[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 19th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 ET - UTC (sec) : 67 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 884)
---------------------------------------
Vector Time (GMT): 2013/259/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6632841
11 A = 6800175
75 meter
Y = -1182084
85 meter E =
0014235
Z = 880793
95 I = 51
76724
XDOT = 66
262463 Wp = 115
01165
YDOT = -4845
768866 meter/sec RA = 16
01681 deg
ZDOT = -5935
077579 TA = 55
48950
MA = 55
35516
Ha = 227
853 n
mi
Hp = 219
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21761289
74 X = -6623408
43
Y = -3878231
15 feet Y = -1256204
67 meter
Z = 2889743
93 Z = 848595
53
XDOT = 217
396533 XDOT = 149
274735
YDOT = -15898
191816 feet/sec YDOT = -4844
564328 meter/sec
ZDOT = -19472
039302 ZDOT = -5934
553565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7976907
14 X = 2431361
30
Y = 20633104
13 feet Y = 6288970
14 meter
Z = 2754812
96 Z = 839666
99
XDOT = -12266
065281 XDOT = -3738
696698
YDOT = 7373
385400 feet/sec YDOT = 2247
407870 meter/sec
ZDOT = -19469
103493 ZDOT = -5934
182745
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 13259
38556477
00016717 00000-0 10270-3 0 9002
2 25544 51
6467 16
4036 0002673 49
9766 310
1619 15
50303032 8854
Satellite: ISS
Catalog Number: 25544
Epoch time: 13259
38556477 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 16
4036 deg
Eccentricity:
0002673
Arg of perigee: 49
9766 deg
Mean anomaly: 310
1619 deg
Mean motion: 15
50303032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 885
Checksum: 310
Coasting Arc #2 (Orbit 899)
---------------------------------------
Vector Time (GMT): 2013/260/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6713418
33 A = 6800430
33 meter
Y = 933175
30 meter E =
0013714
Z = -473270
05 I = 51
73864
XDOT = -248
397853 Wp = 45
22362
YDOT = 4767
878404 meter/sec RA = 11
07025 deg
ZDOT = 5993
542201 TA = 309
68694
MA = 309
80779
Ha = 227
965 n
mi
Hp = 219
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22025650
70 X = 6704783
41
Y = 3061598
77 feet Y = 1008200
68 meter
Z = -1552723
26 Z = -440678
19
XDOT = -814
953586 XDOT = -330
809654
YDOT = 15642
645683 feet/sec YDOT = 4764
640598 meter/sec
ZDOT = 19663
852367 ZDOT = 5992
134764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9157957
36 X = -2791345
40
Y = -20274123
25 feet Y = -6179552
77 meter
Z = -1416110
44 Z = -431630
46
XDOT = 12256
402137 XDOT = 3735
751371
YDOT = -6880
174602 feet/sec YDOT = -2097
077219 meter/sec
ZDOT = 19657
223078 ZDOT = 5991
521594
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 13260
35249850
00016717 00000-0 10270-3 0 9016
2 25544 51
6472 11
6112 0002659 60
8286 299
3131 15
50289835 9004
Satellite: ISS
Catalog Number: 25544
Epoch time: 13260
35249850 = yrday
fracday
Element set: 901
Inclination: 51
6472 deg
RA of node: 11
6112 deg
Eccentricity:
0002659
Arg of perigee: 60
8286 deg
Mean anomaly: 299
3131 deg
Mean motion: 15
50289835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 900
Checksum: 294
Coasting Arc #3 (Orbit 915)
---------------------------------------
Vector Time (GMT): 2013/261/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6757384
70 A = 6800328
18 meter
Y = -719650
10 meter E =
0012963
Z = 6512
70 I = 51
70853
XDOT = 488
687682 Wp = 122
30053
YDOT = -4722
258434 meter/sec RA = 6
12234 deg
ZDOT = -6013
146250 TA = 57
62950
MA = 57
50411
Ha = 227
849 n
mi
Hp = 219
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22169897
30 X = -6748866
82
Y = -2361056
77 feet Y = -795167
85 meter
Z = 21367
12 Z = -26293
16
XDOT = 1603
306043 XDOT = 570
666830
YDOT = -15492
973864 feet/sec YDOT = -4716
