[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 17th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
169/11:01:03
964 1
2 1
7 1
7
N/A 0
3 -0
2 220
5
000/00:04:07
929 -1
2 -0
1 211
9
Coasting Arc #1 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2015/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2393067
67 A = 6778880
65 meter
Y = -4971526
97 meter E =
0010863
Z = -3950413
27 I = 52
00432
XDOT = 3963
146174 Wp = 64
86441
YDOT = 5138
571101 meter/sec RA = 81
69689 deg
ZDOT = -4070
263705 TA = 162
75759
MA = 162
72067
Ha = 220
336 n
mi
Hp = 211
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7851271
87 X = 2467672
21
Y = -16310784
02 feet Y = -4944348
40 meter
Z = -12960673
46 Z = -3938607
76
XDOT = 13002
448079 XDOT = 3925
162681
YDOT = 16858
829071 feet/sec YDOT = 5182
677818 meter/sec
ZDOT = -13353
883548 ZDOT = -4051
103029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15490834
99 X = -4721606
51
Y = -9437002
30 feet Y = -2876398
30 meter
Z = -12908920
19 Z = -3934638
87
XDOT = 17328
832025 XDOT = 5281
828001
YDOT = -10308
895430 feet/sec YDOT = -3142
151327 meter/sec
ZDOT = -13272
478582 ZDOT = -4045
451472
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 15168
52365207
00016717 00000-0 10270-3 0 9008
2 25544 51
6446 82
3546 0004420 52
0878 308
0675 15
55466299 28096
Satellite: ISS
Catalog Number: 25544
Epoch time: 15168
52365207 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 82
3546 deg
Eccentricity:
0004420
Arg of perigee: 52
0878 deg
Mean anomaly: 308
0675 deg
Mean motion: 15
55466299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2809
Checksum: 318
Coasting Arc #2 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2015/169/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 684269
05 A = 6783317
25 meter
Y = -6207248
30 meter E =
0007333
Z = -2652265
88 I = 52
01036
XDOT = 4850
787839 Wp = 103
10024
YDOT = 2770
773168 meter/sec RA = 76
91885 deg
ZDOT = -5246
900773 TA = 106
63614
MA = 106
55561
Ha = 220
535 n
mi
Hp = 211
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2244977
19 X = 766512
78
Y = -20364987
85 feet Y = -6199136
13 meter
Z = -8701659
72 Z = -2648742
97
XDOT = 15914
658266 XDOT = 4844
931229
YDOT = 9090
463149 feet/sec YDOT = 2824
985846 meter/sec
ZDOT = -17214
241380 ZDOT = -5223
350522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18555721
26 X = -5655783
84
Y = -8703026
53 feet Y = -2652682
49 meter
Z = -8685279
05 Z = -2647273
05
XDOT = 13108
318642 XDOT = 3995
415522
YDOT = -10914
848454 feet/sec YDOT = -3326
845809 meter/sec
ZDOT = -17113
489887 ZDOT = -5216
191718
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 15169
48735715
00016717 00000-0 10270-3 0 9010
2 25544 51
6439 77
5405 0003346 68
0866 292
0643 15
55172845 28243
Satellite: ISS
Catalog Number: 25544
Epoch time: 15169
48735715 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 77
5405 deg
Eccentricity:
0003346
Arg of perigee: 68
0866 deg
Mean anomaly: 292
0643 deg
Mean motion: 15
55172845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 327
Coasting Arc #3 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2015/170/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1825042
43 A = 6778780
74 meter
Y = 4991135
64 meter E =
0013136
Z = 4198155
38 I = 51
98688
XDOT = -4642
860431 Wp = 97
06166
YDOT = -4843
127274 meter/sec RA = 71
95284 deg
ZDOT = 3728
042347 TA = 314
82426
MA = 314
93095
Ha = 220
569 n
mi
Hp = 211
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5987672
02 X = -1901111
79
Y = 16375116
92 feet Y = 4970300
95 meter
Z = 13773475
66 Z = 4189105
61
XDOT = -15232
481730 XDOT = -4606
467662
YDOT = -15889
525177 feet/sec YDOT = -4894
843771 meter/sec
ZDOT = 12231
110063 ZDOT = 3705
576157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13754535
27 X = 4192382
35
Y = 10766036
90 feet Y = 3281488
05 meter
Z = 13733554
