[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 28th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
125/08:45:48
798 1
7 8
8 8
8
N/A -5
9 -0
1 216
0
000/00:21:37
597 -6
2 -0
0 214
6
Coasting Arc #1 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2012/118/12:14:22
708
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -128020
50 A = 6767928
86 meter
Y = -4309111
25 meter E =
0007231
Z = -5222163
70 I = 51
71902
XDOT = 7501
219658 Wp = 39
54044
YDOT = 1141
887923 meter/sec RA = 15
35456 deg
ZDOT = -1121
533275 TA = 219
69765
MA = 219
75059
Ha = 214
848 n
mi
Hp = 212
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -420014
76 X = -54457
34
Y = -14137504
11 feet Y = -4310131
47 meter
Z = -17133082
99 Z = -5222606
99
XDOT = 24610
300716 XDOT = 7493
341521
YDOT = 3746
351452 feet/sec YDOT = 1225
727166 meter/sec
ZDOT = -3679
571113 ZDOT = -1085
111533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9082605
89 X = -2768378
28
Y = -10839916
44 feet Y = -3304006
53 meter
Z = -17134481
30 Z = -5222589
90
XDOT = 20779
955525 XDOT = 6333
730444
YDOT = -11807
550100 feet/sec YDOT = -3598
941270 meter/sec
ZDOT = -3530
012824 ZDOT = -1075
947909
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 12118
52786070
00016717 00000-0 10270-3 0 9005
2 25544 51
6430 15
7892 0010130 290
1690 69
8374 15
57502312 10127
Satellite: ISS
Catalog Number: 25544
Epoch time: 12118
52786070 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 15
7892 deg
Eccentricity:
0010130
Arg of perigee: 290
1690 deg
Mean anomaly: 69
8374 deg
Mean motion: 15
57502312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 276
Coasting Arc #2 (Orbit 1027)
---------------------------------------
Vector Time (GMT): 2012/119/12:14:22
708
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2991049
43 A = 6768854
23 meter
Y = 3464327
46 meter E =
0008639
Z = 4993018
54 I = 51
69282
XDOT = -6797
345813 Wp = 329
87167
YDOT = -2891
964777 meter/sec RA = 10
32362 deg
ZDOT = -2059
621226 TA = 140
17491
MA = 140
11148
Ha = 215
076 n
mi
Hp = 212
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9813154
30 X = -3053821
03
Y = 11365903
74 feet Y = 3430528
70 meter
Z = 16381294
44 Z = 4978335
63
XDOT = -22301
003324 XDOT = -6754
496848
YDOT = -9488
073416 feet/sec YDOT = -2967
737310 meter/sec
ZDOT = -6757
287487 ZDOT = -2092
538544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -375117
36 X = -114335
77
Y = 15077311
97 feet Y = 4595564
69 meter
Z = 16320616
52 Z = 4974523
92
XDOT = -22092
105641 XDOT = -6733
673799
YDOT = 6931
508248 feet/sec YDOT = 2112
723714 meter/sec
ZDOT = -6892
270449 ZDOT = -2100
764033
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 12119
55446481
00016717 00000-0 10270-3 0 9019
2 25544 51
6429 10
6450 0010311 293
8227 66
1846 15
57556921 10282
Satellite: ISS
Catalog Number: 25544
Epoch time: 12119
55446481 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 10
6450 deg
Eccentricity:
0010311
Arg of perigee: 293
8227 deg
Mean anomaly: 66
1846 deg
Mean motion: 15
57556921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1028
Checksum: 295
Coasting Arc #3 (Orbit 1042)
---------------------------------------
Vector Time (GMT): 2012/120/12:14:22
708
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5471855
22 A = 6774688
53 meter
Y = -2154047
23 meter E =
0006792
Z = -3354553
89 I = 51
68225
XDOT = 4485
622971 Wp = 318
05895
YDOT = 4122
440578 meter/sec RA = 5
