Date:
January 6th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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
013/09:06:04
394 -3
8 5
1 5
1
N/A -2
9 -0
0 194
2
000/00:12:04
788 -1
7 0
2 187
1
Coasting Arc #1 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2011/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4009409
37 A = 6726468
27 meter
Y = 2588535
18 meter E =
0015854
Z = -4754701
88 I = 51
29307
XDOT = -1540
521718 Wp = 81
18177
YDOT = -7081
405158 meter/sec RA = 274
17775 deg
ZDOT = -2561
073843 TA = 163
56745
MA = 163
51600
Ha = 194
066 n
mi
Hp = 184
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13154230
21 X = -4014959
85
Y = 8492569
50 feet Y = 2543669
08 meter
Z = -15599415
62 Z = -4774192
38
XDOT = -5054
205112 XDOT = -1448
780641
YDOT = -23232
956556 feet/sec YDOT = -7098
118945 meter/sec
ZDOT = -8402
473239 ZDOT = -2568
335552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11390611
63 X = -3471858
42
Y = -10628076
07 feet Y = -3239437
59 meter
Z = -15677922
14 Z = -4778630
67
XDOT = 20566
255771 XDOT = 6268
594759
YDOT = -9627
728911 feet/sec YDOT = -2934
531772 meter/sec
ZDOT = -8431
496693 ZDOT = -2569
920192
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 11005
52038055
00016717 00000-0 10270-3 0 9002
2 25544 51
6467 274
8134 0004814 104
6543 255
5153 15
72533851 15305
Satellite: ISS
Catalog Number: 25544
Epoch time: 11005
52038055 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 274
8134 deg
Eccentricity:
0004814
Arg of perigee: 104
6543 deg
Mean anomaly: 255
5153 deg
Mean motion: 15
72533851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1530
Checksum: 281
Coasting Arc #2 (Orbit 1545)
---------------------------------------
Vector Time (GMT): 2011/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2218397
13 A = 6733317
96 meter
Y = 5772030
61 meter E =
0018489
Z = 2642562
71 I = 51
31419
XDOT = -4088
072309 Wp = 103
90027
YDOT = 3960
082876 meter/sec RA = 268
98713 deg
ZDOT = -5191
962544 TA = 45
87278
MA = 45
72085
Ha = 194
037 n
mi
Hp = 184
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7278205
81 X = 2140851
51
Y = 18937108
29 feet Y = 5796404
22 meter
Z = 8669825
16 Z = 2653151
66
XDOT = -13412
310725 XDOT = -4106
829793
YDOT = 12992
397888 feet/sec YDOT = 3914
263217 meter/sec
ZDOT = -17033
997847 ZDOT = -5211
867148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16434680
90 X = -5009290
74
Y = 11863789
77 feet Y = 3616083
12 meter
Z = 8712288
71 Z = 2655505
60
XDOT = -15118
642209 XDOT = -4608
162145
YDOT = -8313
283401 feet/sec YDOT = -2533
888781 meter/sec
ZDOT = -17114
206620 ZDOT = -5216
410178
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 11006
53716438
00016717 00000-0 10270-3 0 9013
2 25544 51
6459 269
6038 0004828 109
3150 250
8535 15
72525267 15463
Satellite: ISS
Catalog Number: 25544
Epoch time: 11006
53716438 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 269
6038 deg
Eccentricity:
0004828
Arg of perigee: 109
3150 deg
Mean anomaly: 250
8535 deg
Mean motion: 15
72525267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1546
Checksum: 310
Coasting Arc #3 (Orbit 1561)
---------------------------------------
Vector Time (GMT): 2011/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2991390
73 A = 6728243
98 meter
Y = -4238095
76 meter E =
0014502
Z = 4275957
66 I = 51
29938
XDOT = 3439
662845 Wp = 109
49634
YDOT = 5951