21 Z = 4185987
32
XDOT = -19005
544616 XDOT = -5792
889999
YDOT = 8752
428476 feet/sec YDOT = 2667
740200 meter/sec
ZDOT = 12135
433552 ZDOT = 3698
880147
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 15170
51549236
00016717 00000-0 10270-3 0 9028
2 25544 51
6435 72
4070 0003316 72
3444 287
8071 15
55194373 28403
Satellite: ISS
Catalog Number: 25544
Epoch time: 15170
51549236 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 72
4070 deg
Eccentricity:
0003316
Arg of perigee: 72
3444 deg
Mean anomaly: 287
8071 deg
Mean motion: 15
55194373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 295
Coasting Arc #4 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2015/171/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2994365
59 A = 6774964
39 meter
Y = -3252183
27 meter E =
0016866
Z = -5148981
93 I = 51
96443
XDOT = 4051
422089 Wp = 77
11436
YDOT = 6292
853767 meter/sec RA = 66
97112 deg
ZDOT = -1619
385649 TA = 177
31511
MA = 177
30605
Ha = 220
436 n
mi
Hp = 211
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9824034
10 X = 3055521
36
Y = -10669892
61 feet Y = -3218355
79 meter
Z = -16892985
34 Z = -5134287
82
XDOT = 13292
067222 XDOT = 3988
619088
YDOT = 20645
845693 feet/sec YDOT = 6337
808449 meter/sec
ZDOT = -5312
945044 ZDOT = -1599
856618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7364837
44 X = -2244802
45
Y = -12580577
28 feet Y = -3834559
95 meter
Z = -16829125
14 Z = -5129517
34
XDOT = 22687
896237 XDOT = 6915
270773
YDOT = -6288
845021 feet/sec YDOT = -1916
839962 meter/sec
ZDOT = -5230
196710 ZDOT = -1594
163957
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 15171
47935102
00016717 00000-0 10270-3 0 9036
2 25544 51
6441 67
5940 0003307 74
7335 285
4183 15
55240250 28556
Satellite: ISS
Catalog Number: 25544
Epoch time: 15171
47935102 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 67
5940 deg
Eccentricity:
0003307
Arg of perigee: 74
7335 deg
Mean anomaly: 285
4183 deg
Mean motion: 15
55240250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 296
Coasting Arc #5 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2015/172/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4043090
24 A = 6774146
44 meter
Y = 1219698
79 meter E =
0006176
Z = 5291942
92 I = 51
94854
XDOT = -3072
681866 Wp = 69
23064
YDOT = -6994
842612 meter/sec RA = 61
98100 deg
ZDOT = -732
546855 TA = 27
74762
MA = 27
71468
Ha = 220
433 n
mi
Hp = 211
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13264731
75 X = -4082134
79
Y = 4001636
44 feet Y = 1174267
48 meter
Z = 17362017
47 Z = 5272207
80
XDOT = -10080
977250 XDOT = -2990
677081
YDOT = -22948
958701 feet/sec YDOT = -7028
744766 meter/sec
ZDOT = -2403
368947 ZDOT = -747
274730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 228170
21 X = 69546
28
Y = 13959344
48 feet Y = 4254808
20 meter
Z = 17276877
41 Z = 5265992
24
XDOT = -23800
397369 XDOT = -7254
361118
YDOT = 3451
755765 feet/sec YDOT = 1052
095157 meter/sec
ZDOT = -2465
316453 ZDOT = -751
428455
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 15172
50744716
00016717 00000-0 10270-3 0 9041
2 25544 51
6437 62
4601 0003091 77
2352 282
9146 15
55291041 28719
Satellite: ISS
Catalog Number: 25544
Epoch time: 15172
50744716 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 62
4601 deg
Eccentricity:
0003091
Arg of perigee: 77
2352 deg
Mean anomaly: 282
9146 deg
Mean motion: 15
55291041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 294
Coasting Arc #6 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2015/173/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4874071
62 A = 6776944
26 meter
Y = 822543
80 meter E =
0013081
Z = -4648546
21 I = 51
94265
XDOT = 1676
313809 Wp = 102
85963
YDOT = 6856
314452 meter/sec RA = 56
99298 deg
ZDOT = 2975
043171 TA = 196
67521
MA = 196
71826
Ha = 220
337 n
mi
Hp = 211
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15991048
