[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 6th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
065/04:19:10
113 0
4 2
5 2
5
N/A -1
4 -0
2 220
8
000/00:08:20
227 2
1 0
1 215
6
Coasting Arc #1 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2016/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4024527
58 A = 6777282
64 meter
Y = -1689186
77 meter E =
0003097
Z = 5182050
01 I = 51
33689
XDOT = 4198
848073 Wp = 114
35600
YDOT = 6305
932423 meter/sec RA = 229
02413 deg
ZDOT = -1206
092534 TA = 347
25597
MA = 347
26379
Ha = 220
840 n
mi
Hp = 214
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13203830
64 X = 4017945
43
Y = -5541951
34 feet Y = -1644218
18 meter
Z = 17001476
40 Z = 5201584
14
XDOT = 13775
748271 XDOT = 4133
880134
YDOT = 20688
754668 feet/sec YDOT = 6352
523368 meter/sec
ZDOT = -3956
996504 ZDOT = -1185
854106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14201306
94 X = 4328558
36
Y = -693176
36 feet Y = -211280
15 meter
Z = 17086455
33 Z = 5207951
58
XDOT = 5783
338363 XDOT = 1762
761533
YDOT = 23139
625692 feet/sec YDOT = 7052
957911 meter/sec
ZDOT = -3870
277812 ZDOT = -1179
660677
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 16062
54621794
00016717 00000-0 10270-3 0 9000
2 25544 51
6371 229
8399 0003515 187
9537 172
1561 15
54308215 28390
Satellite: ISS
Catalog Number: 25544
Epoch time: 16062
54621794 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 229
8399 deg
Eccentricity:
0003515
Arg of perigee: 187
9537 deg
Mean anomaly: 172
1561 deg
Mean motion: 15
54308215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 324
Coasting Arc #2 (Orbit 2853)
---------------------------------------
Vector Time (GMT): 2016/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5040369
23 A = 6779791
23 meter
Y = 178320
91 meter E =
0011099
Z = -4541983
67 I = 51
36840
XDOT = -3006
400634 Wp = 128
77815
YDOT = -6332
589669 meter/sec RA = 224
00512 deg
ZDOT = 3085
959153 TA = 172
27949
MA = 172
26239
Ha = 220
809 n
mi
Hp = 214
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16536644
44 X = -5019925
90
Y = 585042
35 feet Y = 122070
09 meter
Z = -14901521
22 Z = -4566418
60
XDOT = -9863
519139 XDOT = -2950
354696
YDOT = -20776
212826 feet/sec YDOT = -6365
895613 meter/sec
ZDOT = 10124
537903 ZDOT = 3071
491625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15721934
38 X = -4792045
60
Y = -4842886
66 feet Y = -1476111
85 meter
Z = -15007513
02 Z = -4574289
97
XDOT = -2915
363818 XDOT = -888
602892
YDOT = -21736
300124 feet/sec YDOT = -6625
224278 meter/sec
ZDOT = 10062
831077 ZDOT = 3067
150912
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 16063
51060478
00016717 00000-0 10270-3 0 9015
2 25544 51
6379 225
0298 0003523 191
3421 168
7653 15
54363426 28549
Satellite: ISS
Catalog Number: 25544
Epoch time: 16063
51060478 = yrday
fracday
Element set: 901
Inclination: 51
6379 deg
RA of node: 225
0298 deg
Eccentricity:
0003523
Arg of perigee: 191
3421 deg
Mean anomaly: 168
7653 deg
Mean motion: 15
54363426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2854
Checksum: 308
Coasting Arc #3 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2016/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5758527
98 A = 6783752
75 meter
Y = 1209982
79 meter E =
0011976
Z = 3361976
40 I = 51
40451
XDOT = 1461
838015 Wp = 106
91214
YDOT = 5940
296609 meter/sec RA = 218
99750 deg
ZDOT = -4631
556327 TA = 33
68777
MA = 33
61171
Ha = 220
595 n
mi
Hp = 214
