Date:
February 16th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 2159)
---------------------------------------
Vector Time (GMT): 2011/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1932392
55 A = 6736632
45 meter
Y = 6418960
47 meter E =
0013306
Z = 578926
99 I = 51
98545
XDOT = -4709
973126 Wp = 30
75685
YDOT = 869
529769 meter/sec RA = 69
37498 deg
ZDOT = 6030
978208 TA = 335
51291
MA = 335
57605
Ha = 191
947 n
mi
Hp = 187
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6339870
56 X = 1857658
65
Y = 21059581
61 feet Y = 6440151
78 meter
Z = 1899366
76 Z = 588132
91
XDOT = -15452
667737 XDOT = -4748
642973
YDOT = 2852
787957 feet/sec YDOT = 816
643671 meter/sec
ZDOT = 19786
673912 ZDOT = 6008
003833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7484024
65 X = -2281130
71
Y = 20677219
49 feet Y = 6302416
50 meter
Z = 1936362
40 Z = 590203
26
XDOT = -12691
111227 XDOT = -3868
250702
YDOT = -6452
624947 feet/sec YDOT = -1966
760084 meter/sec
ZDOT = 19693
891722 ZDOT = 6002
698197
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 11045
56242459
00016717 00000-0 10270-3 0 9005
2 25544 51
6445 69
7391 0004676 312
0826 47
9939 15
72384659 21607
Satellite: ISS
Catalog Number: 25544
Epoch time: 11045
56242459 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 69
7391 deg
Eccentricity:
0004676
Arg of perigee: 312
0826 deg
Mean anomaly: 47
9939 deg
Mean motion: 15
72384659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2160
Checksum: 326
Coasting Arc #2 (Orbit 2174)
---------------------------------------
Vector Time (GMT): 2011/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3776342
02 A = 6724659
35 meter
Y = -1724903
42 meter E =
0012091
Z = -5300028
67 I = 51
93353
XDOT = 3282
698366 Wp = 74
99795
YDOT = 6953
726612 meter/sec RA = 64
26765 deg
ZDOT = 79
070813 TA = 195
73156
MA = 195
76916
Ha = 192
000 n
mi
Hp = 187
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12389573
57 X = 3821095
36
Y = -5659131
97 feet Y = -1682423
82 meter
Z = -17388545
50 Z = -5281575
06
XDOT = 10770
007763 XDOT = 3204
312404
YDOT = 22814
063688 feet/sec YDOT = 6989
997450 meter/sec
ZDOT = 259
418678 ZDOT = 94
827338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13451231
92 X = 4099935
49
Y = 2679365
73 feet Y = 816670
67 meter
Z = -17313988
03 Z = -5277303
55
XDOT = -4345
712160 XDOT = -1324
573066
YDOT = 23834
762860 feet/sec YDOT = 7264
835720 meter/sec
ZDOT = 322
847152 ZDOT = 98
403812
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 11046
51573371
00016717 00000-0 10270-3 0 9012
2 25544 51
6446 64
8552 0004695 314
5315 45
5464 15
72402759 21759
Satellite: ISS
Catalog Number: 25544
Epoch time: 11046
51573371 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 64
8552 deg
Eccentricity:
0004695
Arg of perigee: 314
5315 deg
Mean anomaly: 45
5464 deg
Mean motion: 15
72402759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2175
Checksum: 305
Coasting Arc #3 (Orbit 2190)
---------------------------------------
Vector Time (GMT): 2011/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3727310
32 A = 6736533
61 meter
Y = -5590707
07 meter E =
0008447
Z = 427445
92 I = 51
95822
XDOT = 3738
205615 Wp = 125
39674
YDOT = -2960
144324 meter/sec RA = 59
16185 deg
ZDOT = -6041
334659 TA = 49
97955
MA = 49
90545
Ha = 192
080 n
mi
Hp = 187
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12228708
39 X = -3666593
34
Y = -18342214
80 feet Y = -5632048
61 meter
Z = 1402381
61 Z = 409486
82
XDOT = 12264
454117 XDOT = 3800
375413
YDOT = -9711
759593 feet/sec YDOT = -2917
993939 meter/sec
ZDOT = -19820
651769 ZDOT = -6023