63 X = 4887092
25
Y = 2698634
50 feet Y = 877122
05 meter
Z = -15251135
87 Z = -4624837
37
XDOT = 5499
717222 XDOT = 1585
068715
YDOT = 22494
469986 feet/sec YDOT = 6874
549656 meter/sec
ZDOT = 9760
640326 ZDOT = 2982
965288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6701955
90 X = 2042756
16
Y = -14871968
79 feet Y = -4532976
09 meter
Z = -15149314
88 Z = -4617511
18
XDOT = 22054
063111 XDOT = 6722
078436
YDOT = -23
308854 feet/sec YDOT = -7
104539 meter/sec
ZDOT = 9793
331359 ZDOT = 2985
007398
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 15173
47127213
00016717 00000-0 10270-3 0 9056
2 25544 51
6443 57
6467 0003133 80
1789 279
9718 15
55282480 28860
Satellite: ISS
Catalog Number: 25544
Epoch time: 15173
47127213 = yrday
fracday
Element set: 905
Inclination: 51
6443 deg
RA of node: 57
6467 deg
Eccentricity:
0003133
Arg of perigee: 80
1789 deg
Mean anomaly: 279
9718 deg
Mean motion: 15
55282480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 330
Coasting Arc #7 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2015/174/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5311834
80 A = 6781531
44 meter
Y = -2668344
68 meter E =
0015944
Z = 3249864
80 I = 51
93988
XDOT = 72
075111 Wp = 91
21839
YDOT = -5997
892001 meter/sec RA = 52
01688 deg
ZDOT = -4786
971895 TA = 51
24626
MA = 51
10389
Ha = 220
402 n
mi
Hp = 211
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17427279
53 X = -5297388
51
Y = -8754411
69 feet Y = -2727664
58 meter
Z = 10662286
09 Z = 3224095
91
XDOT = 236
466900 XDOT = 162
392844
YDOT = -19678
123362 feet/sec YDOT = -5996
580638 meter/sec
ZDOT = -15705
288369 ZDOT = -4786
402868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12662214
98 X = -3859443
13
Y = 14911677
15 feet Y = 4545079
19 meter
Z = 10551982
61 Z = 3216244
30
XDOT = -17947
817614 XDOT = -5470
494809
YDOT = -4082
757589 feet/sec YDOT = -1244
424513 meter/sec
ZDOT = -15701
620012 ZDOT = -4785
853780
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 15174
49933319
00016717 00000-0 10270-3 0 9062
2 25544 51
6442 52
5126 0003178 84
3602 275
7914 15
55300417 29026
Satellite: ISS
Catalog Number: 25544
Epoch time: 15174
49933319 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 52
5126 deg
Eccentricity:
0003178
Arg of perigee: 84
3602 deg
Mean anomaly: 275
7914 deg
Mean motion: 15
55300417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 302
Coasting Arc #8 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2015/175/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5253070
48 A = 6785007
43 meter
Y = 4062725
04 meter E =
0010973
Z = -1375424
30 I = 51
93253
XDOT = -2004
170267 Wp = 49
27225
YDOT = 4554
141602 meter/sec RA = 47
05359 deg
ZDOT = 5834
947705 TA = 295
79948
MA = 295
91264
Ha = 220
210 n
mi
Hp = 211
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17234483
21 X = 5213930
98
Y = 13329150
40 feet Y = 4121249
58 meter
Z = -4512546
91 Z = -1350000
69
XDOT = -6575
361769 XDOT = -2083
290766
YDOT = 14941
409455 feet/sec YDOT = 4531
286822 meter/sec
ZDOT = 19143
529215 ZDOT = 5825
020020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16814727
96 X = 5125129
08
Y = -13889789
92 feet Y = -4233607
97 meter
Z = -4404021
01 Z = -1342345
60
XDOT = 12080
469733 XDOT = 3682
127175
YDOT = 8608
209570 feet/sec YDOT = 2623
782277 meter/sec
ZDOT = 19099
893327 ZDOT = 5821
647486
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 15175
46312172
00016717 00000-0 10270-3 0 9079
2 25544 51
6449 47
6989 0003003 86
6709 273
4788 15
55351111 29172
Satellite: ISS
Catalog Number: 25544
Epoch time: 15175
46312172 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 47
6989 deg
Eccentricity:
0003003
Arg of perigee: 86
6709 deg
Mean anomaly: 273
4788 deg
Mean motion: 15
55351111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 325
