[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 20th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 26371 58 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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 687)
---------------------------------------
Vector Time (GMT): 2014/139/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2438365
73 A = 6799712
94 meter
Y = 6241457
83 meter E =
0007762
Z = -1143744
62 I = 51
34944
XDOT = -4880
600918 Wp = 124
08825
YDOT = 842
263208 meter/sec RA = 240
81518 deg
ZDOT = -5841
590724 TA = 68
35317
MA = 68
27052
Ha = 227
428 n
mi
Hp = 220
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7999887
56 X = 2373947
08
Y = 20477223
85 feet Y = 6268365
10 meter
Z = -3752442
97 Z = -1132055
35
XDOT = -16012
470204 XDOT = -4861
279844
YDOT = 2763
330736 feet/sec YDOT = 787
793638 meter/sec
ZDOT = -19165
323896 ZDOT = -5865
253130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21689126
03 X = 6610845
61
Y = 3641142
75 feet Y = 1109820
31 meter
Z = -3704000
20 Z = -1128979
26
XDOT = -5532
866351 XDOT = -1686
417664
YDOT = 13470
386495 feet/sec YDOT = 4105
773804 meter/sec
ZDOT = -19265
550053 ZDOT = -5872
139656
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 14139
53788577
00016717 00000-0 10270-3 0 9005
2 25544 51
6475 241
6159 0003099 12
1702 347
9523 15
50377218 6886
Satellite: ISS
Catalog Number: 25544
Epoch time: 14139
53788577 = yrday
fracday
Element set: 900
Inclination: 51
6475 deg
RA of node: 241
6159 deg
Eccentricity:
0003099
Arg of perigee: 12
1702 deg
Mean anomaly: 347
9523 deg
Mean motion: 15
50377218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 688
Checksum: 325
Coasting Arc #2 (Orbit 703)
---------------------------------------
Vector Time (GMT): 2014/140/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2588196
10 A = 6799100
32 meter
Y = -6073683
43 meter E =
0016310
Z = 1587172
98 I = 51
36394
XDOT = 5070
571360 Wp = 54
52834
YDOT = -659
523867 meter/sec RA = 235
84077 deg
ZDOT = 5712
498538 TA = 322
88349
MA = 322
99617
Ha = 227
455 n
mi
Hp = 220
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8491457
02 X = -2527796
44
Y = -19926782
90 feet Y = -6102288
67 meter
Z = 5207260
42 Z = 1574746
22
XDOT = 16635
732807 XDOT = 5049
819855
YDOT = -2163
792216 feet/sec YDOT = -602
937813 meter/sec
ZDOT = 18741
793103 ZDOT = 5737
080321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21521348
89 X = -6559707
14
Y = -2558873
12 feet Y = -779944
53 meter
Z = 5155656
14 Z = 1571443
99
XDOT = 6183
894926 XDOT = 1884
851174
YDOT = -13823
292284 feet/sec YDOT = -4213
339488 meter/sec
ZDOT = 18845
887227 ZDOT = 5744
226427
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 14140
56919541
00016717 00000-0 10270-3 0 9018
2 25544 51
6478 236
5036 0003287 16
2819 343
8436 15
50417746 7047
Satellite: ISS
Catalog Number: 25544
Epoch time: 14140
56919541 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 236
5036 deg
Eccentricity:
0003287
Arg of perigee: 16
2819 deg
Mean anomaly: 343
8436 deg
Mean motion: 15
50417746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 704
Checksum: 309
Coasting Arc #3 (Orbit 718)
---------------------------------------
Vector Time (GMT): 2014/141/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2672092
28 A = 6798258
41 meter
Y = 5899940
01 meter E =
0005683
Z = -2066379
82 I = 51
37880
XDOT = -5293
423263 Wp = 109
61240
YDOT = 471
771823 meter/sec RA = 230
86762 deg
ZDOT = -5512
357242 TA = 93
28194
MA = 93
21693
Ha = 227
463 n
mi
Hp = 219
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8766706
97 X = 2615957
08
Y = 19356758
55 feet Y = 5929507
26 meter
