[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 16th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16059 75 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 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 1640)
---------------------------------------
Vector Time (GMT): 2015/350/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3153804
25 A = 6786076
88 meter
Y = 5758869
79 meter E =
0006044
Z = 1700985
31 I = 51
30559
XDOT = -3636
909098 Wp = 127
76929
YDOT = 3668
516377 meter/sec RA = 253
26932 deg
ZDOT = -5666
758270 TA = 33
48816
MA = 33
44996
Ha = 218
603 n
mi
Hp = 216
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10347126
81 X = 3080910
06
Y = 18893929
75 feet Y = 5793730
04 meter
Z = 5580660
46 Z = 1716129
06
XDOT = -11932
116464 XDOT = -3650
134232
YDOT = 12035
814884 feet/sec YDOT = 3627
772433 meter/sec
ZDOT = -18591
726608 ZDOT = -5684
457472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19653018
46 X = -5990240
03
Y = 8779517
72 feet Y = 2675997
00 meter
Z = 5645026
11 Z = 1720603
96
XDOT = -10418
629487 XDOT = -3175
598268
YDOT = -11297
253887 feet/sec YDOT = -3443
402985 meter/sec
ZDOT = -18668
907746 ZDOT = -5690
283081
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 15350
53961724
00016717 00000-0 10270-3 0 9008
2 25544 51
6429 254
0325 0008142 286
4882 73
5376 15
54815274 16418
Satellite: ISS
Catalog Number: 25544
Epoch time: 15350
53961724 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 254
0325 deg
Eccentricity:
0008142
Arg of perigee: 286
4882 deg
Mean anomaly: 73
5376 deg
Mean motion: 15
54815274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1641
Checksum: 310
Coasting Arc #2 (Orbit 1656)
---------------------------------------
Vector Time (GMT): 2015/351/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2341303
64 A = 6787215
77 meter
Y = -6358402
71 meter E =
0011487
Z = 223553
35 I = 51
31994
XDOT = 4570
498112 Wp = 7
62294
YDOT = -1471
720005 meter/sec RA = 248
27162 deg
ZDOT = 5983
916483 TA = 354
79800
MA = 354
80992
Ha = 218
764 n
mi
Hp = 216
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7681442
38 X = -2271114
34
Y = -20860901
27 feet Y = -6384192
27 meter
Z = 733442
75 Z = 212350
03
XDOT = 14995
072547 XDOT = 4557
548082
YDOT = -4828
477708 feet/sec YDOT = -1420
682333 meter/sec
ZDOT = 19632
271926 ZDOT = 6006
087448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21298411
76 X = 6491755
90
Y = -6373890
45 feet Y = -1942761
81 meter
Z = 686202
61 Z = 209154
56
XDOT = 3427
857939 XDOT = 1044
811100
YDOT = 13587
279296 feet/sec YDOT = 4141
402729 meter/sec
ZDOT = 19728
369210 ZDOT = 6013
206935
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 15351
56797504
00016717 00000-0 10270-3 0 9016
2 25544 51
6431 248
8996 0008264 291
1098 68
9171 15
54850788 16570
Satellite: ISS
Catalog Number: 25544
Epoch time: 15351
56797504 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 248
8996 deg
Eccentricity:
0008264
Arg of perigee: 291
1098 deg
Mean anomaly: 68
9171 deg
Mean motion: 15
54850788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1657
Checksum: 350
Coasting Arc #3 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2015/352/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1271081
24 A = 6785297
65 meter
Y = 6313949
61 meter E =
0003720
Z = -2129251
15 I = 51
32667
XDOT = -5304
399380 Wp = 246
96899
YDOT = -782
201811 meter/sec RA = 243
27422 deg
ZDOT = -5479
790569 TA = 316
73738
MA = 316
76659
Ha = 218
936 n
mi
Hp = 216
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4170214
03 X = 1210725
71
Y = 20715057
78 feet Y = 6327826
28 meter
Z = -6985732
12 Z = -2123222
89
XDOT = -17402