Coasting Arc #9 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2015/176/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4575668
04 A = 6785571
50 meter
Y = -4945369
53 meter E =
0012434
Z = -768131
36 I = 51
91208
XDOT = 3952
165920 Wp = 130
14320
YDOT = -2739
849373 meter/sec RA = 42
09714 deg
ZDOT = -5974
387125 TA = 58
13160
MA = 58
01065
Ha = 220
156 n
mi
Hp = 211
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15012034
27 X = -4516296
36
Y = -16224965
65 feet Y = -4996205
62 meter
Z = -2520116
02 Z = -790215
29
XDOT = 12966
423623 XDOT = 4011
531206
YDOT = -8989
007129 feet/sec YDOT = -2695
321260 meter/sec
ZDOT = -19601
007629 ZDOT = -5955
044270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18945735
32 X = -5774660
13
Y = 11366060
77 feet Y = 3464375
32 meter
Z = -2614085
60 Z = -796773
29
XDOT = -5299
039522 XDOT = -1615
147246
YDOT = -13269
610263 feet/sec YDOT = -4044
577208 meter/sec
ZDOT = -19517
243820 ZDOT = -5948
855916
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 15176
49114629
00016717 00000-0 10270-3 0 9081
2 25544 51
6450 42
5646 0002892 92
9019 267
2465 15
55328410 29334
Satellite: ISS
Catalog Number: 25544
Epoch time: 15176
49114629 = yrday
fracday
Element set: 908
Inclination: 51
6450 deg
RA of node: 42
5646 deg
Eccentricity:
0002892
Arg of perigee: 92
9019 deg
Mean anomaly: 267
2465 deg
Mean motion: 15
55328410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2933
Checksum: 319
Coasting Arc #10 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2015/177/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3322773
45 A = 6782437
33 meter
Y = 5224345
03 meter E =
0016284
Z = 2751422
65 I = 51
87777
XDOT = -5612
323775 Wp = 81
01063
YDOT = 836
023675 meter/sec RA = 37
13372 deg
ZDOT = 5166
809947 TA = 310
06731
MA = 310
20999
Ha = 220
065 n
mi
Hp = 211
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10901487
70 X = 3250741
19
Y = 17140239
61 feet Y = 5261099
46 meter
Z = 9026977
19 Z = 2767389
59
XDOT = -18413
135746 XDOT = -5646
353778
YDOT = 2742
859825 feet/sec YDOT = 773
072269 meter/sec
ZDOT = 16951
476205 ZDOT = 5139
463694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18869208
94 X = 5751334
89
Y = -7440318
71 feet Y = -2267809
14 meter
Z = 9094568
51 Z = 2772024
48
XDOT = -1316
656921 XDOT = -401
317030
YDOT = 17330
913335 feet/sec YDOT = 5282
462385 meter/sec
ZDOT = 16833
683080 ZDOT = 5130
906603
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 15177
51915134
00016717 00000-0 10270-3 0 9096
2 25544 51
6448 37
4298 0002876 90
3713 269
7769 15
55378511 29490
Satellite: ISS
Catalog Number: 25544
Epoch time: 15177
51915134 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 37
4298 deg
Eccentricity:
0002876
Arg of perigee: 90
3713 deg
Mean anomaly: 269
7769 deg
Mean motion: 15
55378511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2949
Checksum: 350
Coasting Arc #11 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2015/178/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1527204
82 A = 6777585
65 meter
Y = -4987591
41 meter E =
0011154
Z = -4338578
10 I = 51
83561
XDOT = 6740
166423 Wp = 74
93550
YDOT = 982
150231 meter/sec RA = 32
15494 deg
ZDOT = -3506
336952 TA = 159
48641
MA = 159
44159
Ha = 219
940 n
mi
Hp = 211
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5010514
49 X = -1450243
59
Y = -16363488
86 feet Y = -5004238
85 meter
Z = -14234180
11 Z = -4345810
57
XDOT = 22113
406899 XDOT = 6745
715381
YDOT = 3222
277662 feet/sec YDOT = 1057
554569 meter/sec
ZDOT = -11503
730158 ZDOT = -3473
580809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16963894
89 X = -5170595
16
Y = 2058763
87 feet Y = 627511
23 meter
Z = -14264244
39 Z = -4347741
69
XDOT = 7105
418990 XDOT = 2165
731708
YDOT = -20075
566208 feet/sec YDOT = -6119
032580 meter/sec
ZDOT = -11363
051806 ZDOT = -3463
458191
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 15178
