[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 4th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
016/01:58:23
471 -1
1 2
9 2
9
N/A 2
6 -0
2 228
6
000/00:06:46
943 -0
8 -0
1 220
9
Coasting Arc #1 (Orbit 2577)
---------------------------------------
Vector Time (GMT): 2014/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6591563
83 A = 6800868
62 meter
Y = 1662850
82 meter E =
0008060
Z = 89963
25 I = 51
56836
XDOT = -1082
027618 Wp = 112
66617
YDOT = 4636
793804 meter/sec RA = 194
76022 deg
ZDOT = -5998
130100 TA = 66
36594
MA = 66
28135
Ha = 227
741 n
mi
Hp = 221
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21625865
58 X = 6572042
56
Y = 5455547
30 feet Y = 1736452
73 meter
Z = 295155
02 Z = 121936
44
XDOT = -3549
959375 XDOT = -1104
660237
YDOT = 15212
578098 feet/sec YDOT = 4624
567738 meter/sec
ZDOT = -19678
904528 ZDOT = -6003
441033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -757954
90 X = -231024
65
Y = 22288318
03 feet Y = 6793479
34 meter
Z = 429602
76 Z = 130942
92
XDOT = -13966
365134 XDOT = -4256
948093
YDOT = -76
640780 feet/sec YDOT = -23
360110 meter/sec
ZDOT = -19701
952253 ZDOT = -6005
155047
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 14003
53251780
00016717 00000-0 10270-3 0 9006
2 25544 51
6450 195
6931 0005595 344
3177 15
7799 15
50163306 25780
Satellite: ISS
Catalog Number: 25544
Epoch time: 14003
53251780 = yrday
fracday
Element set: 900
Inclination: 51
6450 deg
RA of node: 195
6931 deg
Eccentricity:
0005595
Arg of perigee: 344
3177 deg
Mean anomaly: 15
7799 deg
Mean motion: 15
50163306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2578
Checksum: 310
Coasting Arc #2 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2014/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6644099
36 A = 6800925
56 meter
Y = -1377406
05 meter E =
0015913
Z = 285372
69 I = 51
59775
XDOT = 1220
241640 Wp = 31
14837
YDOT = -4614
828812 meter/sec RA = 189
80183 deg
ZDOT = 5999
084459 TA = 331
92527
MA = 332
01100
Ha = 227
805 n
mi
Hp = 221
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21798226
25 X = -6629589
33
Y = -4519048
73 feet Y = -1451623
49 meter
Z = 936262
12 Z = 253132
16
XDOT = 4003
417455 XDOT = 1242
613719
YDOT = -15140
514475 feet/sec YDOT = -4601
058464 meter/sec
ZDOT = 19682
035628 ZDOT = 6005
066288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -578515
79 X = -176331
61
Y = -22259500
66 feet Y = -6784695
80 meter
Z = 800628
46 Z = 244031
55
XDOT = 14001
796144 XDOT = 4267
747465
YDOT = 363
780897 feet/sec YDOT = 110
880417 meter/sec
ZDOT = 19707
904264 ZDOT = 6006
969220
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 14004
56400076
00016717 00000-0 10270-3 0 9015
2 25544 51
6444 190
5805 0005412 347
8242 12
2777 15
50141030 25942
Satellite: ISS
Catalog Number: 25544
Epoch time: 14004
56400076 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 190
5805 deg
Eccentricity:
0005412
Arg of perigee: 347
8242 deg
Mean anomaly: 12
2777 deg
Mean motion: 15
50141030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 271
Coasting Arc #3 (Orbit 2608)
---------------------------------------
Vector Time (GMT): 2014/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6670099
61 A = 6800549
63 meter
Y = 1119986
91 meter E =
0006634
Z = -697644
48 I = 51
62837
XDOT = -1391
917150 Wp = 112
76214
YDOT = 4611
707794 meter/sec RA = 184
84705 deg