336060 meter/sec
ZDOT = -19728
170112 ZDOT = -6010
572496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10165187
96 X = 3098349
29
Y = 19842753
11 feet Y = 6048071
15 meter
Z = -116166
81 Z = -35407
64
XDOT = -12462
695569 XDOT = -3798
629609
YDOT = 6299
949788 feet/sec YDOT = 1920
224695 meter/sec
ZDOT = -19716
655684 ZDOT = -6009
636652
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 13261
38387291
00016717 00000-0 10270-3 0 9023
2 25544 51
6471 6
4992 0002764 58
8243 301
3178 15
50351667 9163
Satellite: ISS
Catalog Number: 25544
Epoch time: 13261
38387291 = yrday
fracday
Element set: 902
Inclination: 51
6471 deg
RA of node: 6
4992 deg
Eccentricity:
0002764
Arg of perigee: 58
8243 deg
Mean anomaly: 301
3178 deg
Mean motion: 15
50351667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 916
Checksum: 310
Coasting Arc #4 (Orbit 931)
---------------------------------------
Vector Time (GMT): 2013/262/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6763590
66 A = 6800233
56 meter
Y = 472298
50 meter E =
0015504
Z = 422367
05 I = 51
67863
XDOT = -712
981524 Wp = 52
79530
YDOT = 4723
251567 meter/sec RA = 1
17231 deg
ZDOT = 5993
295665 TA = 311
75014
MA = 311
88259
Ha = 227
909 n
mi
Hp = 219
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22190258
08 X = 6755754
88
Y = 1549535
75 feet Y = 547889
51 meter
Z = 1385718
66 Z = 455204
89
XDOT = -2339
178228 XDOT = -794
858815
YDOT = 15496
232175 feet/sec YDOT = 4714
821602 meter/sec
ZDOT = 19663
043521 ZDOT = 5989
632516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11182718
69 X = -3408492
66
Y = -19218606
72 feet Y = -5857831
33 meter
Z = 1523413
65 Z = 464336
48
XDOT = 12801
005287 XDOT = 3901
746412
YDOT = -5857
450518 feet/sec YDOT = -1785
350918 meter/sec
ZDOT = 19646
959573 ZDOT = 5988
393278
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 13262
41523017
00016717 00000-0 10270-3 0 9037
2 25544 51
6482 1
3877 0002746 68
5434 291
6010 15
50354678 9320
Satellite: ISS
Catalog Number: 25544
Epoch time: 13262
41523017 = yrday
fracday
Element set: 903
Inclination: 51
6482 deg
RA of node: 1
3877 deg
Eccentricity:
0002746
Arg of perigee: 68
5434 deg
Mean anomaly: 291
6010 deg
Mean motion: 15
50354678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 932
Checksum: 291
Coasting Arc #5 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2013/263/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6730489
92 A = 6799821
36 meter
Y = -272660
21 meter E =
0010998
Z = -904597
80 I = 51
64654
XDOT = 981
006229 Wp = 126
25719
YDOT = -4760
027236 meter/sec RA = 356
21999 deg
ZDOT = -5920
869286 TA = 63
51465
MA = 63
40189
Ha = 227
836 n
mi
Hp = 219
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22081659
86 X = -6722546
43
Y = -894554
50 feet Y = -347880
54 meter
Z = -2967840
54 Z = -937274
76
XDOT = 3218
524374 XDOT = 1062
923137
YDOT = -15616
887256 feet/sec YDOT = -4748
599807 meter/sec
ZDOT = -19425
424166 ZDOT = -5915
903978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11978703
26 X = 3651108
75
Y = 18549350
26 feet Y = 5653841
96 meter
Z = -3104880
06 Z = -946367
44
XDOT = -13337
251891 XDOT = -4065
194376
YDOT = 5394
671081 feet/sec YDOT = 1644
295745 meter/sec
ZDOT = -19403
872510 ZDOT = -5914
300341
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 13263
38210897
00016717 00000-0 10270-3 0 9044
2 25544 51
6478 356
5953 0002832 67
1890 292
9559 15
50395154 9474
Satellite: ISS
Catalog Number: 25544
Epoch time: 13263
38210897 = yrday
fracday
Element set: 904
Inclination: 51
6478 deg
RA of node: 356
5953 deg
Eccentricity:
0002832
Arg of perigee: 67
1890 deg
Mean anomaly: 292
9559 deg
Mean motion: 15
50395154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 947