48288835
00016717 00000-0 10270-3 0 9106
2 25544 51
6444 32
6162 0002643 94
9833 265
1623 15
55412925 29642
Satellite: ISS
Catalog Number: 25544
Epoch time: 15178
48288835 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 32
6162 deg
Eccentricity:
0002643
Arg of perigee: 94
9833 deg
Mean anomaly: 265
1623 deg
Mean motion: 15
55412925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 322
Coasting Arc #12 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2015/179/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -570446
10 A = 6774060
37 meter
Y = 4303170
90 meter E =
0006717
Z = 5195692
96 I = 51
79667
XDOT = -7134
793160 Wp = 113
40048
YDOT = -2514
584276 meter/sec RA = 27
15931 deg
ZDOT = 1295
352495 TA = 324
17470
MA = 324
21973
Ha = 219
982 n
mi
Hp = 211
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1871542
33 X = -643761
62
Y = 14118014
76 feet Y = 4296381
25 meter
Z = 17046236
75 Z = 5192744
27
XDOT = -23408
114043 XDOT = -7112
436563
YDOT = -8249
948412 feet/sec YDOT = -2594
245355 meter/sec
ZDOT = 4249
844144 ZDOT = 1260
746913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13648534
67 X = 4160073
37
Y = 4123293
81 feet Y = 1256779
95 meter
Z = 17032649
48 Z = 5191551
56
XDOT = -11447
368399 XDOT = -3489
157888
YDOT = 20895
906567 feet/sec YDOT = 6369
072322 meter/sec
ZDOT = 4101
538906 ZDOT = 1250
149059
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 15179
51085835
00016717 00000-0 10270-3 0 9117
2 25544 51
6445 27
4815 0002759 97
9482 262
1984 15
55434702 29803
Satellite: ISS
Catalog Number: 25544
Epoch time: 15179
51085835 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 27
4815 deg
Eccentricity:
0002759
Arg of perigee: 97
9482 deg
Mean anomaly: 262
1984 deg
Mean motion: 15
55434702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 334
Coasting Arc #13 (Orbit 2994)
---------------------------------------
Vector Time (GMT): 2015/180/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2748675
45 A = 6773871
42 meter
Y = -3332146
95 meter E =
0016752
Z = -5232654
97 I = 51
76646
XDOT = 6623
821311 Wp = 98
94047
YDOT = 3669
462797 meter/sec RA = 22
15358 deg
ZDOT = 1143
321708 TA = 182
01272
MA = 182
01947
Ha = 219
803 n
mi
Hp = 211
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9017964
08 X = 2811150
36
Y = -10932240
64 feet Y = -3301059
43 meter
Z = -17167503
19 Z = -5219151
12
XDOT = 21731
697213 XDOT = 6576
742361
YDOT = 12038
919938 feet/sec YDOT = 3743
271314 meter/sec
ZDOT = 3751
055473 ZDOT = 1175
385168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9586353
50 X = -2921920
55
Y = -10533481
27 feet Y = -3210605
09 meter
Z = -17108720
77 Z = -5214738
09
XDOT = 14120
254066 XDOT = 4303
853439
YDOT = -19162
756037 feet/sec YDOT = -5840
808040 meter/sec
ZDOT = 3888
177709 ZDOT = 1185
116566
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 15180
47456183
00016717 00000-0 10270-3 0 9123
2 25544 51
6432 22
6665 0002595 100
9597 259
1848 15
55486593 29955
Satellite: ISS
Catalog Number: 25544
Epoch time: 15180
47456183 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 22
6665 deg
Eccentricity:
0002595
Arg of perigee: 100
9597 deg
Mean anomaly: 259
1848 deg
Mean motion: 15
55486593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2995
Checksum: 342
Coasting Arc #14 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2015/181/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4684379
34 A = 6777185
47 meter
Y = 2169970
12 meter E =
0011691
Z = 4382385
84 I = 51
74844
XDOT = -5254
330067 Wp = 77
12361
YDOT = -4435
314348 meter/sec RA = 17
15298 deg
ZDOT = -3410
036808 TA = 47
38097
MA = 47
28245
Ha = 219
772 n
mi
Hp = 211
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15368698
63 X = -4729584
28
Y = 7119324
54 feet Y = 2117332
93 meter
Z = 14377906
30 Z = 4359520
57
XDOT = -17238
615705 XDOT = -5187