024008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 362781
21 X = 110575
71
Y = -22046411
52 feet Y = -6719746
23 meter
Z = 1330020
91 Z = 405390
37
XDOT = 14101
039265 XDOT = 4297
996768
YDOT = -975
599779 feet/sec YDOT = -297
362813 meter/sec
ZDOT = -19746
634128 ZDOT = -6018
774082
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 11047
53258043
00016717 00000-0 10270-3 0 9022
2 25544 51
6432 59
6451 0004615 320
2663 39
8161 15
72444673 21915
Satellite: ISS
Catalog Number: 25544
Epoch time: 11047
53258043 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 59
6451 deg
Eccentricity:
0004615
Arg of perigee: 320
2663 deg
Mean anomaly: 39
8161 deg
Mean motion: 15
72444673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2191
Checksum: 291
Coasting Arc #4 (Orbit 2206)
---------------------------------------
Vector Time (GMT): 2011/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2621242
96 A = 6724812
60 meter
Y = 3345561
25 meter E =
0001835
Z = 5210949
77 I = 51
90166
XDOT = -5119
231492 Wp = 8
99539
YDOT = -5653
171422 meter/sec RA = 54
07059 deg
ZDOT = 1056
095841 TA = 70
97657
MA = 70
95669
Ha = 192
275 n
mi
Hp = 187
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8599878
49 X = -2683771
84
Y = 10976250
83 feet Y = 3315899
56 meter
Z = 17096291
91 Z = 5198064
17
XDOT = -16795
378910 XDOT = -5060
766337
YDOT = -18547
150334 feet/sec YDOT = -5710
090819 meter/sec
ZDOT = 3464
881369 ZDOT = 1031
369736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13327500
91 X = -4062222
28
Y = 4311986
90 feet Y = 1314293
61 meter
Z = 17044168
44 Z = 5195062
54
XDOT = -3399
449376 XDOT = -1036
152170
YDOT = -23786
363158 feet/sec YDOT = -7250
083490 meter/sec
ZDOT = 3365
197240 ZDOT = 1025
712119
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 11048
54940888
00016717 00000-0 10270-3 0 9030
2 25544 51
6426 54
4346 0004700 324
1462 35
9384 15
72467413 22078
Satellite: ISS
Catalog Number: 25544
Epoch time: 11048
54940888 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 54
4346 deg
Eccentricity:
0004700
Arg of perigee: 324
1462 deg
Mean anomaly: 35
9384 deg
Mean motion: 15
72467413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2207
Checksum: 302
Coasting Arc #5 (Orbit 2221)
---------------------------------------
Vector Time (GMT): 2011/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5091592
12 A = 6735521
36 meter
Y = 4168808
68 meter E =
0011195
Z = -1405673
99 I = 51
91972
XDOT = -2113
934081 Wp = 14
49714
YDOT = 4545
730061 meter/sec RA = 48
94453 deg
ZDOT = 5844
786741 TA = 330
11292
MA = 330
17680
Ha = 192
236 n
mi
Hp = 186
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16704698
54 X = 5051425
59
Y = 13677193
84 feet Y = 4225521
26 meter
Z = -4611791
29 Z = -1381037
69
XDOT = -6935
479268 XDOT = -2193
000208
YDOT = 14913
812537 feet/sec YDOT = 4521
649129 meter/sec
ZDOT = 19175
809518 ZDOT = 5834
325187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6698231
54 X = 2041620
97
Y = 20546359
08 feet Y = 6262530
25 meter
Z = -4512430
22 Z = -1375388
73
XDOT = -12488
808548 XDOT = -3806
588845
YDOT = 8258
418492 feet/sec YDOT = 2517
165957 meter/sec
ZDOT = 19133
440961 ZDOT = 5831
872805
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 11049
50266881
00016717 00000-0 10270-3 0 9042
2 25544 51
6429 49
5510 0004579 327
9970 32
0914 15
72536410 22226
Satellite: ISS
Catalog Number: 25544
Epoch time: 11049
50266881 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 49
5510 deg
Eccentricity:
0004579
Arg of perigee: 327
9970 deg
Mean anomaly: 32
0914 deg
Mean motion: 15
72536410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2222
