[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 20th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13024 33 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 579)
---------------------------------------
Vector Time (GMT): 2011/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3417694
92 A = 6763636
17 meter
Y = -3723752
82 meter E =
0014918
Z = -4506278
98 I = 51
64710
XDOT = 6617
552073 Wp = 19
52382
YDOT = -2216
752361 meter/sec RA = 2
58844 deg
ZDOT = -3176
417235 TA = 218
53585
MA = 218
64244
Ha = 213
775 n
mi
Hp = 205
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11212909
85 X = -3353910
99
Y = -12217036
80 feet Y = -3761614
56 meter
Z = -14784379
86 Z = -4522727
15
XDOT = 21711
128847 XDOT = 6657
278507
YDOT = -7272
809583 feet/sec YDOT = -2142
528480 meter/sec
ZDOT = -10421
316389 ZDOT = -3144
173581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6328988
73 X = -1929075
77
Y = 15262907
51 feet Y = 4652134
21 meter
Z = -14850952
13 Z = -4526570
21
XDOT = -14727
557297 XDOT = -4488
959464
YDOT = -16153
527015 feet/sec YDOT = -4923
595034 meter/sec
ZDOT = -10290
195213 ZDOT = -3136
451501
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 11199
52161746
00016717 00000-0 10270-3 0 9000
2 25544 51
6387 2
9728 0011374 338
9720 21
0967 15
59982673 5801
Satellite: ISS
Catalog Number: 25544
Epoch time: 11199
52161746 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 2
9728 deg
Eccentricity:
0011374
Arg of perigee: 338
9720 deg
Mean anomaly: 21
0967 deg
Mean motion: 15
59982673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 580
Checksum: 325
Coasting Arc #2 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2011/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -753837
61 A = 6760743
49 meter
Y = 4195966
22 meter E =
0012522
Z = 5249190
14 I = 51
60611
XDOT = -7625
460170 Wp = 357
42814
YDOT = -324
174956 meter/sec RA = 357
52791 deg
ZDOT = -823
784667 TA = 100
51191
MA = 100
37080
Ha = 214
034 n
mi
Hp = 205
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2473220
49 X = -826200
80
Y = 13766293
37 feet Y = 4187131
38 meter
Z = 17221752
42 Z = 5245352
59
XDOT = -25017
913943 XDOT = -7617
266723
YDOT = -1063
566128 feet/sec YDOT = -409
401627 meter/sec
ZDOT = -2702
705599 ZDOT = -860
808550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13493810
48 X = 4112913
43
Y = -3753759
06 feet Y = -1144145
76 meter
Z = 17205893
78 Z = 5244356
42
XDOT = 9788
815864 XDOT = 2983
631075
YDOT = 21927
519111 feet/sec YDOT = 6683
507825 meter/sec
ZDOT = -2853
073240 ZDOT = -869
616724
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 11200
54659342
00016717 00000-0 10270-3 0 9010
2 25544 51
6382 357
8165 0011321 342
8771 17
2002 15
59937312 5969
Satellite: ISS
Catalog Number: 25544
Epoch time: 11200
54659342 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 357
8165 deg
Eccentricity:
0011321
Arg of perigee: 342
8771 deg
Mean anomaly: 17
2002 deg
Mean motion: 15
59937312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 293
Coasting Arc #3 (Orbit 610)
---------------------------------------
Vector Time (GMT): 2011/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4563504
51 A = 6766892
83 meter
Y = -3470384
22 meter E =
0010694
Z = -3586996
17 I = 51
59850
XDOT = 5607
963395 Wp = 13
16597
YDOT = 2804
606052 meter/sec RA = 352
47852 deg
ZDOT = 4434
013797 TA = 304
23924
MA = 304
34049
Ha = 214
099 n
mi
Hp = 204
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14972127
66 X = 4619396
55
Y = -11385775
01 feet Y = -3419039
60 meter
Z = -11768360
12 Z = -3564691
48
XDOT = 18398
830035 XDOT = 5554