885105 XDOT = -5268
639669
YDOT = -2566
278908 feet/sec YDOT = -841
318987 meter/sec
ZDOT = -17978
315515 ZDOT = -5505
471419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20883108
10 X = -6365171
35
Y = 3278307
33 feet Y = 999228
07 meter
Z = -6960837
17 Z = -2121663
17
XDOT = 3582
500029 XDOT = 1091
946009
YDOT = -15631
458015 feet/sec YDOT = -4764
468403 meter/sec
ZDOT = -18089
172371 ZDOT = -5513
579739
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 15352
53204495
00016717 00000-0 10270-3 0 9027
2 25544 51
6435 244
0883 0008323 293
4763 66
5514 15
54858197 16721
Satellite: ISS
Catalog Number: 25544
Epoch time: 15352
53204495 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 244
0883 deg
Eccentricity:
0008323
Arg of perigee: 293
4763 deg
Mean anomaly: 66
5514 deg
Mean motion: 15
54858197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1672
Checksum: 322
Coasting Arc #4 (Orbit 1687)
---------------------------------------
Vector Time (GMT): 2015/353/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 35549
79 A = 6781132
63 meter
Y = -5646678
04 meter E =
0005057
Z = 3748623
54 I = 51
32832
XDOT = 5735
276042 Wp = 57
87473
YDOT = 2842
941937 meter/sec RA = 238
26698 deg
ZDOT = 4226
479846 TA = 347
23005
MA = 347
24285
Ha = 219
084 n
mi
Hp = 216
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 116633
17 X = 80480
26
Y = -18525846
59 feet Y = -5646029
40 meter
Z = 12298633
65 Z = 3748905
17
XDOT = 18816
522446 XDOT = 5682
528637
YDOT = 9327
237327 feet/sec YDOT = 2906
782515 meter/sec
ZDOT = 13866
403694 ZDOT = 4254
212703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18516461
81 X = 5643817
56
Y = 553131
54 feet Y = 168594
49 meter
Z = 12300880
96 Z = 3749308
52
XDOT = -9805
544781 XDOT = -2988
730049
YDOT = 17110
340719 feet/sec YDOT = 5215
231851 meter/sec
ZDOT = 13985
763199 ZDOT = 4262
860623
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 15353
56037045
00016717 00000-0 10270-3 0 9037
2 25544 51
6436 238
9552 0008287 298
8227 61
2093 15
54894772 16880
Satellite: ISS
Catalog Number: 25544
Epoch time: 15353
56037045 = yrday
fracday
Element set: 903
Inclination: 51
6436 deg
RA of node: 238
9552 deg
Eccentricity:
0008287
Arg of perigee: 298
8227 deg
Mean anomaly: 61
2093 deg
Mean motion: 15
54894772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1688
Checksum: 341
Coasting Arc #5 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2015/354/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1496139
68 A = 6776905
03 meter
Y = 4491098
27 meter E =
0009023
Z = -4856166
93 I = 51
33234
XDOT = -5734
006035 Wp = 27
40936
YDOT = -4492
464904 meter/sec RA = 233
24782 deg
ZDOT = -2382
049421 TA = 219
09977
MA = 219
16501
Ha = 219
229 n
mi
Hp = 215
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4908594
75 X = -1522659
53
Y = 14734574
37 feet Y = 4474219
38 meter
Z = -15932306
19 Z = -4863499
12
XDOT = -18812
355759 XDOT = -5671
772883
YDOT = -14739
058083 feet/sec YDOT = -4556
238277 meter/sec
ZDOT = -7815
122771 ZDOT = -2409
753243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14681198
54 X = -4474829
31
Y = -4962599
79 feet Y = -1512600
42 meter
Z = -15964816
86 Z = -4866076
18
XDOT = 14576
309263 XDOT = 4442
859063
YDOT = -17533
778633 feet/sec YDOT = -5344
295727 meter/sec
ZDOT = -7934
070110 ZDOT = -2418
304570
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 15354
52440913
00016717 00000-0 10270-3 0 9047
2 25544 51
6436 234
1436 0008471 302
0945 57
9385 15
54949516 17030
Satellite: ISS
Catalog Number: 25544
Epoch time: 15354
52440913 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 234
1436 deg
Eccentricity:
0008471
