[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 3rd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4305 56 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 904)
---------------------------------------
Vector Time (GMT): 2014/153/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3302614
56 A = 6789842
53 meter
Y = 3395627
58 meter E =
0015684
Z = -4879438
89 I = 51
68083
XDOT = -6625
002326 Wp = 69
27480
YDOT = 2955
415677 meter/sec RA = 171
29819 deg
ZDOT = -2428
313623 TA = 176
86471
MA = 176
85487
Ha = 228
029 n
mi
Hp = 219
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10835349
62 X = 3288101
23
Y = 11140510
44 feet Y = 3432478
87 meter
Z = -16008657
78 Z = -4863430
14
XDOT = -21735
571937 XDOT = -6645
762076
YDOT = 9696
245659 feet/sec YDOT = 2881
214808 meter/sec
ZDOT = -7966
908213 ZDOT = -2460
547167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14052446
98 X = 4283185
84
Y = -6796657
09 feet Y = -2071621
08 meter
Z = -15941363
94 Z = -4858927
73
XDOT = 1751
937226 XDOT = 533
990466
YDOT = 22622
664036 feet/sec YDOT = 6895
387998 meter/sec
ZDOT = -8103
923692 ZDOT = -2470
075941
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
52405941
00016717 00000-0 10270-3 0 9001
2 25544 51
6455 172
2845 0004093 58
8485 301
3067 15
50541822 9058
Satellite: ISS
Catalog Number: 25544
Epoch time: 14153
52405941 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 172
2845 deg
Eccentricity:
0004093
Arg of perigee: 58
8485 deg
Mean anomaly: 301
3067 deg
Mean motion: 15
50541822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 905
Checksum: 293
Coasting Arc #2 (Orbit 920)
---------------------------------------
Vector Time (GMT): 2014/154/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3008258
86 A = 6789025
03 meter
Y = -3377198
59 meter E =
0008521
Z = 5056254
67 I = 51
70765
XDOT = 6725
803648 Wp = 98
60835
YDOT = -3165
033841 meter/sec RA = 166
34024 deg
ZDOT = 1883
606044 TA = 333
13129
MA = 333
17539
Ha = 228
170 n
mi
Hp = 218
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9869615
68 X = -2994832
38
Y = -11080047
87 feet Y = -3410764
24 meter
Z = 16588762
05 Z = 5041673
27
XDOT = 22066
284935 XDOT = 6751
545927
YDOT = -10383
969294 feet/sec YDOT = -3089
677812 meter/sec
ZDOT = 6179
809857 ZDOT = 1916
341376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13583703
58 X = -4140312
85
Y = 6139086
54 feet Y = 1871193
58 meter
Z = 16527504
79 Z = 5037583
46
XDOT = -2757
923151 XDOT = -840
614977
YDOT = -23149
307587 feet/sec YDOT = -7055
908953 meter/sec
ZDOT = 6319
000575 ZDOT = 1926
031375
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 14154
55527111
00016717 00000-0 10270-3 0 9010
2 25544 51
6444 167
1709 0004199 61
9294 298
2281 15
50545355 9213
Satellite: ISS
Catalog Number: 25544
Epoch time: 14154
55527111 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 167
1709 deg
Eccentricity:
0004199
Arg of perigee: 61
9294 deg
Mean anomaly: 298
2281 deg
Mean motion: 15
50545355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 921
Checksum: 307
Coasting Arc #3 (Orbit 935)
---------------------------------------
Vector Time (GMT): 2014/155/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2712516
38 A = 6788416
97 meter
Y = 3424168
07 meter E =
0017916
Z = -5212023
89 I = 51
73598
XDOT = -6747
235567 Wp = 76
68986
YDOT = 3358
604990 meter/sec RA = 161
38467 deg
ZDOT = -1304
736622 TA = 180
76135
MA = 180
76408
Ha = 228
075 n
mi
Hp = 218
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8899331
96 X = 2699343
36
Y = 11234147
22 feet Y = 3454427
91 meter
Z = -17099815
90 Z = -5198878
57
XDOT = -22136
599628 XDOT = -6777