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18892808
33 X = 5728238
86
Y = 3969759
81 feet Y = 1274209
40 meter
Z = 11030106
31 Z = 3389875
82
XDOT = 4796
056481 XDOT = 1417
801287
YDOT = 19489
162102 feet/sec YDOT = 5956
397237 meter/sec
ZDOT = -15195
394772 ZDOT = -4624
562645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16645072
11 X = 5073417
98
Y = 9641534
99 feet Y = 2938739
87 meter
Z = 11150911
26 Z = 3398797
75
XDOT = -723
784276 XDOT = -220
609447
YDOT = 18828
314794 feet/sec YDOT = 5738
870349 meter/sec
ZDOT = -15166
022043 ZDOT = -4622
603519
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 16064
53927548
00016717 00000-0 10270-3 0 9029
2 25544 51
6371 219
8989 0003507 196
0252 164
0790 15
54359870 28702
Satellite: ISS
Catalog Number: 25544
Epoch time: 16064
53927548 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 219
8989 deg
Eccentricity:
0003507
Arg of perigee: 196
0252 deg
Mean anomaly: 164
0790 deg
Mean motion: 15
54359870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2870
Checksum: 335
Coasting Arc #4 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2016/065/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5319227
09 A = 6789925
01 meter
Y = -4193018
22 meter E =
0011097
Z = 390415
48 I = 51
44171
XDOT = 3239
049889 Wp = 47
03670
YDOT = -3542
905957 meter/sec RA = 215
61442 deg
ZDOT = 5979
699803 TA = 317
18356
MA = 317
26993
Ha = 220
802 n
mi
Hp = 215
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17451532
44 X = -5273840
83
Y = -13756621
45 feet Y = -4252247
54 meter
Z = 1280890
68 Z = 364687
04
XDOT = 10626
804098 XDOT = 3249
380466
YDOT = -11623
707209 feet/sec YDOT = -3506
626446 meter/sec
ZDOT = 19618
437675 ZDOT = 5995
459457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21883013
74 X = 6669942
59
Y = -3899510
29 feet Y = -1188570
74 meter
Z = 1169969
45 Z = 356606
69
XDOT = 1418
358957 XDOT = 432
315810
YDOT = 13974
468079 feet/sec YDOT = 4259
417871 meter/sec
ZDOT = 19687
360929 ZDOT = 6000
707611
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 16065
24650045
00016717 00000-0 10270-3 0 9034
2 25544 51
6410 216
3765 0001706 244
2160 115
8816 15
53905553 28812
Satellite: ISS
Catalog Number: 25544
Epoch time: 16065
24650045 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 216
3765 deg
Eccentricity:
0001706
Arg of perigee: 244
2160 deg
Mean anomaly: 115
8816 deg
Mean motion: 15
53905553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 290
Coasting Arc #5 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2016/066/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4589591
22 A = 6788309
06 meter
Y = 4576304
04 meter E =
0006533
Z = -2008094
08 I = 51
46354
XDOT = -4745
963705 Wp = 156
17408
YDOT = 2328
878279 meter/sec RA = 210
63036 deg
ZDOT = -5551
948980 TA = 46
05751
MA = 46
00362
Ha = 220
781 n
mi
Hp = 215
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15057713
98 X = 4547831
03
Y = 15014120
85 feet Y = 4627394
18 meter
Z = -6588235
17 Z = -1985901
31
XDOT = -15570
747063 XDOT = -4744
684572
YDOT = 7640
676767 feet/sec YDOT = 2275
812322 meter/sec
ZDOT = -18215
055710 ZDOT = -5575
000412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21228078
07 X = -6470318
20
Y = 1666453
64 feet Y = 507935
07 meter
Z = -6492692
16 Z = -1978972
57
XDOT = 4400
053051 XDOT = 1341
136170
YDOT = -15151
004584 feet/sec YDOT = -4618
026197 meter/sec
ZDOT = -18315
418737 ZDOT = -5582
539631
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 16066
