[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 17th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 905 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 691)
---------------------------------------
Vector Time (GMT): 2015/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5220190
59 A = 6781827
35 meter
Y = -1678359
66 meter E =
0016688
Z = 3983010
26 I = 51
52507
XDOT = 4558
572125 Wp = 64
90121
YDOT = 4731
138089 meter/sec RA = 197
43553 deg
ZDOT = -3960
968983 TA = 66
44871
MA = 66
27350
Ha = 222
668 n
mi
Hp = 212
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17126609
56 X = 5219222
02
Y = -5506429
35 feet Y = -1619989
14 meter
Z = 13067618
97 Z = 4008367
31
XDOT = 14955
945291 XDOT = 4524
569935
YDOT = 15522
106592 feet/sec YDOT = 4781
924611 meter/sec
ZDOT = -12995
305061 ZDOT = -3938
906782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13362276
12 X = -4072821
76
Y = 11925331
28 feet Y = 3634840
98 meter
Z = 13177262
07 Z = 4016429
48
XDOT = -19160
080591 XDOT = -5839
992564
YDOT = -7141
791607 feet/sec YDOT = -2176
818082 meter/sec
ZDOT = -12900
896874 ZDOT = -3932
193367
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 15289
54097117
00016717 00000-0 10270-3 0 9006
2 25544 51
6434 198
3749 0006726 41
6054 318
5610 15
54354269 6922
Satellite: ISS
Catalog Number: 25544
Epoch time: 15289
54097117 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 198
3749 deg
Eccentricity:
0006726
Arg of perigee: 41
6054 deg
Mean anomaly: 318
5610 deg
Mean motion: 15
54354269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 692
Checksum: 322
Coasting Arc #2 (Orbit 706)
---------------------------------------
Vector Time (GMT): 2015/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6214248
66 A = 6785544
79 meter
Y = 753444
17 meter E =
0011608
Z = -2614973
49 I = 51
56905
XDOT = -2781
650358 Wp = 49
27583
YDOT = -4864
654783 meter/sec RA = 192
44479 deg
ZDOT = 5231
340994 TA = 281
24786
MA = 281
37830
Ha = 222
644 n
mi
Hp = 212
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20387954
91 X = -6209509
15
Y = 2471929
71 feet Y = 683978
67 meter
Z = -8579309
33 Z = -2645150
29
XDOT = -9126
149470 XDOT = -2752
458316
YDOT = -15960
153489 feet/sec YDOT = -4895
597458 meter/sec
ZDOT = 17163
192238 ZDOT = 5217
899216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17415125
57 X = 5308130
27
Y = -10781455
29 feet Y = -3286187
57 meter
Z = -8709610
42 Z = -2654689
26
XDOT = 14297
405412 XDOT = 4357
849170
YDOT = 9334
719271 feet/sec YDOT = 2845
222434 meter/sec
ZDOT = 17105
982233 ZDOT = 5213
903385
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 15290
50534869
00016717 00000-0 10270-3 0 9015
2 25544 51
6438 193
5653 0006674 44
7218 315
4472 15
54400167 7073
Satellite: ISS
Catalog Number: 25544
Epoch time: 15290
50534869 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 193
5653 deg
Eccentricity:
0006674
Arg of perigee: 44
7218 deg
Mean anomaly: 315
4472 deg
Mean motion: 15
54400167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 707
Checksum: 312
Coasting Arc #3 (Orbit 722)
---------------------------------------
Vector Time (GMT): 2015/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6723792
63 A = 6788186
32 meter
Y = 173960
34 meter E =
0016375
Z = 884968
43 I = 51
60882
XDOT = 666
751316 Wp = 102
39016
YDOT = 4821
676495 meter/sec RA = 187
46605 deg
ZDOT = -5924
432174 TA = 68
02929
MA = 67
85536
Ha = 222
743 n
mi
Hp = 212
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22059687
10 X = 6717048
70
Y = 570736
03 feet Y = 249112
57 meter
Z = 2903439
73 Z = 917615
55
XDOT = 2187
504319 XDOT = 641
563830
YDOT = 15819