952772
YDOT = 11019
045242 feet/sec YDOT = 3282
981415 meter/sec
ZDOT = -4280
631961 ZDOT = -1337
588194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13345942
72 X = 4067843
34
Y = -5401274
45 feet Y = -1646308
45 meter
Z = -17044645
02 Z = -5195207
80
XDOT = 3811
360296 XDOT = 1161
702618
YDOT = 23369
121301 feet/sec YDOT = 7122
908173 meter/sec
ZDOT = -4420
361226 ZDOT = -1347
326102
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 14155
52202806
00016717 00000-0 10270-3 0 9020
2 25544 51
6448 162
3779 0004127 64
6026 295
5552 15
50544521 9366
Satellite: ISS
Catalog Number: 25544
Epoch time: 14155
52202806 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 162
3779 deg
Eccentricity:
0004127
Arg of perigee: 64
6026 deg
Mean anomaly: 295
5552 deg
Mean motion: 15
50544521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 936
Checksum: 300
Coasting Arc #4 (Orbit 951)
---------------------------------------
Vector Time (GMT): 2014/156/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2410132
67 A = 6787955
92 meter
Y = -3496241
32 meter E =
0006621
Z = 5289919
89 I = 51
76294
XDOT = 6751
206562 Wp = 89
20736
YDOT = -3564
047382 meter/sec RA = 156
42967 deg
ZDOT = 719
650272 TA = 353
92624
MA = 353
93427
Ha = 228
164 n
mi
Hp = 218
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7907259
43 X = -2396554
63
Y = -11470608
00 feet Y = -3523117
40 meter
Z = 17355380
20 Z = 5278244
50
XDOT = 22149
627829 XDOT = 6787
062939
YDOT = -11693
068837 feet/sec YDOT = -3488
350615 meter/sec
ZDOT = 2361
057322 ZDOT = 752
533688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13210599
96 X = -4026590
87
Y = 4612570
43 feet Y = 1405911
47 meter
Z = 17306445
74 Z = 5275004
66
XDOT = -4929
215002 XDOT = -1502
424733
YDOT = -23509
661147 feet/sec YDOT = -7165
744718 meter/sec
ZDOT = 2500
968942 ZDOT = 762
295334
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 14156
55323190
00016717 00000-0 10270-3 0 9035
2 25544 51
6439 157
2643 0004166 67
1213 293
0377 15
50556015 9525
Satellite: ISS
Catalog Number: 25544
Epoch time: 14156
55323190 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 157
2643 deg
Eccentricity:
0004166
Arg of perigee: 67
1213 deg
Mean anomaly: 293
0377 deg
Mean motion: 15
50556015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 952
Checksum: 294
Coasting Arc #5 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2014/157/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2129887
06 A = 6787812
28 meter
Y = 3628963
03 meter E =
0018816
Z = -5342450
78 I = 51
79039
XDOT = -6673
258462 Wp = 85
05919
YDOT = 3735
734572 meter/sec RA = 151
47715 deg
ZDOT = -121
665193 TA = 183
77374
MA = 183
78795
Ha = 228
110 n
mi
Hp = 218
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6987818
44 X = 2115100
96
Y = 11906046
68 feet Y = 3652698
45 meter
Z = -17527725
65 Z = -5332139
70
XDOT = -21893
892593 XDOT = -6713
945308
YDOT = 12256
347022 feet/sec YDOT = 3660
882422 meter/sec
ZDOT = -399
164018 ZDOT = -154
181766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13317126
95 X = 4059060
29
Y = -3840297
63 feet Y = -1170522
72 meter
Z = -17484592
20 Z = -5329303
70
XDOT = 6012
525872 XDOT = 1832
617886
YDOT = 23315
409630 feet/sec YDOT = 7106
536855 meter/sec
ZDOT = -537
563170 ZDOT = -163
849254
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 14157
51998167
00016717 00000-0 10270-3 0 9045
2 25544 51
6438 152
4712 0004158 70
0620 290
0978 15
50548868 9671
Satellite: ISS
Catalog Number: 25544
Epoch time: 14157
51998167 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 152
4712 deg
Eccentricity:
0004158
Arg of perigee: 70
0620 deg
Mean anomaly: 290
