[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 17th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
243/07:34:14
242 0
4 1
1 1
1
N/A 1
0 -0
1 227
6
000/00:02:28
485 -0
4 -0
0 220
5
Coasting Arc #1 (Orbit 408)
---------------------------------------
Vector Time (GMT): 2013/228/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6404400
80 A = 6798454
49 meter
Y = 399024
74 meter E =
0001723
Z = -2244558
28 I = 51
73417
XDOT = -2215
617765 Wp = 134
56593
YDOT = 4895
853504 meter/sec RA = 167
54886 deg
ZDOT = -5455
230287 TA = 70
30204
MA = 70
28345
Ha = 226
559 n
mi
Hp = 221
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21011813
66 X = 6410366
17
Y = 1309136
29 feet Y = 470676
23 meter
Z = -7364036
36 Z = -2213432
13
XDOT = -7269
087156 XDOT = -2243
699868
YDOT = 16062
511497 feet/sec YDOT = 4870
920208 meter/sec
ZDOT = -17897
737163 ZDOT = -5466
061501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19173519
18 X = -5844088
65
Y = 8802854
65 feet Y = 2683110
10 meter
Z = -7233608
71 Z = -2204803
93
XDOT = -644
595475 XDOT = -196
472701
YDOT = -16138
660077 feet/sec YDOT = -4919
063591 meter/sec
ZDOT = -17943
742793 ZDOT = -5469
252803
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 13228
70514280
00016717 00000-0 10270-3 0 9000
2 25544 51
6495 168
4818 0004405 318
4644 41
6171 15
50290755 4093
Satellite: ISS
Catalog Number: 25544
Epoch time: 13228
70514280 = yrday
fracday
Element set: 900
Inclination: 51
6495 deg
RA of node: 168
4818 deg
Eccentricity:
0004405
Arg of perigee: 318
4644 deg
Mean anomaly: 41
6171 deg
Mean motion: 15
50290755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 409
Checksum: 297
Coasting Arc #2 (Orbit 424)
---------------------------------------
Vector Time (GMT): 2013/229/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6253070
43 A = 6797557
59 meter
Y = -218393
02 meter E =
0012584
Z = 2637348
83 I = 51
76120
XDOT = 2388
523885 Wp = 57
70148
YDOT = -5068
873487 meter/sec RA = 162
60039 deg
ZDOT = 5231
700852 TA = 331
93674
MA = 332
00453
Ha = 226
785 n
mi
Hp = 221
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20515322
93 X = -6262974
89
Y = -716512
52 feet Y = -288374
25 meter
Z = 8652719
25 Z = 2606948
40
XDOT = 7836
364453 XDOT = 2419
613838
YDOT = -16630
162358 feet/sec YDOT = -5041
989783 meter/sec
ZDOT = 17164
372873 ZDOT = 5243
379300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18303679
53 X = 5578961
52
Y = -9410425
57 feet Y = -2868297
71 meter
Z = 8525293
08 Z = 2598509
33
XDOT = 679
603566 XDOT = 207
143167
YDOT = 16951
902501 feet/sec YDOT = 5166
939882 meter/sec
ZDOT = 17213
958668 ZDOT = 5246
814602
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 13229
73650183
00016717 00000-0 10270-3 0 9018
2 25544 51
6494 163
3693 0004548 324
6498 35
4350 15
50325688 4253
Satellite: ISS
Catalog Number: 25544
Epoch time: 13229
73650183 = yrday
fracday
Element set: 901
Inclination: 51
6494 deg
RA of node: 163
3693 deg
Eccentricity:
0004548
Arg of perigee: 324
6498 deg
Mean anomaly: 35
4350 deg
Mean motion: 15
50325688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 425
Checksum: 315
Coasting Arc #3 (Orbit 439)
---------------------------------------
Vector Time (GMT): 2013/230/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6083032
13 A = 6796601
54 meter
Y = 82538
06 meter E =
0002691
Z = -3034551
63 I = 51
78702
XDOT = -2540
