[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 4th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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 738)
---------------------------------------
Vector Time (GMT): 2015/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2272870
28 A = 6781207
85 meter
Y = -4807163
97 meter E =
0009078
Z = -4217348
58 I = 51
80043
XDOT = 6716
498783 Wp = 27
79257
YDOT = 60
001676 meter/sec RA = 26
07747 deg
ZDOT = -3683
501374 TA = 204
46114
MA = 204
50424
Ha = 220
804 n
mi
Hp = 215
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7456923
50 X = -2198460
73
Y = -15771535
34 feet Y = -4832164
83 meter
Z = -13836445
48 Z = -4228208
52
XDOT = 22035
757162 XDOT = 6733
221276
YDOT = 196
855891 feet/sec YDOT = 135
203269 meter/sec
ZDOT = -12084
978260 ZDOT = -3650
834124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6368468
83 X = 1941109
30
Y = -16202697
90 feet Y = -4938582
32 meter
Z = -13881982
72 Z = -4231228
33
XDOT = 13897
397392 XDOT = 4235
926725
YDOT = 15709
629763 feet/sec YDOT = 4788
295152 meter/sec
ZDOT = -11945
174852 ZDOT = -3640
889295
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 15035
52275114
00016717 00000-0 10270-3 0 9008
2 25544 51
6423 26
5176 0006188 327
9553 32
1223 15
54315133 7390
Satellite: ISS
Catalog Number: 25544
Epoch time: 15035
52275114 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 26
5176 deg
Eccentricity:
0006188
Arg of perigee: 327
9553 deg
Mean anomaly: 32
1223 deg
Mean motion: 15
54315133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 739
Checksum: 282
Coasting Arc #2 (Orbit 754)
---------------------------------------
Vector Time (GMT): 2015/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 558429
34 A = 6777817
78 meter
Y = 4482030
76 meter E =
0002834
Z = 5051571
63 I = 51
76066
XDOT = -7330
332498 Wp = 31
81919
YDOT = -1224
010829 meter/sec RA = 21
09139 deg
ZDOT = 1898
212712 TA = 39
82570
MA = 39
80491
Ha = 220
908 n
mi
Hp = 215
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1832117
27 X = 483730
65
Y = 14704825
32 feet Y = 4487858
13 meter
Z = 16573397
75 Z = 5054102
60
XDOT = -24049
647304 XDOT = -7325
321110
YDOT = -4015
783560 feet/sec YDOT = -1305
955242 meter/sec
ZDOT = 6227
731995 ZDOT = 1862
616461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9281550
63 X = -2829016
63
Y = 11537389
22 feet Y = 3516596
24 meter
Z = 16583350
75 Z = 5054605
31
XDOT = -13173
880114 XDOT = -4015
398659
YDOT = -19322
118861 feet/sec YDOT = -5889
381829 meter/sec
ZDOT = 6075
628600 ZDOT = 1851
851597
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 15036
55144127
00016717 00000-0 10270-3 0 9012
2 25544 51
6423 21
3875 0006315 331
2942 28
7862 15
54355405 7555
Satellite: ISS
Catalog Number: 25544
Epoch time: 15036
55144127 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 21
3875 deg
Eccentricity:
0006315
Arg of perigee: 331
2942 deg
Mean anomaly: 28
7862 deg
Mean motion: 15
54355405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 755
Checksum: 291
Coasting Arc #3 (Orbit 769)
---------------------------------------
Vector Time (GMT): 2015/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1279574
94 A = 6776631
70 meter
Y = -4004121
34 meter E =
0013393
Z = -5325769
09 I = 51
72734
XDOT = 7334
737867 Wp = 65
85063
YDOT = 2206
170356 meter/sec RA = 16
09635 deg
ZDOT = 109
129456 TA = 205
15650
MA = 205
22180
Ha = 220
987 n
mi
Hp = 214
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4198080
50 X = 1350124
92
Y = -13136881
04 feet Y = -3989418
23 meter
Z = -17472995
69 Z = -5319381
64
XDOT = 24064
100615 XDOT = 7308
992722
YDOT = 7238