0978 deg
Mean motion: 15
50548868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 967
Checksum: 330
Coasting Arc #6 (Orbit 982)
---------------------------------------
Vector Time (GMT): 2014/158/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1851585
99 A = 6787794
37 meter
Y = -3786733
40 meter E =
0006815
Z = 5314926
75 I = 51
81684
XDOT = 6584
635351 Wp = 72
04451
YDOT = -3899
672235 meter/sec RA = 146
52558 deg
ZDOT = -481
927729 TA = 22
55659
MA = 22
52665
Ha = 228
146 n
mi
Hp = 218
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6074757
17 X = -1834922
71
Y = -12423666
01 feet Y = -3807346
19 meter
Z = 17437423
71 Z = 5305972
15
XDOT = 21603
134355 XDOT = 6630
094059
YDOT = -12794
200246 feet/sec YDOT = -3825
784406 meter/sec
ZDOT = -1581
127719 ZDOT = -449
830008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13535051
98 X = -4125483
84
Y = 3058433
21 feet Y = 932210
44 meter
Z = 17400064
70 Z = 5303539
72
XDOT = -7075
088932 XDOT = -2156
487106
YDOT = -23045
028915 feet/sec YDOT = -7024
124813 meter/sec
ZDOT = -1444
462063 ZDOT = -440
272037
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 14158
55117736
00016717 00000-0 10270-3 0 9056
2 25544 51
6432 147
3576 0004132 72
3285 287
8317 15
50567686 9838
Satellite: ISS
Catalog Number: 25544
Epoch time: 14158
55117736 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 147
3576 deg
Eccentricity:
0004132
Arg of perigee: 72
3285 deg
Mean anomaly: 287
8317 deg
Mean motion: 15
50567686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 983
Checksum: 328
Coasting Arc #7 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2014/159/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1617422
28 A = 6788132
42 meter
Y = 3993492
16 meter E =
0018211
Z = -5261313
50 I = 51
84316
XDOT = -6421
193564 Wp = 93
25697
YDOT = 4014
919125 meter/sec RA = 141
57636 deg
ZDOT = 1075
660140 TA = 187
03245
MA = 187
05803
Ha = 228
125 n
mi
Hp = 218
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5306503
56 X = 1598204
02
Y = 13102008
40 feet Y = 4011472
14 meter
Z = -17261527
24 Z = -5253502
59
XDOT = -21066
908020 XDOT = -6470
837339
YDOT = 13172
306840 feet/sec YDOT = 3942
835561 meter/sec
ZDOT = 3529
068700 ZDOT = 1044
346196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13972331
01 X = 4258766
49
Y = -2390750
78 feet Y = -728700
84 meter
Z = -17229051
15 Z = -5251414
79
XDOT = 8020
650047 XDOT = 2444
694134
YDOT = 22456
429761 feet/sec YDOT = 6844
719791 meter/sec
ZDOT = 3395
689816 ZDOT = 1035
006256
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 14159
51791956
00016717 00000-0 10270-3 0 9066
2 25544 51
6431 142
5640 0004173 75
3551 284
8062 15
50557196 9985
Satellite: ISS
Catalog Number: 25544
Epoch time: 14159
51791956 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 142
5640 deg
Eccentricity:
0004173
Arg of perigee: 75
3551 deg
Mean anomaly: 284
8062 deg
Mean motion: 15
50557196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 998
Checksum: 325
Coasting Arc #8 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2014/160/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1391878
87 A = 6788574
76 meter
Y = -4220334
93 meter E =
0008950
Z = 5125775
39 I = 51
86850
XDOT = 6257
288589 Wp = 65
51860
YDOT = -4103
771300 meter/sec RA = 136
62864 deg
ZDOT = -1673
816473 TA = 40
62652
MA = 40
55978
Ha = 228
122 n
mi
Hp = 218
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4566531
73 X = -1369482
40
Y = -13846243
22 feet Y = -4235775
04 meter
Z = 16816848
40 Z = 5119067
77
XDOT = 20529
162037 XDOT = 6310
843813
YDOT = -13463
816602 feet/sec YDOT = -4033
498687 meter/sec
ZDOT = -5491
