[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 11th 2012
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) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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 3810)
---------------------------------------
Vector Time (GMT): 2012/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5722968
05 A = 6771684
52 meter
Y = -1863544
93 meter E =
0028179
Z = 3104570
14 I = 51
87970
XDOT = -774
039240 Wp = 52
46635
YDOT = -5856
082601 meter/sec RA = 41
91191 deg
ZDOT = -4894
894017 TA = 91
89254
MA = 91
56979
Ha = 220
469 n
mi
Hp = 201
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18776141
90 X = -5716785
19
Y = -6113992
55 feet Y = -1927507
89 meter
Z = 10185597
56 Z = 3076783
91
XDOT = -2539
498818 XDOT = -684
719988
YDOT = -19212
869425 feet/sec YDOT = -5864
239333 meter/sec
ZDOT = -16059
363573 ZDOT = -4898
436811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10260325
33 X = -3127347
16
Y = -16939750
49 feet Y = -5163235
95 meter
Z = 10071811
38 Z = 3069888
11
XDOT = 9475
592533 XDOT = 2888
160604
YDOT = -15389
017415 feet/sec YDOT = -4690
572508 meter/sec
ZDOT = -16073
408326 ZDOT = -4899
174858
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 12041
53843618
00016717 00000-0 10270-3 0 9003
2 25544 51
6388 42
3362 0020629 27
3635 332
8602 15
58831680 38110
Satellite: ISS
Catalog Number: 25544
Epoch time: 12041
53843618 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 42
3362 deg
Eccentricity:
0020629
Arg of perigee: 27
3635 deg
Mean anomaly: 332
8602 deg
Mean motion: 15
58831680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3811
Checksum: 297
Coasting Arc #2 (Orbit 3825)
---------------------------------------
Vector Time (GMT): 2012/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5432952
98 A = 6775598
07 meter
Y = 4018738
52 meter E =
0032303
Z = -66267
79 I = 51
87016
XDOT = -2788
022681 Wp = 36
22487
YDOT = 3843
842436 meter/sec RA = 36
93124 deg
ZDOT = 6048
608451 TA = 323
06087
MA = 323
28290
Ha = 220
413 n
mi
Hp = 201
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17824648
87 X = 5387932
76
Y = 13184837
67 feet Y = 4079241
43 meter
Z = -217414
02 Z = -39984
78
XDOT = -9147
056039 XDOT = -2860
180429
YDOT = 12611
031614 feet/sec YDOT = 3812
262013 meter/sec
ZDOT = 19844
515914 ZDOT = 6034
889028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5243630
40 X = 1598258
55
Y = 21542923
80 feet Y = 6566283
17 meter
Z = -109978
01 Z = -33521
30
XDOT = -13624
188966 XDOT = -4152
652797
YDOT = 3366
920711 feet/sec YDOT = 1026
237433 meter/sec
ZDOT = 19787
940400 ZDOT = 6031
364234
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 12042
50006721
00016717 00000-0 10270-3 0 9018
2 25544 51
6390 37
5092 0020433 31
4779 328
7594 15
58868518 38267
Satellite: ISS
Catalog Number: 25544
Epoch time: 12042
50006721 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 37
5092 deg
Eccentricity:
0020433
Arg of perigee: 31
4779 deg
Mean anomaly: 328
7594 deg
Mean motion: 15
58868518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3826
Checksum: 309
Coasting Arc #3 (Orbit 3841)
---------------------------------------
Vector Time (GMT): 2012/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3434233
33 A = 6771589
47 meter
Y = -4984491
16 meter E =
0022508
Z = -3068968
17 I = 51
83143
XDOT = 5782
447353 Wp = 45
48495
YDOT = -956
080369 meter/sec RA = 31
94745 deg
ZDOT = -4924
716771 TA = 169
62791
MA = 169
58140
Ha = 220
583 n
mi
Hp = 201
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11267169
73 X = -3363332
33
Y = -16353317
45 feet Y = -5022498
61 meter