Z = -6779461
35 Z = -2053535
24
XDOT = -17366
874224 XDOT = -5271
527905
YDOT = 1547
807817 feet/sec YDOT = 412
699987 meter/sec
ZDOT = -18085
161556 ZDOT = -5538
018881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21201313
39 X = 6462160
32
Y = 1662808
98 feet Y = 506824
18 meter
Z = -6726048
28 Z = -2050099
52
XDOT = -6878
401222 XDOT = -2096
536693
YDOT = 14299
085178 feet/sec YDOT = 4358
361162 meter/sec
ZDOT = -18193
802094 ZDOT = -5545
470878
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 14141
53602355
00016717 00000-0 10270-3 0 9029
2 25544 51
6469 231
7112 0003292 19
0169 341
1104 15
50452357 7190
Satellite: ISS
Catalog Number: 25544
Epoch time: 14141
53602355 = yrday
fracday
Element set: 902
Inclination: 51
6469 deg
RA of node: 231
7112 deg
Eccentricity:
0003292
Arg of perigee: 19
0169 deg
Mean anomaly: 341
1104 deg
Mean motion: 15
50452357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 719
Checksum: 273
Coasting Arc #4 (Orbit 734)
---------------------------------------
Vector Time (GMT): 2014/142/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2729875
60 A = 6797277
12 meter
Y = -5688875
62 meter E =
0015979
Z = 2504048
47 I = 51
39684
XDOT = 5550
177419 Wp = 65
64254
YDOT = -330
434796 meter/sec RA = 225
89410 deg
ZDOT = 5279
828535 TA = 322
52138
MA = 322
63269
Ha = 227
464 n
mi
Hp = 219
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8956284
77 X = -2678222
37
Y = -18664290
08 feet Y = -5719114
09 meter
Z = 8215382
11 Z = 2490912
32
XDOT = 18209
243500 XDOT = 5527
811994
YDOT = -1084
103661 feet/sec YDOT = -268
494339 meter/sec
ZDOT = 17322
272097 ZDOT = 5306
736402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20708213
78 X = -6311863
56
Y = -797665
44 feet Y = -243128
43 meter
Z = 8160690
89 Z = 2487378
58
XDOT = 7474
684003 XDOT = 2278
283684
YDOT = -14983
842647 feet/sec YDOT = -4567
075239 meter/sec
ZDOT = 17436
170798 ZDOT = 5314
544859
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 14142
56728022
00016717 00000-0 10270-3 0 9034
2 25544 51
6474 226
5984 0003417 22
4383 337
6917 15
50503856 7351
Satellite: ISS
Catalog Number: 25544
Epoch time: 14142
56728022 = yrday
fracday
Element set: 903
Inclination: 51
6474 deg
RA of node: 226
5984 deg
Eccentricity:
0003417
Arg of perigee: 22
4383 deg
Mean anomaly: 337
6917 deg
Mean motion: 15
50503856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 735
Checksum: 309
Coasting Arc #5 (Orbit 749)
---------------------------------------
Vector Time (GMT): 2014/143/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2714940
55 A = 6796154
96 meter
Y = 5483583
15 meter E =
0005858
Z = -2964217
92 I = 51
41472
XDOT = -5820
605701 Wp = 77
07915
YDOT = 200
076383 meter/sec RA = 220
92179 deg
ZDOT = -4968
033645 TA = 136
82052
MA = 136
77457
Ha = 227
500 n
mi
Hp = 219
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8907285
26 X = 2667819
48
Y = 17990758
38 feet Y = 5513679
97 meter
Z = -9725124
42 Z = -2951143
27
XDOT = -19096
475397 XDOT = -5798
277000
YDOT = 656
418580 feet/sec YDOT = 135
111612 meter/sec
ZDOT = -16299
322983 ZDOT = -4996
255425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20100607
87 X = 6126665
28
Y = 170903
08 feet Y = 52091
26 meter
Z = -9670652
41 Z = -2947614
85
XDOT = -8022
074489 XDOT = -2445
128304
YDOT = 15757
609220 feet/sec YDOT = 4802
919290 meter/sec
ZDOT = -16418
768978 ZDOT = -5004
440785
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 14143
53406059
00016717 00000-0 10270-3 0 9046
2 25544 51
6465 221
8057 0003496 25
7610 334
3715 15
50525940 7501
Satellite: ISS
Catalog Number: 25544
Epoch time: 14143
53406059 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 221
