[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 30th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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 2823)
---------------------------------------
Vector Time (GMT): 2011/087/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4622582
82 A = 6727474
46 meter
Y = -1446536
27 meter E =
0009090
Z = 4664612
94 I = 51
44335
XDOT = 4549
461975 Wp = 56
19411
YDOT = 5558
652620 meter/sec RA = 212
76188 deg
ZDOT = -2775
836636 TA = 61
30031
MA = 61
20897
Ha = 192
896 n
mi
Hp = 186
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15165954
13 X = 4615755
22
Y = -4745853
92 feet Y = -1394881
59 meter
Z = 15303848
23 Z = 4687052
60
XDOT = 14926
056347 XDOT = 4500
450232
YDOT = 18237
049278 feet/sec YDOT = 5609
253222 meter/sec
ZDOT = -9107
075579 ZDOT = -2753
855160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3108755
99 X = -947548
83
Y = -15494581
02 feet Y = -4722748
29 meter
Z = 15394500
97 Z = 4692243
90
XDOT = 18601
914186 XDOT = 5669
863444
YDOT = -12720
956568 feet/sec YDOT = -3877
347562 meter/sec
ZDOT = -9018
341597 ZDOT = -2748
790519
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 11087
76203218
00016717 00000-0 10270-3 0 9003
2 25544 51
6433 213
5753 0001588 21
6259 338
4970 15
72291953 28241
Satellite: ISS
Catalog Number: 25544
Epoch time: 11087
76203218 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 213
5753 deg
Eccentricity:
0001588
Arg of perigee: 21
6259 deg
Mean anomaly: 338
4970 deg
Mean motion: 15
72291953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 308
Coasting Arc #2 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2011/088/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4839706
68 A = 6735549
24 meter
Y = -4260966
64 meter E =
0015700
Z = 1919054
30 I = 51
49641
XDOT = 4565
295344 Wp = 63
16229
YDOT = -2645
930773 meter/sec RA = 207
66573 deg
ZDOT = 5610
224238 TA = 318
21469
MA = 318
33447
Ha = 193
218 n
mi
Hp = 186
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15878302
76 X = -4801022
32
Y = -13979549
34 feet Y = -4314870
70 meter
Z = 6296109
91 Z = 1895637
71
XDOT = 14978
003098 XDOT = 4567
290301
YDOT = -8680
875240 feet/sec YDOT = -2594
867211 meter/sec
ZDOT = 18406
247499 ZDOT = 5632
407185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15349769
51 X = -4678609
75
Y = 14598445
09 feet Y = 4449606
06 meter
Z = 6201554
24 Z = 1890233
73
XDOT = -6247
857361 XDOT = -1904
346924
YDOT = -14466
551407 feet/sec YDOT = -4409
404869 meter/sec
ZDOT = 18495
879367 ZDOT = 5637
544031
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 11088
77897546
00016717 00000-0 10270-3 0 9019
2 25544 51
6432 208
3660 0001922 30
9366 329
1909 15
72273751 28406
Satellite: ISS
Catalog Number: 25544
Epoch time: 11088
77897546 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 208
3660 deg
Eccentricity:
0001922
Arg of perigee: 30
9366 deg
Mean anomaly: 329
1909 deg
Mean motion: 15
72273751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 319
Coasting Arc #3 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2011/089/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3225050
11 A = 6725689
40 meter
Y = 3034487
09 meter E =
0014377
Z = -5074833
23 I = 51
49288
XDOT = -6343
130477 Wp = 95
46255
YDOT = -4027
481532 meter/sec RA = 202
50189 deg
ZDOT = 1625
427183 TA = 190
19881
MA = 190
22802
Ha = 193
062 n
mi
Hp = 185
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10580873
05 X = -3234090
32
Y = 9955666
30 feet Y = 2998371
54 meter
Z = -16649715
31 Z = -5090522
59
XDOT = -20810
795529 XDOT = -6305
518907
YDOT = -13213
522086 feet/sec YDOT = -4098