21115818
00016717 00000-0 10270-3 0 9047
2 25544 51
6417 211
5685 0001837 246
4880 113
6080 15
53907449 28966
Satellite: ISS
Catalog Number: 25544
Epoch time: 16066
21115818 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 211
5685 deg
Eccentricity:
0001837
Arg of perigee: 246
4880 deg
Mean anomaly: 113
6080 deg
Mean motion: 15
53907449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 317
Coasting Arc #6 (Orbit 2911)
---------------------------------------
Vector Time (GMT): 2016/067/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3508657
50 A = 6785029
98 meter
Y = -4694589
20 meter E =
0010862
Z = 3409605
62 I = 51
48099
XDOT = 6030
902563 Wp = 92
17202
YDOT = -1161
336065 meter/sec RA = 205
64106 deg
ZDOT = 4594
016136 TA = 307
82188
MA = 307
92015
Ha = 220
767 n
mi
Hp = 215
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11511343
52 X = -3472462
77
Y = -15402195
53 feet Y = -4733622
53 meter
Z = 11186370
15 Z = 3392650
25
XDOT = 19786
425731 XDOT = 6021
125332
YDOT = -3810
157694 feet/sec YDOT = -1093
948594 meter/sec
ZDOT = 15072
231418 ZDOT = 4623
288618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19248681
31 X = 5866998
06
Y = 922401
25 feet Y = 281147
90 meter
Z = 11113549
28 Z = 3387409
82
XDOT = -9575
911493 XDOT = -2918
737823
YDOT = 16179
860106 feet/sec YDOT = 4931
621360 meter/sec
ZDOT = 15199
406681 ZDOT = 4632
779156
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 16067
24011739
00016717 00000-0 10270-3 0 9059
2 25544 51
6419 206
4397 0001662 255
5983 104
4985 15
53934145 29126
Satellite: ISS
Catalog Number: 25544
Epoch time: 16067
24011739 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 206
4397 deg
Eccentricity:
0001662
Arg of perigee: 255
5983 deg
Mean anomaly: 104
4985 deg
Mean motion: 15
53934145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2912
Checksum: 319
Coasting Arc #7 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2016/068/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2095396
32 A = 6781238
50 meter
Y = 4620760
16 meter E =
0007765
Z = -4507070
13 I = 51
49858
XDOT = -6972
991528 Wp = 66
87901
YDOT = 69
337491 meter/sec RA = 200
64456 deg
ZDOT = -3172
123069 TA = 171
18354
MA = 171
16989
Ha = 220
590 n
mi
Hp = 215
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6874659
85 X = 2065463
16
Y = 15159974
27 feet Y = 4644024
25 meter
Z = -14786975
49 Z = -4496964
76
XDOT = -22877
268794 XDOT = -6957
840072
YDOT = 227
485208 feet/sec YDOT = -8
554879 meter/sec
ZDOT = -10407
227916 ZDOT = -3205
958772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16187637
24 X = -4933991
83
Y = -4039767
35 feet Y = -1231321
09 meter
Z = -14743849
31 Z = -4493925
27
XDOT = 13791
646281 XDOT = 4203
693786
YDOT = -16761
760000 feet/sec YDOT = -5108
984448 meter/sec
ZDOT = -10554
042275 ZDOT = -3216
872085
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 16068
20475628
00016717 00000-0 10270-3 0 9068
2 25544 51
6425 201
6318 0001822 262
9163 97
1782 15
53970696 29273
Satellite: ISS
Catalog Number: 25544
Epoch time: 16068
20475628 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 201
6318 deg
Eccentricity:
0001822
Arg of perigee: 262
9163 deg
Mean anomaly: 97
1782 deg
Mean motion: 15
53970696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 325
Coasting Arc #8 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2016/069/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -474636
20 A = 6778536
76 meter