Checksum: 302
Coasting Arc #6 (Orbit 2237)
---------------------------------------
Vector Time (GMT): 2011/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 998942
14 A = 6725759
81 meter
Y = -4442301
66 meter E =
0012622
Z = -4961176
78 I = 51
86517
XDOT = 6344
279296 Wp = 52
66978
YDOT = 3794
019206 meter/sec RA = 43
86702 deg
ZDOT = -2115
962573 TA = 196
83009
MA = 196
87201
Ha = 192
340 n
mi
Hp = 186
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3277369
22 X = 1072642
42
Y = -14574480
50 feet Y = -4430719
26 meter
Z = -16276826
70 Z = -4956144
62
XDOT = 20814
564619 XDOT = 6311
661028
YDOT = 12447
569572 feet/sec YDOT = 3864
782202 meter/sec
ZDOT = -6942
134426 ZDOT = -2085
222466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10528987
77 X = 3209235
47
Y = -10628364
58 feet Y = -3239525
52 meter
Z = -16256383
40 Z = -4954945
66
XDOT = 10430
416660 XDOT = 3179
190998
YDOT = 20780
588341 feet/sec YDOT = 6333
923326 meter/sec
ZDOT = -6818
122413 ZDOT = -2078
163711
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 11050
51946211
00016717 00000-0 10270-3 0 9058
2 25544 51
6422 44
3399 0004769 332
0581 28
0325 15
72519345 22389
Satellite: ISS
Catalog Number: 25544
Epoch time: 11050
51946211 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 44
3399 deg
Eccentricity:
0004769
Arg of perigee: 332
0581 deg
Mean anomaly: 28
0325 deg
Mean motion: 15
72519345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2238
Checksum: 291
Coasting Arc #7 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2011/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5858923
40 A = 6734047
94 meter
Y = -2410584
06 meter E =
0011261
Z = 2273176
88 I = 51
87083
XDOT = 99
820841 Wp = 88
90918
YDOT = -5418
787178 meter/sec RA = 38
72179 deg
ZDOT = -5465
683535 TA = 65
66562
MA = 65
54809
Ha = 192
414 n
mi
Hp = 186
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19222189
63 X = -5842574
80
Y = -7908740
35 feet Y = -2476010
46 meter
Z = 7457929
39 Z = 2244754
76
XDOT = 327
496196 XDOT = 186
958080
YDOT = -17778
173157 feet/sec YDOT = -5417
184227 meter/sec
ZDOT = -17932
032594 ZDOT = -5464
986451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12525962
03 X = -3817913
23
Y = -16638464
12 feet Y = -5071403
86 meter
Z = 7343244
90 Z = 2238221
05
XDOT = 8239
753398 XDOT = 2511
476836
YDOT = -14150
359999 feet/sec YDOT = -4313
029728 meter/sec
ZDOT = -17929
061654 ZDOT = -5464
777992
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 11051
53623583
00016717 00000-0 10270-3 0 9066
2 25544 51
6424 39
1294 0004977 335
8731 24
2198 15
72580224 22544
Satellite: ISS
Catalog Number: 25544
Epoch time: 11051
53623583 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 39
1294 deg
Eccentricity:
0004977
Arg of perigee: 335
8731 deg
Mean anomaly: 24
2198 deg
Mean motion: 15
72580224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 304
Coasting Arc #8 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2011/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 853614
50 A = 6727118
64 meter
Y = 4870917
84 meter E =
0006024
Z = 4555051
06 I = 51
82346
XDOT = -6863
522128 Wp = 79
77867
YDOT = -1670
018975 meter/sec RA = 33
65473 deg
ZDOT = 3069
676864 TA = 339
74507
MA = 339
76896
Ha = 192
431 n
mi
Hp = 186
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2800572
52 X = 776956
27
Y = 15980701
58 feet Y = 4880035
23 meter
Z = 14944393
25 Z = 4559011
26
XDOT = -22518
117217 XDOT = -6859
249244
YDOT = -5479
064879 feet/sec YDOT = -1746
746891 meter/sec
ZDOT = 10071
118319 ZDOT = 3036
344929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5569306