091719 feet/sec YDOT = 2288
048231 meter/sec
ZDOT = 358
036273 ZDOT = 144
696747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12285161
10 X = 3744517
10
Y = -6344937
21 feet Y = -1933936
86 meter
Z = -17444875
76 Z = -5317198
13
XDOT = 11614
922468 XDOT = 3540
228368
YDOT = 21137
551677 feet/sec YDOT = 6442
725751 meter/sec
ZDOT = 509
813904 ZDOT = 155
391278
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 15037
51581735
00016717 00000-0 10270-3 0 9020
2 25544 51
6426 16
5780 0006260 335
4863 24
5992 15
54379399 7709
Satellite: ISS
Catalog Number: 25544
Epoch time: 15037
51581735 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 16
5780 deg
Eccentricity:
0006260
Arg of perigee: 335
4863 deg
Mean anomaly: 24
5992 deg
Mean motion: 15
54379399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 770
Checksum: 323
Coasting Arc #4 (Orbit 785)
---------------------------------------
Vector Time (GMT): 2015/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3113850
11 A = 6778046
45 meter
Y = 3392194
98 meter E =
0009785
Z = 4974325
50 I = 51
70204
XDOT = -6715
389127 Wp = 17
48379
YDOT = -3029
568268 meter/sec RA = 11
09945 deg
ZDOT = -2127
533998 TA = 93
27553
MA = 93
16358
Ha = 221
105 n
mi
Hp = 214
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10216043
68 X = -3175713
99
Y = 11129248
64 feet Y = 3357028
39 meter
Z = 16319965
54 Z = 4959048
75
XDOT = -22032
116560 XDOT = -6670
678102
YDOT = -9939
528437 feet/sec YDOT = -3104
414304 meter/sec
ZDOT = -6980
098420 ZDOT = -2160
046626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15147885
85 X = -4617075
61
Y = 959354
88 feet Y = 292411
37 meter
Z = 16253928
49 Z = 4954197
40
XDOT = -9020
165631 XDOT = -2749
346484
YDOT = -21247
689259 feet/sec YDOT = -6476
295686 meter/sec
ZDOT = -7118
632813 ZDOT = -2169
759281
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 15038
54446234
00016717 00000-0 10270-3 0 9039
2 25544 51
6428 11
4478 0006345 338
6427 21
4460 15
54427165 7862
Satellite: ISS
Catalog Number: 25544
Epoch time: 15038
54446234 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 11
4478 deg
Eccentricity:
0006345
Arg of perigee: 338
6427 deg
Mean anomaly: 21
4460 deg
Mean motion: 15
54427165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 786
Checksum: 305
Coasting Arc #5 (Orbit 800)
---------------------------------------
Vector Time (GMT): 2015/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4702142
26 A = 6781534
79 meter
Y = -2722737
44 meter E =
0006205
Z = -4059067
15 I = 51
68298
XDOT = 5483
921977 Wp = 50
67340
YDOT = 3680
050606 meter/sec RA = 6
10818 deg
ZDOT = 3892
052785 TA = 259
61569
MA = 259
68563
Ha = 221
223 n
mi
Hp = 214
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15426975
93 X = 4751956
22
Y = -8932865
60 feet Y = -2669876
83 meter
Z = -13317149
44 Z = -4036104
17
XDOT = 17991
870002 XDOT = 5423
457350
YDOT = 12073
656845 feet/sec YDOT = 3741
037644 meter/sec
ZDOT = 12769
202049 ZDOT = 3918
545049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17467795
23 X = 5324183
99
Y = 3909634
65 feet Y = 1191656
64 meter
Z = -13218359
58 Z = -4028956
00
XDOT = 5311
636557 XDOT = 1618
986823
YDOT = 19733
970042 feet/sec YDOT = 6014
914069 meter/sec
ZDOT = 12881
838474 ZDOT = 3926
384367
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 15039
50879567
00016717 00000-0 10270-3 0 9046
2 25544 51
6431 6
6385 0006370 342
7272 17
3664 15
54440574 8018
Satellite: ISS
Catalog Number: 25544
Epoch time: 15039
50879567 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 6
6385 deg
Eccentricity:
0006370
Arg of perigee: 342
7272 deg
Mean anomaly: 17
3664 deg
Mean motion: 15