Arg of perigee: 302
0945 deg
Mean anomaly: 57
9385 deg
Mean motion: 15
54949516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1703
Checksum: 311
Coasting Arc #6 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2015/355/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3010180
96 A = 6774930
92 meter
Y = -2981703
38 meter E =
0006265
Z = 5290276
94 I = 51
34597
XDOT = 5222
144685 Wp = 315
33211
YDOT = 5610
319163 meter/sec RA = 228
21940 deg
ZDOT = 195
187483 TA = 132
82610
MA = 132
77343
Ha = 219
290 n
mi
Hp = 215
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9875921
79 X = 3017601
08
Y = -9782491
39 feet Y = -2948000
38 meter
Z = 17356551
66 Z = 5304917
73
XDOT = 17133
020620 XDOT = 5158
072445
YDOT = 18406
558935 feet/sec YDOT = 5668
358374 meter/sec
ZDOT = 640
378881 ZDOT = 220
400480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9844918
54 X = 3000731
17
Y = 9699925
85 feet Y = 2956537
40 meter
Z = 17420386
68 Z = 5309733
86
XDOT = -17586
123528 XDOT = -5360
250451
YDOT = 16531
485619 feet/sec YDOT = 5038
796817 meter/sec
ZDOT = 748
370606 ZDOT = 228
103361
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 15355
55270271
00016717 00000-0 10270-3 0 9050
2 25544 51
6437 229
0109 0008429 305
6259 54
4109 15
54965156 17192
Satellite: ISS
Catalog Number: 25544
Epoch time: 15355
55270271 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 229
0109 deg
Eccentricity:
0008429
Arg of perigee: 305
6259 deg
Mean anomaly: 54
4109 deg
Mean motion: 15
54965156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1719
Checksum: 316
Coasting Arc #7 (Orbit 1733)
---------------------------------------
Vector Time (GMT): 2015/356/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4391622
25 A = 6776139
10 meter
Y = 1343174
79 meter E =
0006144
Z = -4986889
07 I = 51
37152
XDOT = -4158
082228 Wp = 70
06688
YDOT = -6115
901082 meter/sec RA = 223
19089 deg
ZDOT = 2018
567003 TA = 219
60831
MA = 219
65322
Ha = 219
423 n
mi
Hp = 215
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14408209
49 X = -4382091
04
Y = 4406741
44 feet Y = 1294118
46 meter
Z = -16361184
63 Z = -5008199
54
XDOT = -13642
002061 XDOT = -4099
189159
YDOT = -20065
292263 feet/sec YDOT = -6162
070374 meter/sec
ZDOT = 6622
595155 ZDOT = 1998
510332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4744119
05 X = -1446007
49
Y = -14194282
05 feet Y = -4326417
17 meter
Z = -16453568
75 Z = -5015047
76
XDOT = 18698
465598 XDOT = 5699
292314
YDOT = -13811
551439 feet/sec YDOT = -4209
760879 meter/sec
ZDOT = 6536
973510 ZDOT = 1992
469526
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 15356
51671307
00016717 00000-0 10270-3 0 9063
2 25544 51
6429 224
1985 0008559 309
1462 50
8930 15
54994496 17348
Satellite: ISS
Catalog Number: 25544
Epoch time: 15356
51671307 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 224
1985 deg
Eccentricity:
0008559
Arg of perigee: 309
1462 deg
Mean anomaly: 50
8930 deg
Mean motion: 15
54994496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1734
Checksum: 335
Coasting Arc #8 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2015/357/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5491403
46 A = 6779864
54 meter
Y = 288890
41 meter E =
0009138
Z = 3968188
30 I = 51
40837
XDOT = 2558
228035 Wp = 28
45670
YDOT = 6039
547302 meter/sec RA = 218
17337 deg
ZDOT = -3968
245143 TA = 103
06793
MA = 102
96590
Ha = 219
628 n
mi
Hp = 214
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18016415
56 X = 5468488
90
Y = 947803
18 feet Y = 350170
41 meter
Z = 13018990
50 Z = 3994808
87
XDOT = 8393
136599 XDOT = 2509
778461
YDOT = 19814
787737 feet/sec YDOT = 6067
884581 meter/sec