30740 deg
ZDOT = 4669
186799 TA = 2
77725
MA = 2
77348
Ha = 215
365 n
mi
Hp = 211
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17952280
91 X = 5511831
28
Y = -7067084
08 feet Y = -2092634
06 meter
Z = -11005754
23 Z = -3327874
61
XDOT = 14716
610798 XDOT = 4416
509651
YDOT = 13525
067513 feet/sec YDOT = 4172
215188 meter/sec
ZDOT = 15318
854327 ZDOT = 4690
809956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9066555
78 X = 2763486
20
Y = -17100625
14 feet Y = -5212270
54 meter
Z = -10895911
13 Z = -3321073
71
XDOT = 18658
954978 XDOT = 5687
249477
YDOT = 74
702447 feet/sec YDOT = 22
769306 meter/sec
ZDOT = 15407
302743 ZDOT = 4696
145876
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 12120
51688474
00016717 00000-0 10270-3 0 9028
2 25544 51
6431 5
8220 0010368 297
3829 62
6270 15
57553750 10431
Satellite: ISS
Catalog Number: 25544
Epoch time: 12120
51688474 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 5
8220 deg
Eccentricity:
0010368
Arg of perigee: 297
3829 deg
Mean anomaly: 62
6270 deg
Mean motion: 15
57553750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1043
Checksum: 293
Coasting Arc #4 (Orbit 1058)
---------------------------------------
Vector Time (GMT): 2012/121/12:14:22
708
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6711880
72 A = 6779160
67 meter
Y = 558495
97 meter E =
0003363
Z = 753166
59 I = 51
66699
XDOT = -1061
706865 Wp = 149
09029
YDOT = -4715
248622 meter/sec RA =
31613 deg
ZDOT = -5955
973598 TA = 22
76477
MA = 22
74986
Ha = 215
418 n
mi
Hp = 211
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22020606
05 X = -6721285
83
Y = 1832335
86 feet Y = 483387
00 meter
Z = 2471018
98 Z = 720537
52
XDOT = -3483
290239 XDOT = -979
968134
YDOT = -15469
975794 feet/sec YDOT = -4726
664383 meter/sec
ZDOT = -19540
595793 ZDOT = -5960
932712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15251079
47 X = -4648529
02
Y = 16009809
66 feet Y = 4879789
98 meter
Z = 2336888
97 Z = 712283
76
XDOT = -11626
030351 XDOT = -3543
614051
YDOT = -8215
337285 feet/sec YDOT = -2504
034804 meter/sec
ZDOT = -19560
509550 ZDOT = -5962
043311
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 12121
54344183
00016717 00000-0 10270-3 0 9039
2 25544 51
6431
6780 0010229 300
4083 59
6060 15
57557470 10592
Satellite: ISS
Catalog Number: 25544
Epoch time: 12121
54344183 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node:
6780 deg
Eccentricity:
0010229
Arg of perigee: 300
4083 deg
Mean anomaly: 59
6060 deg
Mean motion: 15
57557470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1059
Checksum: 275
Coasting Arc #5 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2012/122/12:14:22
708
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6344388
55 A = 6777271
81 meter
Y = 1128655
07 meter E =
0011664
Z = 2073454
44 I = 51
63074
XDOT = -2632
198913 Wp = 21
97627
YDOT = 4616
926432 meter/sec RA = 355
32869 deg
ZDOT = 5541
406285 TA = 1
02024
MA = 1
01786
Ha = 215
529 n
mi
Hp = 211
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20814923
06 X = 6321223
70
Y = 3702936
57 feet Y = 1199472
49 meter
Z = 6802672
03 Z = 2104219
16
XDOT = -8635
823206 XDOT = -2710
549834
YDOT = 15147
396429 feet/sec YDOT = 4587
053651 meter/sec
ZDOT = 18180
466813 ZDOT = 5528
428602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17793384
20 X = 5423423
50
Y = -11341691
66 feet Y = -3456947
62 meter
Z = 6928969
40 Z = 2111949
87
XDOT = 2995