ZDOT = -5952
160772 TA = 74
75789
MA = 74
68455
Ha = 227
892 n
mi
Hp = 220
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21883528
89 X = 6660468
83
Y = 3674497
74 feet Y = 1194522
39 meter
Z = -2288859
83 Z = -665265
74
XDOT = -4566
657317 XDOT = -1414
469438
YDOT = 15130
274916 feet/sec YDOT = 4596
016556 meter/sec
ZDOT = -19528
086522 ZDOT = -5958
977094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1803207
73 X = 549617
72
Y = 22130170
42 feet Y = 6745275
95 meter
Z = -2152591
14 Z = -656109
78
XDOT = -14142
777102 XDOT = -4310
718461
YDOT = -733
760063 feet/sec YDOT = -223
650067 meter/sec
ZDOT = -19557
469967 ZDOT = -5961
116846
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 14005
53100012
00016717 00000-0 10270-3 0 9021
2 25544 51
6449 185
7887 0005610 352
2022 7
9040 15
50212306 26095
Satellite: ISS
Catalog Number: 25544
Epoch time: 14005
53100012 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 185
7887 deg
Eccentricity:
0005610
Arg of perigee: 352
2022 deg
Mean anomaly: 7
9040 deg
Mean motion: 15
50212306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2609
Checksum: 260
Coasting Arc #4 (Orbit 2624)
---------------------------------------
Vector Time (GMT): 2014/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6650500
26 A = 6800348
85 meter
Y = -842766
02 meter E =
0016853
Z = 1081213
69 I = 51
65807
XDOT = 1554
005314 Wp = 40
69872
YDOT = -4659
520368 meter/sec RA = 179
89307 deg
ZDOT = 5887
429831 TA = 331
01456
MA = 331
10804
Ha = 227
967 n
mi
Hp = 220
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21819226
58 X = -6645834
14
Y = -2764980
37 feet Y = -917110
09 meter
Z = 3547288
99 Z = 1048918
02
XDOT = 5098
442632 XDOT = 1577
394556
YDOT = -15287
140314 feet/sec YDOT = -4642
011838 meter/sec
ZDOT = 19315
714670 ZDOT = 5895
035632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3046767
42 X = -928654
71
Y = -21803374
77 feet Y = -6645668
63 meter
Z = 3411316
60 Z = 1039769
30
XDOT = 14465
549791 XDOT = 4409
099576
YDOT = 1026
789448 feet/sec YDOT = 312
965424 meter/sec
ZDOT = 19348
433060 ZDOT = 5897
402397
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 14006
56245432
00016717 00000-0 10270-3 0 9032
2 25544 51
6447 180
6766 0005359 356
0762 4
0345 15
50191169 26253
Satellite: ISS
Catalog Number: 25544
Epoch time: 14006
56245432 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 180
6766 deg
Eccentricity:
0005359
Arg of perigee: 356
0762 deg
Mean anomaly: 4
0345 deg
Mean motion: 15
50191169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2625
Checksum: 299
Coasting Arc #5 (Orbit 2639)
---------------------------------------
Vector Time (GMT): 2014/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6605405
92 A = 6799718
67 meter
Y = 603554
50 meter E =
0005280
Z = -1498002
59 I = 51
68783
XDOT = -1735
590811 Wp = 102
16116
YDOT = 4727
583459 meter/sec RA = 174
94197 deg
ZDOT = -5766
576488 TA = 94
14428
MA = 94
08393
Ha = 228
035 n
mi
Hp = 220
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21671279
26 X = 6605442
70
Y = 1980165
68 feet Y = 677420
60 meter
Z = -4914706
67 Z = -1465914
47
XDOT = -5694
195575 XDOT = -1760
314634
YDOT = 15510
444418 feet/sec YDOT = 4708
036874 meter/sec
ZDOT = -18919
214199 ZDOT = -5775
067653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4136509
99 X = 1260808
25
Y = 21395439
28 feet Y = 6521329
