[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 31st 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3767 37 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 858)
---------------------------------------
Vector Time (GMT): 2014/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5665519
03 A = 6797120
57 meter
Y = -2686802
20 meter E =
0017475
Z = 2600413
04 I = 51
61106
XDOT = 4181
061909 Wp = 70
37400
YDOT = -3722
507126 meter/sec RA = 186
19003 deg
ZDOT = 5240
133518 TA = 318
88377
MA = 319
01531
Ha = 228
103 n
mi
Hp = 219
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18587660
85 X = -5647685
61
Y = -8814967
84 feet Y = -2750058
27 meter
Z = 8531538
83 Z = 2572933
48
XDOT = 13717
394716 XDOT = 4196
921963
YDOT = -12212
949890 feet/sec YDOT = -3675
663755 meter/sec
ZDOT = 17192
039100 ZDOT = 5260
482798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15373745
29 X = -4685917
56
Y = 13741098
18 feet Y = 4188286
73 meter
Z = 8415588
24 Z = 2565071
30
XDOT = -4950
475610 XDOT = -1508
904966
YDOT = -16167
667789 feet/sec YDOT = -4927
905142 meter/sec
ZDOT = 17278
790767 ZDOT = 5266
575426
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
55930288
00016717 00000-0 10270-3 0 9008
2 25544 51
6450 186
9820 0004218 49
0952 311
0564 15
50500796 8591
Satellite: ISS
Catalog Number: 25544
Epoch time: 14150
55930288 = yrday
fracday
Element set: 900
Inclination: 51
6450 deg
RA of node: 186
9820 deg
Eccentricity:
0004218
Arg of perigee: 49
0952 deg
Mean anomaly: 311
0564 deg
Mean motion: 15
50500796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 303
Coasting Arc #2 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2014/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5512461
03 A = 6795910
47 meter
Y = 2542892
13 meter E =
0007574
Z = -3062364
00 I = 51
63942
XDOT = -4475
839803 Wp = 82
60861
YDOT = 3794
858282 meter/sec RA = 181
23211 deg
ZDOT = -4915
183163 TA = 132
44810
MA = 132
38403
Ha = 227
996 n
mi
Hp = 219
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18085502
07 X = 5498492
21
Y = 8342821
94 feet Y = 2604458
26 meter
Z = -10047125
99 Z = -3035618
70
XDOT = -14684
513791 XDOT = -4494
065589
YDOT = 12450
322448 feet/sec YDOT = 3744
705237 meter/sec
ZDOT = -16125
929013 ZDOT = -4936
970126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14513074
84 X = 4423585
21
Y = -13722762
86 feet Y = -4182698
12 meter
Z = -9934245
92 Z = -3027958
16
XDOT = 5105
147987 XDOT = 1556
049106
YDOT = 17117
516386 feet/sec YDOT = 5217
418995 meter/sec
ZDOT = -16218
793420 ZDOT = -4943
488234
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
52607372
00016717 00000-0 10270-3 0 9012
2 25544 51
6460 182
1884 0004113 52
0612 308
0910 15
50540355 8744
Satellite: ISS
Catalog Number: 25544
Epoch time: 14151
52607372 = yrday
fracday
Element set: 901
Inclination: 51
6460 deg
RA of node: 182
1884 deg
Eccentricity:
0004113
Arg of perigee: 52
0612 deg
Mean anomaly: 308
0910 deg
Mean motion: 15
50540355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 270
Coasting Arc #3 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2014/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5328079
25 A = 6794885
11 meter
Y = -2392165
38 meter E =
0016083
Z = 3456611
96 I = 51
66563
XDOT = 4740
043005 Wp = 81
90352
YDOT = -3930
211396 meter/sec RA = 176
27532 deg
ZDOT = 4570
460609 TA = 318
58619
MA = 318
70799
Ha = 228
188 n
mi
Hp = 219
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17480574
95 X = -5317724
68
Y = -7848311
61 feet Y = -2451689
86 meter
Z = 11340590
41 Z = 3430753
69
XDOT = 15551
322195 XDOT = 4761
437320
YDOT = -12894