57 X = -1697524
64
Y = 15222847
44 feet Y = 4639923
90 meter
Z = 14960235
94 Z = 4559879
91
XDOT = -15780
752685 XDOT = -4809
973418
YDOT = -15546
227830 feet/sec YDOT = -4738
490243 meter/sec
ZDOT = 9936
597065 ZDOT = 3028
674785
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 11052
55299132
00016717 00000-0 10270-3 0 9079
2 25544 51
6425 33
9195 0004928 338
1715 21
9237 15
72601385 22709
Satellite: ISS
Catalog Number: 25544
Epoch time: 11052
55299132 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 33
9195 deg
Eccentricity:
0004928
Arg of perigee: 338
1715 deg
Mean anomaly: 21
9237 deg
Mean motion: 15
72601385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 302
Coasting Arc #9 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2011/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5971105
52 A = 6732182
85 meter
Y = 499376
91 meter E =
0006824
Z = -3064041
21 I = 51
81436
XDOT = 2063
686719 Wp = 25
13108
YDOT = 5535
853837 meter/sec RA = 28
49598 deg
ZDOT = 4933
919536 TA = 299
47209
MA = 299
54015
Ha = 192
681 n
mi
Hp = 186
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19590241
20 X = 5979961
96
Y = 1638375
68 feet Y = 566198
76 meter
Z = -10052628
64 Z = -3035012
50
XDOT = 6770
625719 XDOT = 1977
662611
YDOT = 18162
250122 feet/sec YDOT = 5558
450545 meter/sec
ZDOT = 16187
400052 ZDOT = 4943
735501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16442060
72 X = 5011540
11
Y = 10884053
87 feet Y = 3317459
62 meter
Z = -9935450
58 Z = -3028325
34
XDOT = -2087
406285 XDOT = -636
241436
YDOT = 17935
527048 feet/sec YDOT = 5466
748644 meter/sec
ZDOT = 16226
855734 ZDOT = 4945
945628
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 11053
50618270
00016717 00000-0 10270-3 0 9084
2 25544 51
6427 29
0350 0004942 344
0608 16
0399 15
72597990 22859
Satellite: ISS
Catalog Number: 25544
Epoch time: 11053
50618270 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 29
0350 deg
Eccentricity:
0004942
Arg of perigee: 344
0608 deg
Mean anomaly: 16
0399 deg
Mean motion: 15
72597990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 307
Coasting Arc #10 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2011/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2706289
81 A = 6728863
17 meter
Y = -4650255
22 meter E =
0009405
Z = -4051216
03 I = 51
77714
XDOT = 6619
530189 Wp = 38
92971
YDOT = -465
817608 meter/sec RA = 23
43156 deg
ZDOT = -3884
972669 TA = 191
03603
MA = 191
05667
Ha = 192
616 n
mi
Hp = 186
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8878903
59 X = -2634408
83
Y = -15256742
86 feet Y = -4680116
84 meter
Z = -13291391
17 Z = -4064188
23
XDOT = 21717
618729 XDOT = 6643
119309
YDOT = -1528
272991 feet/sec YDOT = -391
662274 meter/sec
ZDOT = -12745
973325 ZDOT = -3852
758118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -682525
83 X = -208033
87
Y = -17599614
96 feet Y = -5364362
64 meter
Z = -13343609
80 Z = -4067132
27
XDOT = 18714
944325 XDOT = 5704
315030
YDOT = 8845
008384 feet/sec YDOT = 2695
958556 meter/sec
ZDOT = -12615
905281 ZDOT = -3845
327930
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 11054
52290066
00016717 00000-0 10270-3 0 9097
2 25544 51
6434 23
8242 0004965 347
5864 12
5173 15
72646636 23018
Satellite: ISS
Catalog Number: 25544
Epoch time: 11054
52290066 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 23
8242 deg
Eccentricity:
0004965
Arg of perigee: 347
5864 deg
Mean anomaly: 12
5173 deg
Mean motion: 15
72646636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 299
Coasting Arc #11 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2011/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5469659