523861 ZDOT = -1643
289282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14506392
12 X = -4421548
32
Y = 1751885
27 feet Y = 533974
63 meter
Z = 16789089
88 Z = 5117314
59
XDOT = -8862
487790 XDOT = -2701
286279
YDOT = -21818
107879 feet/sec YDOT = -6650
159282 meter/sec
ZDOT = -5361
447021 ZDOT = -1634
169052
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 14160
54910685
00016717 00000-0 10270-3 0 9074
2 25544 51
6428 137
4505 0004110 77
7648 282
3963 15
50582454 10146
Satellite: ISS
Catalog Number: 25544
Epoch time: 14160
54910685 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 137
4505 deg
Eccentricity:
0004110
Arg of perigee: 77
7648 deg
Mean anomaly: 282
3963 deg
Mean motion: 15
50582454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 304
Coasting Arc #9 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2014/161/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1228189
38 A = 6789342
89 meter
Y = 4478826
34 meter E =
0016171
Z = -4967183
30 I = 51
89318
XDOT = -6034
063998 Wp = 100
08203
YDOT = 4134
896868 meter/sec RA = 131
68322 deg
ZDOT = 2239
833016 TA = 191
74375
MA = 191
78151
Ha = 228
112 n
mi
Hp = 218
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4029492
73 X = 1202144
18
Y = 14694312
14 feet Y = 4492415
66 meter
Z = -16296533
14 Z = -4961279
61
XDOT = -19796
797894 XDOT = -6090
733436
YDOT = 13565
934606 feet/sec YDOT = 4067
102985 meter/sec
ZDOT = 7348
533516 ZDOT = 2210
382749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15206256
03 X = 4634866
84
Y = -1311832
00 feet Y = -399846
39 meter
Z = -16272230
57 Z = -4959775
88
XDOT = 9521
964430 XDOT = 2902
294758
YDOT = 20920
176476 feet/sec YDOT = 6376
469790 meter/sec
ZDOT = 7222
996695 ZDOT = 2201
569393
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 14161
51584112
00016717 00000-0 10270-3 0 9085
2 25544 51
6431 132
6567 0004147 80
6694 279
4926 15
50569808 10299
Satellite: ISS
Catalog Number: 25544
Epoch time: 14161
51584112 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 132
6567 deg
Eccentricity:
0004147
Arg of perigee: 80
6694 deg
Mean anomaly: 279
4926 deg
Mean motion: 15
50569808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 318
Coasting Arc #10 (Orbit 1044)
---------------------------------------
Vector Time (GMT): 2014/162/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1076585
80 A = 6790184
27 meter
Y = -4748129
18 meter E =
0011760
Z = 4725421
88 I = 51
91673
XDOT = 5823
272571 Wp = 70
21045
YDOT = -4123
677910 meter/sec RA = 126
73977 deg
ZDOT = -2807
239283 TA = 47
55743
MA = 47
45804
Ha = 228
088 n
mi
Hp = 218
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3532105
66 X = -1046366
01
Y = -15577851
63 feet Y = -4759999
91 meter
Z = 15503352
63 Z = 4720264
69
XDOT = 19105
224969 XDOT = 5882
588519
YDOT = -13529
127002 feet/sec YDOT = -4058
226312 meter/sec
ZDOT = -9210
102634 ZDOT = -2778
806730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15966764
09 X = -4866669
69
Y = 927930
75 feet Y = 282833
29 meter
Z = 15482266
11 Z = 4718994
71
XDOT = -10006
959242 XDOT = -3050
121177
YDOT = -20019
816683 feet/sec YDOT = -6102
040125 meter/sec
ZDOT = -9088
860882 ZDOT = -2770
284797
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 14162
54701991
00016717 00000-0 10270-3 0 9096
2 25544 51
6435 127
5432 0004084 83
4295 276
7321 15
50600298 10451
Satellite: ISS
Catalog Number: 25544
Epoch time: 14162
54701991 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 127
5432 deg
Eccentricity:
0004084
Arg of perigee: 83
4295 deg
Mean anomaly: 276
7321 deg
Mean motion: 15
50600298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1045