394345 feet/sec YDOT = -3877
086067 meter/sec
ZDOT = 14994
949504 ZDOT = 4593
538698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13599687
95 X = -4145184
89
Y = 13589664
99 feet Y = 4142129
89 meter
Z = 11231428
22 Z = 3423339
32
XDOT = -5529
265597 XDOT = -1685
320154
YDOT = -18051
293949 feet/sec YDOT = -5502
034396 meter/sec
ZDOT = 15093
316673 ZDOT = 4600
442922
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
55729475
00016717 00000-0 10270-3 0 9026
2 25544 51
6447 177
0753 0004285 55
6740 304
4816 15
50521117 8906
Satellite: ISS
Catalog Number: 25544
Epoch time: 14152
55729475 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 177
0753 deg
Eccentricity:
0004285
Arg of perigee: 55
6740 deg
Mean anomaly: 304
4816 deg
Mean motion: 15
50521117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 306
Coasting Arc #4 (Orbit 904)
---------------------------------------
Vector Time (GMT): 2014/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5104886
24 A = 6793599
03 meter
Y = 2302789
09 meter E =
0010182
Z = -3857046
89 I = 51
69340
XDOT = -4971
293470 Wp = 69
31153
YDOT = 4076
248646 meter/sec RA = 171
31986 deg
ZDOT = -4151
333319 TA = 156
97788
MA = 156
93222
Ha = 228
058 n
mi
Hp = 219
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16748314
43 X = 5097492
86
Y = 7555082
30 feet Y = 2359834
24 meter
Z = -12654353
32 Z = -3832265
75
XDOT = -16310
017945 XDOT = -4996
339641
YDOT = 13373
519180 feet/sec YDOT = 4020
516813 meter/sec
ZDOT = -13619
859971 ZDOT = -4175
543660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12841187
48 X = 3913993
94
Y = -13241081
84 feet Y = -4035881
75 meter
Z = -12549725
83 Z = -3825156
43
XDOT = 6070
034087 XDOT = 1850
146390
YDOT = 18876
390099 feet/sec YDOT = 5753
523702 meter/sec
ZDOT = -13723
059157 ZDOT = -4182
788431
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
52405952
00016717 00000-0 10270-3 0 9036
2 25544 51
6456 172
2819 0004175 58
4171 301
7387 15
50545554 9054
Satellite: ISS
Catalog Number: 25544
Epoch time: 14153
52405952 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 172
2819 deg
Eccentricity:
0004175
Arg of perigee: 58
4171 deg
Mean anomaly: 301
7387 deg
Mean motion: 15
50545554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 905
Checksum: 304
Coasting Arc #5 (Orbit 920)
---------------------------------------
Vector Time (GMT): 2014/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4857668
91 A = 6792487
63 meter
Y = -2220338
93 meter E =
0013784
Z = 4185039
40 I = 51
71919
XDOT = 5167
594009 Wp = 92
46933
YDOT = -4274
021739 meter/sec RA = 166
36528 deg
ZDOT = 3719
433907 TA = 319
31743
MA = 319
42032
Ha = 228
226 n
mi
Hp = 218
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15937233
95 X = -4852809
15
Y = -7284576
56 feet Y = -2274633
70 meter
Z = 13730444
21 Z = 4161453
09
XDOT = 16954
048587 XDOT = 5196
935174
YDOT = -14022
381032 feet/sec YDOT = -4216
070645 meter/sec
ZDOT = 12202
867150 ZDOT = 3744
608306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12094275
60 X = -3686335
20
Y = 12787255
57 feet Y = 3897555
50 meter
Z = 13630853
69 Z = 4154684
21
XDOT = -6844
533996 XDOT = -2086
213962
YDOT = -19635
243825 feet/sec YDOT = -5984
822318 meter/sec
ZDOT = 12310
194240 ZDOT = 3752
147204
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
55527346
00016717 00000-0 10270-3 0 9043
2 25544 51
6446 167
1687 0004275 61
4283 298
7298 15
50537904 9212
Satellite: ISS
Catalog Number: 25544
Epoch time: 14154
55527346 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 167
1687 deg
Eccentricity:
0004275
Arg of perigee: 61
4283 deg
Mean anomaly: 298
7298 deg