203797 meter/sec
ZDOT = 5332
766347 ZDOT = 1594
704431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9168937
48 X = 2794692
14
Y = 11175211
36 feet Y = 3406204
42 meter
Z = -16713121
27 Z = -5094159
36
XDOT = -13874
681401 XDOT = -4229
002891
YDOT = 19160
922189 feet/sec YDOT = 5840
249083 meter/sec
ZDOT = 5208
682446 ZDOT = 1587
606410
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 11089
73232870
00016717 00000-0 10270-3 0 9020
2 25544 51
6444 203
4824 0001826 29
4525 330
6740 15
72333449 28557
Satellite: ISS
Catalog Number: 25544
Epoch time: 11089
73232870 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 203
4824 deg
Eccentricity:
0001826
Arg of perigee: 29
4525 deg
Mean anomaly: 330
6740 deg
Mean motion: 15
72333449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 301
Coasting Arc #4 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2011/090/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6102541
70 A = 6736384
44 meter
Y = 2687497
69 meter E =
0009779
Z = -932805
27 I = 51
55797
XDOT = -2700
928813 Wp = 130
68134
YDOT = 4089
736875 meter/sec RA = 197
39276 deg
ZDOT = -5933
732168 TA = 59
50693
MA = 59
41040
Ha = 193
066 n
mi
Hp = 185
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20021462
26 X = 6076567
39
Y = 8817249
63 feet Y = 2755594
68 meter
Z = -3060384
75 Z = -903222
79
XDOT = -8861
315002 XDOT = -2717
635551
YDOT = 13417
771901 feet/sec YDOT = 4059
439368 meter/sec
ZDOT = -19467
625223 ZDOT = -5946
894201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9912448
91 X = 3021314
43
Y = -19520843
55 feet Y = -5949953
11 meter
Z = -2940887
74 Z = -896382
58
XDOT = 11489
096046 XDOT = 3501
876475
YDOT = 8750
844345 feet/sec YDOT = 2667
257356 meter/sec
ZDOT = -19520
830003 ZDOT = -5949
948985
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 11090
74921130
00016717 00000-0 10270-3 0 9038
2 25544 51
6442 198
2729 0001929 35
6699 324
4592 15
72399097 28710
Satellite: ISS
Catalog Number: 25544
Epoch time: 11090
74921130 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 198
2729 deg
Eccentricity:
0001929
Arg of perigee: 35
6699 deg
Mean anomaly: 324
4592 deg
Mean motion: 15
72399097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 332
Coasting Arc #5 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2011/091/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1417203
80 A = 6724572
17 meter
Y = -3955846
50 meter E =
0004544
Z = 5246923
48 I = 51
54759
XDOT = 7419
576070 Wp = 56
85654
YDOT = 2007
424958 meter/sec RA = 192
25059 deg
ZDOT = -487
823370 TA = 37
79854
MA = 37
76664
Ha = 192
976 n
mi
Hp = 185
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4649618
77 X = 1435845
02
Y = -12978499
02 feet Y = -3939893
64 meter
Z = 17214315
89 Z = 5253853
96
XDOT = 24342
441174 XDOT = 7398
946966
YDOT = 6586
039887 feet/sec YDOT = 2090
279759 meter/sec
ZDOT = -1600
470373 ZDOT = -451
829589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12794919
74 X = -3899891
54
Y = -5038318
97 feet Y = -1535679
62 meter
Z = 17242344
22 Z = 5255466
52
XDOT = 7142
776127 XDOT = 2177
118163
YDOT = -23149
586146 feet/sec YDOT = -7055
993857 meter/sec
ZDOT = -1455
057078 ZDOT = -443
501397
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 11091
76606399
00016717 00000-0 10270-3 0 9049
2 25544 51
6435 193
0635 0002063 38
6293 321
5017 15
72451993 28875
Satellite: ISS
Catalog Number: 25544
Epoch time: 11091
76606399 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 193
0635 deg
Eccentricity:
0002063
Arg of perigee: 38
6293 deg
Mean anomaly: 321
5017 deg
Mean motion: 15
72451993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 318