Y = -4382431
46 meter E =
0003510
Z = 5148328
54 I = 51
52038
XDOT = 7477
500385 Wp = 143
63149
YDOT = 896
994139 meter/sec RA = 195
64126 deg
ZDOT = 1449
643106 TA = 292
37754
MA = 292
41472
Ha = 220
609 n
mi
Hp = 215
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1557205
38 X = -450603
54
Y = -14378055
98 feet Y = -4387603
97 meter
Z = 16890841
65 Z = 5146081
97
XDOT = 24532
481577 XDOT = 7459
872576
YDOT = 2942
894156 feet/sec YDOT = 980
514185 meter/sec
ZDOT = 4756
046937 ZDOT = 1485
923518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12391276
09 X = 3776860
95
Y = 7477703
04 feet Y = 2279203
89 meter
Z = 16881769
70 Z = 5145563
41
XDOT = -16772
512978 XDOT = -5112
261956
YDOT = 16676
982068 feet/sec YDOT = 5083
144134 meter/sec
ZDOT = 4913
332399 ZDOT = 1497
583715
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 16069
23369638
00016717 00000-0 10270-3 0 9076
2 25544 51
6430 196
5033 0001742 266
6497 93
4456 15
53975183 29438
Satellite: ISS
Catalog Number: 25544
Epoch time: 16069
23369638 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 196
5033 deg
Eccentricity:
0001742
Arg of perigee: 266
6497 deg
Mean anomaly: 93
4456 deg
Mean motion: 15
53975183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 338
Coasting Arc #9 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2016/070/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1252351
20 A = 6777749
98 meter
Y = 4047829
32 meter E =
0012940
Z = -5301277
65 I = 51
54905
XDOT = -7445
469387 Wp = 93
27859
YDOT = -1743
625726 meter/sec RA = 190
63488 deg
ZDOT = 427
707214 TA = 180
80951
MA = 180
81161
Ha = 220
504 n
mi
Hp = 215
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4108763
79 X = -1271770
82
Y = 13280279
92 feet Y = 4033715
25 meter
Z = -17392643
22 Z = -5307409
04
XDOT = -24427
393002 XDOT = -7427
495972
YDOT = -5720
556845 feet/sec YDOT = -1826
785348 meter/sec
ZDOT = 1403
238892 ZDOT = 391
583207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8251502
39 X = -2515057
93
Y = -11145070
08 feet Y = -3397017
36 meter
Z = -17419871
81 Z = -5309576
93
XDOT = 18386
602061 XDOT = 5604
236308
YDOT = -15560
696731 feet/sec YDOT = -4742
900364 meter/sec
ZDOT = 1246
748926 ZDOT = 380
009073
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 16070
19831764
00016717 00000-0 10270-3 0 9088
2 25544 51
6428 191
6949 0001862 273
9008 86
1932 15
54009396 29588
Satellite: ISS
Catalog Number: 25544
Epoch time: 16070
19831764 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 191
6949 deg
Eccentricity:
0001862
Arg of perigee: 273
9008 deg
Mean anomaly: 86
1932 deg
Mean motion: 15
54009396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 340
Coasting Arc #10 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2016/071/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2935425
30 A = 6779245
10 meter
Y = -3627527
14 meter E =
0005161
Z = 4915807
90 I = 51
58635
XDOT = 6889
210176 Wp = 43
63155
YDOT = 2489
554258 meter/sec RA = 185
63273 deg
ZDOT = -2271
623127 TA = 68
60691
MA = 68
55186
Ha = 220
340 n
mi
Hp = 215
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9630660
45 X = 2951892
24
Y = -11901335
76 feet Y = -3594608
43 meter
Z = 16127978
66 Z = 4930107
97
XDOT = 22602
395589 XDOT = 6871
893875
YDOT = 8167
828932 feet/sec YDOT = 2566
496810 meter/sec
ZDOT = -7452
831782 ZDOT = -2238
199630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4092290
81 X = 1247330
24
Y = 14684035
58 feet Y = 4475694
05 meter