645659
YDOT = 9201
463426 feet/sec YDOT = 2867
019317 meter/sec
ZDOT = 14547
289360 ZDOT = 4461
127518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16993524
53 X = -5179626
28
Y = -8194506
39 feet Y = -2497685
55 meter
Z = -11677541
21 Z = -3559314
56
XDOT = -758
779892 XDOT = -231
276111
YDOT = -19253
418096 feet/sec YDOT = -5868
441836 meter/sec
ZDOT = 14657
238156 ZDOT = 4467
526190
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 11201
50749491
00016717 00000-0 10270-3 0 9023
2 25544 51
6396 352
9840 0011328 346
0934 13
9908 15
60000240 6113
Satellite: ISS
Catalog Number: 25544
Epoch time: 11201
50749491 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 352
9840 deg
Eccentricity:
0011328
Arg of perigee: 346
0934 deg
Mean anomaly: 13
9908 deg
Mean motion: 15
60000240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 611
Checksum: 280
Coasting Arc #4 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2011/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6564319
60 A = 6772167
18 meter
Y = 1654605
98 meter E =
0007674
Z = 240646
74 I = 51
58614
XDOT = -1377
844161 Wp = 67
70933
YDOT = -4570
494741 meter/sec RA = 347
46802 deg
ZDOT = -6003
366050 TA = 109
69201
MA = 109
60920
Ha = 214
167 n
mi
Hp = 204
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21536481
63 X = -6583502
85
Y = 5428497
30 feet Y = 1581092
48 meter
Z = 789523
41 Z = 208711
19
XDOT = -4520
486092 XDOT = -1297
470706
YDOT = -14995
061486 feet/sec YDOT = -4585
452843 meter/sec
ZDOT = -19696
082841 ZDOT = -6009
864610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14939854
58 X = 4553667
68
Y = 16440118
62 feet Y = 5010948
15 meter
Z = 659709
13 Z = 201079
34
XDOT = -9952
728126 XDOT = -3033
591533
YDOT = 9860
477046 feet/sec YDOT = 3005
473404 meter/sec
ZDOT = -19722
184111 ZDOT = -6011
321717
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 11202
53244576
00016717 00000-0 10270-3 0 9032
2 25544 51
6389 347
8284 0011532 349
6728 10
4189 15
60042538 6273
Satellite: ISS
Catalog Number: 25544
Epoch time: 11202
53244576 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 347
8284 deg
Eccentricity:
0011532
Arg of perigee: 349
6728 deg
Mean anomaly: 10
4189 deg
Mean motion: 15
60042538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 309
Coasting Arc #5 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2011/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5898420
91 A = 6767671
38 meter
Y = 798651
21 meter E =
0016508
Z = 3197175
47 I = 51
54338
XDOT = -3282
290319 Wp = 43
29647
YDOT = 5031
887152 meter/sec RA = 342
45933 deg
ZDOT = 4795
633514 TA = 353
88026
MA = 353
90040
Ha = 214
109 n
mi
Hp = 204
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19351774
65 X = 5873520
71
Y = 2620246
76 feet Y = 864471
48 meter
Z = 10489420
85 Z = 3225769
29
XDOT = -10768
669025 XDOT = -3361
609992
YDOT = 16508
816115 feet/sec YDOT = 4994
738724 meter/sec
ZDOT = 15733
705755 ZDOT = 4779
496019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7091839
62 X = -2161592
72
Y = -18127713
25 feet Y = -5525327
00 meter
Z = 10605500
83 Z = 3232556
65
XDOT = 18386
931292 XDOT = 5604
336658
YDOT = 1978
538084 feet/sec YDOT = 603
058408 meter/sec
ZDOT = 15667
842415 ZDOT = 4775
558368
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 11203
55738564
00016717 00000-0 10270-3 0 9041
2 25544 51
6402 342
6732 0011370 353
3462 6
7541 15
60059304 6434
Satellite: ISS
Catalog Number: 25544
Epoch time: 11203
55738564 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 342
6732 deg
Eccentricity:
0011370
Arg of perigee: 353
3462 deg
Mean anomaly: 6