Checksum: 342
Coasting Arc #6 (Orbit 962)
---------------------------------------
Vector Time (GMT): 2013/264/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6657597
71 A = 6799327
52 meter
Y = 52837
80 meter E =
0016527
Z = 1342206
72 I = 51
61562
XDOT = -1219
830958 Wp = 62
29805
YDOT = 4845
766808 meter/sec RA = 351
26547 deg
ZDOT = 5812
473113 TA = 312
30461
MA = 312
44456
Ha = 227
819 n
mi
Hp = 219
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21842512
16 X = 6649991
91
Y = 173352
36 feet Y = 127244
94 meter
Z = 4403565
36 Z = 1374530
55
XDOT = -4002
070073 XDOT = -1302
162413
YDOT = 15898
185065 feet/sec YDOT = 4831
666306 meter/sec
ZDOT = 19069
793677 ZDOT = 5806
346611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12731812
73 X = -3880656
52
Y = -17714792
27 feet Y = -5399468
68 meter
Z = 4539147
06 Z = 1383532
02
XDOT = 13976
231019 XDOT = 4259
955215
YDOT = -5126
673686 feet/sec YDOT = -1562
610139 meter/sec
ZDOT = 19043
358154 ZDOT = 5804
415565
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 13264
41342780
00016717 00000-0 10270-3 0 9057
2 25544 51
6490 351
4839 0002799 74
7493 285
3967 15
50420054 9635
Satellite: ISS
Catalog Number: 25544
Epoch time: 13264
41342780 = yrday
fracday
Element set: 905
Inclination: 51
6490 deg
RA of node: 351
4839 deg
Eccentricity:
0002799
Arg of perigee: 74
7493 deg
Mean anomaly: 285
3967 deg
Mean motion: 15
50420054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 963
Checksum: 326
Coasting Arc #7 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2013/265/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6547102
30 A = 6798607
79 meter
Y = 106095
87 meter E =
0008701
Z = -1824066
74 I = 51
58267
XDOT = 1483
948323 Wp = 122
94510
YDOT = -4964
768509 meter/sec RA = 346
30799 deg
ZDOT = -5639
291636 TA = 77
08430
MA = 76
98712
Ha = 227
803 n
mi
Hp = 219
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21479994
43 X = -6538941
17
Y = 348083
57 feet Y = 32927
43 meter
Z = -5984470
94 Z = -1855852
52
XDOT = 4868
596861 XDOT = 1566
749629
YDOT = -16288
610593 feet/sec YDOT = -4947
711749 meter/sec
ZDOT = -18501
612979 ZDOT = -5631
880963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13225344
24 X = 4031084
92
Y = 16881583
56 feet Y = 5145506
67 meter
Z = -6117811
82 Z = -1864709
04
XDOT = -14762
869099 XDOT = -4499
722501
YDOT = 4900
284694 feet/sec YDOT = 1493
606775 meter/sec
ZDOT = -18469
772817 ZDOT = -5629
586755
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 13265
38027228
00016717 00000-0 10270-3 0 9062
2 25544 51
6484 346
6912 0002866 74
4936 285
6531 15
50437386 9782
Satellite: ISS
Catalog Number: 25544
Epoch time: 13265
38027228 = yrday
fracday
Element set: 906
Inclination: 51
6484 deg
RA of node: 346
6912 deg
Eccentricity:
0002866
Arg of perigee: 74
4936 deg
Mean anomaly: 285
6531 deg
Mean motion: 15
50437386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 978
Checksum: 338
Coasting Arc #8 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2013/266/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6399233
77 A = 6797729
76 meter
Y = -270803
37 meter E =
0016632
Z = 2254515
30 I = 51
55149
XDOT = -1707
538269 Wp = 73
16966
YDOT = 5130
283455 meter/sec RA = 341
34801 deg
ZDOT = 5434
375993 TA = 311
91478
MA = 312
05648
Ha = 227
716 n
mi
Hp = 219
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20994861
46 X = 6390834
39
Y = -888462
51 feet Y = -199289
81 meter
Z = 7396703
73 Z = 2285582
18
XDOT = -5602
159675 XDOT = -1791
178353
YDOT = 16831
638631 feet/sec YDOT = 5110
721567 meter/sec
ZDOT = 17829
317562 ZDOT = 5425
877152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13633767
15 X = -4155572