ZDOT = -13019
176979 ZDOT = -3955
934859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -213428
48 X = -65053
00
Y = 17956466
39 feet Y = 5473130
96 meter
Z = 13134056
39 Z = 4003260
39
XDOT = -18140
168171 XDOT = -5529
123258
YDOT = 9296
718950 feet/sec YDOT = 2833
639936 meter/sec
ZDOT = -12967
024849 ZDOT = -3952
349174
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 15357
54497454
00016717 00000-0 10270-3 0 9077
2 25544 51
6428 219
0659 0008716 313
2321 46
8104 15
55046889 17504
Satellite: ISS
Catalog Number: 25544
Epoch time: 15357
54497454 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 219
0659 deg
Eccentricity:
0008716
Arg of perigee: 313
2321 deg
Mean anomaly: 46
8104 deg
Mean motion: 15
55046889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1750
Checksum: 325
Coasting Arc #9 (Orbit 1764)
---------------------------------------
Vector Time (GMT): 2015/358/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6105707
71 A = 6784238
59 meter
Y = -1714693
97 meter E =
0010219
Z = -2390747
34 I = 51
44684
XDOT = -559
910705 Wp = 349
20224
YDOT = -5465
340458 meter/sec RA = 213
17011 deg
ZDOT = 5355
933132 TA = 343
98594
MA = 344
01822
Ha = 219
742 n
mi
Hp = 214
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20031849
45 X = -6074466
48
Y = -5625636
40 feet Y = -1782797
10 meter
Z = -7843659
25 Z = -2420331
88
XDOT = -1836
977379 XDOT = -524
771332
YDOT = -17930
907014 feet/sec YDOT = -5471
405843 meter/sec
ZDOT = 17571
959093 ZDOT = 5353
297972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4454808
28 X = 1357825
56
Y = -20274582
97 feet Y = -6179692
89 meter
Z = -7971307
06 Z = -2429654
39
XDOT = 16307
060224 XDOT = 4970
391956
YDOT = -3313
801258 feet/sec YDOT = -1010
046624 meter/sec
ZDOT = 17561
537465 ZDOT = 5352
756619
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 15358
50895710
00016717 00000-0 10270-3 0 9082
2 25544 51
6412 214
2529 0008730 316
3188 43
7273 15
55017024 17659
Satellite: ISS
Catalog Number: 25544
Epoch time: 15358
50895710 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 214
2529 deg
Eccentricity:
0008730
Arg of perigee: 316
3188 deg
Mean anomaly: 43
7273 deg
Mean motion: 15
55017024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1765
Checksum: 305
Coasting Arc #10 (Orbit 1780)
---------------------------------------
Vector Time (GMT): 2015/359/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6128004
98 A = 6786571
50 meter
Y = 2878419
71 meter E =
0004723
Z = 448288
56 I = 51
48162
XDOT = -1672
897101 Wp = 110
80526
YDOT = 4499
880567 meter/sec RA = 208
18125 deg
ZDOT = -5975
805942 TA = 64
35076
MA = 64
30198
Ha = 219
960 n
mi
Hp = 214
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20105003
20 X = 6093184
73
Y = 9443634
21 feet Y = 2946752
37 meter
Z = 1470762
99 Z = 477972
71
XDOT = -5488
507550 XDOT = -1694
063558
YDOT = 14763
387686 feet/sec YDOT = 4481
055433 meter/sec
ZDOT = -19605
662539 ZDOT = -5983
983402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7903360
49 X = -2408944
28
Y = 20749402
77 feet Y = 6324417
96 meter
Z = 1598656
38 Z = 487270
46
XDOT = -13610
444495 XDOT = -4148
463482
YDOT = -3659
354302 feet/sec YDOT = -1115
371191 meter/sec
ZDOT = -19641
834911 ZDOT = -5986
831281
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 15359
53718948
00016717 00000-0 10270-3 0 9094
2 25544 51
6408 209
1201 0008629 320
3253 39
7268 15
55041489 17818
Satellite: ISS
Catalog Number: 25544
Epoch time: 15359
53718948 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 209
1201 deg
Eccentricity:
0008629
Arg of perigee: 320
3253 deg
Mean anomaly: 39
7268 deg
Mean motion: 15