8057 deg
Eccentricity:
0003496
Arg of perigee: 25
7610 deg
Mean anomaly: 334
3715 deg
Mean motion: 15
50525940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 750
Checksum: 291
Coasting Arc #6 (Orbit 765)
---------------------------------------
Vector Time (GMT): 2014/144/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2662695
42 A = 6794890
87 meter
Y = -5253102
55 meter E =
0014604
Z = 3373228
11 I = 51
43568
XDOT = 6114
819686 Wp = 77
07696
YDOT = -120
654654 meter/sec RA = 215
94950 deg
ZDOT = 4625
172558 TA = 322
39040
MA = 322
49244
Ha = 227
489 n
mi
Hp = 219
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8735877
37 X = -2620142
45
Y = -17234588
42 feet Y = -5282640
72 meter
Z = 11067021
35 Z = 3360396
07
XDOT = 20061
744375 XDOT = 6093
246456
YDOT = -395
848602 feet/sec YDOT = -52
395607 meter/sec
ZDOT = 15174
450650 ZDOT = 4654
825545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19349369
85 X = -5897687
93
Y = 359892
81 feet Y = 109695
33 meter
Z = 11013533
34 Z = 3356924
96
XDOT = 8423
642753 XDOT = 2567
526311
YDOT = -16707
781587 feet/sec YDOT = -5092
531828 meter/sec
ZDOT = 15299
949866 ZDOT = 4663
424719
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 14144
56526610
00016717 00000-0 10270-3 0 9057
2 25544 51
6471 216
6927 0003574 28
6961 331
4386 15
50584285 7660
Satellite: ISS
Catalog Number: 25544
Epoch time: 14144
56526610 = yrday
fracday
Element set: 905
Inclination: 51
6471 deg
RA of node: 216
6927 deg
Eccentricity:
0003574
Arg of perigee: 28
6961 deg
Mean anomaly: 331
4386 deg
Mean motion: 15
50584285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 766
Checksum: 321
Coasting Arc #7 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2014/145/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2536673
61 A = 6793606
92 meter
Y = 5043822
84 meter E =
0008949
Z = -3789186
32 I = 51
45647
XDOT = -6396
772913 Wp = 60
75656
YDOT = 63
484481 meter/sec RA = 210
97789 deg
ZDOT = -4201
068952 TA = 164
68270
MA = 164
65559
Ha = 227
541 n
mi
Hp = 219
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8322419
99 X = 2498490
88
Y = 16547975
20 feet Y = 5071976
26 meter
Z = -12431713
64 Z = -3776955
77
XDOT = -20986
787771 XDOT = -6376
599582
YDOT = 208
282419 feet/sec YDOT = -7
935323 meter/sec
ZDOT = -13783
034620 ZDOT = -4232
095122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18546792
38 X = 5653062
32
Y = -616115
96 feet Y = -187792
14 meter
Z = -12380733
23 Z = -3773647
49
XDOT = -8694
088242 XDOT = -2649
958096
YDOT = 17674
991118 feet/sec YDOT = 5387
337293 meter/sec
ZDOT = -13914
347414 ZDOT = -4241
093092
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 14145
53199993
00016717 00000-0 10270-3 0 9066
2 25544 51
6463 211
8994 0003707 32
7088 327
4292 15
50599098 7812
Satellite: ISS
Catalog Number: 25544
Epoch time: 14145
53199993 = yrday
fracday
Element set: 906
Inclination: 51
6463 deg
RA of node: 211
8994 deg
Eccentricity:
0003707
Arg of perigee: 32
7088 deg
Mean anomaly: 327
4292 deg
Mean motion: 15
50599098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 342
Coasting Arc #8 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2014/146/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2366229
69 A = 6792225
52 meter
Y = -4824372
86 meter E =
0012353
Z = 4143529
56 I = 51
47959
XDOT = 6690
061576 Wp = 87
59523
YDOT = -55
002259 meter/sec RA = 206
00686 deg
ZDOT = 3747
256210 TA = 323
71067
MA = 323
79438
Ha = 227
540 n
mi
Hp = 219
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7763220
75 X = -2332234
89
Y = -15827994
95 feet Y = -4850643
78 meter
Z = 13594257
09 Z = 4132116
77
XDOT = 21949