129819 meter/sec RA = 263
88599 deg
ZDOT = 3477
743412 TA = 305
09222
MA = 305
22811
Ha = 193
898 n
mi
Hp = 184
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9814274
06 X = 3017788
20
Y = -13904513
64 feet Y = -4204496
96 meter
Z = 14028732
48 Z = 4290553
32
XDOT = 11284
983087 XDOT = 3355
966660
YDOT = 19524
704130 feet/sec YDOT = 5989
125964 meter/sec
ZDOT = 11409
919332 ZDOT = 3494
250107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16040033
63 X = 4889002
25
Y = 5542407
16 feet Y = 1689325
70 meter
Z = 14087578
00 Z = 4293893
77
XDOT = -15294
385132 XDOT = -4661
728588
YDOT = 14973
561595 feet/sec YDOT = 4563
941574 meter/sec
ZDOT = 11476
208655 ZDOT = 3497
948398
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 11007
55392834
00016717 00000-0 10270-3 0 9027
2 25544 51
6461 264
3938 0004736 112
1449 248
0217 15
72566472 15625
Satellite: ISS
Catalog Number: 25544
Epoch time: 11007
55392834 = yrday
fracday
Element set: 902
Inclination: 51
6461 deg
RA of node: 264
3938 deg
Eccentricity:
0004736
Arg of perigee: 112
1449 deg
Mean anomaly: 248
0217 deg
Mean motion: 15
72566472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1562
Checksum: 306
Coasting Arc #4 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2011/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3674907
67 A = 6731090
12 meter
Y = -4510282
09 meter E =
0009299
Z = -3395222
27 I = 51
31382
XDOT = 2627
071448 Wp = 103
07722
YDOT = -5585
887869 meter/sec RA = 258
68714 deg
ZDOT = 4585
412064 TA = 216
70344
MA = 216
76716
Ha = 193
817 n
mi
Hp = 184
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12056783
69 X = -3607706
66
Y = -14797513
43 feet Y = -4551001
18 meter
Z = -11139180
68 Z = -3412911
67
XDOT = 8619
000813 XDOT = 2667
063974
YDOT = -18326
403771 feet/sec YDOT = -5556
287035 meter/sec
ZDOT = 15044
002836 ZDOT = 4598
270939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10670759
05 X = 3252447
36
Y = -15775880
00 feet Y = -4808488
23 meter
Z = -11210276
28 Z = -3416892
21
XDOT = 18863
867266 XDOT = 5749
706743
YDOT = 2052
046966 feet/sec YDOT = 625
463915 meter/sec
ZDOT = 15095
883417 ZDOT = 4601
225265
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 11008
50712765
00016717 00000-0 10270-3 0 9033
2 25544 51
6461 259
5093 0004568 115
6581 244
5054 15
72602962 15772
Satellite: ISS
Catalog Number: 25544
Epoch time: 11008
50712765 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 259
5093 deg
Eccentricity:
0004568
Arg of perigee: 115
6581 deg
Mean anomaly: 244
5054 deg
Mean motion: 15
72602962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1577
Checksum: 309
Coasting Arc #5 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2011/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1527033
81 A = 6730041
97 meter
Y = 5393172
72 meter E =
0009669
Z = -3732453
04 I = 51
31727
XDOT = -4791
151175 Wp = 95
56335
YDOT = -4277
569689 meter/sec RA = 253
59045 deg
ZDOT = -4230
995712 TA = 129
67309
MA = 129
58776
Ha = 193
702 n
mi
Hp = 184
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5009953
45 X = -1569096
51
Y = 17694136
21 feet Y = 5375861
50 meter
Z = -12245580
84 Z = -3739973
16
XDOT = -15718
999917 XDOT = -4722
409428
YDOT = -14034
021288 feet/sec YDOT = -4330
762670 meter/sec
ZDOT = -13881
219529 ZDOT = -4254
103974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18354598
55 X = -5594481
64
Y = 738783