Mean motion: 15
50537904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 921
Checksum: 329
Coasting Arc #6 (Orbit 935)
---------------------------------------
Vector Time (GMT): 2014/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4588668
96 A = 6791309
77 meter
Y = 2206615
04 meter E =
0013578
Z = -4507767
97 I = 51
74565
XDOT = -5310
601388 Wp = 68
34450
YDOT = 4466
540910 meter/sec RA = 161
41205 deg
ZDOT = -3222
408172 TA = 169
23452
MA = 169
20543
Ha = 228
105 n
mi
Hp = 218
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15054688
20 X = 4585550
40
Y = 7239550
65 feet Y = 2257911
38 meter
Z = -14789265
01 Z = -4485484
21
XDOT = -17423
232899 XDOT = -5344
499101
YDOT = 14654
005610 feet/sec YDOT = 4406
965062 meter/sec
ZDOT = -10572
205290 ZDOT = -3248
288400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11559319
03 X = 3523280
44
Y = -12174189
27 feet Y = -3710692
89 meter
Z = -14695181
14 Z = -4479091
21
XDOT = 7694
004968 XDOT = 2345
132714
YDOT = 20188
405853 feet/sec YDOT = 6153
426104 meter/sec
ZDOT = -10682
565762 ZDOT = -3256
046044
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
52203235
00016717 00000-0 10270-3 0 9050
2 25544 51
6449 162
3754 0004219 64
4384 295
7202 15
50548856 9366
Satellite: ISS
Catalog Number: 25544
Epoch time: 14155
52203235 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 162
3754 deg
Eccentricity:
0004219
Arg of perigee: 64
4384 deg
Mean anomaly: 295
7202 deg
Mean motion: 15
50548856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 936
Checksum: 310
Coasting Arc #7 (Orbit 951)
---------------------------------------
Vector Time (GMT): 2014/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4305348
33 A = 6790294
06 meter
Y = -2209933
28 meter E =
0010974
Z = 4754740
66 I = 51
77068
XDOT = 5419
357393 Wp = 100
26311
YDOT = -4695
848618 meter/sec RA = 156
45967 deg
ZDOT = 2717
348528 TA = 322
88477
MA = 322
96060
Ha = 228
237 n
mi
Hp = 218
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14125158
57 X = -4303413
47
Y = -7250437
26 feet Y = -2258067
94 meter
Z = 15599542
85 Z = 4733830
34
XDOT = 17780
043939 XDOT = 5458
264595
YDOT = -15406
327487 feet/sec YDOT = -4635
028519 meter/sec
ZDOT = 8915
185460 ZDOT = 2743
769314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11088434
69 X = -3379754
89
Y = 11483978
31 feet Y = 3500316
59 meter
Z = 15511271
39 Z = 4727835
52
XDOT = -8717
173624 XDOT = -2656
994521
YDOT = -20643
046802 feet/sec YDOT = -6292
000665 meter/sec
ZDOT = 9027
885351 ZDOT = 2751
699455
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
55323921
00016717 00000-0 10270-3 0 9060
2 25544 51
6441 157
2621 0004232 66
7201 293
4395 15
50549968 9523
Satellite: ISS
Catalog Number: 25544
Epoch time: 14156
55323921 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 157
2621 deg
Eccentricity:
0004232
Arg of perigee: 66
7201 deg
Mean anomaly: 293
4395 deg
Mean motion: 15
50549968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 952
Checksum: 307
Coasting Arc #8 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2014/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4021197
55 A = 6789389
44 meter
Y = 2282962
18 meter E =
0016580
Z = -4986621
31 I = 51
79565
XDOT = -5461
483743 Wp = 73
33581
YDOT = 4900
365676 meter/sec RA = 151
50842 deg
ZDOT = -2161
984122 TA = 175
59183
MA = 175
57721
Ha = 228
139 n
mi
Hp = 218
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13192905
36 X = 4019593
66
Y = 7490033
41 feet Y = 2327921
14 meter
Z = -16360306
12 Z = -4967090
51
XDOT = -17918
253749 XDOT = -5505
372538
YDOT = 16077
315209 feet/sec YDOT = 4839
046591 meter/sec