26 A = 6730070
38 meter
Y = 1270851
87 meter E =
0012519
Z = 3705685
86 I = 51
75274
XDOT = -4070
074613 Wp = 60
47706
YDOT = -4916
370825 meter/sec RA = 18
26450 deg
ZDOT = -4304
556138 TA = 74
98826
MA = 74
84973
Ha = 192
714 n
mi
Hp = 185
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17945076
31 X = -5501464
92
Y = 4169461
52 feet Y = 1209509
08 meter
Z = 12157762
01 Z = 3679037
39
XDOT = -13353
263165 XDOT = -3993
885899
YDOT = -16129
825542 feet/sec YDOT = -4961
458963 meter/sec
ZDOT = -14122
559509 ZDOT = -4324
143081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17964762
27 X = -5475659
54
Y = -4391223
68 feet Y = -1338444
98 meter
Z = 12050137
82 Z = 3672882
01
XDOT = -4902
562592 XDOT = -1494
301078
YDOT = -19067
623032 feet/sec YDOT = -5811
811500 meter/sec
ZDOT = -14201
468037 ZDOT = -4328
607458
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 11055
53959837
00016717 00000-0 10270-3 0 9109
2 25544 51
6434 18
6141 0005065 350
2727 9
8337 15
72683770 23177
Satellite: ISS
Catalog Number: 25544
Epoch time: 11055
53959837 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 18
6141 deg
Eccentricity:
0005065
Arg of perigee: 350
2727 deg
Mean anomaly: 9
8337 deg
Mean motion: 15
72683770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 310
Coasting Arc #12 (Orbit 2332)
---------------------------------------
Vector Time (GMT): 2011/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4333218
82 A = 6730528
29 meter
Y = 3811353
90 meter E =
0012580
Z = 3449060
75 I = 51
72638
XDOT = -5729
205984 Wp = 68
61184
YDOT = 2364
779342 meter/sec RA = 13
19811 deg
ZDOT = 4575
892029 TA = 332
19258
MA = 332
25977
Ha = 192
547 n
mi
Hp = 185
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14216597
17 X = 4273522
89
Y = 12504441
93 feet Y = 3859476
84 meter
Z = 11315816
11 Z = 3469966
07
XDOT = -18796
607560 XDOT = -5777
452016
YDOT = 7758
462409 feet/sec YDOT = 2300
442198 meter/sec
ZDOT = 15012
769123 ZDOT = 4547
942865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7301537
43 X = 2225508
61
Y = 17413962
26 feet Y = 5307775
70 meter
Z = 11400081
88 Z = 3474744
96
XDOT = -19110
954984 XDOT = -5825
019079
YDOT = -1759
911642 feet/sec YDOT = -536
421069 meter/sec
ZDOT = 14899
855039 ZDOT = 4541
475816
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 11056
55627515
00016717 00000-0 10270-3 0 9118
2 25544 51
6441 13
4039 0004899 353
3137 6
7960 15
72736045 23337
Satellite: ISS
Catalog Number: 25544
Epoch time: 11056
55627515 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 13
4039 deg
Eccentricity:
0004899
Arg of perigee: 353
3137 deg
Mean anomaly: 6
7960 deg
Mean motion: 15
72736045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2333
Checksum: 299
Coasting Arc #13 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2011/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4421730
45 A = 6728060
40 meter
Y = -2769821
59 meter E =
0007823
Z = -4252736
44 I = 51
68751
XDOT = 5735
952022 Wp = 73
35734
YDOT = 3667
632303 meter/sec RA = 8
02674 deg
ZDOT = 3582
756717 TA = 233
01316
MA = 233
08479
Ha = 192
817 n
mi
Hp = 185
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14506989
66 X = 4473033
03
Y = -9087341
16 feet Y = -2720088
33 meter
Z = -13952547
38 Z = -4231131
53
XDOT = 18818
740231 XDOT = 5677
109579
YDOT = 12032
914379 feet/sec YDOT = 3731
446234 meter/sec
ZDOT = 11754
451170 ZDOT = 3610
478339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17056357
83 X = 5198777
87
Y = -2131229
68 feet Y = -649598
81 meter
Z = -13865230
41 Z = -4226122