89 meter
Z = -4779561
26 Z = -1456810
27
XDOT = -14887
722842 XDOT = -4537
777922
YDOT = -1342
410895 feet/sec YDOT = -409
166841 meter/sec
ZDOT = -18955
677225 ZDOT = -5777
690418
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 14007
52942676
00016717 00000-0 10270-3 0 9044
2 25544 51
6450 175
8847 0005580
4205 359
6949 15
50252427 26402
Satellite: ISS
Catalog Number: 25544
Epoch time: 14007
52942676 = yrday
fracday
Element set: 904
Inclination: 51
6450 deg
RA of node: 175
8847 deg
Eccentricity:
0005580
Arg of perigee:
4205 deg
Mean anomaly: 359
6949 deg
Mean motion: 15
50252427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2640
Checksum: 310
Coasting Arc #6 (Orbit 2655)
---------------------------------------
Vector Time (GMT): 2014/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6513765
52 A = 6799213
49 meter
Y = -357509
16 meter E =
0017078
Z = 1880297
67 I = 51
71672
XDOT = 1898
075003 Wp = 50
57230
YDOT = -4847
382349 meter/sec RA = 169
99191 deg
ZDOT = 5630
152933 TA = 330
08821
MA = 330
18569
Ha = 228
108 n
mi
Hp = 220
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21370621
79 X = -6518417
53
Y = -1172930
32 feet Y = -430376
32 meter
Z = 6168955
60 Z = 1848643
44
XDOT = 6227
280195 XDOT = 1924
789008
YDOT = -15903
485396 feet/sec YDOT = -4826
007680 meter/sec
ZDOT = 18471
630358 ZDOT = 5639
438230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5189111
68 X = -1581641
24
Y = -20803365
83 feet Y = -6340865
91 meter
Z = 6035589
82 Z = 1839647
78
XDOT = 15479
911992 XDOT = 4718
277175
YDOT = 1532
305480 feet/sec YDOT = 467
046710 meter/sec
ZDOT = 18511
463661 ZDOT = 5642
294124
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 14008
56085079
00016717 00000-0 10270-3 0 9055
2 25544 51
6450 170
7728 0005334 4
2378 355
8816 15
50246728 26569
Satellite: ISS
Catalog Number: 25544
Epoch time: 14008
56085079 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 170
7728 deg
Eccentricity:
0005334
Arg of perigee: 4
2378 deg
Mean anomaly: 355
8816 deg
Mean motion: 15
50246728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2656
Checksum: 318
Coasting Arc #7 (Orbit 2670)
---------------------------------------
Vector Time (GMT): 2014/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6401235
35 A = 6798385
81 meter
Y = 159268
37 meter E =
0005055
Z = -2290337
78 I = 51
74480
XDOT = -2063
983944 Wp = 77
36255
YDOT = 4983
822119 meter/sec RA = 165
04392 deg
ZDOT = -5431
082415 TA = 128
03451
MA = 127
98888
Ha = 228
159 n
mi
Hp = 220
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21001428
32 X = 6410104
34
Y = 522534
03 feet Y = 230900
76 meter
Z = -7514231
57 Z = -2259219
95
XDOT = -6771
600866 XDOT = -2093
178315
YDOT = 16351
122438 feet/sec YDOT = 4960
578341 meter/sec
ZDOT = -17818
511861 ZDOT = -5441
179642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6052172
93 X = 1844702
31
Y = 20165762
83 feet Y = 6146524
51 meter
Z = -7383083
47 Z = -2250363
84
XDOT = -16139
819540 XDOT = -4919
416996
YDOT = -1684
587646 feet/sec YDOT = -513
462315 meter/sec
ZDOT = -17861
795343 ZDOT = -5444
275221
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 14009
52779582
00016717 00000-0 10270-3 0 9062
2 25544 51
6452 165
9807 0005543 8
2958 351
8283 15
50284631 26711
Satellite: ISS
Catalog Number: 25544
Epoch time: 14009
52779582 = yrday
fracday
Element set: 906
Inclination: 51
6452 deg