Z = -10068793
20 Z = -3085478
83
XDOT = 18971
283968 XDOT = 5816
631561
YDOT = -3136
746619 feet/sec YDOT = -891
226618 meter/sec
ZDOT = -16157
207255 ZDOT = -4896
543142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1530022
91 X = 466350
98
Y = -19765622
23 feet Y = -6024561
66 meter
Z = -10136069
73 Z = -3089474
05
XDOT = 15378
322553 XDOT = 4687
312714
YDOT = 9405
265611 feet/sec YDOT = 2866
724958 meter/sec
ZDOT = -16041
607910 ZDOT = -4889
482091
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 12043
52579099
00016717 00000-0 10270-3 0 9025
2 25544 51
6387 32
3577 0020642 35
0223 325
2285 15
58846361 38429
Satellite: ISS
Catalog Number: 25544
Epoch time: 12043
52579099 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 32
3577 deg
Eccentricity:
0020642
Arg of perigee: 35
0223 deg
Mean anomaly: 325
2285 deg
Mean motion: 15
58846361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 308
Coasting Arc #4 (Orbit 3857)
---------------------------------------
Vector Time (GMT): 2012/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 197234
91 A = 6764795
28 meter
Y = 4522952
13 meter E =
0021753
Z = 5007688
21 I = 51
78245
XDOT = -7184
932777 Wp = 53
06184
YDOT = -1887
923427 meter/sec RA = 26
93029 deg
ZDOT = 1995
008361 TA = 17
70027
MA = 17
62460
Ha = 220
618 n
mi
Hp = 200
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 647096
16 X = 122317
72
Y = 14839081
78 feet Y = 4524739
02 meter
Z = 16429423
25 Z = 5008464
23
XDOT = -23572
614099 XDOT = -7172
978840
YDOT = -6193
974499 feet/sec YDOT = -1968
202867 meter/sec
ZDOT = 6545
303021 ZDOT = 1960
133741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8675673
48 X = -2644345
28
Y = 12052300
83 feet Y = 3673541
29 meter
Z = 16432217
26 Z = 5008539
82
XDOT = -13961
762121 XDOT = -4255
545094
YDOT = -18748
754894 feet/sec YDOT = -5714
620492 meter/sec
ZDOT = 6402
474766 ZDOT = 1951
474309
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 12044
55149766
00016717 00000-0 10270-3 0 9034
2 25544 51
6386 27
2077 0020581 38
3233 321
9380 15
58875841 38586
Satellite: ISS
Catalog Number: 25544
Epoch time: 12044
55149766 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 27
2077 deg
Eccentricity:
0020581
Arg of perigee: 38
3233 deg
Mean anomaly: 321
9380 deg
Mean motion: 15
58875841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3858
Checksum: 324
Coasting Arc #5 (Orbit 3872)
---------------------------------------
Vector Time (GMT): 2012/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3253361
24 A = 6764549
51 meter
Y = -3037087
78 meter E =
0029544
Z = -5114093
66 I = 51
75399
XDOT = 6327
272858 Wp = 64
88311
YDOT = 3973
698140 meter/sec RA = 21
88983 deg
ZDOT = 1685
119089 TA = 221
27353
MA = 221
49723
Ha = 220
697 n
mi
Hp = 200
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10673757
35 X = 3311923
60
Y = -9964198
75 feet Y = -3000379
32 meter
Z = -16778522
51 Z = -5098146
88
XDOT = 20758
769218 XDOT = 6274
182075
YDOT = 13037
067387 feet/sec YDOT = 4044
156780 meter/sec
ZDOT = 5528
605935 ZDOT = 1715
727336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14599513
73 X = 4449931
79
Y = -1505706
91 feet Y = -458939
47 meter
Z = -16712875
75 Z = -5094084
53
XDOT = 8645
807367 XDOT = 2635
242086
YDOT = 21800
896150 feet/sec YDOT = 6644
913146 meter/sec
ZDOT = 5653
756363 ZDOT = 1723
264939
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 12045
51308315
00016717 00000-0 10270-3 0 9049
2 25544 51
6389 22
3796 0020634 41
9999 318
2734 15
58873451 38735
Satellite: ISS
Catalog Number: 25544
Epoch time: 12045
51308315 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 22
3796 deg