823992 Wp = 38
71214
YDOT = 5258
441893 meter/sec RA = 157
65433 deg
ZDOT = -4950
613707 TA = 175
90528
MA = 175
90307
Ha = 226
714 n
mi
Hp = 221
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19957454
51 X = 6096397
81
Y = 270794
16 feet Y = 150637
12 meter
Z = -9955878
06 Z = -3004968
94
XDOT = -8336
036718 XDOT = -2575
387939
YDOT = 17252
105949 feet/sec YDOT = 5229
835552 meter/sec
ZDOT = -16242
170955 ZDOT = -4963
040483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17439718
09 X = -5315626
07
Y = 9832794
87 feet Y = 2997035
88 meter
Z = -9831846
52 Z = -2996746
82
XDOT = -839
088508 XDOT = -255
754177
YDOT = -17780
487536 feet/sec YDOT = -5419
492601 meter/sec
ZDOT = -16294
923709 ZDOT = -4966
692746
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 13230
70339088
00016717 00000-0 10270-3 0 9026
2 25544 51
6493 158
5774 0004527 325
5905 34
4952 15
50331332 4405
Satellite: ISS
Catalog Number: 25544
Epoch time: 13230
70339088 = yrday
fracday
Element set: 902
Inclination: 51
6493 deg
RA of node: 158
5774 deg
Eccentricity:
0004527
Arg of perigee: 325
5905 deg
Mean anomaly: 34
4952 deg
Mean motion: 15
50331332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 440
Checksum: 295
Coasting Arc #4 (Orbit 455)
---------------------------------------
Vector Time (GMT): 2013/231/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5878890
80 A = 6795562
04 meter
Y = 28101
17 meter E =
0011088
Z = 3395195
14 I = 51
81186
XDOT = 2661
836148 Wp = 67
79765
YDOT = -5485
996904 meter/sec RA = 152
70834 deg
ZDOT = 4646
416227 TA = 331
71747
MA = 331
77763
Ha = 226
969 n
mi
Hp = 221
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19287699
48 X = -5895260
68
Y = 92195
43 feet Y = -37731
78 meter
Z = 11139091
66 Z = 3366596
89
XDOT = 8733
058227 XDOT = 2700
413396
YDOT = -17998
677507 feet/sec YDOT = -5456
014773 meter/sec
ZDOT = 15244
147727 ZDOT = 4659
440713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16513311
79 X = 5033257
43
Y = -10099102
02 feet Y = -3078206
30 meter
Z = 11019159
97 Z = 3358639
96
XDOT = 1188
669730 XDOT = 362
306534
YDOT = 18666
004913 feet/sec YDOT = 5689
398297 meter/sec
ZDOT = 15299
439794 ZDOT = 4663
269249
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 13231
73472978
00016717 00000-0 10270-3 0 9037
2 25544 51
6493 153
4649 0004643 330
9603 29
1289 15
50353114 4567
Satellite: ISS
Catalog Number: 25544
Epoch time: 13231
73472978 = yrday
fracday
Element set: 903
Inclination: 51
6493 deg
RA of node: 153
4649 deg
Eccentricity:
0004643
Arg of perigee: 330
9603 deg
Mean anomaly: 29
1289 deg
Mean motion: 15
50353114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 456
Checksum: 308
Coasting Arc #5 (Orbit 470)
---------------------------------------
Vector Time (GMT): 2013/232/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5669118
78 A = 6794447
41 meter
Y = -89079
89 meter E =
0006265
Z = -3751619
73 I = 51
83453
XDOT = -2747
835713 Wp = 34
53375
YDOT = 5715
657056 meter/sec RA = 147
76435 deg
ZDOT = -4286
486678 TA = 190
04229
MA = 190
05481
Ha = 226
870 n
mi
Hp = 221
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18599471
06 X = 5687917
51
Y = -292256
85 feet Y = -25579
27 meter
Z = -12308463
69 Z = -3724034
59
XDOT = -9015
209032 XDOT = -2790
723068
YDOT = 18752
155695 feet/sec YDOT = 5684
689024 meter/sec
ZDOT = -14063
276504 ZDOT = -4299