Coasting Arc #6 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2011/092/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6684191
19 A = 6736406
70 meter
Y = -777809
62 meter E =
0014086
Z = -72570
44 I = 51
61889
XDOT = 495
579046 Wp = 44
16952
YDOT = -4755
688543 meter/sec RA = 187
12681 deg
ZDOT = 6035
489094 TA = 315
04227
MA = 315
15624
Ha = 192
921 n
mi
Hp = 185
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21929761
13 X = -6674644
26
Y = -2551868
85 feet Y = -852502
93 meter
Z = -238092
00 Z = -105018
95
XDOT = 1625
915504 XDOT = 519
401922
YDOT = -15602
652699 feet/sec YDOT = -4750
012802 meter/sec
ZDOT = 19801
473404 ZDOT = 6037
955012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3010813
27 X = -917695
88
Y = 21869655
75 feet Y = 6665871
07 meter
Z = -369197
17 Z = -112531
30
XDOT = -13972
089058 XDOT = -4258
692745
YDOT = -1614
456149 feet/sec YDOT = -492
086234 meter/sec
ZDOT = 19811
469686 ZDOT = 6038
535960
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 11092
71933669
00016717 00000-0 10270-3 0 9059
2 25544 51
6442 188
1803 0002064 40
1623 319
9692 15
72512462 29028
Satellite: ISS
Catalog Number: 25544
Epoch time: 11092
71933669 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 188
1803 deg
Eccentricity:
0002064
Arg of perigee: 40
1623 deg
Mean anomaly: 319
9692 deg
Mean motion: 15
72512462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 301
Coasting Arc #7 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2011/093/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 536908
18 A = 6724472
92 meter
Y = 4182739
21 meter E =
0016411
Z = -5251963
89 I = 51
60863
XDOT = -7659
210412 Wp = 80
13511
YDOT = 215
429928 meter/sec RA = 182
00717 deg
ZDOT = -610
286657 TA = 184
04425
MA = 184
05752
Ha = 192
961 n
mi
Hp = 185
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1761509
77 X = 515609
27
Y = 13722897
68 feet Y = 4188623
62 meter
Z = -17230852
67 Z = -5249407
75
XDOT = -25128
643084 XDOT = -7658
085464
YDOT = 706
791102 feet/sec YDOT = 129
786218 meter/sec
ZDOT = -2002
252811 ZDOT = -647
492518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13729110
68 X = 4184632
94
Y = -1813050
34 feet Y = -552617
74 meter
Z = -17220554
27 Z = -5248824
94
XDOT = 480
206769 XDOT = 146
367023
YDOT = 24117
546628 feet/sec YDOT = 7351
028212 meter/sec
ZDOT = -2152
596748 ZDOT = -656
111489
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 11093
73613197
00016717 00000-0 10270-3 0 9064
2 25544 51
6436 182
9702 0002132 40
6490 319
4832 15
72518587 29186
Satellite: ISS
Catalog Number: 25544
Epoch time: 11093
73613197 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 182
9702 deg
Eccentricity:
0002132
Arg of perigee: 40
6490 deg
Mean anomaly: 319
4832 deg
Mean motion: 15
72518587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2918
Checksum: 314
Coasting Arc #8 (Orbit 2933)
---------------------------------------
Vector Time (GMT): 2011/094/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6561618
25 A = 6735762
13 meter
Y = -1132959
63 meter E =
0014322
Z = 977643
32 I = 51
67682
XDOT = 1688
507588 Wp = 115
21886
YDOT = 4605
230176 meter/sec RA = 176
86778 deg
ZDOT = -5934
406058 TA = 54
11056
MA = 53
97769
Ha = 192
945 n
mi
Hp = 185
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21527618
94 X = 6569050
30
Y = -3717059
17 feet Y = -1059542
00 meter
Z = 3207491
20 Z = 1009538
02
XDOT = 5539
723058 XDOT = 1665
713998
YDOT = 15109
022887 feet/sec YDOT = 4623
984119 meter/sec
ZDOT = -19469
836147 ZDOT = -5926
259009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4005826
26 X = -1220975
84
Y = -21456112