Eccentricity:
0020634
Arg of perigee: 41
9999 deg
Mean anomaly: 318
2734 deg
Mean motion: 15
58873451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3873
Checksum: 328
Coasting Arc #6 (Orbit 3888)
---------------------------------------
Vector Time (GMT): 2012/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5879318
10 A = 6771049
12 meter
Y = 881060
17 meter E =
0030745
Z = 3232940
27 I = 51
74753
XDOT = -3395
207593 Wp = 63
10303
YDOT = -4961
970249 meter/sec RA = 16
86511 deg
ZDOT = -4773
607482 TA = 79
42597
MA = 79
07978
Ha = 220
712 n
mi
Hp = 200
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19289101
39 X = -5904437
99
Y = 2890617
34 feet Y = 815173
55 meter
Z = 10606759
41 Z = 3204318
22
XDOT = -11139
132523 XDOT = -3316
280741
YDOT = -16279
429951 feet/sec YDOT = -4999
496240 meter/sec
ZDOT = -15661
441869 ZDOT = -4789
909303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17373907
15 X = -5295566
90
Y = -9002763
80 feet Y = -2744042
41 meter
Z = 10489329
84 Z = 3197147
74
XDOT = -59
981020 XDOT = -18
282215
YDOT = -18396
745492 feet/sec YDOT = -5607
328026 meter/sec
ZDOT = -15727
844718 ZDOT = -4793
847070
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 12046
53875725
00016717 00000-0 10270-3 0 9057
2 25544 51
6388 17
2285 0020646 45
5031 314
7807 15
58932502 38892
Satellite: ISS
Catalog Number: 25544
Epoch time: 12046
53875725 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 17
2285 deg
Eccentricity:
0020646
Arg of perigee: 45
5031 deg
Mean anomaly: 314
7807 deg
Mean motion: 15
58932502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 323
Coasting Arc #7 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2012/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6644201
53 A = 6775319
14 meter
Y = 1234779
35 meter E =
0032413
Z = -201149
44 I = 51
73286
XDOT = -712
230912 Wp = 47
13037
YDOT = 4711
703429 meter/sec RA = 11
87330 deg
ZDOT = 6031
067666 TA = 310
69795
MA = 310
97911
Ha = 220
680 n
mi
Hp = 200
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21798561
43 X = 6630877
28
Y = 4051113
35 feet Y = 1309004
41 meter
Z = -659939
11 Z = -168905
19
XDOT = -2336
715590 XDOT = -794
162188
YDOT = 15458
344582 feet/sec YDOT = 4703
280687 meter/sec
ZDOT = 19786
967407 ZDOT = 6027
408768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15562376
89 X = 4743412
48
Y = 15797408
84 feet Y = 4815050
22 meter
Z = -527843
61 Z = -160886
73
XDOT = -9708
669042 XDOT = -2959
202324
YDOT = 10138
025080 feet/sec YDOT = 3090
070044 meter/sec
ZDOT = 19771
549702 ZDOT = 6026
368349
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 12047
50031179
00016717 00000-0 10270-3 0 9063
2 25544 51
6389 12
4006 0020616 49
5384 310
7564 15
58959835 39045
Satellite: ISS
Catalog Number: 25544
Epoch time: 12047
50031179 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 12
4006 deg
Eccentricity:
0020616
Arg of perigee: 49
5384 deg
Mean anomaly: 310
7564 deg
Mean motion: 15
58959835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 312
Coasting Arc #8 (Orbit 3919)
---------------------------------------
Vector Time (GMT): 2012/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5284379
35 A = 6771343
10 meter
Y = -3022504
71 meter E =
0023472
Z = -2997038
22 I = 51
69092
XDOT = 4742
187177 Wp = 61
56432
YDOT = -3382
072832 meter/sec RA = 6
88034 deg
ZDOT = -4969
322069 TA = 152
69140
MA = 152
56780
Ha = 220
683 n
mi
Hp = 200
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17337202
60 X = -5235629
77
Y = -9916354
03 feet Y = -3081325
33 meter
Z = -9832802
55 Z = -3022590
46
XDOT = 15558
356881 XDOT = 4803
793010
YDOT = -11096