23
Y = -15929492
69 feet Y = -4855309
37 meter
Z = 7527048
24 Z = 2294244
30
XDOT = 15606
526204 XDOT = 4756
869187
YDOT = -4906
317547 feet/sec YDOT = -1495
445588 meter/sec
ZDOT = 17792
888281 ZDOT = 5423
272348
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 13266
41155279
00016717 00000-0 10270-3 0 9076
2 25544 51
6494 341
5794 0002840 79
8488 280
2983 15
50482853 9947
Satellite: ISS
Catalog Number: 25544
Epoch time: 13266
41155279 = yrday
fracday
Element set: 907
Inclination: 51
6494 deg
RA of node: 341
5794 deg
Eccentricity:
0002840
Arg of perigee: 79
8488 deg
Mean anomaly: 280
2983 deg
Mean motion: 15
50482853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 994
Checksum: 347
Coasting Arc #9 (Orbit 1008)
---------------------------------------
Vector Time (GMT): 2013/267/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6220760
43 A = 6796740
50 meter
Y = 362461
72 meter E =
0007215
Z = -2717183
09 I = 51
51910
XDOT = 1936
186820 Wp = 106
20796
YDOT = -5319
282953 meter/sec RA = 336
38493 deg
ZDOT = -5155
690176 TA = 104
49582
MA = 104
41576
Ha = 227
753 n
mi
Hp = 219
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20409319
00 X = -6211151
73
Y = 1189178
86 feet Y = 292950
71 meter
Z = -8914642
67 Z = -2747379
99
XDOT = 6352
318962 XDOT = 2020
569521
YDOT = -17451
715725 feet/sec YDOT = -5297
159918 meter/sec
ZDOT = -16914
994015 ZDOT = -5146
078831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13763601
61 X = 4195145
77
Y = 15041363
05 feet Y = 4584607
46 meter
Z = -9041347
84 Z = -2755802
82
XDOT = -16518
046194 XDOT = -5034
700480
YDOT = 4997
996733 feet/sec YDOT = 1523
389404 meter/sec
ZDOT = -16873
870857 ZDOT = -5143
155837
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 13267
37836268
00016717 00000-0 10270-3 0 9087
2 25544 51
6491 336
7865 0002881 80
7639 279
3837 15
50482613 10092
Satellite: ISS
Catalog Number: 25544
Epoch time: 13267
37836268 = yrday
fracday
Element set: 908
Inclination: 51
6491 deg
RA of node: 336
7865 deg
Eccentricity:
0002881
Arg of perigee: 80
7639 deg
Mean anomaly: 279
3837 deg
Mean motion: 15
50482613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1009
Checksum: 343
Coasting Arc #10 (Orbit 1024)
---------------------------------------
Vector Time (GMT): 2013/268/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6011716
06 A = 6795563
98 meter
Y = -446411
28 meter E =
0015769
Z = 3121539
84 I = 51
48867
XDOT = -2116
516019 Wp = 84
97133
YDOT = 5547
805139 meter/sec RA = 331
41904 deg
ZDOT = 4849
734504 TA = 311
01899
MA = 311
15522
Ha = 227
620 n
mi
Hp = 219
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19723477
88 X = 6001097
39
Y = -1464603
93 feet Y = -379243
58 meter
Z = 10241272
45 Z = 3150718
71
XDOT = -6943
950193 XDOT = -2201
954391
YDOT = 18201
460429 feet/sec YDOT = 5523
659578 meter/sec
ZDOT = 15911
202440 ZDOT = 4839
244610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13783781
16 X = -4201296
50
Y = -14094149
19 feet Y = -4295896
67 meter
Z = 10363717
55 Z = 3158861
11
XDOT = 17431
773695 XDOT = 5313
204622
YDOT = -5333
804790 feet/sec YDOT = -1625
743700 meter/sec
ZDOT = 15866
361971 ZDOT = 4836
067129
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 13268
40960536
00016717 00000-0 10270-3 0 9099
2 25544 51
6499 331
6743 0002895 84
4083 275
7398 15
50541631 10254
Satellite: ISS
Catalog Number: 25544
Epoch time: 13268
40960536 = yrday
fracday
Element set: 909
Inclination: 51
6499 deg
RA of node: 331
6743 deg
Eccentricity:
0002895
Arg of perigee: 84
4083 deg
Mean anomaly: 275
7398 deg
Mean motion: 15
50541631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1025
Checksum: 327
Coasting Arc #11 (Orbit 1039)