45 feet Y = -6539823
07 meter
Z = 3336390
34 Z = 1016931
78
XDOT = 13466
206850 XDOT = 4104
499848
YDOT = -5566
671240 feet/sec YDOT = -1696
721394 meter/sec
ZDOT = -19436
949987 ZDOT = -5924
382356
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 11094
75289794
00016717 00000-0 10270-3 0 9070
2 25544 51
6424 177
7598 0002341 44
0884 316
0465 15
72584223 29348
Satellite: ISS
Catalog Number: 25544
Epoch time: 11094
75289794 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 177
7598 deg
Eccentricity:
0002341
Arg of perigee: 44
0884 deg
Mean anomaly: 316
0465 deg
Mean motion: 15
72584223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2934
Checksum: 332
Coasting Arc #9 (Orbit 2949)
---------------------------------------
Vector Time (GMT): 2011/095/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2367989
99 A = 6724971
53 meter
Y = -3713472
48 meter E =
0005938
Z = 5077484
95 I = 51
67021
XDOT = 7157
643270 Wp = 102
99501
YDOT = -2335
325192 meter/sec RA = 171
76861 deg
ZDOT = 1627
249978 TA = 331
36607
MA = 331
39866
Ha = 192
974 n
mi
Hp = 185
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7768996
03 X = -2350954
95
Y = -12183308
67 feet Y = -3739857
17 meter
Z = 16658415
20 Z = 5066022
80
XDOT = 23483
081593 XDOT = 7175
320391
YDOT = -7661
828059 feet/sec YDOT = -2255
185130 meter/sec
ZDOT = 5338
746646 ZDOT = 1662
065201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11935777
21 X = -3638024
90
Y = 8238181
00 feet Y = 2510997
57 meter
Z = 16612125
17 Z = 5063375
75
XDOT = -7775
932667 XDOT = -2370
104277
YDOT = -22334
536920 feet/sec YDOT = -6807
566853 meter/sec
ZDOT = 5479
471389 ZDOT = 1670
142879
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 11095
76963454
00016717 00000-0 10270-3 0 9085
2 25544 51
6414 172
5492 0002339 44
5199 315
6151 15
72613169 29501
Satellite: ISS
Catalog Number: 25544
Epoch time: 11095
76963454 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 172
5492 deg
Eccentricity:
0002339
Arg of perigee: 44
5199 deg
Mean anomaly: 315
6151 deg
Mean motion: 15
72613169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2950
Checksum: 320
Coasting Arc #10 (Orbit 2964)
---------------------------------------
Vector Time (GMT): 2011/096/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5801795
61 A = 6734398
42 meter
Y = 2873736
50 meter E =
0009559
Z = -1841919
24 I = 51
73266
XDOT = -3638
099332 Wp = 41
97728
YDOT = -3728
668815 meter/sec RA = 166
61824 deg
ZDOT = 5665
915188 TA = 297
62611
MA = 297
72313
Ha = 192
839 n
mi
Hp = 185
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19034762
50 X = -5824551
28
Y = 9428269
35 feet Y = 2808729
97 meter
Z = -6043042
13 Z = -1870160
03
XDOT = -11936
021431 XDOT = -3623
658486
YDOT = -12233
165403 feet/sec YDOT = -3769
271213 meter/sec
ZDOT = 18588
960590 ZDOT = 5648
276418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10325996
03 X = 3147363
59
Y = 18525531
22 feet Y = 5646581
92 meter
Z = -6157215
57 Z = -1876719
30
XDOT = -10291
242072 XDOT = -3136
770584
YDOT = 11865
393255 feet/sec YDOT = 3616
571864 meter/sec
ZDOT = 18517
705670 ZDOT = 5644
196688
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 11096
72279802
00016717 00000-0 10270-3 0 9090
2 25544 51
6411 167
6652 0002447 49
8783 310
2593 15
72680867 29654
Satellite: ISS
Catalog Number: 25544
Epoch time: 11096
72279802 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 167
6652 deg
Eccentricity:
0002447
Arg of perigee: 49
8783 deg
Mean anomaly: 310
2593 deg
Mean motion: 15
72680867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2965
Checksum: 338