939557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15654138
69 X = -4771381
47
Y = 10188646
63 feet Y = 3105499
49 meter
Z = -12192761
69 Z = -3716353
76
XDOT = -1679
694630 XDOT = -511
970923
YDOT = -19484
634429 feet/sec YDOT = -5938
916574 meter/sec
ZDOT = -14120
397769 ZDOT = -4303
897240
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 13232
70159943
00016717 00000-0 10270-3 0 9040
2 25544 51
6486 148
6728 0004589 332
9731 27
1181 15
50373102 4711
Satellite: ISS
Catalog Number: 25544
Epoch time: 13232
70159943 = yrday
fracday
Element set: 904
Inclination: 51
6486 deg
RA of node: 148
6728 deg
Eccentricity:
0004589
Arg of perigee: 332
9731 deg
Mean anomaly: 27
1181 deg
Mean motion: 15
50373102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 471
Checksum: 305
Coasting Arc #6 (Orbit 486)
---------------------------------------
Vector Time (GMT): 2013/233/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5434346
21 A = 6793384
09 meter
Y = 114277
61 meter E =
0008987
Z = 4065835
07 I = 51
85643
XDOT = 2800
082642 Wp = 76
64317
YDOT = -5973
080128 meter/sec RA = 142
82030 deg
ZDOT = 3905
216369 TA = 332
96303
MA = 333
00982
Ha = 227
136 n
mi
Hp = 221
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17829219
84 X = -5454970
55
Y = 374926
54 feet Y = 53392
25 meter
Z = 13339353
91 Z = 4039385
89
XDOT = 9186
622842 XDOT = 2847
696686
YDOT = -19596
719580 feet/sec YDOT = -5941
501347 meter/sec
ZDOT = 12812
389661 ZDOT = 3918
934707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14791767
73 X = 4508530
80
Y = -10108062
98 feet Y = -3080937
60 meter
Z = 13228404
39 Z = 4032017
66
XDOT = 2351
812692 XDOT = 716
832509
YDOT = 20307
988002 feet/sec YDOT = 6189
874743 meter/sec
ZDOT = 12870
660828 ZDOT = 3922
977420
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 13233
73291812
00016717 00000-0 10270-3 0 9057
2 25544 51
6485 143
5601 0004677 337
3750 22
7194 15
50377753 4870
Satellite: ISS
Catalog Number: 25544
Epoch time: 13233
73291812 = yrday
fracday
Element set: 905
Inclination: 51
6485 deg
RA of node: 143
5601 deg
Eccentricity:
0004677
Arg of perigee: 337
3750 deg
Mean anomaly: 22
7194 deg
Mean motion: 15
50377753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 487
Checksum: 311
Coasting Arc #7 (Orbit 501)
---------------------------------------
Vector Time (GMT): 2013/234/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5209549
50 A = 6792241
66 meter
Y = -89742
23 meter E =
0009778
Z = -4367509
45 I = 51
87557
XDOT = -2807
587097 Wp = 42
05768
YDOT = 6214
622120 meter/sec RA = 137
87754 deg
ZDOT = -3474
014727 TA = 192
68888
MA = 192
71351
Ha = 227
019 n
mi
Hp = 221
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17091697
85 X = 5231381
72
Y = -294429
87 feet Y = -31364
01 meter
Z = -14329099
24 Z = -4342149
25
XDOT = -9211
243757 XDOT = -2859
996106
YDOT = 20389
180185 feet/sec YDOT = 6182
932594 meter/sec
ZDOT = -11397
686112 ZDOT = -3487
781321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14055433
69 X = -4284096
19
Y = 9884083
81 feet Y = 3012668
75 meter
Z = -14222713
54 Z = -4335083
09
XDOT = -3152
611425 XDOT = -960
915962
YDOT = -20980
186124 feet/sec YDOT = -6394
760731 meter/sec
ZDOT = -11456
195987 ZDOT = -3491
848537
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 13234
69976831
00016717 00000-0 10270-3 0 9065
2 25544 51
6472 138
7676 0004572 340
5821 19
5155 15
50411339 5021