067003 XDOT = 912
896423
YDOT = 15771
902251 feet/sec YDOT = 4807
275806 meter/sec
ZDOT = 18126
689958 ZDOT = 5525
015099
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 12122
56997143
00016717 00000-0 10270-3 0 9043
2 25544 51
6428 355
5326 0010508 304
9302 55
0865 15
57629961 10755
Satellite: ISS
Catalog Number: 25544
Epoch time: 12122
56997143 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 355
5326 deg
Eccentricity:
0010508
Arg of perigee: 304
9302 deg
Mean anomaly: 55
0865 deg
Mean motion: 15
57629961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 312
Coasting Arc #6 (Orbit 1089)
---------------------------------------
Vector Time (GMT): 2012/123/12:14:22
708
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4482720
86 A = 6771105
86 meter
Y = -2698216
29 meter E =
0009542
Z = -4303637
12 I = 51
57942
XDOT = 5664
262141 Wp = 357
93370
YDOT = -3792
521213 meter/sec RA = 350
32014 deg
ZDOT = -3512
616662 TA = 236
24226
MA = 236
33321
Ha = 215
720 n
mi
Hp = 210
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14707089
42 X = -4431309
31
Y = -8852415
66 feet Y = -2748057
56 meter
Z = -14119544
36 Z = -4325289
28
XDOT = 18583
537208 XDOT = 5723
313624
YDOT = -12442
654899 feet/sec YDOT = -3728
849886 meter/sec
ZDOT = -11524
332881 ZDOT = -3484
955990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16692936
10 X = -5088006
92
Y = 3673836
12 feet Y = 1119785
25 meter
Z = -14208240
13 Z = -4330671
59
XDOT = 5191
986856 XDOT = 1582
517594
YDOT = -20658
195153 feet/sec YDOT = -6296
617883 meter/sec
ZDOT = -11410
313016 ZDOT = -3477
863407
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 12123
53232111
00016717 00000-0 10270-3 0 9059
2 25544 51
6421 350
7098 0010612 307
9114 52
1081 15
57659867 10904
Satellite: ISS
Catalog Number: 25544
Epoch time: 12123
53232111 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 350
7098 deg
Eccentricity:
0010612
Arg of perigee: 307
9114 deg
Mean anomaly: 52
1081 deg
Mean motion: 15
57659867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1090
Checksum: 277
Coasting Arc #7 (Orbit 1105)
---------------------------------------
Vector Time (GMT): 2012/124/12:14:22
708
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1554788
99 A = 6767047
86 meter
Y = 3933655
06 meter E =
0008195
Z = 5286479
04 I = 51
53628
XDOT = -7307
294266 Wp = 318
92354
YDOT = 2290
214814 meter/sec RA = 345
28241 deg
ZDOT = 451
431050 TA = 126
80381
MA = 126
72859
Ha = 215
880 n
mi
Hp = 210
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5101013
74 X = 1485005
51
Y = 12905692
46 feet Y = 3950651
66 meter
Z = 17344091
34 Z = 5293862
64
XDOT = -23974
062553 XDOT = -7334
553803
YDOT = 7513
828131 feet/sec YDOT = 2208
347725 meter/sec
ZDOT = 1481
073000 ZDOT = 415
865619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12618685
78 X = 3846175
43
Y = 5683862
63 feet Y = 1732441
33 meter
Z = 17374038
62 Z = 5295606
97
XDOT = -11388
448640 XDOT = -3471
199145
YDOT = 21268
034545 feet/sec YDOT = 6482
496929 meter/sec
ZDOT = 1334
730894 ZDOT = 406
825976
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 12124
55880431
00016717 00000-0 10270-3 0 9067
2 25544 51
6422 345
5647 0010535 312
0397 47
9860 15
57691725 11065
Satellite: ISS
Catalog Number: 25544
Epoch time: 12124
55880431 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 345
5647 deg
Eccentricity:
0010535
Arg of perigee: 312
0397 deg
Mean anomaly: 47
9860 deg