020918 XDOT = 6671
976100
YDOT = -180
453606 feet/sec YDOT = 19
708917 meter/sec
ZDOT = 12294
147672 ZDOT = 3779
712254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17651044
48 X = -5380038
36
Y = 724168
84 feet Y = 220726
66 meter
Z = 13546699
02 Z = 4129033
86
XDOT = 8794
271548 XDOT = 2680
493968
YDOT = -18762
357987 feet/sec YDOT = -5718
766714 meter/sec
ZDOT = 12431
524554 ZDOT = 3789
128684
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 14146
56315583
00016717 00000-0 10270-3 0 9076
2 25544 51
6464 206
7864 0003782 35
7188 324
4215 15
50658291 7979
Satellite: ISS
Catalog Number: 25544
Epoch time: 14146
56315583 = yrday
fracday
Element set: 907
Inclination: 51
6464 deg
RA of node: 206
7864 deg
Eccentricity:
0003782
Arg of perigee: 35
7188 deg
Mean anomaly: 324
4215 deg
Mean motion: 15
50658291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 329
Coasting Arc #9 (Orbit 811)
---------------------------------------
Vector Time (GMT): 2014/147/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2128599
88 A = 6790964
34 meter
Y = 4643244
48 meter E =
0012882
Z = -4488337
27 I = 51
50353
XDOT = -6941
502522 Wp = 61
26933
YDOT = 72
528206 meter/sec RA = 201
03588 deg
ZDOT = -3217
968166 TA = 176
23095
MA = 176
22123
Ha = 227
573 n
mi
Hp = 219
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6983595
40 X = 2098323
14
Y = 15233741
73 feet Y = 4666878
96 meter
Z = -14725515
99 Z = -4478069
78
XDOT = -22773
958404 XDOT = -6926
165509
YDOT = 237
953432 feet/sec YDOT = -5
010092 meter/sec
ZDOT = -10557
638340 ZDOT = -3251
652343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16786679
67 X = 5116579
96
Y = -549424
46 feet Y = -167464
58 meter
Z = -14682773
29 Z = -4475309
30
XDOT = -8709
436673 XDOT = -2654
636298
YDOT = 19764
477096 feet/sec YDOT = 6024
212619 meter/sec
ZDOT = -10700
232831 ZDOT = -3261
430967
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 14147
52984365
00016717 00000-0 10270-3 0 9084
2 25544 51
6461 201
9925 0003899 39
7608 320
3828 15
50671550 8127
Satellite: ISS
Catalog Number: 25544
Epoch time: 14147
52984365 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 201
9925 deg
Eccentricity:
0003899
Arg of perigee: 39
7608 deg
Mean anomaly: 320
3828 deg
Mean motion: 15
50671550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 812
Checksum: 325
Coasting Arc #10 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2014/148/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1844839
38 A = 6789685
20 meter
Y = -4467684
04 meter E =
0009555
Z = 4760290
51 I = 51
52846
XDOT = 7190
901235 Wp = 94
25735
YDOT = -129
032090 meter/sec RA = 196
06593 deg
ZDOT = 2660
406841 TA = 329
41109
MA = 329
46677
Ha = 227
594 n
mi
Hp = 218
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6052622
65 X = -1817867
93
Y = -14657756
04 feet Y = -4488163
91 meter
Z = 15617751
02 Z = 4751393
45
XDOT = 23592
195654 XDOT = 7178
886054
YDOT = -423
333630 feet/sec YDOT = -48
686273 meter/sec
ZDOT = 8728
368901 ZDOT = 2695
310574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15893358
00 X = -4844295
52
Y = 196775
58 feet Y = 59977
20 meter
Z = 15580778
25 Z = 4749021
21
XDOT = 8460
999189 XDOT = 2578
912553
YDOT = -20814
279125 feet/sec YDOT = -6344
192277 meter/sec
ZDOT = 8876
153958 ZDOT = 2705
451726
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 14148
56095103
00016717 00000-0 10270-3 0 9093
2 25544 51
6453 196
8791 0004013 43
2688 316
8778 15
50728910 8282
Satellite: ISS
Catalog Number: 25544
Epoch time: 14148
56095103 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 196
8791 deg
Eccentricity:
0004013
Arg of perigee: 43
2688 deg
Mean anomaly: 316