Coasting Arc #11 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2011/097/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3876394
94 A = 6725997
21 meter
Y = 2698752
53 meter E =
0013914
Z = -4801575
39 I = 51
73311
XDOT = -5988
689205 Wp = 68
34973
YDOT = 4103
183482 meter/sec RA = 161
53529 deg
ZDOT = -2529
373091 TA = 176
87903
MA = 176
87034
Ha = 192
858 n
mi
Hp = 185
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12717831
17 X = 3869254
23
Y = 8854174
95 feet Y = 2742060
63 meter
Z = -15753200
08 Z = -4782761
16
XDOT = -19647
930464 XDOT = -6021
839359
YDOT = 13461
888065 feet/sec YDOT = 4036
028889 meter/sec
ZDOT = -8298
468145 ZDOT = -2558
547021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8001917
92 X = 2438984
58
Y = -13360326
70 feet Y = -4072227
58 meter
Z = -15677178
85 Z = -4778404
11
XDOT = 13732
857282 XDOT = 4185
774899
YDOT = 18097
835827 feet/sec YDOT = 5516
220360 meter/sec
ZDOT = -8416
442936 ZDOT = -2565
331807
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 11097
73947824
00016717 00000-0 10270-3 0 9100
2 25544 51
6404 162
4533 0002467 49
7249 310
4129 15
72698024 29814
Satellite: ISS
Catalog Number: 25544
Epoch time: 11097
73947824 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 162
4533 deg
Eccentricity:
0002467
Arg of perigee: 49
7249 deg
Mean anomaly: 310
4129 deg
Mean motion: 15
72698024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 318
Coasting Arc #12 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2011/098/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4579749
32 A = 6732765
96 meter
Y = -4207046
90 meter E =
0015339
Z = 2564654
25 I = 51
78531
XDOT = 5099
583414 Wp = 95
70237
YDOT = 2312
881937 meter/sec RA = 156
37629 deg
ZDOT = -5286
935350 TA = 55
26919
MA = 55
12483
Ha = 192
719 n
mi
Hp = 184
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15025424
29 X = 4613994
26
Y = -13802647
31 feet Y = -4155641
84 meter
Z = 8414219
99 Z = 2586986
06
XDOT = 16730
916711 XDOT = 5099
024414
YDOT = 7588
195332 feet/sec YDOT = 2369
905328 meter/sec
ZDOT = -17345
588420 ZDOT = -5262
162864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14986022
41 X = -4567739
63
Y = -13790114
18 feet Y = -4203226
80 meter
Z = 8504553
44 Z = 2592187
89
XDOT = 5173
051459 XDOT = 1576
746085
YDOT = -16308
118645 feet/sec YDOT = -4970
714563 meter/sec
ZDOT = -17245
468880 ZDOT = -5256
418915
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 11098
75612856
00016717 00000-0 10270-3 0 9118
2 25544 51
6402 157
2421 0002517 48
2029 311
9348 15
72769571 29978
Satellite: ISS
Catalog Number: 25544
Epoch time: 11098
75612856 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 157
2421 deg
Eccentricity:
0002517
Arg of perigee: 48
2029 deg
Mean anomaly: 311
9348 deg
Mean motion: 15
72769571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 320
Coasting Arc #13 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2011/099/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4913534
56 A = 6727177
15 meter
Y = -1266439
72 meter E =
0010853
Z = 4408698
69 I = 51
79462
XDOT = 4384
678499 Wp = 99
80595
YDOT = -5387
929734 meter/sec RA = 151
30733 deg
ZDOT = 3330
307640 TA = 316
77458
MA = 316
85970
Ha = 192
773 n
mi
Hp = 184
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16120520
22 X = -4920424
50
Y = -4154985
97 feet Y = -1321424
29 meter
Z = 14464234
56 Z = 4384812
00
XDOT = 14385
428146 XDOT = 4428
423420
YDOT = -17676
934824 feet/sec YDOT = -5338
652952 meter/sec
ZDOT = 10926
206167 ZDOT = 3351
714786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2524603
20 X = -769499
06
Y = 16539211
72 feet Y = 5041151
73 meter
Z = 14367672
61 Z = 4379266
61
XDOT = -17804