19 feet Y = 225181
12 meter
Z = -12275962
34 Z = -3741713
32
XDOT = 8604
981736 XDOT = 2622
798433
YDOT = -17853
510121 feet/sec YDOT = -5441
749885 meter/sec
ZDOT = -13974
140946 ZDOT = -4259
318160
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 11009
52385629
00016717 00000-0 10270-3 0 9042
2 25544 51
6459 254
2988 0004425 120
8148 239
3451 15
72616871 15938
Satellite: ISS
Catalog Number: 25544
Epoch time: 11009
52385629 = yrday
fracday
Element set: 904
Inclination: 51
6459 deg
RA of node: 254
2988 deg
Eccentricity:
0004425
Arg of perigee: 120
8148 deg
Mean anomaly: 239
3451 deg
Mean motion: 15
72616871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1593
Checksum: 324
Coasting Arc #6 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2011/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4576344
61 A = 6728896
83 meter
Y = 2889330
37 meter E =
0014287
Z = 3985979
66 I = 51
32391
XDOT = -751
262499 Wp = 90
38487
YDOT = 6597
710125 meter/sec RA = 248
39079 deg
ZDOT = -3908
007149 TA = 40
18594
MA = 40
08039
Ha = 193
470 n
mi
Hp = 184
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15014253
98 X = 4524332
55
Y = 9479430
35 feet Y = 2940214
82 meter
Z = 13077361
09 Z = 4008085
04
XDOT = -2464
771978 XDOT = -805
999361
YDOT = 21646
030593 feet/sec YDOT = 6589
003177 meter/sec
ZDOT = -12821
545766 ZDOT = -3911
789396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4136652
89 X = -1260851
80
Y = 17200055
30 feet Y = 5242576
86 meter
Z = 13166282
54 Z = 4013082
92
XDOT = -19999
457731 XDOT = -6095
834716
YDOT = 5046
307974 feet/sec YDOT = 1538
114670 meter/sec
ZDOT = -12836
899651 ZDOT = -3912
687014
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 11010
54056640
00016717 00000-0 10270-3 0 9055
2 25544 51
6458 249
0883 0004384 122
4058 237
7529 15
72691857 16098
Satellite: ISS
Catalog Number: 25544
Epoch time: 11010
54056640 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 249
0883 deg
Eccentricity:
0004384
Arg of perigee: 122
4058 deg
Mean anomaly: 237
7529 deg
Mean motion: 15
72691857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1609
Checksum: 317
Coasting Arc #7 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2011/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -255916
79 A = 6731876
63 meter
Y = -5977621
18 meter E =
0016646
Z = 3072901
60 I = 51
34541
XDOT = 5510
526690 Wp = 94
74494
YDOT = 2281
298923 meter/sec RA = 243
29336 deg
ZDOT = 4872
650851 TA = 301
06004
MA = 301
22334
Ha = 193
568 n
mi
Hp = 184
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -839622
01 X = -203982
33
Y = -19611618
03 feet Y = -5980192
75 meter
Z = 10081698
17 Z = 3071784
24
XDOT = 18079
155806 XDOT = 5460
937011
YDOT = 7484
576519 feet/sec YDOT = 2342
643459 meter/sec
ZDOT = 15986
387308 ZDOT = 4899
300366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18138366
47 X = 5528574
10
Y = -7510566
61 feet Y = -2289220
70 meter
Z = 10077311
95 Z = 3071564
68
XDOT = -1476
216189 XDOT = -449
950695
YDOT = 18134
271158 feet/sec YDOT = 5527
325849 meter/sec
ZDOT = 16093
619144 ZDOT = 4905
335115
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 11011
55726015
00016717 00000-0 10270-3 0 9068
2 25544 51
6454 243
8772 0004342 126
1823 233
9741 15
72668241 16251
Satellite: ISS
Catalog Number: 25544
Epoch time: 11011
55726015 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 243
8772 deg
Eccentricity:
0004342
Arg of perigee: 126
1823 deg
Mean anomaly: 233
9741 deg
Mean motion: 15
72668241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1625
Checksum: 293
Coasting Arc #8 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2011/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4905328
63 A = 6726989
70 meter
Y = -1089096
15 meter E =
0013998
Z = -4486690
03 I = 51
34394
XDOT = -1335
923877 Wp = 116
92457
YDOT = -6890
521663 meter/sec RA = 238
09846 deg
ZDOT = 3134
457733 TA = 184
54675
MA = 184
55948
Ha = 193
404 n
mi
Hp = 184
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16093597
87 X = -4870990
22
Y = -3573150
09 feet Y = -1143758
25 meter
Z = -14720111
65 Z = -4510436
58
XDOT = -4382
952352 XDOT = -1273
999988
YDOT = -22606
698371 feet/sec YDOT = -6905
114705 meter/sec
ZDOT = 10283
653980 ZDOT = 3128
117904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2357512
76 X = -718569
89
Y = -16229311
16 feet Y = -4946694
04 meter
Z = -14815686
76 Z = -4515821
32
XDOT = 18360
274278 XDOT = 5596
211600
YDOT = -12027
975061 feet/sec YDOT = -3666
126798 meter/sec
ZDOT = 10258
255816 ZDOT = 3126
716373
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 11012
51039193
00016717 00000-0 10270-3 0 9070
2 25544 51
6449 238
9917 0004255 131
5342 228
6186 15
72720518 16407
Satellite: ISS
Catalog Number: 25544
Epoch time: 11012
51039193 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 238
9917 deg
Eccentricity:
0004255
Arg of perigee: 131
5342 deg
Mean anomaly: 228
6186 deg
Mean motion: 15
72720518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1640
Checksum: 301
Coasting Arc #9 (Orbit 1653)
---------------------------------------
Vector Time (GMT): 2011/013/09:12:06
788
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3145475
66 A = 6726615
74 meter
Y = 2811019
75 meter E =
0015009
Z = -5251625
89 I = 51
34866
XDOT = -4784
044303 Wp = 106
18688
YDOT = -6006
418878 meter/sec RA = 233
57947 deg
ZDOT = -354
576449 TA = 160
45583
MA = 160
39823
Ha = 194
154 n
mi
Hp = 187
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10319802
02 X = -3151163
95
Y = 9222505
74 feet Y = 2775813
68 meter
Z = -17229743
73 Z = -5266920
14
XDOT = -15695
683410 XDOT = -4714
801380
YDOT = -19706
098681 feet/sec YDOT = -6059
529766 meter/sec
ZDOT = -1163
308559 ZDOT = -377
649387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5115761
58 X = -1559284
13
Y = -12777114
24 feet Y = -3894464
42 meter
Z = -17291365
77 Z = -5270408
29
XDOT = 22986
351746 XDOT = 7006
240012
YDOT = -7525
438412 feet/sec YDOT = -2293
753628 meter/sec
ZDOT = -1256
092470 ZDOT = -382
856985
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 11013
39997557
00016717 00000-0 10270-3 0 9085
2 25544 51
6455 234
4328 0004920 186
0278 174
0826 15
71734150 16549
Satellite: ISS
Catalog Number: 25544
Epoch time: 11013
39997557 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 234
4328 deg
Eccentricity:
0004920
Arg of perigee: 186
0278 deg
Mean anomaly: 174
0826 deg
Mean motion: 15
71734150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1654
Checksum: 318
Coasting Arc #10 (Orbit 1669)
---------------------------------------
Vector Time (GMT): 2011/014/09:12:06
788
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4992076
26 A = 6738214
15 meter
Y = 4392727
68 meter E =
0016435
Z = 1027475
29 I = 51
40637
XDOT = -2522
266325 Wp = 140
09008
YDOT = 4256