039476 feet/sec YDOT = -3328
698326 meter/sec
ZDOT = -16303
550095 ZDOT = -4946
135650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8803671
59 X = -2683359
10
Y = -17870144
03 feet Y = -5446819
90 meter
Z = -9937303
27 Z = -3028890
04
XDOT = 17881
836381 XDOT = 5450
383729
YDOT = 169
912969 feet/sec YDOT = 51
789473 meter/sec
ZDOT = -16208
184373 ZDOT = -4940
254597
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 12048
52595279
00016717 00000-0 10270-3 0 9073
2 25544 51
6398 7
2490 0020667 52
8800 307
4239 15
58984480 39204
Satellite: ISS
Catalog Number: 25544
Epoch time: 12048
52595279 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 7
2490 deg
Eccentricity:
0020667
Arg of perigee: 52
8800 deg
Mean anomaly: 307
4239 deg
Mean motion: 15
58984480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 331
Coasting Arc #9 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2012/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2154582
66 A = 6764390
71 meter
Y = 4013149
76 meter E =
0023327
Z = 4979575
64 I = 51
63820
XDOT = -7288
913881 Wp = 69
44696
YDOT = 1380
722019 meter/sec RA = 1
85353 deg
ZDOT = 2041
371514 TA =
77787
MA =
77425
Ha = 220
538 n
mi
Hp = 200
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7068840
76 X = 2085357
70
Y = 13166501
84 feet Y = 4036856
67 meter
Z = 16337190
41 Z = 4989874
00
XDOT = -23913
759452 XDOT = -7313
727914
YDOT = 4529
927885 feet/sec YDOT = 1299
074186 meter/sec
ZDOT = 6697
413104 ZDOT = 2005
902983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1308744
55 X = -398905
34
Y = 14840571
55 feet Y = 4523406
21 meter
Z = 16379062
70 Z = 4992338
31
XDOT = -21485
630992 XDOT = -6548
820327
YDOT = -9124
646804 feet/sec YDOT = -2781
192346 meter/sec
ZDOT = 6551
866423 ZDOT = 1997
008886
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 12049
55157517
00016717 00000-0 10270-3 0 9087
2 25544 51
6403 2
0990 0020433 56
6184 303
6923 15
59037169 39366
Satellite: ISS
Catalog Number: 25544
Epoch time: 12049
55157517 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 2
0990 deg
Eccentricity:
0020433
Arg of perigee: 56
6184 deg
Mean anomaly: 303
6923 deg
Mean motion: 15
59037169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 307
Coasting Arc #10 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2012/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1664452
80 A = 6764151
05 meter
Y = -4144380
09 meter E =
0031669
Z = -5104778
34 I = 51
60666
XDOT = 7410
834194 Wp = 76
29763
YDOT = 922
122079 meter/sec RA = 356
80078 deg
ZDOT = 1683
830241 TA = 209
90971
MA = 210
09104
Ha = 220
687 n
mi
Hp = 199
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5460803
14 X = 1735469
51
Y = -13597047
54 feet Y = -4125370
28 meter
Z = -16747960
45 Z = -5096520
09
XDOT = 24313
760478 XDOT = 7391
792625
YDOT = 3025
334906 feet/sec YDOT = 1004
888196 meter/sec
ZDOT = 5524
377431 ZDOT = 1719
784392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11914963
45 X = 3631680
86
Y = -8595276
52 feet Y = -2619840
28 meter
Z = -16713740
44 Z = -5094348
08
XDOT = 18374
709936 XDOT = 5600
611589
YDOT = 14545
604900 feet/sec YDOT = 4433
500373 meter/sec
ZDOT = 5671
711798 ZDOT = 1728
737756
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 12050
51308275
00016717 00000-0 10270-3 0 9095
2 25544 51
6405 357
2697 0020547 60
0609 300
2583 15
59015628 39512
Satellite: ISS
Catalog Number: 25544
Epoch time: 12050
51308275 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 357
2697 deg
Eccentricity:
0020547
Arg of perigee: 60
0609 deg
Mean anomaly: 300
2583 deg
Mean motion: 15
59015628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 301