---------------------------------------
Vector Time (GMT): 2013/269/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5784433
79 A = 6794399
42 meter
Y = 448375
24 meter E =
0008170
Z = -3543866
81 I = 51
45817
XDOT = 2282
879042 Wp = 84
02324
YDOT = -5782
675371 meter/sec RA = 326
45031 deg
ZDOT = -4465
902588 TA = 137
77092
MA = 137
70797
Ha = 227
694 n
mi
Hp = 219
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18977801
14 X = -5771802
44
Y = 1471047
37 feet Y = 383760
38 meter
Z = -11626859
62 Z = -3571936
60
XDOT = 7489
760638 XDOT = 2369
066806
YDOT = -18972
032058 feet/sec YDOT = -5756
665205 meter/sec
ZDOT = -14651
911378 ZDOT = -4454
602708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13533219
65 X = 4124925
35
Y = 13282315
87 feet Y = 4048449
88 meter
Z = -11744651
20 Z = -3579769
69
XDOT = -18313
480385 XDOT = -5581
948821
YDOT = 5769
584407 feet/sec YDOT = 1758
569327 meter/sec
ZDOT = -14603
641970 ZDOT = -4451
190073
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 13269
37638034
00016717 00000-0 10270-3 0 9103
2 25544 51
6499 326
8816 0002900 86
3023 273
8460 15
50532069 10404
Satellite: ISS
Catalog Number: 25544
Epoch time: 13269
37638034 = yrday
fracday
Element set: 910
Inclination: 51
6499 deg
RA of node: 326
8816 deg
Eccentricity:
0002900
Arg of perigee: 86
3023 deg
Mean anomaly: 273
8460 deg
Mean motion: 15
50532069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1040
Checksum: 301
Coasting Arc #12 (Orbit 1055)
---------------------------------------
Vector Time (GMT): 2013/270/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5537061
32 A = 6793069
63 meter
Y = -431765
05 meter E =
0013984
Z = 3900880
78 I = 51
42963
XDOT = -2398
145768 Wp = 97
07150
YDOT = 6046
244756 meter/sec RA = 321
47843 deg
ZDOT = 4059
018088 TA = 310
24756
MA = 310
36979
Ha = 227
531 n
mi
Hp = 219
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18166211
67 X = 5522528
37
Y = -1416551
99 feet Y = -369927
05 meter
Z = 12798165
29 Z = 3927744
18
XDOT = -7867
932309 XDOT = -2485
295669
YDOT = 19836
761010 feet/sec YDOT = 6018
940207 meter/sec
ZDOT = 13316
988477 ZDOT = 4047
155893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13170456
78 X = -4014355
23
Y = -12476330
21 feet Y = -3802785
45 meter
Z = 12910892
83 Z = 3935240
14
XDOT = 19142
819515 XDOT = 5834
731388
YDOT = -6431
558559 feet/sec YDOT = -1960
339049 meter/sec
ZDOT = 13266
326624 ZDOT = 4043
576355
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 13270
40758561
00016717 00000-0 10270-3 0 9118
2 25544 51
6503 321
7690 0002955 88
9640 271
1850 15
50597188 10561
Satellite: ISS
Catalog Number: 25544
Epoch time: 13270
40758561 = yrday
fracday
Element set: 911
Inclination: 51
6503 deg
RA of node: 321
7690 deg
Eccentricity:
0002955
Arg of perigee: 88
9640 deg
Mean anomaly: 271
1850 deg
Mean motion: 15
50597188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1056
Checksum: 313
Coasting Arc #13 (Orbit 1070)
---------------------------------------
Vector Time (GMT): 2013/271/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5288278
10 A = 6791887
38 meter
Y = 329730
08 meter E =
0011116
Z = -4260337
91 I = 51
40204
XDOT = 2484
804305 Wp = 74
95449
YDOT = -6292
989581 meter/sec RA = 316
50420 deg
ZDOT = -3576
403899 TA = 158
34544
MA = 158
29840
Ha = 227
630 n
mi
Hp = 219
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17349993
78 X = -5270876
54
Y = 1081791
59 feet Y = 270690
12 meter
Z = -13977486
59 Z = -4285985
73
XDOT = 8152
245096 XDOT = 2572
362477
YDOT = -20646
291276 feet/sec YDOT = -6264
713667 meter/sec
ZDOT = -11733
608592 ZDOT = -3564
119681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12576180
25 X = 3833219
74
Y = 11874862