778145
YDOT = -14551
556259 feet/sec YDOT = -4493
699094 meter/sec
ZDOT = -11187
784803 ZDOT = -3435
400299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5224225
83 X = 1592344
03
Y = 16199396
13 feet Y = 4937575
94 meter
Z = 14279107
06 Z = 4352271
83
XDOT = -15316
597665 XDOT = -4668
498968
YDOT = 14926
112050 feet/sec YDOT = 4549
478953 meter/sec
ZDOT = -11295
924857 ZDOT = -3442
997896
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 15181
50249417
00016717 00000-0 10270-3 0 9139
2 25544 51
6435 17
5316 0002410 103
5507 256
5915 15
55534571 30116
Satellite: ISS
Catalog Number: 25544
Epoch time: 15181
50249417 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 17
5316 deg
Eccentricity:
0002410
Arg of perigee: 103
5507 deg
Mean anomaly: 256
5915 deg
Mean motion: 15
55534571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 279
Coasting Arc #15 (Orbit 3025)
---------------------------------------
Vector Time (GMT): 2015/182/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6087431
42 A = 6781948
10 meter
Y = -971945
42 meter E =
0006606
Z = -2830482
42 I = 51
73219
XDOT = 3130
582418 Wp = 75
46631
YDOT = 4789
964090 meter/sec RA = 12
16389 deg
ZDOT = 5099
615187 TA = 252
42867
MA = 252
50084
Ha = 219
693 n
mi
Hp = 211
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19971887
87 X = 6111596
87
Y = -3188797
30 feet Y = -903736
24 meter
Z = -9286359
63 Z = -2800852
46
XDOT = 10270
939692 XDOT = 3052
015336
YDOT = 15715
105281 feet/sec YDOT = 4824
532261 meter/sec
ZDOT = 16731
020956 ZDOT = 5114
632750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1124223
46 X = -342663
31
Y = -20251793
77 feet Y = -6172746
74 meter
Z = -9158721
50 Z = -2791578
31
XDOT = 15197
069985 XDOT = 4632
066931
YDOT = -8421
443966 feet/sec YDOT = -2566
856121 meter/sec
ZDOT = 16794
587644 ZDOT = 5118
990314
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 15182
46616582
00016717 00000-0 10270-3 0 9147
2 25544 51
6420 12
7163 0002448 108
5840 251
5579 15
55529109 30261
Satellite: ISS
Catalog Number: 25544
Epoch time: 15182
46616582 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 12
7163 deg
Eccentricity:
0002448
Arg of perigee: 108
5840 deg
Mean anomaly: 251
5579 deg
Mean motion: 15
55529109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3026
Checksum: 302
Coasting Arc #16 (Orbit 3041)
---------------------------------------
Vector Time (GMT): 2015/183/11:03:07
929
Vector Time (MET): N/A
Weight (LBS) : 877564
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6730545
42 A = 6784902
99 meter
Y = -243342
88 meter E =
0015546
Z = 761046
88 I = 51
71155
XDOT = -508
978539 Wp = 123
99850
YDOT = -4805
981538 meter/sec RA = 7
18849 deg
ZDOT = -5959
420133 TA = 47
77676
MA = 47
64494
Ha = 219
568 n
mi
Hp = 211
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22081841
92 X = -6731020
92
Y = -798369
04 feet Y = -318611
01 meter
Z = 2496872
97 Z = 728350
32
XDOT = -1669
877096 XDOT = -426
250727
YDOT = -15767
655963 feet/sec YDOT = -4811
209866 meter/sec
ZDOT = -19551
903325 ZDOT = -5961
692374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2676893
64 X = -815917
18
Y = 21949067
76 feet Y = 6690075
85 meter
Z = 2356305
42 Z = 718201
89
XDOT = -14243
264652 XDOT = -4341
347066
YDOT = 392
131323 feet/sec YDOT = 119
521627 meter/sec
ZDOT = -19560
651903 ZDOT = -5962
086700
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 15183
49406268
00016717 00000-0 10270-3 0 9150
2 25544 51
6422 7
5809 0002395 108
5932 251
5478 15
55577965 30424
Satellite: ISS
Catalog Number: 25544
Epoch time: 15183
49406268 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 7
5809 deg
Eccentricity:
0002395
Arg of perigee: 108
5932 deg
Mean anomaly: 251
5478 deg
Mean motion: 15
55577965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3042
Checksum: 328
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