Mean motion: 15
57691725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1106
Checksum: 306
Coasting Arc #8 (Orbit 1118)
---------------------------------------
Vector Time (GMT): 2012/125/08:56:37
597
Vector Time (MET): N/A
Weight (LBS) : 911690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3817448
25 A = 6774496
18 meter
Y = -2772912
14 meter E =
0004041
Z = -4863493
48 I = 51
51741
XDOT = 6027
428142 Wp = 12
33680
YDOT = -4092
479214 meter/sec RA = 340
96811 deg
ZDOT = -2394
222564 TA = 234
13939
MA = 234
17693
Ha = 215
981 n
mi
Hp = 214
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12524436
51 X = -3762530
99
Y = -9097480
78 feet Y = -2815294
22 meter
Z = -15956343
43 Z = -4881905
43
XDOT = 19775
026714 XDOT = 6084
373945
YDOT = -13426
769076 feet/sec YDOT = -4024
758418 meter/sec
ZDOT = -7855
060907 ZDOT = -2364
802569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11763150
56 X = -3585408
29
Y = -9941989
48 feet Y = -3030318
39 meter
Z = -16031709
08 Z = -4886464
93
XDOT = 19984
640531 XDOT = 6091
318434
YDOT = -11156
034942 feet/sec YDOT = -3400
359450 meter/sec
ZDOT = -7733
792397 ZDOT = -2357
259923
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 12125
39283343
00016717 00000-0 10270-3 0 9070
2 25544 51
6425 341
3851 0010593 272
3731 87
6209 15
55742240 11192
Satellite: ISS
Catalog Number: 25544
Epoch time: 12125
39283343 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 341
3851 deg
Eccentricity:
0010593
Arg of perigee: 272
3731 deg
Mean anomaly: 87
6209 deg
Mean motion: 15
55742240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1119
Checksum: 296
Coasting Arc #9 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2012/126/08:56:37
597
Vector Time (MET): N/A
Weight (LBS) : 911690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1623545
20 A = 6772548
22 meter
Y = 3897320
17 meter E =
0008400
Z = 5302708
39 I = 51
48237
XDOT = -7028
921062 Wp = 279
04570
YDOT = 3056
649724 meter/sec RA = 335
94217 deg
ZDOT = -93
307251 TA = 171
85256
MA = 171
83891
Ha = 216
326 n
mi
Hp = 214
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5326591
85 X = 1554083
92
Y = 12786483
50 feet Y = 3915087
20 meter
Z = 17397337
25 Z = 5310427
02
XDOT = -23060
764638 XDOT = -7062
125452
YDOT = 10028
378361 feet/sec YDOT = 2977
862326 meter/sec
ZDOT = -306
126153 ZDOT = -127
534867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4542242
49 X = 1384475
51
Y = 13043926
72 feet Y = 3975788
86 meter
Z = 17428657
24 Z = 5312254
73
XDOT = -22601
883852 XDOT = -6889
054198
YDOT = 8472
999369 feet/sec YDOT = 2582
570208 meter/sec
ZDOT = -447
040305 ZDOT = -136
257885
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 12126
42060056
00016717 00000-0 10270-3 0 9080
2 25544 51
6421 336
2485 0010761 276
0687 83
9240 15
55782196 11358
Satellite: ISS
Catalog Number: 25544
Epoch time: 12126
42060056 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 336
2485 deg
Eccentricity:
0010761
Arg of perigee: 276
0687 deg
Mean anomaly: 83
9240 deg
Mean motion: 15
55782196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1135
Checksum: 302
Coasting Arc #10 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2012/127/08:56:37
597
Vector Time (MET): N/A
Weight (LBS) : 911690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 685592
44 A = 6774767
16 meter
Y = -4744942
35 meter E =
0001699
Z = -4787562
35 I = 51
46261
XDOT = 7051
249053 Wp = 175
37988