ZDOT = -7093
123759 ZDOT = -2188
621729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10863805
83 X = 3311288
02
Y = -10715461
31 feet Y = -3266072
61 meter
Z = -16277886
24 Z = -4961499
73
XDOT = 9744
681748 XDOT = 2970
178997
YDOT = 20820
767868 feet/sec YDOT = 6346
170046 meter/sec
ZDOT = -7206
788306 ZDOT = -2196
629076
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
51999199
00016717 00000-0 10270-3 0 9074
2 25544 51
6439 152
4687 0004250 70
1470 290
0138 15
50552389 9671
Satellite: ISS
Catalog Number: 25544
Epoch time: 14157
51999199 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 152
4687 deg
Eccentricity:
0004250
Arg of perigee: 70
1470 deg
Mean anomaly: 290
0138 deg
Mean motion: 15
50552389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 967
Checksum: 329
Coasting Arc #9 (Orbit 982)
---------------------------------------
Vector Time (GMT): 2014/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3733236
79 A = 6788642
36 meter
Y = -2378632
52 meter E =
0008252
Z = 5140311
75 I = 51
81957
XDOT = 5475
025089 Wp = 101
32354
YDOT = -5124
728933 meter/sec RA = 146
55832 deg
ZDOT = 1601
150241 TA = 333
25091
MA = 333
29345
Ha = 228
239 n
mi
Hp = 218
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12248152
20 X = -3731331
14
Y = -7803912
48 feet Y = -2420369
64 meter
Z = 16864539
88 Z = 5122180
52
XDOT = 17962
680738 XDOT = 5524
146106
YDOT = -16813
415134 feet/sec YDOT = -5063
229132 meter/sec
ZDOT = 5253
117588 ZDOT = 1627
866397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10737015
44 X = -3272642
31
Y = 9910017
55 feet Y = 3020573
35 meter
Z = 16788062
40 Z = 5117001
42
XDOT = -10870
242402 XDOT = -3313
249884
YDOT = -20890
587215 feet/sec YDOT = -6367
450983 meter/sec
ZDOT = 5367
165489 ZDOT = 1635
912041
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
55119168
00016717 00000-0 10270-3 0 9080
2 25544 51
6433 147
3555 0004202 72
0152 288
1456 15
50559215 9831
Satellite: ISS
Catalog Number: 25544
Epoch time: 14158
55119168 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 147
3555 deg
Eccentricity:
0004202
Arg of perigee: 72
0152 deg
Mean anomaly: 288
1456 deg
Mean motion: 15
50559215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 983
Checksum: 305
Coasting Arc #10 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2014/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3466732
15 A = 6788135
73 meter
Y = 2537774
83 meter E =
0018516
Z = -5271721
15 I = 51
84316
XDOT = -5417
502228 Wp = 80
85241
YDOT = 5304
250810 meter/sec RA = 141
60909 deg
ZDOT = -1009
328445 TA = 179
48748
MA = 179
48558
Ha = 228
153 n
mi
Hp = 218
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11373793
16 X = 3463705
17
Y = 8326032
91 feet Y = 2576525
51 meter
Z = -17295673
05 Z = -5254887
21
XDOT = -17773
957441 XDOT = -5471
509870
YDOT = 17402
397670 feet/sec YDOT = 5243
366916 meter/sec
ZDOT = -3311
445030 ZDOT = -1035
777044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10860120
99 X = 3310164
88
Y = -9121030
99 feet Y = -2780090
24 meter
Z = -17224716
74 Z = -5250093
66
XDOT = 11913
251963 XDOT = 3631
159198
YDOT = 20650
567050 feet/sec YDOT = 6294
292837 meter/sec
ZDOT = -3424
404351 ZDOT = -1043
758446
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
51793780
00016717 00000-0 10270-3 0 9096
2 25544 51
6432 142
5616 0004259 75
5986 284
5638 15
50558662 9983
Satellite: ISS
Catalog Number: 25544
Epoch time: 14159
51793780 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 142
5616 deg
Eccentricity:
0004259
Arg of perigee: 75
5986 deg
Mean anomaly: 284
5638 deg
Mean motion: 15