Z = 16190594
93 Z = 4934893
34
XDOT = -18790
000656 XDOT = -5727
192200
YDOT = 13312
856404 feet/sec YDOT = 4057
758632 meter/sec
ZDOT = -7308
162540 ZDOT = -2227
527942
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 16071
22723696
00016717 00000-0 10270-3 0 9098
2 25544 51
6430 186
5667 0001976 279
5190 80
5739 15
54041821 29741
Satellite: ISS
Catalog Number: 25544
Epoch time: 16071
22723696 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 186
5667 deg
Eccentricity:
0001976
Arg of perigee: 279
5190 deg
Mean anomaly: 80
5739 deg
Mean motion: 15
54041821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 333
Coasting Arc #11 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2016/072/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4425845
56 A = 6782553
26 meter
Y = 3162962
08 meter E =
0005356
Z = -4056739
03 I = 51
62818
XDOT = -5807
003279 Wp = 111
08518
YDOT = -3142
788305 meter/sec RA = 180
63848 deg
ZDOT = 3887
249348 TA = 199
22833
MA = 199
24855
Ha = 220
438 n
mi
Hp = 215
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14520490
69 X = -4441179
77
Y = 10377172
17 feet Y = 3113383
03 meter
Z = -13309511
25 Z = -4078276
35
XDOT = -19051
848027 XDOT = -5790
310827
YDOT = -10310
985254 feet/sec YDOT = -3207
632198 meter/sec
ZDOT = 12753
442742 ZDOT = 3859
081382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -294050
83 X = -89626
69
Y = -17774528
16 feet Y = -5417676
18 meter
Z = -13403474
35 Z = -4085378
98
XDOT = 18082
912573 XDOT = 5511
671752
YDOT = -9818
927177 feet/sec YDOT = -2992
809004 meter/sec
ZDOT = 12631
671063 ZDOT = 3850
133340
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 16072
19184142
00016717 00000-0 10270-3 0 9104
2 25544 51
6419 181
7580 0001985 283
5947 76
4985 15
54027316 29890
Satellite: ISS
Catalog Number: 25544
Epoch time: 16072
19184142 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 181
7580 deg
Eccentricity:
0001985
Arg of perigee: 283
5947 deg
Mean anomaly: 76
4985 deg
Mean motion: 15
54027316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 338
Coasting Arc #12 (Orbit 3004)
---------------------------------------
Vector Time (GMT): 2016/073/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5608294
85 A = 6786174
24 meter
Y = -2620687
84 meter E =
0011434
Z = 2768361
64 I = 51
67261
XDOT = 4292
919224 Wp = 98
37088
YDOT = 3745
059268 meter/sec RA = 175
65707 deg
ZDOT = -5135
031469 TA = 50
27032
MA = 50
16961
Ha = 220
385 n
mi
Hp = 215
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18399917
49 X = 5623735
70
Y = -8598057
21 feet Y = -2557885
49 meter
Z = 9082551
31 Z = 2795643
15
XDOT = 14084
380655 XDOT = 4275
665760
YDOT = 12286
939857 feet/sec YDOT = 3792
968455 meter/sec
ZDOT = -16847
216107 ZDOT = -5114
219901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3050583
95 X = -929817
99
Y = 20025106
64 feet Y = 6103652
50 meter
Z = 9201376
62 Z = 2804579
59
XDOT = -16641
828387 XDOT = -5072
429292
YDOT = 5189
301218 feet/sec YDOT = 1581
699011 meter/sec
ZDOT = -16757
457716 ZDOT = -5107
673112
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 16073
22074168
00016717 00000-0 10270-3 0 9116
2 25544 51
6419 176
6295 0002020 292
2597 67
8341 15
54067065 30050
Satellite: ISS
Catalog Number: 25544
Epoch time: 16073
22074168 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 176
6295 deg
Eccentricity:
0002020
Arg of perigee: 292
2597 deg
Mean anomaly: 67
8341 deg
Mean motion: 15