453354 meter/sec RA = 228
42967 deg
ZDOT = -5903
133422 TA = 28
64313
MA = 28
55295
Ha = 194
097 n
mi
Hp = 187
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16378202
96 X = 4937593
68
Y = 14411836
22 feet Y = 4448247
38 meter
Z = 3370981
92 Z = 1051594
66
XDOT = -8275
151984 XDOT = -2540
999158
YDOT = 13964
741975 feet/sec YDOT = 4228
143591 meter/sec
ZDOT = -19367
235636 ZDOT = -5915
431668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19001739
97 X = -5791730
34
Y = 10687226
42 feet Y = 3257466
61 meter
Z = 3468017
29 Z = 1057051
67
XDOT = -9710
855843 XDOT = -2959
868861
YDOT = -10923
921409 feet/sec YDOT = -3329
611245 meter/sec
ZDOT = -19416
824110 ZDOT = -5918
247989
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 11014
41727664
00016717 00000-0 10270-3 0 9090
2 25544 51
6452 229
2266 0005018 189
9565 170
1498 15
71712967 16701
Satellite: ISS
Catalog Number: 25544
Epoch time: 11014
41727664 = yrday
fracday
Element set: 909
Inclination: 51
6452 deg
RA of node: 229
2266 deg
Eccentricity:
0005018
Arg of perigee: 189
9565 deg
Mean anomaly: 170
1498 deg
Mean motion: 15
71712967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1670
Checksum: 325
Coasting Arc #11 (Orbit 1685)
---------------------------------------
Vector Time (GMT): 2011/015/09:12:06
788
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1103177
90 A = 6727811
41 meter
Y = -4406085
56 meter E =
0008843
Z = 4962385
88 I = 51
39303
XDOT = 6373
087238 Wp = 155
34406
YDOT = 3836
456104 meter/sec RA = 223
32062 deg
ZDOT = 1980
401630 TA = 275
38404
MA = 275
48492
Ha = 193
869 n
mi
Hp = 187
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3619350
05 X = 1128259
41
Y = -14455661
28 feet Y = -4393609
41 meter
Z = 16280793
57 Z = 4967805
56
XDOT = 20909
078865 XDOT = 6320
093248
YDOT = 12586
798240 feet/sec YDOT = 3907
427306 meter/sec
ZDOT = 6497
380676 ZDOT = 2011
233496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12621028
43 X = 3846889
46
Y = 7877943
40 feet Y = 2401197
15 meter
Z = 16302690
77 Z = 4969060
15
XDOT = -17922
923867 XDOT = -5462
907195
YDOT = 14948
991293 feet/sec YDOT = 4556
452546 meter/sec
ZDOT = 6621
466555 ZDOT = 2018
223006
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 11015
43455866
00016717 00000-0 10270-3 0 9107
2 25544 51
6454 224
0202 0004837 194
8169 165
2852 15
71770908 16864
Satellite: ISS
Catalog Number: 25544
Epoch time: 11015
43455866 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 224
0202 deg
Eccentricity:
0004837
Arg of perigee: 194
8169 deg
Mean anomaly: 165
2852 deg
Mean motion: 15
71770908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1686
Checksum: 315
Coasting Arc #12 (Orbit 1700)
---------------------------------------
Vector Time (GMT): 2011/016/09:12:06
788
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5898246
47 A = 6735884
64 meter
Y = -2211406
37 meter E =
0002495
Z = -2389211
19 I = 51
44351
XDOT = -102
626174 Wp = 107
34954
YDOT = -5514
065117 meter/sec RA = 218
14882 deg
ZDOT = 5360
934799 TA = 225
68176
MA = 225
70222
Ha = 193
665 n
mi
Hp = 187
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19351202
32 X = -5861473
51
Y = -7255270
25 feet Y = -2277158
24 meter
Z = -7838619
40 Z = -2417775
47
XDOT = -336
700047 XDOT = -67
001378
YDOT = -18090
764819 feet/sec YDOT = -5515
014165 meter/sec
ZDOT = 17588
368763 ZDOT = 5360
522152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12665744