50558662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 998
Checksum: 353
Coasting Arc #11 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2014/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3206182
67 A = 6787792
25 meter
Y = -2720226
62 meter E =
0006632
Z = 5322963
72 I = 51
86574
XDOT = 5341
438439 Wp = 90
15134
YDOT = -5486
277784 meter/sec RA = 136
66146 deg
ZDOT = 413
163516 TA = 355
91808
MA = 355
92349
Ha = 228
234 n
mi
Hp = 218
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10518972
02 X = -3201383
80
Y = -8924628
03 feet Y = -2756053
86 meter
Z = 17463791
73 Z = 5307399
73
XDOT = 17524
404326 XDOT = 5400
383210
YDOT = -17999
599028 feet/sec YDOT = -5426
216844 meter/sec
ZDOT = 1355
523346 ZDOT = 439
254540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11092019
99 X = -3380847
69
Y = 8339657
99 feet Y = 2541927
76 meter
Z = 17398246
36 Z = 5302985
49
XDOT = -12972
726058 XDOT = -3954
086903
YDOT = -20317
817245 feet/sec YDOT = -6192
870696 meter/sec
ZDOT = 1467
015370 ZDOT = 447
146285
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
54913018
00016717 00000-0 10270-3 0 9101
2 25544 51
6429 137
4484 0004193 77
6100 282
5520 15
50568888 10142
Satellite: ISS
Catalog Number: 25544
Epoch time: 14160
54913018 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 137
4484 deg
Eccentricity:
0004193
Arg of perigee: 77
6100 deg
Mean anomaly: 282
5520 deg
Mean motion: 15
50568888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 297
Coasting Arc #12 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2014/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2987852
33 A = 6787753
75 meter
Y = 2952891
71 meter E =
0019003
Z = -5348071
44 I = 51
88786
XDOT = -5199
209814 Wp = 89
25468
YDOT = 5606
462888 meter/sec RA = 131
71469 deg
ZDOT = 191
702788 TA = 182
56592
MA = 182
57568
Ha = 228
141 n
mi
Hp = 218
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9802665
13 X = 2980589
95
Y = 9687964
92 feet Y = 2986263
77 meter
Z = -17546166
13 Z = -5333573
97
XDOT = -17057
774981 XDOT = -5262
447382
YDOT = 18393
907114 feet/sec YDOT = 5547
968381 meter/sec
ZDOT = 628
946155 ZDOT = 166
292394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11543840
48 X = 3518562
58
Y = -7669752
89 feet Y = -2337740
68 meter
Z = -17485179
19 Z = -5329482
62
XDOT = 13863
648513 XDOT = 4225
640067
YDOT = 19686
417134 feet/sec YDOT = 6000
419942 meter/sec
ZDOT = 520
298641 ZDOT = 158
587026
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
51586920
00016717 00000-0 10270-3 0 9118
2 25544 51
6433 132
6543 0004225 80
9610 279
2019 15
50568747 10295
Satellite: ISS
Catalog Number: 25544
Epoch time: 14161
51586920 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 132
6543 deg
Eccentricity:
0004225
Arg of perigee: 80
9610 deg
Mean anomaly: 279
2019 deg
Mean motion: 15
50568747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 297
Coasting Arc #13 (Orbit 1044)
---------------------------------------
Vector Time (GMT): 2014/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2782983
89 A = 6787885
83 meter
Y = -3204739
48 meter E =
0007221
Z = 5291403
18 I = 51
90889
XDOT = 5052
041531 Wp = 74
31624
YDOT = -5712
880132 meter/sec RA = 126
76996 deg
ZDOT = -800
106204 TA = 23
31862
MA = 23
28588
Ha = 228
211 n
mi
Hp = 218
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9130524
57 X = -2772645
20
Y = -10514237
13 feet Y = -3235803
48 meter
Z = 17360246
66 Z = 5277908
35
XDOT = 16574
939406 XDOT = 5119
435485
YDOT = -18743
045052 feet/sec YDOT = -5656
008032 meter/sec
ZDOT = -2625
020354 ZDOT = -775
400821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12091760