YDOT = -1578
012063 meter/sec RA = 330
91443 deg
ZDOT = 2572
126464 TA = 120
01583
MA = 119
99898
Ha = 216
707 n
mi
Hp = 214
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2249319
04 X = 761857
83
Y = -15567396
16 feet Y = -4736848
99 meter
Z = -15707225
54 Z = -4784046
66
XDOT = 23134
019203 XDOT = 7055
875535
YDOT = -5177
204930 feet/sec YDOT = -1499
134886 meter/sec
ZDOT = 8438
735118 ZDOT = 2606
393073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2893003
49 X = 881787
46
Y = -15475860
09 feet Y = -4717042
16 meter
Z = -15692306
36 Z = -4783014
98
XDOT = 22122
088406 XDOT = 6742
812546
YDOT = -4569
547349 feet/sec YDOT = -1392
798032 meter/sec
ZDOT = 8579
661726 ZDOT = 2615
080894
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 12127
38411347
00016717 00000-0 10270-3 0 9090
2 25544 51
6422 331
4327 0010804 280
1084 79
8851 15
55793865 11500
Satellite: ISS
Catalog Number: 25544
Epoch time: 12127
38411347 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 331
4327 deg
Eccentricity:
0010804
Arg of perigee: 280
1084 deg
Mean anomaly: 79
8851 deg
Mean motion: 15
55793865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1150
Checksum: 304
Coasting Arc #11 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2012/128/08:56:37
597
Vector Time (MET): N/A
Weight (LBS) : 911690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2781918
43 A = 6779524
80 meter
Y = 5160568
22 meter E =
0003280
Z = 3405549
92 I = 51
45258
XDOT = -6131
804815 Wp = 37
86790
YDOT = -269
878634 meter/sec RA = 325
89880 deg
ZDOT = -4595
083359 TA = 102
17278
MA = 102
13604
Ha = 217
085 n
mi
Hp = 214
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9127028
97 X = -2855961
90
Y = 16930998
10 feet Y = 5129044
84 meter
Z = 11173064
05 Z = 3391855
75
XDOT = -20117
469866 XDOT = -6106
008937
YDOT = -885
428590 feet/sec YDOT = -338
303697 meter/sec
ZDOT = -15075
732805 ZDOT = -4624
809327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9499929
99 X = -2895578
66
Y = 16762404
97 feet Y = 5109181
04 meter
Z = 11116286
44 Z = 3388244
11
XDOT = -18783
689469 XDOT = -5725
268550
YDOT = -556
064457 feet/sec YDOT = -169
488446 meter/sec
ZDOT = -15197
822217 ZDOT = -4632
296212
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 12128
41183874
00016717 00000-0 10270-3 0 9108
2 25544 51
6420 326
2961 0010779 284
4264 75
5693 15
55825769 11665
Satellite: ISS
Catalog Number: 25544
Epoch time: 12128
41183874 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 326
2961 deg
Eccentricity:
0010779
Arg of perigee: 284
4264 deg
Mean anomaly: 75
5693 deg
Mean motion: 15
55825769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1166
Checksum: 327
Coasting Arc #12 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2012/129/08:56:37
597
Vector Time (MET): N/A
Weight (LBS) : 911690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4375577
78 A = 6783507
83 meter
Y = -4983557
79 meter E =
0011484
Z = -1389586
02 I = 51
44194
XDOT = 4474
258129 Wp = 333
25109
YDOT = 2311
397648 meter/sec RA = 320
89760 deg
ZDOT = 5790
604177 TA = 11
54492
MA = 11
51860
Ha = 217
358 n
mi
Hp = 214
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14355570
14 X = 4437730
12
Y = -16350255
21 feet Y = -4934279
74 meter
Z = -4559009
24 Z = -1368178
84
XDOT = 14679
324571 XDOT = 4419
949239
YDOT = 7583
325616 feet/sec YDOT = 2361
127398 meter/sec
ZDOT = 18998
045200 ZDOT = 5812
208509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14397857