148607 feet/sec YDOT = 4828
991374 meter/sec
ZDOT = -19437
113431 ZDOT = -5921
254621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20089439
50 X = -6123261
16
Y = 9084731
70 feet Y = 2769026
22 meter
Z = 3044267
92 Z = 927892
86
XDOT = -8306
939171 XDOT = -2531
955059
YDOT = -11766
955040 feet/sec YDOT = -3586
567896 meter/sec
ZDOT = -19424
174406 ZDOT = -5920
488359
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 15291
53399946
00016717 00000-0 10270-3 0 9025
2 25544 51
6437 188
4349 0006605 48
9682 311
2041 15
54396369 7234
Satellite: ISS
Catalog Number: 25544
Epoch time: 15291
53399946 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 188
4349 deg
Eccentricity:
0006605
Arg of perigee: 48
9682 deg
Mean anomaly: 311
2041 deg
Mean motion: 15
54396369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 723
Checksum: 333
Coasting Arc #4 (Orbit 738)
---------------------------------------
Vector Time (GMT): 2015/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6642255
91 A = 6788114
68 meter
Y = -1004714
13 meter E =
0020077
Z = 903237
71 I = 51
64070
XDOT = 1517
450862 Wp = 53
57283
YDOT = -4630
426778 meter/sec RA = 182
49291 deg
ZDOT = 5928
537160 TA = 316
21144
MA = 316
37047
Ha = 222
722 n
mi
Hp = 212
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21792178
17 X = -6634914
94
Y = -3296306
21 feet Y = -1078951
12 meter
Z = 2963378
32 Z = 870988
29
XDOT = 4978
513326 XDOT = 1540
317560
YDOT = -15191
688903 feet/sec YDOT = -4613
329461 meter/sec
ZDOT = 19450
581233 ZDOT = 5935
964556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20953668
64 X = 6386678
20
Y = -6892961
94 feet Y = -2100974
80 meter
Z = 2824379
85 Z = 860870
98
XDOT = 2014
192660 XDOT = 613
925923
YDOT = 14218
840537 feet/sec YDOT = 4333
902596 meter/sec
ZDOT = 19483
371159 ZDOT = 5938
531529
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 15292
56262918
00016717 00000-0 10270-3 0 9038
2 25544 51
6438 183
3044 0006668 51
0007 309
1739 15
54440798 7399
Satellite: ISS
Catalog Number: 25544
Epoch time: 15292
56262918 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 183
3044 deg
Eccentricity:
0006668
Arg of perigee: 51
0007 deg
Mean anomaly: 309
1739 deg
Mean motion: 15
54440798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 739
Checksum: 321
Coasting Arc #5 (Orbit 753)
---------------------------------------
Vector Time (GMT): 2015/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5974678
45 A = 6785486
67 meter
Y = 1837637
98 meter E =
0009298
Z = -2648838
95 I = 51
66418
XDOT = -3623
164351 Wp = 86
32827
YDOT = 4284
766959 meter/sec RA = 177
51833 deg
ZDOT = -5215
014675 TA = 123
50099
MA = 123
41211
Ha = 222
675 n
mi
Hp = 212
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19601963
42 X = 5966552
72
Y = 6028995
99 feet Y = 1904405
18 meter
Z = -8690416
51 Z = -2619834
58
XDOT = -11887
022150 XDOT = -3645
475448
YDOT = 14057
634379 feet/sec YDOT = 4244
125290 meter/sec
ZDOT = -17109
628200 ZDOT = -5232
669983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20200544
51 X = -6157125
97
Y = 3831276
84 feet Y = 1167773
18 meter
Z = -8565536
84 Z = -2610775
63
XDOT = 4145
549052 XDOT = 1263
563351
YDOT = -16452
757662 feet/sec YDOT = -5014
800535 meter/sec
ZDOT = -17186
507238 ZDOT = -5238
447406
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 15293
52695132
00016717 00000-0 10270-3 0 9044
2 25544 51
6441 178
4945 0006438 54
6009 305
5744 15
54455000 7549
Satellite: ISS
Catalog Number: 25544
Epoch time: 15293
52695132 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 178
4945 deg
Eccentricity:
0006438
Arg of perigee: 54
6009 deg
Mean anomaly: 305
5744 deg