55041489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1781
Checksum: 326
Coasting Arc #11 (Orbit 1796)
---------------------------------------
Vector Time (GMT): 2015/360/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5467361
65 A = 6785562
68 meter
Y = -3687580
60 meter E =
0015215
Z = 1554403
85 I = 51
50594
XDOT = 3868
961912 Wp = 28
14016
YDOT = -3311
243280 meter/sec RA = 203
19467 deg
ZDOT = 5743
251910 TA = 348
90473
MA = 348
93825
Ha = 220
046 n
mi
Hp = 214
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17937538
22 X = -5433270
49
Y = -12098361
55 feet Y = -3748529
80 meter
Z = 5099750
17 Z = 1527927
23
XDOT = 12693
444593 XDOT = 3877
803292
YDOT = -10863
659056 feet/sec YDOT = -3267
929155 meter/sec
ZDOT = 18842
689993 ZDOT = 5762
067468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10384517
06 X = 3165200
80
Y = -19011474
20 feet Y = -5794697
34 meter
Z = 4985853
54 Z = 1519688
16
XDOT = 10591
471247 XDOT = 3228
280436
YDOT = 10757
011459 feet/sec YDOT = 3278
737093 meter/sec
ZDOT = 18924
677614 ZDOT = 5768
241737
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 15360
56540446
00016717 00000-0 10270-3 0 9107
2 25544 51
6396 203
9852 0008685 323
4290 36
6269 15
55089208 17970
Satellite: ISS
Catalog Number: 25544
Epoch time: 15360
56540446 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 203
9852 deg
Eccentricity:
0008685
Arg of perigee: 323
4290 deg
Mean anomaly: 36
6269 deg
Mean motion: 15
55089208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1797
Checksum: 331
Coasting Arc #12 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2015/361/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4173158
95 A = 6781838
92 meter
Y = 4173595
87 meter E =
0007029
Z = -3348087
25 I = 51
52232
XDOT = -5746
005269 Wp =
44682
YDOT = 2005
406820 meter/sec RA = 198
20343 deg
ZDOT = -4655
318524 TA = 218
62381
MA = 218
67411
Ha = 220
215 n
mi
Hp = 214
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13691466
37 X = 4142442
11
Y = 13692899
85 feet Y = 4220091
45 meter
Z = -10984538
23 Z = -3327889
41
XDOT = -18851
723322 XDOT = -5745
389736
YDOT = 6579
418702 feet/sec YDOT = 1941
155055 meter/sec
ZDOT = -15273
354739 ZDOT = -4683
229383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12101465
14 X = -3688526
58
Y = 15179022
54 feet Y = 4626566
07 meter
Z = -10897873
82 Z = -3321671
94
XDOT = -7486
417033 XDOT = -2281
859912
YDOT = -17037
286184 feet/sec YDOT = -5192
964829 meter/sec
ZDOT = -15394
477269 ZDOT = -4692
236672
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 15361
52934383
00016717 00000-0 10270-3 0 9112
2 25544 51
6386 199
1725 0008741 327
6540 32
4077 15
55096643 18121
Satellite: ISS
Catalog Number: 25544
Epoch time: 15361
52934383 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 199
1725 deg
Eccentricity:
0008741
Arg of perigee: 327
6540 deg
Mean anomaly: 32
4077 deg
Mean motion: 15
55096643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1812
Checksum: 317
Coasting Arc #13 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2015/362/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2328252
05 A = 6777396
95 meter
Y = -4340450
17 meter E =
0005323
Z = 4650569
70 I = 51
53809
XDOT = 7072
978470 Wp = 38
38635
YDOT = -699
529652 meter/sec RA = 193
19871 deg
ZDOT = 2890
430454 TA = 22
86802
MA = 22
84433
Ha = 220
418 n
mi
Hp = 213
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7638622
21 X = -2302133
36
Y = -14240322
09 feet Y = -4366340
52 meter
Z = 15257774
61 Z = 4639322
83
XDOT = 23205
309940 XDOT = 7066
234725
YDOT = -2295
044791 feet/sec YDOT = -620
472845 meter/sec
ZDOT = 9483
039547 ZDOT = 2924
772578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13144342