RA of node: 165
9807 deg
Eccentricity:
0005543
Arg of perigee: 8
2958 deg
Mean anomaly: 351
8283 deg
Mean motion: 15
50284631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2671
Checksum: 327
Coasting Arc #8 (Orbit 2686)
---------------------------------------
Vector Time (GMT): 2014/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6244839
23 A = 6797571
51 meter
Y = 32450
83 meter E =
0016524
Z = 2660133
86 I = 51
77223
XDOT = 2202
999051 Wp = 60
39014
YDOT = -5169
275068 meter/sec RA = 160
09703 deg
ZDOT = 5218
374488 TA = 329
53542
MA = 329
63132
Ha = 228
229 n
mi
Hp = 220
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20488317
67 X = -6257660
03
Y = 106465
99 feet Y = -37454
78 meter
Z = 8727473
29 Z = 2629766
20
XDOT = 7227
687175 XDOT = 2235
290149
YDOT = -16959
563870 feet/sec YDOT = -5144
459475 meter/sec
ZDOT = 17120
651206 ZDOT = 5229
154472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6827069
21 X = -2080890
70
Y = -19375034
77 feet Y = -5905510
60 meter
Z = 8599444
17 Z = 2621110
58
XDOT = 16941
967832 XDOT = 5163
911795
YDOT = 1673
809587 feet/sec YDOT = 510
177162 meter/sec
ZDOT = 17166
849582 ZDOT = 5232
455752
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 14010
55918866
00016717 00000-0 10270-3 0 9078
2 25544 51
6456 160
8687 0005362 11
7914 348
3361 15
50303954 26870
Satellite: ISS
Catalog Number: 25544
Epoch time: 14010
55918866 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 160
8687 deg
Eccentricity:
0005362
Arg of perigee: 11
7914 deg
Mean anomaly: 348
3361 deg
Mean motion: 15
50303954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2687
Checksum: 322
Coasting Arc #9 (Orbit 2701)
---------------------------------------
Vector Time (GMT): 2014/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6076155
97 A = 6796609
91 meter
Y = -168350
61 meter E =
0006851
Z = -3050332
09 I = 51
79810
XDOT = -2328
829280 Wp = 56
96714
YDOT = 5362
132418 meter/sec RA = 155
15171 deg
ZDOT = -4939
301652 TA = 157
83552
MA = 157
80589
Ha = 228
264 n
mi
Hp = 219
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19934894
90 X = 6092404
39
Y = -552331
41 feet Y = -100312
10 meter
Z = -10007651
22 Z = -3020775
62
XDOT = -7640
516011 XDOT = -2364
623293
YDOT = 17592
297959 feet/sec YDOT = 5335
890162 meter/sec
ZDOT = -16205
057915 ZDOT = -4950
701320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7390740
46 X = 2252697
69
Y = 18589280
18 feet Y = 5666012
60 meter
Z = -9883005
90 Z = -3012340
20
XDOT = -17754
869343 XDOT = -5411
684176
YDOT = -1574
613528 feet/sec YDOT = -479
942203 meter/sec
ZDOT = -16253
907974 ZDOT = -4954
191151
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 14011
52610571
00016717 00000-0 10270-3 0 9089
2 25544 51
6458 156
0765 0005538 15
5003 344
6317 15
50315252 27024
Satellite: ISS
Catalog Number: 25544
Epoch time: 14011
52610571 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 156
0765 deg
Eccentricity:
0005538
Arg of perigee: 15
5003 deg
Mean anomaly: 344
6317 deg
Mean motion: 15
50315252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2702
Checksum: 277
Coasting Arc #10 (Orbit 2717)
---------------------------------------
Vector Time (GMT): 2014/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5869702
73 A = 6795546
36 meter
Y = 285090
68 meter E =
0015226
Z = 3394591
74 I = 51
82351
XDOT = 2422
823910 Wp = 69
71758
YDOT = -5598