7541 deg
Mean motion: 15
60059304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 279
Coasting Arc #6 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2011/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2985978
62 A = 6760699
99 meter
Y = -3206812
41 meter E =
0019266
Z = -5162714
28 I = 51
49176
XDOT = 6486
827979 Wp = 43
12813
YDOT = -3857
865373 meter/sec RA = 337
40898 deg
ZDOT = -1344
693680 TA = 213
85703
MA = 213
98018
Ha = 214
378 n
mi
Hp = 204
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9796517
77 X = -2924818
17
Y = -10521038
08 feet Y = -3239861
03 meter
Z = -16938038
97 Z = -5177071
76
XDOT = 21282
244024 XDOT = 6536
017483
YDOT = -12657
038624 feet/sec YDOT = -3785
050561 meter/sec
ZDOT = -4411
724671 ZDOT = -1313
061790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4243668
96 X = -1293470
30
Y = 13663218
71 feet Y = 4164549
06 meter
Z = -16996143
54 Z = -5180424
55
XDOT = -20638
247893 XDOT = -6290
537958
YDOT = -11781
798861 feet/sec YDOT = -3591
092293 meter/sec
ZDOT = -4283
011058 ZDOT = -1305
461770
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 11204
51825688
00016717 00000-0 10270-3 0 9053
2 25544 51
6405 337
8414 0011540 357
3566 2
7527 15
60064618 6588
Satellite: ISS
Catalog Number: 25544
Epoch time: 11204
51825688 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 337
8414 deg
Eccentricity:
0011540
Arg of perigee: 357
3566 deg
Mean anomaly: 2
7527 deg
Mean motion: 15
60064618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 305
Coasting Arc #7 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2011/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1005072
05 A = 6762780
37 meter
Y = 4755078
20 meter E =
0016770
Z = 4703027
88 I = 51
47093
XDOT = -7062
963945 Wp = 25
59278
YDOT = 1237
370013 meter/sec RA = 332
33584 deg
ZDOT = -2741
966180 TA = 91
66923
MA = 91
47713
Ha = 214
594 n
mi
Hp = 203
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3297480
48 X = -1081015
83
Y = 15600650
26 feet Y = 4743413
77 meter
Z = 15429881
48 Z = 4697961
29
XDOT = -23172
453888 XDOT = -7062
955654
YDOT = 4059
612903 feet/sec YDOT = 1158
387971 meter/sec
ZDOT = -8995
952035 ZDOT = -2776
277635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15112390
29 X = 4606256
56
Y = -5149104
16 feet Y = -1569446
95 meter
Z = 15409000
45 Z = 4696663
34
XDOT = 15033
701339 XDOT = 4582
272168
YDOT = 16603
135101 feet/sec YDOT = 5060
635579 meter/sec
ZDOT = -9135
378307 ZDOT = -2784
463308
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 11205
54317526
00016717 00000-0 10270-3 0 9065
2 25544 51
6406 332
6850 0011498 1
5870 358
5320 15
60039059 6746
Satellite: ISS
Catalog Number: 25544
Epoch time: 11205
54317526 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 332
6850 deg
Eccentricity:
0011498
Arg of perigee: 1
5870 deg
Mean anomaly: 358
5320 deg
Mean motion: 15
60039059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 295
Coasting Arc #8 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2011/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4348107
50 A = 6770317
12 meter
Y = -4747349
27 meter E =
0017486
Z = -2066621
13 I = 51
47103
XDOT = 4900
859530 Wp = 16
95802
YDOT = 2091
289672 meter/sec RA = 327
29677 deg
ZDOT = 5535
431722 TA = 320
04269
MA = 320
17125
Ha = 214
698 n
mi
Hp = 203
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14265444
54 X = 4410909
29
Y = -15575292
89 feet Y = -4698374
70 meter
Z = -6780253
05 Z = -2045346
22
XDOT = 16078
935466 XDOT = 4850
220210
YDOT = 6861
186587 feet/sec YDOT = 2145
810291 meter/sec
ZDOT = 18160
865230 ZDOT = 5559