Mean motion: 15
54455000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 754
Checksum: 307
Coasting Arc #6 (Orbit 769)
---------------------------------------
Vector Time (GMT): 2015/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4774344
74 A = 6781429
39 meter
Y = -2595618
62 meter E =
0016291
Z = 4041650
30 I = 51
68278
XDOT = 5393
394821 Wp = 85
50843
YDOT = -3819
594410 meter/sec RA = 172
53538 deg
ZDOT = 3905
832291 TA = 324
01049
MA = 324
12008
Ha = 222
808 n
mi
Hp = 211
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15663860
69 X = -4764598
11
Y = -8515809
11 feet Y = -2648953
71 meter
Z = 13260007
54 Z = 4018481
05
XDOT = 17694
864899 XDOT = 5416
732314
YDOT = -12531
477722 feet/sec YDOT = -3759
151152 meter/sec
ZDOT = 12814
410403 ZDOT = 3932
089608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17902317
66 X = 5456626
42
Y = -117260
68 feet Y = -35741
06 meter
Z = 13160418
26 Z = 4011295
49
XDOT = -9414
905938 XDOT = -2869
663330
YDOT = 18155
618164 feet/sec YDOT = 5533
832416 meter/sec
ZDOT = 12928
352710 ZDOT = 3940
561906
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 15294
55554345
00016717 00000-0 10270-3 0 9059
2 25544 51
6441 173
3636 0006649 57
8737 302
3060 15
54492956 7702
Satellite: ISS
Catalog Number: 25544
Epoch time: 15294
55554345 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 173
3636 deg
Eccentricity:
0006649
Arg of perigee: 57
8737 deg
Mean anomaly: 302
3060 deg
Mean motion: 15
54492956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 770
Checksum: 325
Coasting Arc #7 (Orbit 784)
---------------------------------------
Vector Time (GMT): 2015/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3161267
37 A = 6777645
88 meter
Y = 3341377
61 meter E =
0018850
Z = -4995138
48 I = 51
70202
XDOT = -6649
190838 Wp = 69
88526
YDOT = 3161
737823 meter/sec RA = 167
54264 deg
ZDOT = -2093
192228 TA = 179
72274
MA = 179
72169
Ha = 222
577 n
mi
Hp = 211
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10371612
09 X = 3147933
10
Y = 10962524
96 feet Y = 3376654
00 meter
Z = -16388249
61 Z = -4979814
16
XDOT = -21814
930572 XDOT = -6673
883916
YDOT = 10373
155588 feet/sec YDOT = 3087
243941 meter/sec
ZDOT = -6867
428571 ZDOT = -2125
553315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14535137
14 X = -4430309
80
Y = -4315494
49 feet Y = -1315362
72 meter
Z = -16322631
89 Z = -4975138
20
XDOT = 13436
166484 XDOT = 4095
343544
YDOT = -18750
740104 feet/sec YDOT = -5715
225584 meter/sec
ZDOT = -7007
627234 ZDOT = -2135
924781
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 15295
51982912
00016717 00000-0 10270-3 0 9062
2 25544 51
6439 168
5534 0006479 60
1127 300
0669 15
54549760 7855
Satellite: ISS
Catalog Number: 25544
Epoch time: 15295
51982912 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 168
5534 deg
Eccentricity:
0006479
Arg of perigee: 60
1127 deg
Mean anomaly: 300
0669 deg
Mean motion: 15
54549760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 785
Checksum: 331
Coasting Arc #8 (Orbit 800)
---------------------------------------
Vector Time (GMT): 2015/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1291168
21 A = 6776046
61 meter
Y = -3989949
85 meter E =
0008630
Z = 5315289
80 I = 51
72819
XDOT = 7314
769702 Wp = 72
52687
YDOT = -2327
042760 meter/sec RA = 162
54433 deg
ZDOT = 32
556894 TA = 17
17818
MA = 17
14899
Ha = 222
607 n
mi
Hp = 211
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4236116
16 X = -1272275
67
Y = -13090386
65 feet Y = -4004282
38 meter
Z = 17438614
82 Z = 5309063
76
XDOT = 23998
588260 XDOT = 7340
089457
YDOT = -7634
654723 feet/sec YDOT = -2245
102604 meter/sec
ZDOT = 106