26 X = 3860518
85
Y = -16274852
55 feet Y = -4960575
06 meter
Z = -7953617
30 Z = -2424262
55
XDOT = 16216
863225 XDOT = 4942
899911
YDOT = 4031
961582 feet/sec YDOT = 1228
941890 meter/sec
ZDOT = 17586
796906 ZDOT = 5360
455697
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 11016
38824526
00016717 00000-0 10270-3 0 9116
2 25544 51
6452 219
1388 0004758 200
3783 159
7190 15
71802801 17018
Satellite: ISS
Catalog Number: 25544
Epoch time: 11016
38824526 = yrday
fracday
Element set: 911
Inclination: 51
6452 deg
RA of node: 219
1388 deg
Eccentricity:
0004758
Arg of perigee: 200
3783 deg
Mean anomaly: 159
7190 deg
Mean motion: 15
71802801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1701
Checksum: 298
Coasting Arc #13 (Orbit 1716)
---------------------------------------
Vector Time (GMT): 2011/017/09:12:06
788
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1310597
04 A = 6730248
41 meter
Y = 4979021
36 meter E =
0006294
Z = -4339122
60 I = 51
44854
XDOT = -6793
468240 Wp = 100
84174
YDOT = -1179
262706 meter/sec RA = 213
06154 deg
ZDOT = -3410
430253 TA = 134
64891
MA = 134
59759
Ha = 193
470 n
mi
Hp = 187
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4299859
06 X = 1275901
60
Y = 16335371
92 feet Y = 4993483
77 meter
Z = -14235966
53 Z = -4332839
50
XDOT = -22288
281627 XDOT = -6763
209623
YDOT = -3868
972134 feet/sec YDOT = -1255
061772 meter/sec
ZDOT = -11189
075632 ZDOT = -3443
359016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16908809
62 X = -5153805
17
Y = -378148
35 feet Y = -115259
62 meter
Z = -14210737
77 Z = -4331432
87
XDOT = 9925
449262 XDOT = 3025
276935
YDOT = -19007
755400 feet/sec YDOT = -5793
563846 meter/sec
ZDOT = -11321
686533 ZDOT = -3450
850055
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 11017
40549405
00016717 00000-0 10270-3 0 9121
2 25544 51
6445 213
9320 0004769 206
3469 153
7451 15
71822150 17177
Satellite: ISS
Catalog Number: 25544
Epoch time: 11017
40549405 = yrday
fracday
Element set: 912
Inclination: 51
6445 deg
RA of node: 213
9320 deg
Eccentricity:
0004769
Arg of perigee: 206
3469 deg
Mean anomaly: 153
7451 deg
Mean motion: 15
71822150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1717
Checksum: 292
Coasting Arc #14 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2011/018/09:12:06
788
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5724595
78 A = 6732696
12 meter
Y = -149076
80 meter E =
0010332
Z = 3529026
83 I = 51
48376
XDOT = 2903
961511 Wp = 108
94020
YDOT = 5559
750791 meter/sec RA = 207
88037 deg
ZDOT = -4468
452749 TA = 28
95250
MA = 28
89523
Ha = 193
121 n
mi
Hp = 187
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18781482
20 X = 5708694
33
Y = -489097
12 feet Y = -85150
23 meter
Z = 11578172
02 Z = 3556797
66
XDOT = 9527
432778 XDOT = 2863
281950
YDOT = 18240
652200 feet/sec YDOT = 5591
997692 meter/sec
ZDOT = -14660
278049 ZDOT = -4454
443800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4473018
02 X = -1363375
89
Y = 18176146
66 feet Y = 5540089
50 meter
Z = 11690045
31 Z = 3563125
81
XDOT = -18806
860706 XDOT = -5732
331143
YDOT = 4779
658642 feet/sec YDOT = 1456
839954 meter/sec
ZDOT = -14603
926789 ZDOT = -4451
276885
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 11018
42272531
00016717 00000-0 10270-3 0 9138
2 25544 51
6445 208
7251 0004604 210
3264 149
7632 15
71882800 17330