8778 deg
Mean motion: 15
50728910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 329
Coasting Arc #11 (Orbit 842)
---------------------------------------
Vector Time (GMT): 2014/149/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1509130
66 A = 6788679
40 meter
Y = 4346325
41 meter E =
0016262
Z = -5006804
55 I = 51
55581
XDOT = -7369
780698 Wp = 68
31490
YDOT = 206
334063 meter/sec RA = 191
09606 deg
ZDOT = -2041
734594 TA = 181
75906
MA = 181
76479
Ha = 227
585 n
mi
Hp = 218
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4951216
08 X = 1484738
65
Y = 14259597
79 feet Y = 4363065
67 meter
Z = -16426524
12 Z = -4999532
06
XDOT = -24179
070530 XDOT = -7361
622016
YDOT = 676
949026 feet/sec YDOT = 123
966296 meter/sec
ZDOT = -6698
604310 ZDOT = -2077
516565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15121883
23 X = 4609150
01
Y = 409709
65 feet Y = 124879
50 meter
Z = -16396406
62 Z = -4997624
74
XDOT = -8016
287384 XDOT = -2443
364395
YDOT = 21663
318423 feet/sec YDOT = 6602
979455 meter/sec
ZDOT = -6850
140829 ZDOT = -2087
922925
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 14149
52759311
00016717 00000-0 10270-3 0 9100
2 25544 51
6458 192
0847 0004047 46
5938 313
5549 15
50742835 8437
Satellite: ISS
Catalog Number: 25544
Epoch time: 14149
52759311 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 192
0847 deg
Eccentricity:
0004047
Arg of perigee: 46
5938 deg
Mean anomaly: 313
5549 deg
Mean motion: 15
50742835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 843
Checksum: 321
Coasting Arc #12 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2014/150/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1131537
35 A = 6787743
47 meter
Y = -4244300
16 meter E =
0006983
Z = 5168794
03 I = 51
58273
XDOT = 7533
850013 Wp = 89
97550
YDOT = -305
416449 meter/sec RA = 186
12739 deg
ZDOT = 1396
868176 TA = 346
57127
MA = 346
58985
Ha = 227
613 n
mi
Hp = 218
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3712392
90 X = -1109101
10
Y = -13924869
30 feet Y = -4256828
91 meter
Z = 16957985
67 Z = 5163351
12
XDOT = 24717
355685 XDOT = 7529
919715
YDOT = -1002
022469 feet/sec YDOT = -221
190243 meter/sec
ZDOT = 4582
900840 ZDOT = 1433
457321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14388013
56 X = -4385466
53
Y = -1194897
49 feet Y = -364204
75 meter
Z = 16935595
94 Z = 5161969
64
XDOT = 7450
155728 XDOT = 2270
807466
YDOT = -22481
562657 feet/sec YDOT = -6852
380298 meter/sec
ZDOT = 4737
893030 ZDOT = 1444
109796
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 14150
55865266
00016717 00000-0 10270-3 0 9113
2 25544 51
6446 186
9706 0004205 50
6192 309
5331 15
50799247 8594
Satellite: ISS
Catalog Number: 25544
Epoch time: 14150
55865266 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 186
9706 deg
Eccentricity:
0004205
Arg of perigee: 50
6192 deg
Mean anomaly: 309
5331 deg
Mean motion: 15
50799247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 321
Coasting Arc #13 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2014/151/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 725473
81 A = 6787223
91 meter
Y = 4207738
86 meter E =
0018224
Z = -5291724
78 I = 51
61315
XDOT = -7605
038080 Wp = 77
81976
YDOT = 411
559120 meter/sec RA = 181
15977 deg
ZDOT = -713
698192 TA = 185
33442
MA = 185
35386
Ha = 227
572 n
mi
Hp = 218
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2380163
43 X = 704073
66
Y = 13804917
51 feet Y = 4215732
54 meter
Z = -17361301
79 Z = -5288252
00
XDOT = -24950
912335 XDOT = -7605
608064
YDOT = 1350
259579 feet/sec YDOT = 326
511597 meter/sec
ZDOT = -2341
529501 ZDOT = -750