Coasting Arc #11 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2012/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4984025
54 A = 6770776
82 meter
Y = 3274840
54 meter E =
0032370
Z = 3188525
09 I = 51
59956
XDOT = -5137
066657 Wp = 74
94967
YDOT = -3099
081250 meter/sec RA = 351
76543 deg
ZDOT = -4797
979001 TA = 68
06284
MA = 67
71907
Ha = 220
716 n
mi
Hp = 199
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16351789
82 X = -5035763
73
Y = 10744227
48 feet Y = 3218817
00 meter
Z = 10461040
32 Z = 3164187
76
XDOT = -16853
893230 XDOT = -5078
723490
YDOT = -10167
589402 feet/sec YDOT = -3156
201179 meter/sec
ZDOT = -15741
400921 ZDOT = -4822
792008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19603861
49 X = -5975256
98
Y = 769153
75 feet Y = 234438
06 meter
Z = 10360976
63 Z = 3158025
68
XDOT = -9083
047867 XDOT = -2768
512990
YDOT = -15911
313898 feet/sec YDOT = -4849
768476 meter/sec
ZDOT = -15842
866441 ZDOT = -4828
905691
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 12051
53867228
00016717 00000-0 10270-3 0 9108
2 25544 51
6412 352
1186 0020566 63
8469 296
4798 15
59061726 39674
Satellite: ISS
Catalog Number: 25544
Epoch time: 12051
53867228 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 352
1186 deg
Eccentricity:
0020566
Arg of perigee: 63
8469 deg
Mean anomaly: 296
4798 deg
Mean motion: 15
59061726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 336
Coasting Arc #12 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2012/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6562010
72 A = 6775004
49 meter
Y = -1637055
76 meter E =
0031946
Z = -114763
92 I = 51
58388
XDOT = 1234
197127 Wp = 58
67733
YDOT = 4612
876217 meter/sec RA = 346
76315 deg
ZDOT = 6018
451071 TA = 300
08187
MA = 300
39826
Ha = 220
671 n
mi
Hp = 199
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21528906
57 X = 6580386
39
Y = -5370917
85 feet Y = -1563572
57 meter
Z = -376522
04 Z = -82842
07
XDOT = 4049
203171 XDOT = 1153
287807
YDOT = 15134
108324 feet/sec YDOT = 4626
225875 meter/sec
ZDOT = 19745
574381 ZDOT = 6024
249682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21334326
20 X = 6502702
62
Y = 6104801
05 feet Y = 1860743
36 meter
Z = -245510
41 Z = -74831
57
XDOT = -3713
079718 XDOT = -1131
746698
YDOT = 13518
173255 feet/sec YDOT = 4120
339208 meter/sec
ZDOT = 19768
955155 ZDOT = 6025
577531
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 12052
50014664
00016717 00000-0 10270-3 0 9115
2 25544 51
6411 347
2904 0020520 67
3861 292
9462 15
59070332 39820
Satellite: ISS
Catalog Number: 25544
Epoch time: 12052
50014664 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 347
2904 deg
Eccentricity:
0020520
Arg of perigee: 67
3861 deg
Mean anomaly: 292
9462 deg
Mean motion: 15
59070332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 289
Coasting Arc #13 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2012/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5999372
13 A = 6770667
75 meter
Y = -618846
42 meter E =
0024501
Z = -3104354
90 I = 51
54158
XDOT = 3030
387672 Wp = 76
34989
YDOT = -5072
967670 meter/sec RA = 341
75900 deg
ZDOT = -4871
864795 TA = 139
41344
MA = 139
23053
Ha = 220
610 n
mi
Hp = 199
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19682979
44 X = -5976926
29
Y = -2030336
04 feet Y = -685809
91 meter
Z = -10184891
41 Z = -3133444
30
XDOT = 9942
216771 XDOT = 3110
555244
YDOT = -16643
594718 feet/sec YDOT = -5038
632242 meter/sec
ZDOT = -15983
808384 ZDOT = -4856
948447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16178170
32 X = -4931106
31
Y = -11285673