Satellite: ISS
Catalog Number: 25544
Epoch time: 13234
69976831 = yrday
fracday
Element set: 906
Inclination: 51
6472 deg
RA of node: 138
7676 deg
Eccentricity:
0004572
Arg of perigee: 340
5821 deg
Mean anomaly: 19
5155 deg
Mean motion: 15
50411339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 502
Checksum: 310
Coasting Arc #8 (Orbit 517)
---------------------------------------
Vector Time (GMT): 2013/235/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4970904
86 A = 6791279
91 meter
Y = 22320
09 meter E =
0006604
Z = 4621088
56 I = 51
89423
XDOT = 2783
342823 Wp = 81
50012
YDOT = -6471
648443 meter/sec RA = 132
93470 deg
ZDOT = 3022
566554 TA = 338
41416
MA = 338
44199
Ha = 227
289 n
mi
Hp = 220
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16308742
97 X = -4993232
78
Y = 73228
64 feet Y = -33392
19 meter
Z = 15161051
72 Z = 4596886
36
XDOT = 9131
702174 XDOT = 2840
820674
YDOT = -21232
442398 feet/sec YDOT = -6440
201715 meter/sec
ZDOT = 9916
556937 ZDOT = 3036
227787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13374327
72 X = 4076495
09
Y = -9496103
68 feet Y = -2894412
40 meter
Z = 15059525
96 Z = 4590143
51
XDOT = 4101
527742 XDOT = 1250
145656
YDOT = 21609
377311 feet/sec YDOT = 6586
538204 meter/sec
ZDOT = 9974
665712 ZDOT = 3040
278109
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 13235
73106645
00016717 00000-0 10270-3 0 9070
2 25544 51
6470 133
6546 0004645 344
3169 15
7838 15
50400832 5186
Satellite: ISS
Catalog Number: 25544
Epoch time: 13235
73106645 = yrday
fracday
Element set: 907
Inclination: 51
6470 deg
RA of node: 133
6546 deg
Eccentricity:
0004645
Arg of perigee: 344
3169 deg
Mean anomaly: 15
7838 deg
Mean motion: 15
50400832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 518
Checksum: 300
Coasting Arc #9 (Orbit 532)
---------------------------------------
Vector Time (GMT): 2013/236/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4758747
88 A = 6790255
33 meter
Y = 89157
67 meter E =
0012786
Z = -4854759
97 I = 51
91040
XDOT = -2710
777876 Wp = 51
72322
YDOT = 6693
387975 meter/sec RA = 127
99278 deg
ZDOT = -2531
061584 TA = 193
40888
MA = 193
44289
Ha = 227
159 n
mi
Hp = 220
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15612689
90 X = 4780980
19
Y = 292512
03 feet Y = 142496
94 meter
Z = -15927690
18 Z = -4831588
55
XDOT = -8893
628203 XDOT = -2773
128193
YDOT = 21959
934301 feet/sec YDOT = 6662
725525 meter/sec
ZDOT = -8304
007822 ZDOT = -2544
382170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12865932
29 X = -3921536
16
Y = 9021979
55 feet Y = 2749899
37 meter
Z = -15830496
99 Z = -4825135
48
XDOT = -5136
868749 XDOT = -1565
717595
YDOT = -22014
162094 feet/sec YDOT = -6709
916606 meter/sec
ZDOT = -8360
727026 ZDOT = -2548
349597
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 13236
69789714
00016717 00000-0 10270-3 0 9081
2 25544 51
6459 128
8616 0004501 348
4863 11
6184 15
50445673 5332
Satellite: ISS
Catalog Number: 25544
Epoch time: 13236
69789714 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 128
8616 deg
Eccentricity:
0004501
Arg of perigee: 348
4863 deg
Mean anomaly: 11
6184 deg
Mean motion: 15
50445673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 533
Checksum: 327
Coasting Arc #10 (Orbit 548)
---------------------------------------
Vector Time (GMT): 2013/237/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4544560