951361 XDOT = -5426
949175
YDOT = -12309
725476 feet/sec YDOT = -3752
004325 meter/sec
ZDOT = 11012
831553 ZDOT = 3356
711057
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 11099
77275008
00016717 00000-0 10270-3 0 9126
2 25544 51
6404 152
0314 0002388 52
1486 307
9893 15
72826219 30134
Satellite: ISS
Catalog Number: 25544
Epoch time: 11099
77275008 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 152
0314 deg
Eccentricity:
0002388
Arg of perigee: 52
1486 deg
Mean anomaly: 307
9893 deg
Mean motion: 15
72826219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 304
Coasting Arc #14 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2011/100/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3024951
47 A = 6730966
78 meter
Y = 5078931
44 meter E =
0007074
Z = -3222223
17 I = 51
83401
XDOT = -5988
150959 Wp = 73
26404
YDOT = -527
063641 meter/sec RA = 146
14418 deg
ZDOT = 4801
410326 TA = 249
23838
MA = 249
31419
Ha = 192
739 n
mi
Hp = 184
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9924381
47 X = -3065867
28
Y = 16663160
90 feet Y = 5044875
76 meter
Z = -10571598
32 Z = -3237017
83
XDOT = -19646
164564 XDOT = -6005
136512
YDOT = -1729
211420 feet/sec YDOT = -594
121653 meter/sec
ZDOT = 15752
658551 ZDOT = 4772
278706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17697243
32 X = 5394119
77
Y = 7854416
92 feet Y = 2394026
28 meter
Z = -10631494
87 Z = -3240479
64
XDOT = 1153
623424 XDOT = 351
624420
YDOT = 18516
610015 feet/sec YDOT = 5643
862732 meter/sec
ZDOT = 15634
866647 ZDOT = 4765
507354
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 11100
72580819
00016717 00000-0 10270-3 0 9134
2 25544 51
6405 147
1454 0002636 55
1208 305
0202 15
72822906 30284
Satellite: ISS
Catalog Number: 25544
Epoch time: 11100
72580819 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 147
1454 deg
Eccentricity:
0002636
Arg of perigee: 55
1208 deg
Mean anomaly: 305
0202 deg
Mean motion: 15
72822906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 272
Coasting Arc #15 (Orbit 3043)
---------------------------------------
Vector Time (GMT): 2011/101/17:15:31
808
Vector Time (MET): N/A
Weight (LBS) : 877946
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5418919
78 A = 6728565
89 meter
Y = -354466
16 meter E =
0009458
Z = -3982934
22 I = 51
85203
XDOT = -2530
745737 Wp = 68
76234
YDOT = 6068
791136 meter/sec RA = 141
08210 deg
ZDOT = -3987
475492 TA = 160
00511
MA = 159
96803
Ha = 192
683 n
mi
Hp = 184
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17778608
21 X = 5441829
02
Y = -1162946
71 feet Y = -293740
53 meter
Z = -13067369
49 Z = -3956553
58
XDOT = -8302
971577 XDOT = -2579
049684
YDOT = 19910
732073 feet/sec YDOT = 6040
220603 meter/sec
ZDOT = -13082
268675 ZDOT = -3999
887303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3536275
19 X = -1077856
68
Y = -17541468
06 feet Y = -5346639
46 meter
Z = -12960677
31 Z = -3950414
45
XDOT = 19550
600432 XDOT = 5959
023012
YDOT = 5751
515869 feet/sec YDOT = 1753
062037 meter/sec
ZDOT = -13132
552460 ZDOT = -4002
801990
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 11101
74237451
00016717 00000-0 10270-3 0 9149
2 25544 51
6414 141
9334 0002646 57
7244 302
4175 15
72891690 30446
Satellite: ISS
Catalog Number: 25544
Epoch time: 11101
74237451 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 141
9334 deg
Eccentricity:
0002646
Arg of perigee: 57
7244 deg
Mean anomaly: 302
4175 deg
Mean motion: 15
72891690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3044
Checksum: 289
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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