813957 ZDOT = 68
152810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10427713
50 X = 3178367
07
Y = 9026640
75 feet Y = 2751320
10 meter
Z = 17412373
11 Z = 5307291
32
XDOT = -16063
322202 XDOT = -4896
100607
YDOT = 18069
180724 feet/sec YDOT = 5507
486285 meter/sec
ZDOT = 260
859372 ZDOT = 79
509937
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 15296
54838316
00016717 00000-0 10270-3 0 9075
2 25544 51
6442 163
4227 0006452 64
3209 295
8609 15
54573211 8012
Satellite: ISS
Catalog Number: 25544
Epoch time: 15296
54838316 = yrday
fracday
Element set: 907
Inclination: 51
6442 deg
RA of node: 163
4227 deg
Eccentricity:
0006452
Arg of perigee: 64
3209 deg
Mean anomaly: 295
8609 deg
Mean motion: 15
54573211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 801
Checksum: 311
Coasting Arc #9 (Orbit 815)
---------------------------------------
Vector Time (GMT): 2015/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -613499
82 A = 6777283
71 meter
Y = 4531878
70 meter E =
0018275
Z = -5017765
66 I = 51
76183
XDOT = -7269
849899 Wp = 92
83522
YDOT = 1266
470141 meter/sec RA = 157
54670 deg
ZDOT = 2038
213477 TA = 196
94790
MA = 197
00902
Ha = 222
505 n
mi
Hp = 211
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2012794
69 X = -639755
98
Y = 14868368
45 feet Y = 4524870
78 meter
Z = -16462485
75 Z = -5020810
24
XDOT = -23851
213579 XDOT = -7293
372599
YDOT = 4155
085763 feet/sec YDOT = 1185
042584 meter/sec
ZDOT = 6687
052089 ZDOT = 2002
840120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6196511
62 X = -1888696
74
Y = -13647932
98 feet Y = -4159889
97 meter
Z = -16476356
67 Z = -5021993
51
XDOT = 17141
233086 XDOT = 5224
647845
YDOT = -15648
950507 feet/sec YDOT = -4769
800115 meter/sec
ZDOT = 6534
122653 ZDOT = 1991
600585
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 15297
51263481
00016717 00000-0 10270-3 0 9089
2 25544 51
6432 158
6116 0006375 66
9134 293
2691 15
54604095 8167
Satellite: ISS
Catalog Number: 25544
Epoch time: 15297
51263481 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 158
6116 deg
Eccentricity:
0006375
Arg of perigee: 66
9134 deg
Mean anomaly: 293
2691 deg
Mean motion: 15
54604095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 816
Checksum: 320
Coasting Arc #10 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2015/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2413855
10 A = 6780706
82 meter
Y = -4854480
51 meter E =
0016872
Z = 4061727
86 I = 51
80302
XDOT = 6613
919487 Wp = 74
62469
YDOT = 16
869152 meter/sec RA = 152
55931 deg
ZDOT = -3892
629741 TA = 55
65148
MA = 55
49197
Ha = 222
359 n
mi
Hp = 211
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7919472
13 X = 2448228
93
Y = -15926773
31 feet Y = -4827294
54 meter
Z = 13325878
82 Z = 4073538
17
XDOT = 21699
210914 XDOT = 6632
148611
YDOT = 55
344987 feet/sec YDOT = 90
931858 meter/sec
ZDOT = -12771
094952 ZDOT = -3860
455678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2016181
47 X = 614532
11
Y = 17633278
58 feet Y = 5374623
31 meter
Z = 13377656
45 Z = 4077509
69
XDOT = -17068
493719 XDOT = -5202
476886
YDOT = 11579
288314 feet/sec YDOT = 3529
367078 meter/sec
ZDOT = -12632
173006 ZDOT = -3850
286332
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 15298
54115019
00016717 00000-0 10270-3 0 9097
2 25544 51
6432 153
4806 0006299 69
2739 290
9088 15
54664814 8325
Satellite: ISS
Catalog Number: 25544
Epoch time: 15298
54115019 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 153
4806 deg
Eccentricity:
0006299
Arg of perigee: 69
2739 deg
Mean anomaly: 290
9088 deg
Mean motion: 15
54664814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 832