92 A = 6789524
72 meter
Y = -246428
67 meter E =
0004522
Z = 5034114
63 I = 51
92579
XDOT = 2613
097541 Wp = 74
48893
YDOT = -6917
541594 meter/sec RA = 123
05076 deg
ZDOT = 2020
025625 TA = 355
95195
MA = 355
95560
Ha = 227
433 n
mi
Hp = 220
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14909976
77 X = -4565921
81
Y = -808493
02 feet Y = -297367
95 meter
Z = 16516124
12 Z = 5011985
78
XDOT = 8573
154663 XDOT = 2680
444091
YDOT = -22695
346437 feet/sec YDOT = -6887
943595 meter/sec
ZDOT = 6627
380661 ZDOT = 2032
883790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12462319
50 X = 3798514
98
Y = -8408840
73 feet Y = -2563014
66 meter
Z = 16423319
22 Z = 5005827
70
XDOT = 6266
426614 XDOT = 1910
006832
YDOT = 22340
299080 feet/sec YDOT = 6809
323160 meter/sec
ZDOT = 6682
202229 ZDOT = 2036
735239
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 13237
72917470
00016717 00000-0 10270-3 0 9099
2 25544 51
6457 123
7482 0004571 352
1003 8
0075 15
50423708 5491
Satellite: ISS
Catalog Number: 25544
Epoch time: 13237
72917470 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 123
7482 deg
Eccentricity:
0004571
Arg of perigee: 352
1003 deg
Mean anomaly: 8
0075 deg
Mean motion: 15
50423708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 549
Checksum: 294
Coasting Arc #11 (Orbit 563)
---------------------------------------
Vector Time (GMT): 2013/238/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4372284
56 A = 6788751
82 meter
Y = 436089
64 meter E =
0014950
Z = -5187864
67 I = 51
93957
XDOT = -2470
350987 Wp = 61
80131
YDOT = 7088
313503 meter/sec RA = 118
10993 deg
ZDOT = -1482
533918 TA = 193
93202
MA = 193
97331
Ha = 227
290 n
mi
Hp = 220
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14344765
61 X = 4392284
31
Y = 1430740
29 feet Y = 485094
86 meter
Z = -17020553
39 Z = -5166576
03
XDOT = -8104
826074 XDOT = -2542
228731
YDOT = 23255
621728 feet/sec YDOT = 7060
286506 meter/sec
ZDOT = -4863
956425 ZDOT = -1494
709561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12257048
21 X = -3735948
29
Y = 7785541
74 feet Y = 2373033
12 meter
Z = -16931292
47 Z = -5160657
95
XDOT = -7416
416575 XDOT = -2260
523772
YDOT = -22392
614936 feet/sec YDOT = -6825
269033 meter/sec
ZDOT = -4915
951779 ZDOT = -1498
382102
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 13238
69598594
00016717 00000-0 10270-3 0 9100
2 25544 51
6456 118
9552 0004422 356
7315 3
3807 15
50478532 5648
Satellite: ISS
Catalog Number: 25544
Epoch time: 13238
69598594 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 118
9552 deg
Eccentricity:
0004422
Arg of perigee: 356
7315 deg
Mean anomaly: 3
3807 deg
Mean motion: 15
50478532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 564
Checksum: 322
Coasting Arc #12 (Orbit 579)
---------------------------------------
Vector Time (GMT): 2013/239/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4208852
09 A = 6788372
90 meter
Y = -670081
84 meter E =
0004031
Z = 5280841
27 I = 51
95151
XDOT = 2313
633312 Wp = 48
53135
YDOT = -7248
936109 meter/sec RA = 113
16864 deg
ZDOT = 926
304925 TA = 32
65401
MA = 32
62910
Ha = 227
566 n
mi
Hp = 220
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13808569
84 X = -4226699
06
Y = -2198431
22 feet Y = -717247
48 meter
Z = 17325594
72 Z = 5260351
81
XDOT = 7590
660471 XDOT = 2390
020825
YDOT = -23782
598782 feet/sec YDOT = -7222