090349 meter/sec RA = 150
20736 deg
ZDOT = 4647
807203 TA = 329
79778
MA = 329
88546
Ha = 228
344 n
mi
Hp = 219
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19257554
89 X = -5888944
16
Y = 935336
88 feet Y = 219344
08 meter
Z = 11137112
01 Z = 3366031
01
XDOT = 7948
897343 XDOT = 2462
665519
YDOT = -18366
438154 feet/sec YDOT = -5570
774365 meter/sec
ZDOT = 15248
711296 ZDOT = 4659
673226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7825754
87 X = -2385290
09
Y = -17696183
97 feet Y = -5393796
88 meter
Z = 11016631
65 Z = 3357869
33
XDOT = 18670
449705 XDOT = 5690
753070
YDOT = 1292
252344 feet/sec YDOT = 393
878514 meter/sec
ZDOT = 15299
573888 ZDOT = 4663
310121
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 14012
55746708
00016717 00000-0 10270-3 0 9096
2 25544 51
6467 150
9645 0005451 18
8363 341
2989 15
50358614 27187
Satellite: ISS
Catalog Number: 25544
Epoch time: 14012
55746708 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 150
9645 deg
Eccentricity:
0005451
Arg of perigee: 18
8363 deg
Mean anomaly: 341
2989 deg
Mean motion: 15
50358614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2718
Checksum: 327
Coasting Arc #11 (Orbit 2732)
---------------------------------------
Vector Time (GMT): 2014/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5663397
27 A = 6794521
45 meter
Y = -341423
72 meter E =
0009933
Z = -3750466
70 I = 51
84673
XDOT = -2488
687326 Wp = 51
27624
YDOT = 5826
734556 meter/sec RA = 145
26432 deg
ZDOT = -4290
103570 TA = 173
25158
MA = 173
23819
Ha = 228
355 n
mi
Hp = 219
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18580699
71 X = 5685012
62
Y = -1120156
56 feet Y = -277970
86 meter
Z = -12304680
78 Z = -3722902
50
XDOT = -8164
984666 XDOT = -2532
818458
YDOT = 19116
583190 feet/sec YDOT = 5798
658039 meter/sec
ZDOT = -14075
142947 ZDOT = -4302
299902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8048805
59 X = 2453275
94
Y = 16868979
81 feet Y = 5141665
05 meter
Z = -12188378
50 Z = -3715017
77
XDOT = -19519
442282 XDOT = -5949
526007
YDOT = -890
213150 feet/sec YDOT = -271
336968 meter/sec
ZDOT = -14127
443659 ZDOT = -4306
044827
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 14013
52435565
00016717 00000-0 10270-3 0 9102
2 25544 51
6470 146
1723 0005587 22
2591 337
8802 15
50350348 27335
Satellite: ISS
Catalog Number: 25544
Epoch time: 14013
52435565 = yrday
fracday
Element set: 910
Inclination: 51
6470 deg
RA of node: 146
1723 deg
Eccentricity:
0005587
Arg of perigee: 22
2591 deg
Mean anomaly: 337
8802 deg
Mean motion: 15
50350348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2733
Checksum: 291
Coasting Arc #12 (Orbit 2748)
---------------------------------------
Vector Time (GMT): 2014/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5428283
91 A = 6793326
04 meter
Y = 367851
99 meter E =
0013317
Z = 4054571
63 I = 51
86935
XDOT = 2521
479021 Wp = 77
78426
YDOT = -6089
945467 meter/sec RA = 140
32199 deg
ZDOT = 3920
175845 TA = 331
64937
MA = 331
72178
Ha = 228
461 n
mi
Hp = 219
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17809330
42 X = -5451689
43
Y = 1206863
50 feet Y = 307018
30 meter
Z = 13302400
36 Z = 4028145
30
XDOT = 8272
568968 XDOT = 2570
348035
YDOT = -19980
136045 feet/sec YDOT = -6061
475715 meter/sec
ZDOT = 12861
469309 ZDOT = 3932
542948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8118020