Checksum: 336
Coasting Arc #11 (Orbit 846)
---------------------------------------
Vector Time (GMT): 2015/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3868404
49 A = 6784813
52 meter
Y = 4911334
98 meter E =
0011057
Z = -2637611
61 I = 51
84272
XDOT = -5399
918048 Wp = 65
54481
YDOT = -1449
820851 meter/sec RA = 147
58475 deg
ZDOT = 5241
782413 TA = 264
82848
MA = 264
95468
Ha = 222
408 n
mi
Hp = 211
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12691615
78 X = -3910223
88
Y = 16113303
73 feet Y = 4867841
84 meter
Z = -8653581
39 Z = -2656506
09
XDOT = -17716
266563 XDOT = -5408
767707
YDOT = -4756
630088 feet/sec YDOT = -1510
255259 meter/sec
ZDOT = 17197
448860 ZDOT = 5215
528663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1571933
23 X = 479125
25
Y = -20415973
78 feet Y = -6222788
81 meter
Z = -8735970
45 Z = -2662723
79
XDOT = 15979
607583 XDOT = 4870
584391
YDOT = -6049
806299 feet/sec YDOT = -1843
980960 meter/sec
ZDOT = 17084
314137 ZDOT = 5207
298949
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 15299
50536796
00016717 00000-0 10270-3 0 9105
2 25544 51
6415 148
6692 0006248 73
5109 286
6730 15
54645558 8474
Satellite: ISS
Catalog Number: 25544
Epoch time: 15299
50536796 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 148
6692 deg
Eccentricity:
0006248
Arg of perigee: 73
5109 deg
Mean anomaly: 286
6730 deg
Mean motion: 15
54645558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 847
Checksum: 343
Coasting Arc #12 (Orbit 862)
---------------------------------------
Vector Time (GMT): 2015/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4934909
31 A = 6787396
90 meter
Y = -4578379
82 meter E =
0018170
Z = 818794
22 I = 51
87780
XDOT = 3784
735902 Wp = 110
99074
YDOT = 2995
470524 meter/sec RA = 142
62344 deg
ZDOT = -5961
210223 TA = 60
18047
MA = 59
99995
Ha = 222
406 n
mi
Hp = 211
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16190647
34 X = 4981761
59
Y = -15020931
16 feet Y = -4522932
37 meter
Z = 2686332
75 Z = 842881
87
XDOT = 12417
112539 XDOT = 3779
916652
YDOT = 9827
659200 feet/sec YDOT = 3037
766525 meter/sec
ZDOT = -19557
776321 ZDOT = -5942
836147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4750316
90 X = -1447896
59
Y = 21555185
20 feet Y = 6570020
45 meter
Z = 2791110
55 Z = 850730
49
XDOT = -14332
849097 XDOT = -4368
652405
YDOT = -595
492879 feet/sec YDOT = -181
506229 meter/sec
ZDOT = -19478
917867 ZDOT = -5937
174166
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 15300
53384696
00016717 00000-0 10270-3 0 9112
2 25544 51
6412 143
5375 0006309 76
7981 283
3875 15
54688712 8635
Satellite: ISS
Catalog Number: 25544
Epoch time: 15300
53384696 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 143
5375 deg
Eccentricity:
0006309
Arg of perigee: 76
7981 deg
Mean anomaly: 283
3875 deg
Mean motion: 15
54688712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 863
Checksum: 331
Coasting Arc #13 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2015/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5469632
68 A = 6787203
30 meter
Y = 3863595
98 meter E =
0019391
Z = 1055299
73 I = 51
90060
XDOT = -1993
712508 Wp = 64
19036
YDOT = -4459
290595 meter/sec RA = 137
66597 deg
ZDOT = 5916
612375 TA = 307
21869
MA = 307
39549
Ha = 222
364 n
mi
Hp = 211
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17944989
11 X = -5517556
23
Y = 12675839
83 feet Y = 3802163
04 meter
Z = 3462269
44 Z = 1028611
96
XDOT = -6541
051537 XDOT = -1972
440944
YDOT = -14630
218486 feet/sec YDOT = -4481
466350 meter/sec
ZDOT = 19411
457922 ZDOT = 5906
978943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7203120