Checksum: 301
Coasting Arc #11 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2014/163/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 998150
18 A = 6791266
27 meter
Y = 5028185
02 meter E =
0013097
Z = -4467201
35 I = 51
93868
XDOT = -5574
499887 Wp = 103
39067
YDOT = 4053
881782 meter/sec RA = 121
79868 deg
ZDOT = 3322
634106 TA = 200
05433
MA = 200
10584
Ha = 228
073 n
mi
Hp = 218
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3274770
92 X = 963550
12
Y = 16496670
01 feet Y = 5039154
18 meter
Z = -14656172
42 Z = -4462435
73
XDOT = -18289
041623 XDOT = -5635
557446
YDOT = 13300
137080 feet/sec YDOT = 3991
202259 meter/sec
ZDOT = 10901
030533 ZDOT = 3295
405998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16816304
95 X = 5125609
75
Y = -802256
50 feet Y = -244527
78 meter
Z = -14636799
79 Z = -4461296
58
XDOT = 10276
182627 XDOT = 3132
180465
YDOT = 18950
348420 feet/sec YDOT = 5776
066198 meter/sec
ZDOT = 10784
885698 ZDOT = 3287
233161
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 14163
51374621
00016717 00000-0 10270-3 0 9102
2 25544 51
6441 122
7496 0004079 86
2243 273
9374 15
50585480 10602
Satellite: ISS
Catalog Number: 25544
Epoch time: 14163
51374621 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 122
7496 deg
Eccentricity:
0004079
Arg of perigee: 86
2243 deg
Mean anomaly: 273
9374 deg
Mean motion: 15
50585480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 298
Coasting Arc #12 (Orbit 1075)
---------------------------------------
Vector Time (GMT): 2014/164/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -930875
83 A = 6792375
39 meter
Y = -5306729
93 meter E =
0014443
Z = 4125696
70 I = 51
95929
XDOT = 5352
715353 Wp = 80
22858
YDOT = -3930
127639 meter/sec RA = 116
85973 deg
ZDOT = -3833
665664 TA = 49
24117
MA = 49
11590
Ha = 228
044 n
mi
Hp = 218
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3054054
57 X = -891506
98
Y = -17410531
27 feet Y = -5316920
10 meter
Z = 13535750
34 Z = 4121269
42
XDOT = 17561
402076 XDOT = 5414
887905
YDOT = -12894
119550 feet/sec YDOT = -3869
921915 meter/sec
ZDOT = -12577
643256 ZDOT = -3807
512401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17674499
73 X = -5387187
52
Y = 741451
22 feet Y = 225994
33 meter
Z = 13517865
79 Z = 4120245
49
XDOT = -10321
609324 XDOT = -3146
026522
YDOT = -17941
366632 feet/sec YDOT = -5468
528549 meter/sec
ZDOT = -12466
056642 ZDOT = -3799
654064
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 14164
54491658
00016717 00000-0 10270-3 0 9117
2 25544 51
6451 117
6365 0004046 89
3074 270
8540 15
50618188 10761
Satellite: ISS
Catalog Number: 25544
Epoch time: 14164
54491658 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 117
6365 deg
Eccentricity:
0004046
Arg of perigee: 89
3074 deg
Mean anomaly: 270
8540 deg
Mean motion: 15
50618188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1076
Checksum: 312
Coasting Arc #13 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2014/165/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 940484
09 A = 6793599
02 meter
Y = 5574308
50 meter E =
0009885
Z = -3777416
16 I = 51
97687
XDOT = -5116
639046 Wp = 98
61088
YDOT = 3756
023398 meter/sec RA = 111
92298 deg
ZDOT = 4276
935507 TA = 216
53780
MA = 216
60528
Ha = 228
021 n
mi
Hp = 218
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3085577
72 X = 896430
46
Y = 18288413
71 feet Y = 5584579
85 meter
Z = -12393097
64 Z = -3772953
58
XDOT = -16786
873511 XDOT = -5179
035432
YDOT = 12322
911411 feet/sec YDOT = 3698
456325 meter/sec
ZDOT = 14031
940640 ZDOT = 4251
928625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18533776