54440574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 801
Checksum: 308
Coasting Arc #6 (Orbit 816)
---------------------------------------
Vector Time (GMT): 2015/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5934529
25 A = 6785391
04 meter
Y = 1965586
98 meter E =
0012131
Z = 2632751
68 I = 51
66537
XDOT = -3719
467241 Wp = 74
78480
YDOT = -4203
559853 meter/sec RA = 1
12580 deg
ZDOT = -5222
576928 TA = 75
55872
MA = 75
42413
Ha = 221
195 n
mi
Hp = 214
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19470240
32 X = -5968856
61
Y = 6448776
17 feet Y = 1899031
48 meter
Z = 8637636
74 Z = 2603839
70
XDOT = -12202
976513 XDOT = -3646
816584
YDOT = -13791
206866 feet/sec YDOT = -4244
747568 meter/sec
ZDOT = -17134
438740 ZDOT = -5240
468361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18886499
65 X = -5756605
09
Y = -8130520
48 feet Y = -2478182
64 meter
Z = 8513548
51 Z = 2594929
59
XDOT = -488
664572 XDOT = -148
944962
YDOT = -16966
666774 feet/sec YDOT = -5171
440033 meter/sec
ZDOT = -17210
164867 ZDOT = -5245
658252
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 15040
53739475
00016717 00000-0 10270-3 0 9055
2 25544 51
6435 1
5080 0006396 346
2635 13
8343 15
54501833 8176
Satellite: ISS
Catalog Number: 25544
Epoch time: 15040
53739475 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 1
5080 deg
Eccentricity:
0006396
Arg of perigee: 346
2635 deg
Mean anomaly: 13
8343 deg
Mean motion: 15
54501833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 817
Checksum: 295
Coasting Arc #7 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2015/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6614830
23 A = 6787828
61 meter
Y = -1168821
95 meter E =
0015006
Z = -912559
84 I = 51
64230
XDOT = 1623
518172 Wp = 20
11687
YDOT = 4592
966251 meter/sec RA = 356
15134 deg
ZDOT = 5928
287529 TA = 329
99818
MA = 330
08408
Ha = 221
249 n
mi
Hp = 214
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21702198
90 X = 6631841
47
Y = -3834717
70 feet Y = -1094755
57 meter
Z = -2993962
74 Z = -880385
20
XDOT = 5326
503190 XDOT = 1543
240763
YDOT = 15068
786914 feet/sec YDOT = 4610
673069 meter/sec
ZDOT = 19449
762234 ZDOT = 5935
978863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18990395
95 X = 5788272
69
Y = 11218822
60 feet Y = 3419497
13 meter
Z = -2856079
65 Z = -870533
08
XDOT = -5035
135526 XDOT = -1534
709308
YDOT = 13445
361102 feet/sec YDOT = 4098
146064 meter/sec
ZDOT = 19481
767361 ZDOT = 5938
042692
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 15041
50168432
00016717 00000-0 10270-3 0 9063
2 25544 51
6435 356
6984 0006326 349
8699 10
2325 15
54534608 8329
Satellite: ISS
Catalog Number: 25544
Epoch time: 15041
50168432 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 356
6984 deg
Eccentricity:
0006326
Arg of perigee: 349
8699 deg
Mean anomaly: 10
2325 deg
Mean motion: 15
54534608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 832
Checksum: 316
Coasting Arc #8 (Orbit 847)
---------------------------------------
Vector Time (GMT): 2015/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6713752
89 A = 6787608
01 meter
Y = 272745
44 meter E =
0005460
Z = -959405
20 I = 51
61150
XDOT = 643
639865 Wp = 102
97410
YDOT = -4837
275382 meter/sec RA = 351
17831 deg
ZDOT = -5908
822216 TA = 87
41519
MA = 87
35269
Ha = 221
259 n
mi
Hp = 213
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22026748
32 X = -6711643
42
Y = 894834
13 feet Y = 197679
62 meter
Z = -3147654
85 Z = -992013
90
XDOT = 2111
679347 XDOT = 726
386163
YDOT = -15870
326055 feet/sec YDOT = -4829
615494 meter/sec
ZDOT = -19385
899658 ZDOT = -5905