Satellite: ISS
Catalog Number: 25544
Epoch time: 11018
42272531 = yrday
fracday
Element set: 913
Inclination: 51
6445 deg
RA of node: 208
7251 deg
Eccentricity:
0004604
Arg of perigee: 210
3264 deg
Mean anomaly: 149
7632 deg
Mean motion: 15
71882800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1733
Checksum: 282
Coasting Arc #15 (Orbit 1748)
---------------------------------------
Vector Time (GMT): 2011/019/09:12:06
788
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3682050
37 A = 6733302
84 meter
Y = -4487172
51 meter E =
0010607
Z = 3407863
64 I = 51
51197
XDOT = 6009
339755 Wp = 111
16341
YDOT = -1433
110410 meter/sec RA = 202
80147 deg
ZDOT = 4590
612436 TA = 289
13949
MA = 289
25429
Ha = 193
165 n
mi
Hp = 187
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12080217
76 X = -3648154
64
Y = -14721694
60 feet Y = -4528158
22 meter
Z = 11180655
00 Z = 3390058
64
XDOT = 19715
681612 XDOT = 6002
618686
YDOT = -4701
805806 feet/sec YDOT = -1365
948357 meter/sec
ZDOT = 15061
064422 ZDOT = 4619
788553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17270376
42 X = 5264010
73
Y = -8123524
88 feet Y = -2476050
38 meter
Z = 11108980
18 Z = 3386017
16
XDOT = -896
837340 XDOT = -273
356021
YDOT = 18919
007385 feet/sec YDOT = 5766
513451 meter/sec
ZDOT = 15178
632982 ZDOT = 4626
447333
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 11019
43994003
00016717 00000-0 10270-3 0 9146
2 25544 51
6437 203
5171 0004582 215
1519 144
9342 15
71860703 17496
Satellite: ISS
Catalog Number: 25544
Epoch time: 11019
43994003 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 203
5171 deg
Eccentricity:
0004582
Arg of perigee: 215
1519 deg
Mean anomaly: 144
9342 deg
Mean motion: 15
71860703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1749
Checksum: 296
Coasting Arc #16 (Orbit 1763)
---------------------------------------
Vector Time (GMT): 2011/020/09:12:06
788
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4563400
23 A = 6729548
66 meter
Y = 2236067
54 meter E =
0009169
Z = -4420596
18 I = 51
52819
XDOT = -5355
259606 Wp = 139
98500
YDOT = -4436
722711 meter/sec RA = 197
62367 deg
ZDOT = 3280
898734 TA = 163
05386
MA = 163
02322
Ha = 192
917 n
mi
Hp = 187
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14971785
54 X = -4566591
39
Y = 7336179
60 feet Y = 2185019
29 meter
Z = -14503268
32 Z = -4442772
12
XDOT = -17569
749365 XDOT = -5321
186856
YDOT = -14556
176873 feet/sec YDOT = -4496
418159 meter/sec
ZDOT = 10764
103459 ZDOT = 3254
966137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3700460
89 X = -1127900
48
Y = -16176518
39 feet Y = -4930602
81 meter
Z = -14592653
20 Z = -4447840
69
XDOT = 17054
373505 XDOT = 5198
173044
YDOT = -13526
452430 feet/sec YDOT = -4122
862701 meter/sec
ZDOT = 10659
662173 ZDOT = 3249
065030
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 11020
39356038
00016717 00000-0 10270-3 0 9154
2 25544 51
6431 198
6345 0004689 219
4947 140
5874 15
71915378 17645
Satellite: ISS
Catalog Number: 25544
Epoch time: 11020
39356038 = yrday
fracday
Element set: 915
Inclination: 51
6431 deg
RA of node: 198
6345 deg
Eccentricity:
0004689
Arg of perigee: 219
4947 deg
Mean anomaly: 140
5874 deg
Mean motion: 15
71915378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1764
Checksum: 333
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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