5041697
26 I = 51
95665
XDOT = -551
593089 Wp = 344
73047
YDOT = -7446
653026 meter/sec RA = 74
52358 deg
ZDOT = -1860
033621 TA = 123
18496
MA = 123
10140
Ha = 191
894 n
mi
Hp = 187
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14285977
73 X = -4368002
49
Y = -3090066
62 feet Y = -990622
38 meter
Z = 16541001
50 Z = 5020510
12
XDOT = -1809
688613 XDOT = -459
246366
YDOT = -24431
276333 feet/sec YDOT = -7452
304680 meter/sec
ZDOT = -6102
472511 ZDOT = -1862
490008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11045793
64 X = 3366757
90
Y = 9717964
36 feet Y = 2962035
54 meter
Z = 16455820
04 Z = 5015733
95
XDOT = -9669
956163 XDOT = -2947
402639
YDOT = 21383
007041 feet/sec YDOT = 6517
540546 meter/sec
ZDOT = -6112
155092 ZDOT = -1862
984872
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 10339
26022105
00016717 00000-0 10270-3 0 9113
2 25544 51
6440 75
0209 0008626 307
4006 52
6370 15
72749047 10388
Satellite: ISS
Catalog Number: 25544
Epoch time: 10339
26022105 = yrday
fracday
Element set: 911
Inclination: 51
6440 deg
RA of node: 75
0209 deg
Eccentricity:
0008626
Arg of perigee: 307
4006 deg
Mean anomaly: 52
6370 deg
Mean motion: 15
72749047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1038
Checksum: 275
Coasting Arc #13 (Orbit 1053)
---------------------------------------
Vector Time (GMT): 2010/340/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1385328
90 A = 6734967
26 meter
Y = 6462984
48 meter E =
0013996
Z = 1243068
25 I = 51
98102
XDOT = -4953
746653 Wp = 22
75451
YDOT = -74
623335 meter/sec RA = 69
44682 deg
ZDOT = 5899
351957 TA = 350
81392
MA = 350
83950
Ha = 191
988 n
mi
Hp = 187
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4545042
32 X = 1306916
97
Y = 21204017
32 feet Y = 6478037
45 meter
Z = 4078307
90 Z = 1249608
74
XDOT = -16252
449648 XDOT = -4981
202361
YDOT = -244
827216 feet/sec YDOT = -130
173481 meter/sec
ZDOT = 19354
829254 ZDOT = 5875
219652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6048159
68 X = 1843479
07
Y = -20820032
72 feet Y = -6345945
97 meter
Z = 4104431
48 Z = 1251030
71
XDOT = 12786
389155 XDOT = 3897
291415
YDOT = 7516
836116 feet/sec YDOT = 2291
131648 meter/sec
ZDOT = 19257
773441 ZDOT = 5869
769345
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 10340
27685129
00016717 00000-0 10270-3 0 9128
2 25544 51
6431 69
8090 0008586 311
5450 48
4976 15
72783591 10546
Satellite: ISS
Catalog Number: 25544
Epoch time: 10340
27685129 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 69
8090 deg
Eccentricity:
0008586
Arg of perigee: 311
5450 deg
Mean anomaly: 48
4976 deg
Mean motion: 15
72783591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1054
Checksum: 318
Coasting Arc #14 (Orbit 1068)
---------------------------------------
Vector Time (GMT): 2010/341/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4163656
64 A = 6723807
30 meter
Y = -788008
99 meter E =
0009425
Z = -5227049
26 I = 51
93126
XDOT = 2591
668880 Wp = 63
94658
YDOT = 7176
223098 meter/sec RA = 64
32220 deg
ZDOT = 987
973002 TA = 215
40983
MA = 215
47244
Ha = 192
157 n
mi
Hp = 187
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13660290
81 X = 4197551
09
Y = -2585331
32 feet Y = -741258
20 meter
Z = -17149111
74 Z = -5206739
85
XDOT = 8502
850657 XDOT = 2506
430966
YDOT = 23544
039034 feet/sec YDOT = 7204
727963 meter/sec
ZDOT = 3241
381239 ZDOT = 1000
357424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13418970
08 X = -4090102
08
Y = -4001825
66 feet Y = -1219756
46 meter
Z = -17067400
20 Z = -5202143
58
XDOT = 2945
673909 XDOT = 897
841407
YDOT = -23837