117114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20793979
18 X = -6338004
85
Y = -3856337
99 feet Y = -1175411
82 meter
Z = -6693547
27 Z = -2040193
21
XDOT = -2942
490459 XDOT = -896
871092
YDOT = -15660
040175 feet/sec YDOT = -4773
180245 meter/sec
ZDOT = 18256
923945 ZDOT = 5564
710418
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 11206
50402297
00016717 00000-0 10270-3 0 9073
2 25544 51
6413 327
8521 0011693 4
4863 355
6396 15
60074869 6891
Satellite: ISS
Catalog Number: 25544
Epoch time: 11206
50402297 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 327
8521 deg
Eccentricity:
0011693
Arg of perigee: 4
4863 deg
Mean anomaly: 355
6396 deg
Mean motion: 15
60074869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 318
Coasting Arc #9 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2011/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5886142
30 A = 6770854
24 meter
Y = 2961454
96 meter E =
0008411
Z = -1578560
77 I = 51
44857
XDOT = -986
509573 Wp = 50
88245
YDOT = -5004
124514 meter/sec RA = 322
28585 deg
ZDOT = -5724
784232 TA = 146
44944
MA = 146
39615
Ha = 214
721 n
mi
Hp = 203
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19311490
50 X = -5911152
13
Y = 9716059
58 feet Y = 2895492
90 meter
Z = -5179005
16 Z = -1607215
68
XDOT = -3236
579964 XDOT = -902
669538
YDOT = -16417
731344 feet/sec YDOT = -5014
686766 meter/sec
ZDOT = -18782
100500 ZDOT = -5729
373625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18657754
90 X = 5686883
69
Y = 10862904
63 feet Y = 3311013
33 meter
Z = -5295569
73 Z = -1614089
65
XDOT = -11267
184895 XDOT = -3434
237956
YDOT = 10211
039748 feet/sec YDOT = 3112
324915 meter/sec
ZDOT = -18800
422067 ZDOT = -5730
368646
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 11207
52891721
00016717 00000-0 10270-3 0 9081
2 25544 51
6413 322
6964 0011685 8
4535 351
6816 15
60117864 7051
Satellite: ISS
Catalog Number: 25544
Epoch time: 11207
52891721 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 322
6964 deg
Eccentricity:
0011685
Arg of perigee: 8
4535 deg
Mean anomaly: 351
6816 deg
Mean motion: 15
60117864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 306
Coasting Arc #10 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2011/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5077856
24 A = 6763255
88 meter
Y = 144788
72 meter E =
0013427
Z = 4451260
65 I = 51
40106
XDOT = -3009
560491 Wp = 52
68950
YDOT = 6293
248181 meter/sec RA = 317
24865 deg
ZDOT = 3229
814395 TA = 4
79657
MA = 4
78372
Ha = 214
637 n
mi
Hp = 203
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16659633
34 X = 5054236
72
Y = 475028
60 feet Y = 201439
75 meter
Z = 14603873
51 Z = 4475871
13
XDOT = -9873
886126 XDOT = -3095
398736
YDOT = 20647
139703 feet/sec YDOT = 6259
113074 meter/sec
ZDOT = 10596
503919 ZDOT = 3214
986508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8880008
01 X = -2706626
44
Y = -13999476
33 feet Y = -4267040
39 meter
Z = 14703818
45 Z = 4481723
86
XDOT = 21651
944502 XDOT = 6599
512684
YDOT = -2672
552379 feet/sec YDOT = -814
593965 meter/sec
ZDOT = 10535
886960 ZDOT = 3211
338345
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 11208
55379872
00016717 00000-0 10270-3 0 9094
2 25544 51
6421 317
5409 0011689 12
0431 348
1002 15
60154712 7216
Satellite: ISS
Catalog Number: 25544
Epoch time: 11208
55379872 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 317
5409 deg
Eccentricity:
0011689
Arg of perigee: 12
0431 deg
Mean anomaly: 348
1002 deg
Mean motion: 15
60154712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 284