23
XDOT = 11817
742085 XDOT = 3602
047787
YDOT = 17542
903704 feet/sec YDOT = 5347
077049 meter/sec
ZDOT = 11866
239580 ZDOT = 3616
829824
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 11057
50939308
00016717 00000-0 10270-3 0 9121
2 25544 51
6440 8
5186 0005073 357
0295 3
0837 15
72723168 23486
Satellite: ISS
Catalog Number: 25544
Epoch time: 11057
50939308 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 8
5186 deg
Eccentricity:
0005073
Arg of perigee: 357
0295 deg
Mean anomaly: 3
0837 deg
Mean motion: 15
72723168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 301
Coasting Arc #14 (Orbit 2363)
---------------------------------------
Vector Time (GMT): 2011/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5574811
79 A = 6732125
52 meter
Y = -2518496
55 meter E =
0005171
Z = -2818442
70 I = 51
67236
XDOT = 4303
618397 Wp = 54
25510
YDOT = -3818
360832 meter/sec RA = 2
95175 deg
ZDOT = -5104
017366 TA = 157
98166
MA = 157
95944
Ha = 192
783 n
mi
Hp = 185
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18290064
93 X = -5532544
04
Y = -8262783
95 feet Y = -2580601
20 meter
Z = -9246859
25 Z = -2845421
67
XDOT = 14119
482929 XDOT = 4370
789896
YDOT = -12527
430552 feet/sec YDOT = -3769
859715 meter/sec
ZDOT = -16745
463798 ZDOT = -5082
947711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13346637
91 X = -4068055
24
Y = -14921219
81 feet Y = -4547987
80 meter
Z = -9355690
00 Z = -2851614
31
XDOT = 16978
686415 XDOT = 5175
103619
YDOT = -4748
149391 feet/sec YDOT = -1447
235934 meter/sec
ZDOT = -16660
271823 ZDOT = -5078
050852
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 11058
52603111
00016717 00000-0 10270-3 0 9135
2 25544 51
6448 3
3075 0005099 1
1195 358
9978 15
72778348 23644
Satellite: ISS
Catalog Number: 25544
Epoch time: 11058
52603111 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 3
3075 deg
Eccentricity:
0005099
Arg of perigee: 1
1195 deg
Mean anomaly: 358
9978 deg
Mean motion: 15
72778348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2364
Checksum: 313
Coasting Arc #15 (Orbit 2379)
---------------------------------------
Vector Time (GMT): 2011/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3027776
93 A = 6726285
54 meter
Y = 3801013
72 meter E =
0011608
Z = 4647941
78 I = 51
62229
XDOT = -6875
363572 Wp = 41
52975
YDOT = -1986
100123 meter/sec RA = 357
78171 deg
ZDOT = -2841
991918 TA = 76
62173
MA = 76
49234
Ha = 192
893 n
mi
Hp = 185
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9933651
35 X = -3092633
75
Y = 12470517
44 feet Y = 3766792
84 meter
Z = 15249152
83 Z = 4633075
59
XDOT = -22556
967099 XDOT = -6838
838161
YDOT = -6516
076519 feet/sec YDOT = -2062
780491 meter/sec
ZDOT = -9324
120465 ZDOT = -2875
302637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14077326
82 X = -4290769
22
Y = 7605971
34 feet Y = 2318300
07 meter
Z = 15189008
06 Z = 4629609
66
XDOT = -17656
549473 XDOT = -5381
716279
YDOT = -13707
919115 feet/sec YDOT = -4178
173746 meter/sec
ZDOT = -9458
531736 ZDOT = -2882
960473
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 11059
54264889
00016717 00000-0 10270-3 0 9144
2 25544 51
6451 358
0970 0005050 4
8353 355
2857 15
72798018 23805
Satellite: ISS
Catalog Number: 25544
Epoch time: 11059
54264889 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 358
0970 deg
Eccentricity:
0005050
Arg of perigee: 4
8353 deg
Mean anomaly: 355
2857 deg
Mean motion: 15
72798018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2380
Checksum: 323
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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