643966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13857991
28 X = 4223915
74
Y = 2164444
81 feet Y = 659722
78 meter
Z = -17347247
09 Z = -5287440
91
XDOT = -6725
341177 XDOT = -2049
883991
YDOT = 22994
365701 feet/sec YDOT = 7008
682666 meter/sec
ZDOT = -2498
071138 ZDOT = -761
412083
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 14151
52524932
00016717 00000-0 10270-3 0 9124
2 25544 51
6456 182
1760 0004146 53
1043 307
0487 15
50812720 8744
Satellite: ISS
Catalog Number: 25544
Epoch time: 14151
52524932 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 182
1760 deg
Eccentricity:
0004146
Arg of perigee: 53
1043 deg
Mean anomaly: 307
0487 deg
Mean motion: 15
50812720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 282
Coasting Arc #14 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2014/152/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -287178
48 A = 6786844
92 meter
Y = -4199356
60 meter E =
0006424
Z = 5318693
96 I = 51
64228
XDOT = 7650
919380 Wp = 70
19503
YDOT = -515
559669 meter/sec RA = 176
19323 deg
ZDOT = 8
167215 TA = 19
73957
MA = 19
71472
Ha = 227
575 n
mi
Hp = 218
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -942186
61 X = -266035
57
Y = -13777416
67 feet Y = -4202450
38 meter
Z = 17449783
32 Z = 5317349
77
XDOT = 25101
441536 XDOT = 7656
076176
YDOT = -1691
468730 feet/sec YDOT = -429
973343 meter/sec
ZDOT = 26
795325 ZDOT = 45
346918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13420150
92 X = -4090462
00
Y = -3283352
86 feet Y = -1000765
95 meter
Z = 17444741
52 Z = 5317157
22
XDOT = 5956
631428 XDOT = 1815
581259
YDOT = -23404
148158 feet/sec YDOT = -7133
584359 meter/sec
ZDOT = 184
365939 ZDOT = 56
194738
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 14152
55626126
00016717 00000-0 10270-3 0 9137
2 25544 51
6443 177
0612 0004306 57
3140 302
8425 15
50870696 8900
Satellite: ISS
Catalog Number: 25544
Epoch time: 14152
55626126 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 177
0612 deg
Eccentricity:
0004306
Arg of perigee: 57
3140 deg
Mean anomaly: 302
8425 deg
Mean motion: 15
50870696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 291
Coasting Arc #15 (Orbit 904)
---------------------------------------
Vector Time (GMT): 2014/153/12:11:14
535
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -149993
60 A = 6786973
15 meter
Y = 4259901
77 meter E =
0018208
Z = -5297129
99 I = 51
67473
XDOT = -7592
942201 Wp = 87
78389
YDOT = 606
918856 meter/sec RA = 171
22920 deg
ZDOT = 705
868092 TA = 188
95458
MA = 188
98710
Ha = 227
537 n
mi
Hp = 218
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -492104
98 X = -171885
83
Y = 13976055
66 feet Y = 4258102
55 meter
Z = -17379035
41 Z = -5297911
40
XDOT = -24911
227695 XDOT = -7602
593468
YDOT = 1991
203595 feet/sec YDOT = 521
955667 meter/sec
ZDOT = 2315
840197 ZDOT = 668
959174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13241960
50 X = 4036149
56
Y = 4481598
18 feet Y = 1365991
12 meter
Z = -17383006
95 Z = -5298340
52
XDOT = -5110
592704 XDOT = -1557
708656
YDOT = 23440
713524 feet/sec YDOT = 7144
729482 meter/sec
ZDOT = 2159
381840 ZDOT = 658
179585
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 14153
52281277
00016717 00000-0 10270-3 0 9140
2 25544 51
6452 172
2667 0004209 59
4134 300
7432 15
50881312 9054
Satellite: ISS
Catalog Number: 25544
Epoch time: 14153
52281277 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 172
2667 deg
Eccentricity:
0004209
Arg of perigee: 59
4134 deg
Mean anomaly: 300
7432 deg
Mean motion: 15
50881312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 905
Checksum: 288
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