58 X = 4388466
99
Y = -16337490
18 feet Y = -4979667
01 meter
Z = -4470561
09 Z = -1362627
02
XDOT = 13365
207167 XDOT = 4073
715145
YDOT = 6547
773522 feet/sec YDOT = 1995
761369 meter/sec
ZDOT = 19086
566824 ZDOT = 5817
585568
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 12129
37531003
00016717 00000-0 10270-3 0 9116
2 25544 51
6423 321
4793 0010955 288
0436 71
9523 15
55861639 11810
Satellite: ISS
Catalog Number: 25544
Epoch time: 12129
37531003 = yrday
fracday
Element set: 911
Inclination: 51
6423 deg
RA of node: 321
4793 deg
Eccentricity:
0010955
Arg of perigee: 288
0436 deg
Mean anomaly: 71
9523 deg
Mean motion: 15
55861639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1181
Checksum: 300
Coasting Arc #13 (Orbit 1196)
---------------------------------------
Vector Time (GMT): 2012/130/08:56:37
597
Vector Time (MET): N/A
Weight (LBS) : 911690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5293351
47 A = 6783970
21 meter
Y = 4144449
19 meter E =
0005533
Z = -886137
08 I = 51
42045
XDOT = -2358
219764 Wp = 226
03843
YDOT = -4279
760560 meter/sec RA = 315
90511 deg
ZDOT = -5910
250132 TA = 323
58462
MA = 323
62225
Ha = 217
608 n
mi
Hp = 214
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17366638
68 X = -5334997
43
Y = 13597274
24 feet Y = 4085022
88 meter
Z = -2907273
89 Z = -911952
95
XDOT = -7736
941483 XDOT = -2281
476443
YDOT = -14041
209186 feet/sec YDOT = -4305
702008 meter/sec
ZDOT = -19390
584423 ZDOT = -5921
520327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17124748
10 X = -5219623
22
Y = 13877988
17 feet Y = 4230010
79 meter
Z = -3013750
82 Z = -918591
25
XDOT = -6834
597042 XDOT = -2083
185178
YDOT = -12667
625295 feet/sec YDOT = -3861
092190 meter/sec
ZDOT = -19436
456405 ZDOT = -5924
231912
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 12130
40299262
00016717 00000-0 10270-3 0 9121
2 25544 51
6422 316
3428 0011003 291
0770 68
9207 15
55849604 11977
Satellite: ISS
Catalog Number: 25544
Epoch time: 12130
40299262 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 316
3428 deg
Eccentricity:
0011003
Arg of perigee: 291
0770 deg
Mean anomaly: 68
9207 deg
Mean motion: 15
55849604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1197
Checksum: 292
Coasting Arc #14 (Orbit 1212)
---------------------------------------
Vector Time (GMT): 2012/131/08:56:37
597
Vector Time (MET): N/A
Weight (LBS) : 911690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5466748
49 A = 6780223
61 meter
Y = -2635730
73 meter E =
0006998
Z = 3012571
22 I = 51
38700
XDOT = 117
935751 Wp = 25
12793
YDOT = 5877
664337 meter/sec RA = 310
90326 deg
ZDOT = 4930
422868 TA = 9
55435
MA = 9
54104
Ha = 217
793 n
mi
Hp = 214
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17935526
54 X = 5481181
01
Y = -8647410
54 feet Y = -2574517
71 meter
Z = 9883763
85 Z = 3039163
41
XDOT = 386
928317 XDOT = 28
250761
YDOT = 19283
675647 feet/sec YDOT = 5878
481324 meter/sec
ZDOT = 16175
928043 ZDOT = 4930
778414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17575406
30 X = 5356983
84
Y = -9240620
49 feet Y = -2816541
12 meter
Z = 9993279
52 Z = 3045951
60
XDOT = 260
346727 XDOT = 79
353682
YDOT = 17982
566049 feet/sec YDOT = 5481
086132 meter/sec
ZDOT = 16176
804041 ZDOT = 4930
689872
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 12131
43065195
00016717 00000-0 10270-3 0 9132
2 25544 51
6417 311
2045 0011149 296