494280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17526337
83 X = -5342027
77
Y = -13338209
07 feet Y = -4065486
13 meter
Z = -3287211
83 Z = -1001942
17
XDOT = 10866
313193 XDOT = 3312
052261
YDOT = -9527
247593 feet/sec YDOT = -2903
905066 meter/sec
ZDOT = -19370
713291 ZDOT = -5904
193411
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 15042
53023652
00016717 00000-0 10270-3 0 9072
2 25544 51
6444 351
5676 0006388 353
1868 6
9197 15
54572107 8487
Satellite: ISS
Catalog Number: 25544
Epoch time: 15042
53023652 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 351
5676 deg
Eccentricity:
0006388
Arg of perigee: 353
1868 deg
Mean anomaly: 6
9197 deg
Mean motion: 15
54572107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 848
Checksum: 323
Coasting Arc #9 (Orbit 863)
---------------------------------------
Vector Time (GMT): 2015/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6178560
38 A = 6784760
19 meter
Y = 683584
45 meter E =
0015644
Z = 2694421
78 I = 51
57129
XDOT = -2808
185065 Wp = 54
85132
YDOT = 4920
706176 meter/sec RA = 346
19876 deg
ZDOT = 5178
601498 TA = 335
65709
MA = 335
73090
Ha = 221
190 n
mi
Hp = 213
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20270867
38 X = 6157368
81
Y = 2242731
15 feet Y = 752558
79 meter
Z = 8839966
48 Z = 2724384
22
XDOT = -9213
205595 XDOT = -2888
156308
YDOT = 16144
049134 feet/sec YDOT = 4888
856341 meter/sec
ZDOT = 16990
162394 ZDOT = 5164
765524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14394644
89 X = 4387487
76
Y = 14368434
68 feet Y = 4379498
89 meter
Z = 8968009
71 Z = 2733449
36
XDOT = -16311
148962 XDOT = -4971
638203
YDOT = 5749
010403 feet/sec YDOT = 1752
298371 meter/sec
ZDOT = 16930
007964 ZDOT = 5160
266427
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 15043
55876420
00016717 00000-0 10270-3 0 9085
2 25544 51
6443 346
4369 0006323 356
8603 3
2509 15
54609771 8647
Satellite: ISS
Catalog Number: 25544
Epoch time: 15043
55876420 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 346
4369 deg
Eccentricity:
0006323
Arg of perigee: 356
8603 deg
Mean anomaly: 3
2509 deg
Mean motion: 15
54609771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 864
Checksum: 316
Coasting Arc #10 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2015/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5106436
89 A = 6780483
07 meter
Y = -1725716
21 meter E =
0011557
Z = -4126145
79 I = 51
52742
XDOT = 4662
999607 Wp = 38
73993
YDOT = -4758
014481 meter/sec RA = 341
20556 deg
ZDOT = -3777
769464 TA = 192
19197
MA = 192
21996
Ha = 221
337 n
mi
Hp = 213
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16753401
86 X = -5066716
97
Y = -5661798
60 feet Y = -1782597
80 meter
Z = -13537223
72 Z = -4150855
03
XDOT = 15298
555141 XDOT = 4734
209051
YDOT = -15610
283729 feet/sec YDOT = -4705
471778 meter/sec
ZDOT = -12394
256771 ZDOT = -3754
944641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9742636
57 X = -2969555
63
Y = -14661163
22 feet Y = -4468722
55 meter
Z = -13642587
34 Z = -4158260
62
XDOT = 20640
470629 XDOT = 6291
215448
YDOT = -2265
230794 feet/sec YDOT = -690
442346 meter/sec
ZDOT = -12295
684723 ZDOT = -3747
724704
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 15044
52298689
00016717 00000-0 10270-3 0 9099
2 25544 51
6447 341
6263 0006397
5589 359
5570 15
54654266 8798
Satellite: ISS
Catalog Number: 25544
Epoch time: 15044
52298689 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 341
6263 deg
Eccentricity:
0006397
Arg of perigee:
5589 deg
Mean anomaly: 359
5570 deg
Mean motion: 15
54654266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 879
Checksum: 351