69 feet Y = -3439873
34 meter
Z = -10304092
96 Z = -3140687
53
XDOT = 16025
049827 XDOT = 4884
435187
YDOT = -8513
876055 feet/sec YDOT = -2595
029421 meter/sec
ZDOT = -15922
231476 ZDOT = -4853
096154
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 12053
52570200
00016717 00000-0 10270-3 0 9122
2 25544 51
6421 342
1387 0020550 71
2157 289
1225 15
59115611 39987
Satellite: ISS
Catalog Number: 25544
Epoch time: 12053
52570200 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 342
1387 deg
Eccentricity:
0020550
Arg of perigee: 71
2157 deg
Mean anomaly: 289
1225 deg
Mean motion: 15
59115611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 283
Coasting Arc #14 (Orbit 4013)
---------------------------------------
Vector Time (GMT): 2012/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3485989
68 A = 6763794
21 meter
Y = 2852430
14 meter E =
0024218
Z = 5024362
58 I = 51
49008
XDOT = -6145
733141 Wp = 84
47123
YDOT = 4245
515092 meter/sec RA = 336
71914 deg
ZDOT = 1848
400490 TA = 347
62176
MA = 347
68114
Ha = 220
420 n
mi
Hp = 199
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11436974
00 X = 3429427
41
Y = 9358366
60 feet Y = 2891096
91 meter
Z = 16484129
21 Z = 5041159
33
XDOT = -20163
166472 XDOT = -6201
729512
YDOT = 13928
855290 feet/sec YDOT = 4176
476819 meter/sec
ZDOT = 6064
306069 ZDOT = 1818
408933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5614837
72 X = 1711402
54
Y = 13586393
46 feet Y = 4141132
73 meter
Z = 16552746
77 Z = 5045277
22
XDOT = -23384
015268 XDOT = -7127
447854
YDOT = 2404
462954 feet/sec YDOT = 732
880308 meter/sec
ZDOT = 5941
007901 ZDOT = 1810
819208
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 12054
55123840
00016717 00000-0 10270-3 0 9131
2 25544 51
6418 336
9884 0020351 75
2195 285
1213 15
59163650 40140
Satellite: ISS
Catalog Number: 25544
Epoch time: 12054
55123840 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 336
9884 deg
Eccentricity:
0020351
Arg of perigee: 75
2195 deg
Mean anomaly: 285
1213 deg
Mean motion: 15
59163650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4014
Checksum: 295
Coasting Arc #15 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2012/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 10401
45 A = 6764053
28 meter
Y = -4555588
85 meter E =
0032523
Z = -5027711
63 I = 51
46346
XDOT = 7105
838866 Wp = 88
12167
YDOT = -2093
015091 meter/sec RA = 331
65507 deg
ZDOT = 1922
999292 TA = 200
54985
MA = 200
68097
Ha = 220
567 n
mi
Hp = 199
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 34125
49 X = 85765
28
Y = -14946157
63 feet Y = -4555051
70 meter
Z = -16495116
89 Z = -5027477
54
XDOT = 23313
119640 XDOT = 7119
373914
YDOT = -6866
847412 feet/sec YDOT = -2013
477325 meter/sec
ZDOT = 6309
052795 ZDOT = 1957
551678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6909713
38 X = 2106080
64
Y = -13254762
29 feet Y = -4040051
55 meter
Z = -16493780
99 Z = -5027304
45
XDOT = 22886
971619 XDOT = 6975
948950
YDOT = 3952
042157 feet/sec YDOT = 1204
582449 meter/sec
ZDOT = 6450
858211 ZDOT = 1966
221583
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 12055
51266515
00016717 00000-0 10270-3 0 9146
2 25544 51
6422 332
1590 0020438 78
4670 281
8779 15
59151498 40299
Satellite: ISS
Catalog Number: 25544
Epoch time: 12055
51266515 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 332
1590 deg
Eccentricity:
0020438
Arg of perigee: 78
4670 deg
Mean anomaly: 281
8779 deg
Mean motion: 15
59151498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 319
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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