4153 63
5856 15
55905526 12131
Satellite: ISS
Catalog Number: 25544
Epoch time: 12131
43065195 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 311
2045 deg
Eccentricity:
0011149
Arg of perigee: 296
4153 deg
Mean anomaly: 63
5856 deg
Mean motion: 15
55905526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1213
Checksum: 287
Coasting Arc #15 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2012/132/08:56:37
597
Vector Time (MET): N/A
Weight (LBS) : 911690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4965909
35 A = 6775056
84 meter
Y = 629029
11 meter E =
0009039
Z = -4570022
40 I = 51
35013
XDOT = 1926
445376 Wp = 358
26813
YDOT = -6779
846919 meter/sec RA = 305
88375 deg
ZDOT = -3017
491388 TA = 241
42506
MA = 241
51606
Ha = 218
036 n
mi
Hp = 213
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16292353
52 X = -4950374
01
Y = 2063743
80 feet Y = 573584
38 meter
Z = -14993511
83 Z = -4594108
86
XDOT = 6320
358844 XDOT = 2016
774152
YDOT = -22243
592255 feet/sec YDOT = -6757
798974 meter/sec
ZDOT = -9899
906127 ZDOT = -3007
913787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16075424
41 X = -4899789
36
Y = 2881207
05 feet Y = 878191
91 meter
Z = -15092534
40 Z = -4600204
48
XDOT = 5455
096758 XDOT = 1662
713492
YDOT = -21366
729156 feet/sec YDOT = -6512
579047 meter/sec
ZDOT = -9859
890028 ZDOT = -3005
294481
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 12132
39406163
00016717 00000-0 10270-3 0 9143
2 25544 51
6409 306
3885 0011274 299
5552 60
4478 15
55948841 12284
Satellite: ISS
Catalog Number: 25544
Epoch time: 12132
39406163 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 306
3885 deg
Eccentricity:
0011274
Arg of perigee: 299
5552 deg
Mean anomaly: 60
4478 deg
Mean motion: 15
55948841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1228
Checksum: 321
Coasting Arc #16 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2012/133/08:56:37
597
Vector Time (MET): N/A
Weight (LBS) : 911690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3920725
17 A = 6772082
04 meter
Y = 1663478
46 meter E =
0008538
Z = 5270662
99 I = 51
32349
XDOT = -3560
752635 Wp = 307
23444
YDOT = 6770
383742 meter/sec RA = 300
84614 deg
ZDOT = 517
608679 TA = 137
83756
MA = 137
77185
Ha = 218
207 n
mi
Hp = 213
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12863271
57 X = 3876228
67
Y = 5457606
50 feet Y = 1707073
42 meter
Z = 17292201
43 Z = 5289601
74
XDOT = -11682
259302 XDOT = -3638
710231
YDOT = 22212
545084 feet/sec YDOT = 6730
129295 meter/sec
ZDOT = 1698
191203 ZDOT = 500
121593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13098741
12 X = 3992496
29
Y = 4580466
26 feet Y = 1396126
12 meter
Z = 17369852
17 Z = 5294330
94
XDOT = -9824
282552 XDOT = -2994
441322
YDOT = 21999
614342 feet/sec YDOT = 6705
482452 meter/sec
ZDOT = 1625
688186 ZDOT = 495
509759
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 12133
42167863
00016717 00000-0 10270-3 0 9150
2 25544 51
6410 301
2509 0011200 303
6667 56
3418 15
55967505 12440
Satellite: ISS
Catalog Number: 25544
Epoch time: 12133
42167863 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 301
2509 deg
Eccentricity:
0011200
Arg of perigee: 303
6667 deg
Mean anomaly: 56
3418 deg
Mean motion: 15
55967505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1244
Checksum: 284
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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