Coasting Arc #11 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2011/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2507674
34 A = 6760080
26 meter
Y = -3473417
92 meter E =
0020231
Z = -5243426
27 I = 51
36890
XDOT = 5572
262419 Wp = 60
68241
YDOT = -5204
936413 meter/sec RA = 312
17235 deg
ZDOT = 795
018727 TA = 216
87645
MA = 217
01574
Ha = 214
891 n
mi
Hp = 202
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8227278
03 X = -2443176
44
Y = -11395728
08 feet Y = -3501098
98 meter
Z = -17202842
08 Z = -5255452
07
XDOT = 18281
700849 XDOT = 5626
188908
YDOT = -17076
563035 feet/sec YDOT = -5142
322561 meter/sec
ZDOT = 2608
329156 ZDOT = 822
218559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4671996
86 X = -1424024
64
Y = 13192711
79 feet Y = 4021138
55 meter
Z = -17251472
36 Z = -5258248
78
XDOT = -23504
497419 XDOT = -7164
170813
YDOT = -4819
592096 feet/sec YDOT = -1469
011671 meter/sec
ZDOT = 2719
123858 ZDOT = 828
788952
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 11209
51461667
00016717 00000-0 10270-3 0 9107
2 25544 51
6422 312
7088 0011871 15
6989 344
4533 15
60157716 7368
Satellite: ISS
Catalog Number: 25544
Epoch time: 11209
51461667 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 312
7088 deg
Eccentricity:
0011871
Arg of perigee: 15
6989 deg
Mean anomaly: 344
4533 deg
Mean motion: 15
60157716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 309
Coasting Arc #12 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2011/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -799568
55 A = 6766620
79 meter
Y = 5721109
55 meter E =
0019964
Z = 3521004
29 I = 51
37094
XDOT = -5937
500308 Wp = 54
16440
YDOT = 1935
767145 meter/sec RA = 307
10465 deg
ZDOT = -4464
370913 TA = 84
05913
MA = 83
83162
Ha = 215
072 n
mi
Hp = 202
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2623256
39 X = -880587
66
Y = 18770044
44 feet Y = 5711714
90 meter
Z = 11551851
36 Z = 3516923
91
XDOT = -19479
987886 XDOT = -5937
018572
YDOT = 6350
942077 feet/sec YDOT = 1869
373578 meter/sec
ZDOT = -14646
886199 ZDOT = -4493
213204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16768012
80 X = 5110890
30
Y = -8855525
64 feet Y = -2699164
22 meter
Z = 11534934
97 Z = 3515848
18
XDOT = 15890
352967 XDOT = 4843
379584
YDOT = 10731
863378 feet/sec YDOT = 3271
071958 meter/sec
ZDOT = -14764
152156 ZDOT = -4500
113577
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 11210
53947782
00016717 00000-0 10270-3 0 9119
2 25544 51
6420 307
5531 0011887 19
9760 340
1859 15
60145478 7526
Satellite: ISS
Catalog Number: 25544
Epoch time: 11210
53947782 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 307
5531 deg
Eccentricity:
0011887
Arg of perigee: 19
9760 deg
Mean anomaly: 340
1859 deg
Mean motion: 15
60145478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 309
Coasting Arc #13 (Orbit 766)
---------------------------------------
Vector Time (GMT): 2011/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3478106
61 A = 6771878
09 meter
Y = -5792919
02 meter E =
0023543
Z = -162006
19 I = 51
37167
XDOT = 4184
037932 Wp = 33
20540
YDOT = 2356
331901 meter/sec RA = 302
07872 deg
ZDOT = 6002
539094 TA = 325
03634
MA = 325
19071
Ha = 215
167 n
mi
Hp = 202
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11411110
91 X = 3543412
63
Y = -19005639
84 feet Y = -5753659
56 meter
Z = -531516
39 Z = -144951
87
XDOT = 13727
158568 XDOT = 4128
219546
YDOT = 7730
747708 feet/sec YDOT = 2402
807760 meter/sec
ZDOT = 19693
369731 ZDOT = 6022
729221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22048234
32 X = -6720301
82
Y = 2317824
92 feet Y = 706473