636451 meter/sec
ZDOT = 3039
058154 ZDOT = 937
730116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12190150
50 X = 3715557
87
Y = -7062470
34 feet Y = -2152640
96 meter
Z = 17239712
20 Z = 5254664
28
XDOT = 8591
110833 XDOT = 2618
570582
YDOT = 22349
180484 feet/sec YDOT = 6812
030212 meter/sec
ZDOT = 3087
941493 ZDOT = 941
204567
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 13239
72724311
00016717 00000-0 10270-3 0 9114
2 25544 51
6454 113
8417 0004492
5684 359
5471 15
50448130 5802
Satellite: ISS
Catalog Number: 25544
Epoch time: 13239
72724311 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 113
8417 deg
Eccentricity:
0004492
Arg of perigee:
5684 deg
Mean anomaly: 359
5471 deg
Mean motion: 15
50448130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 580
Checksum: 290
Coasting Arc #13 (Orbit 594)
---------------------------------------
Vector Time (GMT): 2013/240/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4099534
55 A = 6787957
31 meter
Y = 919449
70 meter E =
0015963
Z = -5344804
70 I = 51
96280
XDOT = -2121
564156 Wp = 71
48896
YDOT = 7342
360898 meter/sec RA = 108
22926 deg
ZDOT = -360
141246 TA = 195
06103
MA = 195
10862
Ha = 227
411 n
mi
Hp = 220
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13449916
50 X = 4114911
83
Y = 3016567
26 feet Y = 965379
11 meter
Z = -17535448
50 Z = -5324852
33
XDOT = -6960
512322 XDOT = -2201
760902
YDOT = 24089
110559 feet/sec YDOT = 7318
187806 meter/sec
ZDOT = -1181
565769 ZDOT = -370
642573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12319658
71 X = -3755031
97
Y = 6414897
48 feet Y = 1955260
75 meter
Z = -17451847
62 Z = -5319323
16
XDOT = -9707
579765 XDOT = -2958
870312
YDOT = -22016
425147 feet/sec YDOT = -6710
606385 meter/sec
ZDOT = -1226
600164 ZDOT = -373
867730
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 13240
69403495
00016717 00000-0 10270-3 0 9120
2 25544 51
6463 109
0491 0004371 4
9119 355
2074 15
50511110 5955
Satellite: ISS
Catalog Number: 25544
Epoch time: 13240
69403495 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 109
0491 deg
Eccentricity:
0004371
Arg of perigee: 4
9119 deg
Mean anomaly: 355
2074 deg
Mean motion: 15
50511110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 595
Checksum: 279
Coasting Arc #14 (Orbit 610)
---------------------------------------
Vector Time (GMT): 2013/241/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4007336
21 A = 6788014
00 meter
Y = -1207762
22 meter E =
0005734
Z = 5341587
42 I = 51
97107
XDOT = 1930
679291 Wp = 33
03830
YDOT = -7414
746717 meter/sec RA = 103
28872 deg
ZDOT = -223
301460 TA = 59
10935
MA = 59
05298
Ha = 227
677 n
mi
Hp = 220
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13147428
52 X = -4019480
69
Y = -3962474
48 feet Y = -1252642
54 meter
Z = 17524893
11 Z = 5322090
84
XDOT = 6334
249641 XDOT = 2014
533845
YDOT = -24326
596841 feet/sec YDOT = -7392
687786 meter/sec
ZDOT = -732
616340 ZDOT = -213
718572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12600201
30 X = 3840541
36
Y = -5713694
08 feet Y = -1741533
95 meter
Z = 17443238
99 Z = 5316699
24
XDOT = 10770
826832 XDOT = 3282
948018
YDOT = 21593
510749 feet/sec YDOT = 6581
702076 meter/sec
ZDOT = -691
412309 ZDOT = -210
742472
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 13241
72527177
00016717 00000-0 10270-3 0 9130
2 25544 51
6459 103
9354 0004438 8
9613 351