91 feet Y = 3619458
22 meter
Z = -14085098
85 Z = -4293138
13
XDOT = -19835
341827 XDOT = -6045
812189
YDOT = 7170
835402 feet/sec YDOT = 2185
670631 meter/sec
ZDOT = -11681
147513 ZDOT = -3560
413762
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 13271
37432537
00016717 00000-0 10270-3 0 9128
2 25544 51
6503 316
9765 0002924 91
4150 268
7336 15
50584073 10718
Satellite: ISS
Catalog Number: 25544
Epoch time: 13271
37432537 = yrday
fracday
Element set: 912
Inclination: 51
6503 deg
RA of node: 316
9765 deg
Eccentricity:
0002924
Arg of perigee: 91
4150 deg
Mean anomaly: 268
7336 deg
Mean motion: 15
50584073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1071
Checksum: 300
Coasting Arc #14 (Orbit 1086)
---------------------------------------
Vector Time (GMT): 2013/272/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5032159
15 A = 6790589
92 meter
Y = -202271
33 meter E =
0011436
Z = 4547475
02 I = 51
37677
XDOT = -2523
710429 Wp = 108
20870
YDOT = 6554
853840 meter/sec RA = 311
52652 deg
ZDOT = 3074
367502 TA = 310
86229
MA = 310
96134
Ha = 227
439 n
mi
Hp = 219
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16509708
51 X = 5011956
53
Y = -663619
85 feet Y = -146111
04 meter
Z = 14919537
48 Z = 4571871
80
XDOT = -8279
889860 XDOT = -2611
755159
YDOT = 21505
425985 feet/sec YDOT = 6526
140123 meter/sec
ZDOT = 10086
507554 ZDOT = 3061
893013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11889699
66 X = -3623980
46
Y = -11339381
17 feet Y = -3456243
38 meter
Z = 15021882
09 Z = 4578669
66
XDOT = 20431
268582 XDOT = 6227
450664
YDOT = -8088
610971 feet/sec YDOT = -2465
408624 meter/sec
ZDOT = 10033
219210 ZDOT = 3058
125215
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 13272
40549317
00016717 00000-0 10270-3 0 9139
2 25544 51
6503 311
8636 0002991 93
7971 266
3522 15
50651328 10875
Satellite: ISS
Catalog Number: 25544
Epoch time: 13272
40549317 = yrday
fracday
Element set: 913
Inclination: 51
6503 deg
RA of node: 311
8636 deg
Eccentricity:
0002991
Arg of perigee: 93
7971 deg
Mean anomaly: 266
3522 deg
Mean motion: 15
50651328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1087
Checksum: 308
Coasting Arc #15 (Orbit 1101)
---------------------------------------
Vector Time (GMT): 2013/273/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4794047
54 A = 6789592
13 meter
Y = -6609
27 meter E =
0014378
Z = -4821369
75 I = 51
35303
XDOT = 2526
430411 Wp = 76
73031
YDOT = -6773
469607 meter/sec RA = 306
54698 deg
ZDOT = -2505
927428 TA = 168
49256
MA = 168
45965
Ha = 227
561 n
mi
Hp = 218
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15728502
41 X = -4770196
35
Y = -21683
94 feet Y = -60086
54 meter
Z = -15818142
21 Z = -4844600
92
XDOT = 8288
813686 XDOT = 2614
158216
YDOT = -22222
669314 feet/sec YDOT = -6744
727225 meter/sec
ZDOT = -8221
546680 ZDOT = -2493
440374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11041987
54 X = 3365597
80
Y = 11062059
68 feet Y = 3371715
79 meter
Z = -15915565
59 Z = -4851064
39
XDOT = -20799
196878 XDOT = -6339
595208
YDOT = 9024
000882 feet/sec YDOT = 2750
515469 meter/sec
ZDOT = -8168
184753 ZDOT = -2489
662713
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 13273
37219730
00016717 00000-0 10270-3 0 9140
2 25544 51
6498 307
0711 0002948 96
2734 263
8753 15
50636667 11021
Satellite: ISS
Catalog Number: 25544
Epoch time: 13273
37219730 = yrday
fracday
Element set: 914
Inclination: 51
6498 deg
RA of node: 307
0711 deg
Eccentricity:
0002948
Arg of perigee: 96
2734 deg
Mean anomaly: 263
8753 deg
Mean motion: 15
50636667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1102
Checksum: 315
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