090911 feet/sec YDOT = -7265
545310 meter/sec
ZDOT = 3290
982170 ZDOT = 1003
091365
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 10341
22992538
00016717 00000-0 10270-3 0 9130
2 25544 51
6424 64
9231 0008467 315
7454 44
3031 15
72814952 10698
Satellite: ISS
Catalog Number: 25544
Epoch time: 10341
22992538 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 64
9231 deg
Eccentricity:
0008467
Arg of perigee: 315
7454 deg
Mean anomaly: 44
3031 deg
Mean motion: 15
72814952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1069
Checksum: 302
Coasting Arc #15 (Orbit 1084)
---------------------------------------
Vector Time (GMT): 2010/342/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3094049
84 A = 6735258
05 meter
Y = -5960506
79 meter E =
0002445
Z = -499348
70 I = 51
95663
XDOT = 4425
923915 Wp = 133
10371
YDOT = -1793
751302 meter/sec RA = 59
23100 deg
ZDOT = -6032
624156 TA = 52
29892
MA = 52
27676
Ha = 192
246 n
mi
Hp = 186
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10151082
16 X = -3024742
63
Y = -19555468
46 feet Y = -5994718
73 meter
Z = -1638283
13 Z = -514212
11
XDOT = 14520
747754 XDOT = 4474
958512
YDOT = -5885
010834 feet/sec YDOT = -1743
982963 meter/sec
ZDOT = -19792
074003 ZDOT = -6011
004091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 441375
20 X = 134531
16
Y = 22024240
05 feet Y = 6712988
37 meter
Z = -1697888
49 Z = -517516
41
XDOT = -14125
625235 XDOT = -4305
490572
YDOT = -1231
117285 feet/sec YDOT = -375
244548 meter/sec
ZDOT = -19705
054044 ZDOT = -6006
100473
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 10342
24651822
00016717 00000-0 10270-3 0 9142
2 25544 51
6428 59
7123 0008679 320
5853 39
4677 15
72875203 10851
Satellite: ISS
Catalog Number: 25544
Epoch time: 10342
24651822 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 59
7123 deg
Eccentricity:
0008679
Arg of perigee: 320
5853 deg
Mean anomaly: 39
4677 deg
Mean motion: 15
72875203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1085
Checksum: 317
Coasting Arc #16 (Orbit 1100)
---------------------------------------
Vector Time (GMT): 2010/343/05:10:38
981
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3464982
60 A = 6723473
95 meter
Y = 2287921
67 meter E =
0007616
Z = 5290467
87 I = 51
89899
XDOT = -4411
614334 Wp = 340
50518
YDOT = -6306
041939 meter/sec RA = 54
11728 deg
ZDOT = -155
302108 TA = 111
00470
MA = 110
92321
Ha = 192
505 n
mi
Hp = 186
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11368053
14 X = -3516009
18
Y = 7506304
68 feet Y = 2248888
20 meter
Z = 17357178
04 Z = 5273511
31
XDOT = -14473
800307 XDOT = -4340
016683
YDOT = -20689
113972 feet/sec YDOT = -6354
974922 meter/sec
ZDOT = -509
521352 ZDOT = -176
560593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13578298
87 X = 4138665
49
Y = -1890160
16 feet Y = -576120
82 meter
Z = 17288897
20 Z = 5269655
87
XDOT = 4113
135226 XDOT = 1253
683617
YDOT = 23896
907325 feet/sec YDOT = 7283
777353 meter/sec
ZDOT = -594
839093 ZDOT = -181
306955
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 10343
26309562
00016717 00000-0 10270-3 0 9157
2 25544 51
6420 54
4999 0008399 324
4259 35
6343 15
72819629 11015
Satellite: ISS
Catalog Number: 25544
Epoch time: 10343
26309562 = yrday
fracday
Element set: 915
Inclination: 51
6420 deg
RA of node: 54
4999 deg
Eccentricity:
0008399
Arg of perigee: 324
4259 deg
Mean anomaly: 35
6343 deg
Mean motion: 15
72819629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1101
Checksum: 316
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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