84 X = 2195511
23
Y = -20775075
91 feet Y = -6332243
14 meter
Z = 3346360
74 Z = 1019970
75
XDOT = 12430
155033 XDOT = 3788
711254
YDOT = 7471
472609 feet/sec YDOT = 2277
304851 meter/sec
ZDOT = 19370
592983 ZDOT = 5904
156741
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 15301
56230642
00016717 00000-0 10270-3 0 9128
2 25544 51
6398 138
4045 0006216 81
2677 278
9180 15
54710213 8793
Satellite: ISS
Catalog Number: 25544
Epoch time: 15301
56230642 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 138
4045 deg
Eccentricity:
0006216
Arg of perigee: 81
2677 deg
Mean anomaly: 278
9180 deg
Mean motion: 15
54710213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 879
Checksum: 305
Coasting Arc #14 (Orbit 893)
---------------------------------------
Vector Time (GMT): 2015/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5535021
31 A = 6784172
13 meter
Y = -2690688
62 meter E =
0010445
Z = -2861221
08 I = 51
91313
XDOT = 155
435995 Wp = 99
14518
YDOT = 5719
812312 meter/sec RA = 132
70626 deg
ZDOT = -5095
663272 TA = 113
24098
MA = 113
13098
Ha = 222
357 n
mi
Hp = 211
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18159518
73 X = 5578596
97
Y = -8827718
57 feet Y = -2628548
81 meter
Z = -9387208
27 Z = -2834226
40
XDOT = 509
960614 XDOT = 116
217571
YDOT = 18765
788424 feet/sec YDOT = 5721
331057 meter/sec
ZDOT = -16718
055355 ZDOT = -5095
003614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9344365
05 X = -2848162
47
Y = 17960054
65 feet Y = 5474224
66 meter
Z = -9270150
68 Z = -2825541
93
XDOT = -10388
337151 XDOT = -3166
365164
YDOT = -14003
099175 feet/sec YDOT = -4268
144628 meter/sec
ZDOT = -16716
170551 ZDOT = -5095
088784
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 15302
52646992
00016717 00000-0 10270-3 0 9135
2 25544 51
6393 133
5930 0006252 84
0492 276
1373 15
54736642 8948
Satellite: ISS
Catalog Number: 25544
Epoch time: 15302
52646992 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 133
5930 deg
Eccentricity:
0006252
Arg of perigee: 84
0492 deg
Mean anomaly: 276
1373 deg
Mean motion: 15
54736642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 894
Checksum: 317
Coasting Arc #15 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2015/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5134339
66 A = 6779915
15 meter
Y = 1189441
28 meter E =
0016047
Z = 4253139
54 I = 51
91994
XDOT = 1497
612066 Wp = 99
30625
YDOT = -6591
670736 meter/sec RA = 127
73562 deg
ZDOT = 3637
154543 TA = 313
61700
MA = 313
75002
Ha = 222
379 n
mi
Hp = 211
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16844946
40 X = -5167919
31
Y = 3902366
42 feet Y = 1131838
03 meter
Z = 13953869
89 Z = 4228115
77
XDOT = 4913
425414 XDOT = 1553
542099
YDOT = -21626
216325 feet/sec YDOT = -6574
610665 meter/sec
ZDOT = 11932
921730 ZDOT = 3644
565779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11024238
39 X = 3360187
86
Y = -13433454
20 feet Y = -4094516
84 meter
Z = 13845564
04 Z = 4220127
92
XDOT = 8398
143290 XDOT = 2559
754075
YDOT = 19273
479530 feet/sec YDOT = 5874
556561 meter/sec
ZDOT = 11966
063610 ZDOT = 3647
256188
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 15303
55489188
00016717 00000-0 10270-3 0 9142
2 25544 51
6392 128
4599 0006137 87
9834 272
2022 15
54762267 9104
Satellite: ISS
Catalog Number: 25544
Epoch time: 15303
55489188 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 128
4599 deg
Eccentricity:
0006137
Arg of perigee: 87
9834 deg
Mean anomaly: 272
2022 deg
Mean motion: 15
54762267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 910
Checksum: 330
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