98 X = -2474372
80
Y = -15990030
94 feet Y = -4873761
43 meter
Z = 13190878
31 Z = 4020579
71
XDOT = 20425
457228 XDOT = 6225
679363
YDOT = 306
042862 feet/sec YDOT = 93
281864 meter/sec
ZDOT = 12914
540201 ZDOT = 3936
351853
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 14014
55568568
00016717 00000-0 10270-3 0 9117
2 25544 51
6482 141
0604 0005594 25
7695 334
3734 15
50409317 27495
Satellite: ISS
Catalog Number: 25544
Epoch time: 14014
55568568 = yrday
fracday
Element set: 911
Inclination: 51
6482 deg
RA of node: 141
0604 deg
Eccentricity:
0005594
Arg of perigee: 25
7695 deg
Mean anomaly: 334
3734 deg
Mean motion: 15
50409317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2749
Checksum: 316
Coasting Arc #13 (Orbit 2763)
---------------------------------------
Vector Time (GMT): 2014/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5208664
93 A = 6792331
27 meter
Y = -334179
59 meter E =
0013355
Z = -4360870
95 I = 51
88944
XDOT = -2515
266855 Wp = 53
79738
YDOT = 6326
815538 meter/sec RA = 135
38079 deg
ZDOT = -3488
873893 TA = 180
77905
MA = 180
78114
Ha = 228
441 n
mi
Hp = 219
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17088795
69 X = 5233198
06
Y = -1096389
75 feet Y = -275795
54 meter
Z = -14307319
40 Z = -4335508
82
XDOT = -8252
187846 XDOT = -2568
880213
YDOT = 20757
268825 feet/sec YDOT = 6298
388662 meter/sec
ZDOT = -11446
436657 ZDOT = -3501
222353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8000093
32 X = 2438428
44
Y = 15240702
53 feet Y = 4645366
13 meter
Z = -14200277
83 Z = -4328244
68
XDOT = -21177
116942 XDOT = -6454
785244
YDOT = 401
096977 feet/sec YDOT = 122
254359 meter/sec
ZDOT = -11499
474207 ZDOT = -3505
039738
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 14015
52254532
00016717 00000-0 10270-3 0 9129
2 25544 51
6485 136
2685 0005685 28
9098 331
2367 15
50391377 27647
Satellite: ISS
Catalog Number: 25544
Epoch time: 14015
52254532 = yrday
fracday
Element set: 912
Inclination: 51
6485 deg
RA of node: 136
2685 deg
Eccentricity:
0005685
Arg of perigee: 28
9098 deg
Mean anomaly: 331
2367 deg
Mean motion: 15
50391377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2764
Checksum: 320
Coasting Arc #14 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2014/016/02:01:46
943
Vector Time (MET): N/A
Weight (LBS) : 900891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3885665
40 A = 6790167
89 meter
Y = 1866330
73 meter E =
0016400
Z = -5260436
85 I = 51
89076
XDOT = -4441
304693 Wp = 66
33357
YDOT = 6129
887968 meter/sec RA = 132
48206 deg
ZDOT = -1102
126197 TA = 193
09415
MA = 193
13677
Ha = 228
611 n
mi
Hp = 220
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12748246
06 X = 3890059
96
Y = 6123132
33 feet Y = 1909807
57 meter
Z = -17258651
08 Z = -5241550
38
XDOT = -14571
209623 XDOT = -4504
166696
YDOT = 20111
180999 feet/sec YDOT = 6079
871042 meter/sec
ZDOT = -3615
899595 ZDOT = -1123
853429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7032833
93 X = -2143607
78
Y = -12380796
94 feet Y = -3773666
91 meter
Z = -17179251
39 Z = -5236235
82
XDOT = 22540
875621 XDOT = 6870
458889
YDOT = -7641
585626 feet/sec YDOT = -2329
155299 meter/sec
ZDOT = -3708
480639 ZDOT = -1130
344899
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 14016
10265665
00016717 00000-0 10270-3 0 9134
2 25544 51
6493 133
3965 0004626 12
1843 347
9419 15