Coasting Arc #11 (Orbit 894)
---------------------------------------
Vector Time (GMT): 2015/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3582602
85 A = 6776802
30 meter
Y = 2790585
83 meter E =
0005800
Z = 5025038
51 I = 51
48618
XDOT = -6044
040340 Wp = 57
23363
YDOT = 4325
797373 meter/sec RA = 336
19842 deg
ZDOT = 1908
303817 TA = 14
24321
MA = 14
22686
Ha = 221
180 n
mi
Hp = 213
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11753946
37 X = 3526722
22
Y = 9155465
32 feet Y = 2830336
55 meter
Z = 16486346
83 Z = 5042306
02
XDOT = -19829
528674 XDOT = -6101
232905
YDOT = 14192
248599 feet/sec YDOT = 4257
889258 meter/sec
ZDOT = 6260
839295 ZDOT = 1878
804434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3881788
79 X = 1183169
22
Y = 14299878
93 feet Y = 4358603
10 meter
Z = 16559668
20 Z = 5047386
87
XDOT = -23370
004932 XDOT = -7123
177503
YDOT = -753
611059 feet/sec YDOT = -229
700651 meter/sec
ZDOT = 6133
804133 ZDOT = 1869
583500
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 15045
55146621
00016717 00000-0 10270-3 0 9103
2 25544 51
6449 336
4955 0006261 2
9452 357
1736 15
54710585 8958
Satellite: ISS
Catalog Number: 25544
Epoch time: 15045
55146621 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 336
4955 deg
Eccentricity:
0006261
Arg of perigee: 2
9452 deg
Mean anomaly: 357
1736 deg
Mean motion: 15
54710585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 895
Checksum: 315
Coasting Arc #12 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2015/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1828483
56 A = 6775672
51 meter
Y = -3817477
41 meter E =
0016681
Z = -5304202
67 I = 51
45421
XDOT = 6787
600439 Wp = 69
25904
YDOT = -3539
799521 meter/sec RA = 331
18064 deg
ZDOT = 214
107098 TA = 202
75252
MA = 202
82653
Ha = 221
383 n
mi
Hp = 213
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5998961
81 X = -1759894
39
Y = -12524532
19 feet Y = -3837541
38 meter
Z = -17402239
74 Z = -5312918
20
XDOT = 22269
030313 XDOT = 6825
638813
YDOT = -11613
515488 feet/sec YDOT = -3463
683459 meter/sec
ZDOT = 702
451108 ZDOT = 247
171825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2517454
19 X = 767320
04
Y = -13610317
11 feet Y = -4148424
66 meter
Z = -17438781
20 Z = -5315340
51
XDOT = 23867
391469 XDOT = 7274
780920
YDOT = 3359
074023 feet/sec YDOT = 1023
845762 meter/sec
ZDOT = 844
579573 ZDOT = 257
427854
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 15046
51564599
00016717 00000-0 10270-3 0 9119
2 25544 51
6453 331
6844 0006359 7
2752 352
8492 15
54714178 9107
Satellite: ISS
Catalog Number: 25544
Epoch time: 15046
51564599 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 331
6844 deg
Eccentricity:
0006359
Arg of perigee: 7
2752 deg
Mean anomaly: 352
8492 deg
Mean motion: 15
54714178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 910
Checksum: 320
Coasting Arc #13 (Orbit 925)
---------------------------------------
Vector Time (GMT): 2015/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -31468
35 A = 6777397
98 meter
Y = 4703100
73 meter E =
0012059
Z = 4877389
58 I = 51
43309
XDOT = -6905
711390 Wp = 35
44877
YDOT = 2388
206446 meter/sec RA = 326
16233 deg
ZDOT = -2334
876657 TA = 77
52895
MA = 77
39405
Ha = 221
428 n
mi
Hp = 212
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -103242
60 X = -107749
18
Y = 15430120
51 feet Y = 4702322
54 meter
Z = 16001934
33 Z = 4877051
23
XDOT = -22656
533431 XDOT = -6920
561935
YDOT = 7835
322986 feet/sec YDOT = 2310
899142 meter/sec
ZDOT = -7660
356485 ZDOT = -2368
458674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8947007
03 X = -2727047
74
Y = 12574802