61 X = -3685568
63
Y = 7047711
91 feet Y = 2148142
59 meter
Z = 17303551
89 Z = 5274122
62
XDOT = -14693
140618 XDOT = -4478
469260
YDOT = -19000
890321 feet/sec YDOT = -5791
471370 meter/sec
ZDOT = -2519
321486 ZDOT = -767
889189
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
54705420
00016717 00000-0 10270-3 0 9121
2 25544 51
6436 127
5413 0004177 83
5250 276
6377 15
50581245 10456
Satellite: ISS
Catalog Number: 25544
Epoch time: 14162
54705420 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 127
5413 deg
Eccentricity:
0004177
Arg of perigee: 83
5250 deg
Mean anomaly: 276
6377 deg
Mean motion: 15
50581245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1045
Checksum: 291
Coasting Arc #14 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2014/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2636917
84 A = 6788319
17 meter
Y = 3487762
17 meter E =
0017939
Z = -5208458
50 I = 51
92887
XDOT = -4851
815390 Wp = 97
43875
YDOT = 5746
880942 meter/sec RA = 121
82634 deg
ZDOT = 1393
805678 TA = 185
93374
MA = 185
95502
Ha = 228
103 n
mi
Hp = 218
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8651305
26 X = 2623022
17
Y = 11442789
28 feet Y = 3517172
96 meter
Z = -17088118
44 Z = -5195681
83
XDOT = -15918
029496 XDOT = -4922
488445
YDOT = 18854
596267 feet/sec YDOT = 5692
229464 meter/sec
ZDOT = 4572
853274 ZDOT = 1370
065199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12798703
89 X = 3901044
95
Y = -6618515
69 feet Y = -2017323
58 meter
Z = -17034515
83 Z = -5192120
43
XDOT = 15287
132725 XDOT = 4659
518055
YDOT = 18069
684060 feet/sec YDOT = 5507
639701 meter/sec
ZDOT = 4471
216967 ZDOT = 1362
826931
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
51378611
00016717 00000-0 10270-3 0 9138
2 25544 51
6443 122
7474 0004152 86
4813 273
6812 15
50582210 10609
Satellite: ISS
Catalog Number: 25544
Epoch time: 14163
51378611 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 122
7474 deg
Eccentricity:
0004152
Arg of perigee: 86
4813 deg
Mean anomaly: 273
6812 deg
Mean motion: 15
50582210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 281
Coasting Arc #15 (Orbit 1075)
---------------------------------------
Vector Time (GMT): 2014/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2508115
86 A = 6788921
76 meter
Y = -3781843
94 meter E =
0009530
Z = 5042647
49 I = 51
94758
XDOT = 4662
851756 Wp = 70
16736
YDOT = -5753
297414 meter/sec RA = 116
88499 deg
ZDOT = -1989
402643 TA = 39
10345
MA = 39
03461
Ha = 228
167 n
mi
Hp = 218
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8228726
58 X = -2490135
68
Y = -12407624
46 feet Y = -3809791
55 meter
Z = 16544119
05 Z = 5030506
44
XDOT = 15298
070066 XDOT = 4736
503803
YDOT = -18875
647684 feet/sec YDOT = -5700
742289 meter/sec
ZDOT = -6526
911558 ZDOT = -1966
573055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13568288
49 X = -4135614
33
Y = 6264411
11 feet Y = 1909392
51 meter
Z = 16493261
11 Z = 5027145
99
XDOT = -15754
608483 XDOT = -4802
004665
YDOT = -17142
822651 feet/sec YDOT = -5225
132344 meter/sec
ZDOT = -6429
115090 ZDOT = -1959
594279
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
54496372
00016717 00000-0 10270-3 0 9148
2 25544 51
6452 117
6347 0004136 89
6474 270
5151 15
50596080 10760
Satellite: ISS
Catalog Number: 25544
Epoch time: 14164
54496372 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 117
6347 deg
Eccentricity:
0004136
Arg of perigee: 89
6474 deg
Mean anomaly: 270
5151 deg
Mean motion: 15
50596080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1076
Checksum: 312
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