69 X = 5649095
14
Y = -965094
69 feet Y = -294160
86 meter
Z = -12375114
09 Z = -3771934
77
XDOT = 10158
589516 XDOT = 3096
338084
YDOT = 16869
498270 feet/sec YDOT = 5141
823073 meter/sec
ZDOT = 13925
227404 ZDOT = 4244
409313
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 14165
51163502
00016717 00000-0 10270-3 0 9120
2 25544 51
6455 112
8432 0004004 92
2196 267
9413 15
50602695 10918
Satellite: ISS
Catalog Number: 25544
Epoch time: 14165
51163502 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 112
8432 deg
Eccentricity:
0004004
Arg of perigee: 92
2196 deg
Mean anomaly: 267
9413 deg
Mean motion: 15
50602695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 282
Coasting Arc #14 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2014/166/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -955124
08 A = 6794796
63 meter
Y = -5826819
74 meter E =
0016549
Z = 3347316
41 I = 51
99286
XDOT = 4922
337559 Wp = 92
40347
YDOT = -3522
039254 meter/sec RA = 106
98804 deg
ZDOT = -4707
074430 TA = 48
84832
MA = 48
70565
Ha = 228
004 n
mi
Hp = 218
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3133609
18 X = -906156
37
Y = -19116862
67 feet Y = -5837227
22 meter
Z = 10982009
23 Z = 3342794
71
XDOT = 16149
401439 XDOT = 4984
221301
YDOT = -11555
246897 feet/sec YDOT = -3466
647847 meter/sec
ZDOT = -15443
157580 ZDOT = -4683
012702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19342689
36 X = -5895651
72
Y = 1238320
95 feet Y = 377440
23 meter
Z = 10963822
38 Z = 3341773
06
XDOT = -9751
070967 XDOT = -2972
126431
YDOT = -15928
342677 feet/sec YDOT = -4854
958848 meter/sec
ZDOT = -15340
478343 ZDOT = -4675
777799
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 14166
54279701
00016717 00000-0 10270-3 0 9134
2 25544 51
6465 107
7302 0004016 95
5499 264
6110 15
50631647 11078
Satellite: ISS
Catalog Number: 25544
Epoch time: 14166
54279701 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 107
7302 deg
Eccentricity:
0004016
Arg of perigee: 95
5499 deg
Mean anomaly: 264
6110 deg
Mean motion: 15
50631647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 296
Coasting Arc #15 (Orbit 1121)
---------------------------------------
Vector Time (GMT): 2014/167/12:05:07
679
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1042681
85 A = 6795954
27 meter
Y = 6048730
63 meter E =
0008184
Z = -2922522
91 I = 52
00468
XDOT = -4735
980596 Wp = 80
75145
YDOT = 3254
292469 meter/sec RA = 102
05472 deg
ZDOT = 5059
053757 TA = 246
18888
MA = 246
27471
Ha = 227
971 n
mi
Hp = 218
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3420872
21 X = 989162
65
Y = 19844916
77 feet Y = 6060091
68 meter
Z = -9588329
77 Z = -2917587
02
XDOT = -15537
994081 XDOT = -4796
593926
YDOT = 10676
812563 feet/sec YDOT = 3200
992176 meter/sec
ZDOT = 16597
945398 ZDOT = 5035
900356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20067690
47 X = 6116632
06
Y = -1786656
58 feet Y = -544572
93 meter
Z = -9568427
95 Z = -2916456
84
XDOT = 9183
908367 XDOT = 2799
255270
YDOT = 15027
217178 feet/sec YDOT = 4580
295796 meter/sec
ZDOT = 16499
153706 ZDOT = 5028
942050
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 14167
50950739
00016717 00000-0 10270-3 0 9149
2 25544 51
6463 102
9369 0003956 98
6817 261
4782 15
50620119 11225
Satellite: ISS
Catalog Number: 25544
Epoch time: 14167
50950739 = yrday
fracday
Element set: 914
Inclination: 51
6463 deg
RA of node: 102
9369 deg
Eccentricity:
0003956
Arg of perigee: 98
6817 deg
Mean anomaly: 261
4782 deg
Mean motion: 15
50620119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1122
Checksum: 318
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