25 feet Y = 3832799
72 meter
Z = 15999581
06 Z = 4876672
31
XDOT = -22132
892333 XDOT = -6746
105583
YDOT = -5765
205800 feet/sec YDOT = -1757
234728 meter/sec
ZDOT = -7804
469621 ZDOT = -2378
802340
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 15047
54407942
00016717 00000-0 10270-3 0 9122
2 25544 51
6453 326
5534 0006364 10
7713 349
3575 15
54757968 9262
Satellite: ISS
Catalog Number: 25544
Epoch time: 15047
54407942 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 326
5534 deg
Eccentricity:
0006364
Arg of perigee: 10
7713 deg
Mean anomaly: 349
3575 deg
Mean motion: 15
54757968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 926
Checksum: 328
Coasting Arc #14 (Orbit 940)
---------------------------------------
Vector Time (GMT): 2015/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1725597
23 A = 6781187
70 meter
Y = -5320102
00 meter E =
0008858
Z = -3837153
75 I = 51
42097
XDOT = 6387
620285 Wp = 58
20147
YDOT = -905
207901 meter/sec RA = 321
15065 deg
ZDOT = 4139
224389 TA = 255
44031
MA = 255
53857
Ha = 221
447 n
mi
Hp = 212
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5661408
23 X = 1803598
60
Y = -17454402
90 feet Y = -5300369
38 meter
Z = -12589087
11 Z = -3828581
54
XDOT = 20956
759465 XDOT = 6377
161501
YDOT = -2969
842196 feet/sec YDOT = -833
835573 meter/sec
ZDOT = 13580
132510 ZDOT = 4170
228078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14458751
43 X = 4407027
44
Y = -11340176
90 feet Y = -3456485
92 meter
Z = -12551403
63 Z = -3825667
83
XDOT = 18185
433478 XDOT = 5542
920124
YDOT = 8051
202061 feet/sec YDOT = 2454
006388 meter/sec
ZDOT = 13712
927273 ZDOT = 4179
700233
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 15048
50821404
00016717 00000-0 10270-3 0 9133
2 25544 51
6459 321
7424 0006338 14
3903 345
7429 15
54792479 9416
Satellite: ISS
Catalog Number: 25544
Epoch time: 15048
50821404 = yrday
fracday
Element set: 913
Inclination: 51
6459 deg
RA of node: 321
7424 deg
Eccentricity:
0006338
Arg of perigee: 14
3903 deg
Mean anomaly: 345
7429 deg
Mean motion: 15
54792479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 941
Checksum: 313
Coasting Arc #15 (Orbit 956)
---------------------------------------
Vector Time (GMT): 2015/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3189392
26 A = 6785263
95 meter
Y = 5548111
74 meter E =
0015181
Z = 2245120
73 I = 51
41047
XDOT = -5348
982683 Wp = 83
84912
YDOT = -865
739498 meter/sec RA = 316
15051 deg
ZDOT = -5426
047340 TA = 71
09325
MA = 70
92874
Ha = 221
494 n
mi
Hp = 212
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10463885
38 X = -3262101
20
Y = 18202466
32 feet Y = 5512039
54 meter
Z = 7365881
66 Z = 2229450
57
XDOT = -17549
155784 XDOT = -5312
547200
YDOT = -2840
352683 feet/sec YDOT = -925
352084 meter/sec
ZDOT = -17801
992585 ZDOT = -5451
942417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18678796
32 X = -5693297
12
Y = 9639683
21 feet Y = 2938175
44 meter
Z = 7297805
55 Z = 2224371
13
XDOT = -12434
102804 XDOT = -3789
914535
YDOT = -10449
292769 feet/sec YDOT = -3184
944436 meter/sec
ZDOT = -17912
595891 ZDOT = -5459
759228
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 15049
53660138
00016717 00000-0 10270-3 0 9143
2 25544 51
6457 316
6108 0006276 18
2312 341
9065 15
54806112 9575
Satellite: ISS
Catalog Number: 25544
Epoch time: 15049
53660138 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 316
6108 deg
Eccentricity:
0006276
Arg of perigee: 18
2312 deg
Mean anomaly: 341
9065 deg
Mean motion: 15
54806112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 957
Checksum: 302
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