03 meter
Z = -461907
63 Z = -140789
45
XDOT = -1842
829070 XDOT = -561
694301
YDOT = -13913
828384 feet/sec YDOT = -4240
934891 meter/sec
ZDOT = 19775
242470 ZDOT = 6027
493905
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 11211
50027318
00016717 00000-0 10270-3 0 9122
2 25544 51
6424 302
7201 0012084 22
8063 337
3627 15
60151005 7670
Satellite: ISS
Catalog Number: 25544
Epoch time: 11211
50027318 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 302
7201 deg
Eccentricity:
0012084
Arg of perigee: 22
8063 deg
Mean anomaly: 337
3627 deg
Mean motion: 15
60151005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 767
Checksum: 256
Coasting Arc #14 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2011/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4765899
77 A = 6766999
39 meter
Y = 3490292
19 meter E =
0014566
Z = -3321044
70 I = 51
33956
XDOT = -1132
557500 Wp = 43
81331
YDOT = -5978
201841 meter/sec RA = 297
05423 deg
ZDOT = -4659
539974 TA = 175
05908
MA = 175
04469
Ha = 215
191 n
mi
Hp = 202
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15636154
12 X = -4788442
10
Y = 11451089
86 feet Y = 3436871
14 meter
Z = -10895815
94 Z = -3344251
36
XDOT = -3715
739829 XDOT = -1042
989328
YDOT = -19613
523101 feet/sec YDOT = -5990
365719 meter/sec
ZDOT = -15287
204638 ZDOT = -4664
824576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18606848
83 X = 5671367
52
Y = 5228249
96 feet Y = 1593570
59 meter
Z = -10990275
63 Z = -3349836
01
XDOT = -12850
749366 XDOT = -3916
908407
YDOT = 13568
471020 feet/sec YDOT = 4135
669967 meter/sec
ZDOT = -15308
335435 ZDOT = -4665
980641
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 11212
52511167
00016717 00000-0 10270-3 0 9136
2 25544 51
6413 297
5648 0011969 26
7479 333
4292 15
60184490 7836
Satellite: ISS
Catalog Number: 25544
Epoch time: 11212
52511167 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 297
5648 deg
Eccentricity:
0011969
Arg of perigee: 26
7479 deg
Mean anomaly: 333
4292 deg
Mean motion: 15
60184490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 316
Coasting Arc #15 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2011/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4312374
48 A = 6760003
97 meter
Y = 404194
80 meter E =
0012373
Z = 5180898
20 I = 51
30392
XDOT = -2007
581697 Wp = 47
52716
YDOT = 7337
363554 meter/sec RA = 291
98508 deg
ZDOT = 1105
140531 TA = 31
89532
MA = 31
82046
Ha = 215
071 n
mi
Hp = 202
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14148210
23 X = 4282366
95
Y = 1326098
43 feet Y = 452250
45 meter
Z = 16997697
50 Z = 5201774
32
XDOT = -6586
554123 XDOT = -2094
848752
YDOT = 24072
715072 feet/sec YDOT = 7314
425577 meter/sec
ZDOT = 3625
789145 ZDOT = 1095
176226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7799776
06 X = -2377371
74
Y = -11756049
30 feet Y = -3583243
83 meter
Z = 17082473
72 Z = 5206737
99
XDOT = 22016
597915 XDOT = 6710
659045
YDOT = -9429
202490 feet/sec YDOT = -2874
020919 meter/sec
ZDOT = 3584
918049 ZDOT = 1092
683021
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 11213
54993723
00016717 00000-0 10270-3 0 9142
2 25544 51
6414 292
4085 0012012 30
1073 330
0771 15
60235798 7995
Satellite: ISS
Catalog Number: 25544
Epoch time: 11213
54993723 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 292
4085 deg
Eccentricity:
0012012
Arg of perigee: 30
1073 deg
Mean anomaly: 330
0771 deg
Mean motion: 15
60235798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 291
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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