49884423 27731
Satellite: ISS
Catalog Number: 25544
Epoch time: 14016
10265665 = yrday
fracday
Element set: 913
Inclination: 51
6493 deg
RA of node: 133
3965 deg
Eccentricity:
0004626
Arg of perigee: 12
1843 deg
Mean anomaly: 347
9419 deg
Mean motion: 15
49884423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 319
Coasting Arc #15 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2014/017/02:01:46
943
Vector Time (MET): N/A
Weight (LBS) : 900891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3817272
95 A = 6789850
59 meter
Y = -1848415
17 meter E =
0004924
Z = 5298496
77 I = 51
91028
XDOT = 4156
923426 Wp = 53
93432
YDOT = -6394
423206 meter/sec RA = 127
54492 deg
ZDOT = 766
423231 TA = 28
78064
MA = 28
75348
Ha = 228
719 n
mi
Hp = 220
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12523861
38 X = -3822057
78
Y = -6064354
23 feet Y = -1891129
30 meter
Z = 17383519
58 Z = 5279941
64
XDOT = 13638
200217 XDOT = 4224
395372
YDOT = -20979
078759 feet/sec YDOT = -6347
560605 meter/sec
ZDOT = 2514
511912 ZDOT = 786
780260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7092120
45 X = 2161678
31
Y = 12084348
19 feet Y = 3683309
33 meter
Z = 17305507
95 Z = 5274718
82
XDOT = -22135
329329 XDOT = -6746
848379
YDOT = 9276
561648 feet/sec YDOT = 2827
495990 meter/sec
ZDOT = 2601
363929 ZDOT = 792
895725
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 14017
13431328
00016717 00000-0 10270-3 0 9140
2 25544 51
6493 128
2869 0004610 14
6437 345
4847 15
49913022 27899
Satellite: ISS
Catalog Number: 25544
Epoch time: 14017
13431328 = yrday
fracday
Element set: 914
Inclination: 51
6493 deg
RA of node: 128
2869 deg
Eccentricity:
0004610
Arg of perigee: 14
6437 deg
Mean anomaly: 345
4847 deg
Mean motion: 15
49913022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 313
Coasting Arc #16 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2014/018/02:01:46
943
Vector Time (MET): N/A
Weight (LBS) : 900891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3783424
35 A = 6789671
63 meter
Y = 1848517
05 meter E =
0017071
Z = -5340508
91 I = 51
92849
XDOT = -3832
218985 Wp = 71
76004
YDOT = 6606
601868 meter/sec RA = 122
60890 deg
ZDOT = -424
061905 TA = 194
17786
MA = 194
22583
Ha = 228
691 n
mi
Hp = 220
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12412809
56 X = 3788414
63
Y = 6064688
48 feet Y = 1890853
72 meter
Z = -17521354
68 Z = -5322117
75
XDOT = -12572
896934 XDOT = -3903
750744
YDOT = 21675
202980 feet/sec YDOT = 6563
347600 meter/sec
ZDOT = -1391
279215 ZDOT = -442
851561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7206317
91 X = -2196485
70
Y = -11900881
90 feet Y = -3627388
80 meter
Z = -17444029
06 Z = -5316940
06
XDOT = 21467
822671 XDOT = 6543
392350
YDOT = -10822
684265 feet/sec YDOT = -3298
754164 meter/sec
ZDOT = -1471
560426 ZDOT = -448
531618
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 14018
10147830
00016717 00000-0 10270-3 0 9151
2 25544 51
6499 123
4966 0004752 18
1952 341
9368 15
49931768 28042
Satellite: ISS
Catalog Number: 25544
Epoch time: 14018
10147830 = yrday
fracday
Element set: 915
Inclination: 51
6499 deg
RA of node: 123
4966 deg
Eccentricity:
0004752
Arg of perigee: 18
1952 deg
Mean anomaly: 341
9368 deg
Mean motion: 15
49931768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2804
Checksum: 327
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