91 X = 4006395
72
Y = -9477418
19 feet Y = -2888717
07 meter
Z = 15209858
72 Z = 4635964
94
XDOT = 4515
938860 XDOT = 1376
458165
YDOT = 21708
593786 feet/sec YDOT = 6616
779386 meter/sec
ZDOT = 9631
781366 ZDOT = 2935
766960
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 15362
55753098
00016717 00000-0 10270-3 0 9129
2 25544 51
6386 194
0374 0008795 331
6260 28
4413 15
55089766 18282
Satellite: ISS
Catalog Number: 25544
Epoch time: 15362
55753098 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 194
0374 deg
Eccentricity:
0008795
Arg of perigee: 331
6260 deg
Mean anomaly: 28
4413 deg
Mean motion: 15
55089766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 335
Coasting Arc #14 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2015/363/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 184936
41 A = 6774594
56 meter
Y = 4257825
23 meter E =
0014342
Z = -5276534
29 I = 51
56000
XDOT = -7610
904855 Wp = 49
95610
YDOT = -538
515795 meter/sec RA = 188
18452 deg
ZDOT = -693
524450 TA = 213
36210
MA = 213
45256
Ha = 220
423 n
mi
Hp = 213
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 606746
74 X = 162941
59
Y = 13969242
88 feet Y = 4259770
60 meter
Z = -17311464
21 Z = -5275689
12
XDOT = -24970
160287 XDOT = -7600
948560
YDOT = -1766
784104 feet/sec YDOT = -623
570258 meter/sec
ZDOT = -2275
342685 ZDOT = -730
471943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13719498
71 X = -4181703
21
Y = 2717415
09 feet Y = 828268
12 meter
Z = -17308543
90 Z = -5275644
18
XDOT = -1639
271531 XDOT = -499
649963
YDOT = -23949
537151 feet/sec YDOT = -7299
818924 meter/sec
ZDOT = -2435
165209 ZDOT = -742
238356
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 15363
52144060
00016717 00000-0 10270-3 0 9131
2 25544 51
6380 189
2240 0008642 335
3330 24
7409 15
55141193 18438
Satellite: ISS
Catalog Number: 25544
Epoch time: 15363
52144060 = yrday
fracday
Element set: 913
Inclination: 51
6380 deg
RA of node: 189
2240 deg
Eccentricity:
0008642
Arg of perigee: 335
3330 deg
Mean anomaly: 24
7409 deg
Mean motion: 15
55141193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 283
Coasting Arc #15 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2015/364/12:05:54
436
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2064938
61 A = 6775251
03 meter
Y = -3942860
05 meter E =
0010918
Z = 5110037
73 I = 51
59442
XDOT = 7298
893223 Wp = 5
04795
YDOT = 1697
348407 meter/sec RA = 183
16879 deg
ZDOT = -1628
873468 TA = 100
74053
MA = 100
61759
Ha = 220
497 n
mi
Hp = 213
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6774732
98 X = 2084052
93
Y = -12935892
56 feet Y = -3919661
86 meter
Z = 16765215
66 Z = 5120114
92
XDOT = 23946
500074 XDOT = 7287
282915
YDOT = 5568
728368 feet/sec YDOT = 1778
904598 meter/sec
ZDOT = -5344
073059 ZDOT = -1593
445578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13837625
99 X = 4217708
40
Y = 4501890
77 feet Y = 1372176
31 meter
Z = 16809517
12 Z = 5123540
82
XDOT = -1313
858689 XDOT = -400
464128
YDOT = 23554
362674 feet/sec YDOT = 7179
369743 meter/sec
ZDOT = -5191
008614 ZDOT = -1582
219426
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 15364
54959678
00016717 00000-0 10270-3 0 9144
2 25544 51
6383 184
0897 0008654 338
8695 21
2100 15
55137323 18594
Satellite: ISS
Catalog Number: 25544
Epoch time: 15364
54959678 = yrday
fracday
Element set: 914
Inclination: 51
6383 deg
RA of node: 184
0897 deg
Eccentricity:
0008654
Arg of perigee: 338
8695 deg
Mean anomaly: 21
2100 deg
Mean motion: 15
55137323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 342
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