1616 15
50476220 6116
Satellite: ISS
Catalog Number: 25544
Epoch time: 13241
72527177 = yrday
fracday
Element set: 913
Inclination: 51
6459 deg
RA of node: 103
9354 deg
Eccentricity:
0004438
Arg of perigee: 8
9613 deg
Mean anomaly: 351
1616 deg
Mean motion: 15
50476220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 611
Checksum: 290
Coasting Arc #15 (Orbit 625)
---------------------------------------
Vector Time (GMT): 2013/242/16:15:15
655
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3976362
50 A = 6788022
34 meter
Y = 1490493
23 meter E =
0015616
Z = -5308624
38 I = 51
97910
XDOT = -1719
061254 Wp = 80
01051
YDOT = 7413
102528 meter/sec RA = 98
35078 deg
ZDOT = 798
348088 TA = 197
57330
MA = 197
62738
Ha = 227
516 n
mi
Hp = 219
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13045808
74 X = 3985187
54
Y = 4890069
67 feet Y = 1535008
60 meter
Z = -17416746
66 Z = -5289286
39
XDOT = -5639
964744 XDOT = -1805
706541
YDOT = 24321
202521 feet/sec YDOT = 7393
394461 meter/sec
ZDOT = 2619
252258 ZDOT = 789
786423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13044931
06 X = -3976094
99
Y = 5171947
62 feet Y = 1576409
63 meter
Z = -17335792
53 Z = -5283949
56
XDOT = -11699
523645 XDOT = -3566
014807
YDOT = -20904
555169 feet/sec YDOT = -6371
708416 meter/sec
ZDOT = 2582
321781 ZDOT = 787
091679
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 13242
69204412
00016717 00000-0 10270-3 0 9142
2 25544 51
6471 99
1434 0004364 12
3386 347
7870 15
50542031 6262
Satellite: ISS
Catalog Number: 25544
Epoch time: 13242
69204412 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 99
1434 deg
Eccentricity:
0004364
Arg of perigee: 12
3386 deg
Mean anomaly: 347
7870 deg
Mean motion: 15
50542031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 626
Checksum: 288
Coasting Arc #16 (Orbit 635)
---------------------------------------
Vector Time (GMT): 2013/243/07:35:28
485
Vector Time (MET): N/A
Weight (LBS) : 957353
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4080979
05 A = 6790197
57 meter
Y = -2291069
34 meter E =
0014100
Z = -4932663
61 I = 51
98910
XDOT = 1188
004843 Wp = 56
17901
YDOT = 7183
475792 meter/sec RA = 95
22608 deg
ZDOT = -2350
816429 TA = 190
85348
MA = 190
88394
Ha = 227
612 n
mi
Hp = 220
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13389038
87 X = 4130256
24
Y = -7516631
68 feet Y = -2245157
91 meter
Z = -16183279
55 Z = -4912719
03
XDOT = 3897
653684 XDOT = 1119
008847
YDOT = 23567
833964 feet/sec YDOT = 7196
374945 meter/sec
ZDOT = -7712
652326 ZDOT = -2345
213145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8144601
47 X = -2482474
53
Y = -13120357
75 feet Y = -3999085
04 meter
Z = -16099264
90 Z = -4907055
94
XDOT = 22398
608204 XDOT = 6827
095781
YDOT = -4456
717431 feet/sec YDOT = -1358
407473 meter/sec
ZDOT = -7690
110633 ZDOT = -2343
945721
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 13243
33655590
00016717 00000-0 10270-3 0 9152
2 25544 51
6492 95
9515 0004366 3
2386 356
8792 15
50351893 6369
Satellite: ISS
Catalog Number: 25544
Epoch time: 13243
33655590 = yrday
fracday
Element set: 915
Inclination: 51
6492 deg
RA of node: 95
9515 deg
Eccentricity:
0004366
Arg of perigee: 3
2386 deg
Mean anomaly: 356
8792 deg
Mean motion: 15
50351893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 636
Checksum: 325
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