54067065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3005
Checksum: 300
Coasting Arc #13 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2016/074/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6360423
17 A = 6788916
34 meter
Y = 2019982
69 meter E =
0008741
Z = -1220960
15 I = 51
71176
XDOT = -2479
581346 Wp = 24
94118
YDOT = -4280
173512 meter/sec RA = 170
68513 deg
ZDOT = 5858
838595 TA = 321
80360
MA = 321
86550
Ha = 220
444 n
mi
Hp = 215
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20867530
09 X = -6376607
51
Y = 6627239
79 feet Y = 1948765
59 meter
Z = -4005774
78 Z = -1251896
98
XDOT = -8135
109404 XDOT = -2459
994783
YDOT = -14042
564016 feet/sec YDOT = -4307
791716 meter/sec
ZDOT = 19221
911400 ZDOT = 5846
841440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5716095
96 X = 1742266
05
Y = -21109328
57 feet Y = -6434123
35 meter
Z = -4140391
92 Z = -1261991
46
XDOT = 14736
741291 XDOT = 4491
758746
YDOT = 244
712672 feet/sec YDOT = 74
588422 meter/sec
ZDOT = 19170
492876 ZDOT = 5843
166229
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 16074
18532750
00016717 00000-0 10270-3 0 9129
2 25544 51
6404 171
8203 0002074 294
0998 65
9938 15
54037269 30205
Satellite: ISS
Catalog Number: 25544
Epoch time: 16074
18532750 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 171
8203 deg
Eccentricity:
0002074
Arg of perigee: 294
0998 deg
Mean anomaly: 65
9938 deg
Mean motion: 15
54037269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 308
Coasting Arc #14 (Orbit 3035)
---------------------------------------
Vector Time (GMT): 2016/075/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6641991
79 A = 6789469
71 meter
Y = -1297835
96 meter E =
0009331
Z = -482485
31 I = 51
74480
XDOT = 497
884748 Wp = 142
92487
YDOT = 4752
191084 meter/sec RA = 165
72129 deg
ZDOT = -5996
551087 TA = 42
27093
MA = 42
19904
Ha = 220
526 n
mi
Hp = 215
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21791311
65 X = 6658354
57
Y = -4257992
00 feet Y = -1223469
35 meter
Z = -1582957
05 Z = -450180
43
XDOT = 1633
480145 XDOT = 473
836124
YDOT = 15591
178096 feet/sec YDOT = 4757
623737 meter/sec
ZDOT = -19673
724039 ZDOT = -5994
191352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7870994
36 X = -2399079
08
Y = 20771715
69 feet Y = 6331218
94 meter
Z = -1442493
52 Z = -439672
02
XDOT = -12661
444138 XDOT = -3859
208173
YDOT = -6146
456169 feet/sec YDOT = -1873
439840 meter/sec
ZDOT = -19664
218767 ZDOT = -5993
653880
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 16075
21420951
00016717 00000-0 10270-3 0 9134
2 25544 51
6401 166
6915 0002004 297
0627 63
0321 15
54051475 30366
Satellite: ISS
Catalog Number: 25544
Epoch time: 16075
21420951 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 166
6915 deg
Eccentricity:
0002004
Arg of perigee: 297
0627 deg
Mean anomaly: 63
0321 deg
Mean motion: 15
54051475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3036
Checksum: 274
Coasting Arc #15 (Orbit 3051)
---------------------------------------
Vector Time (GMT): 2016/076/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6424858
22 A = 6787602
78 meter
Y = 477988
11 meter E =
0012688
Z = 2115135
45 I = 51
76886
XDOT = 1445
709278 Wp = 62
70356
YDOT = -5117
564972 meter/sec RA = 160
75591 deg
ZDOT = 5528
178182 TA = 320
69295
MA = 320
78499
Ha = 220
493 n
mi
Hp = 215
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21078931
17 X = -6440000
04
Y = 1568202
47 feet Y = 406056
61 meter
Z = 6939420
78 Z = 2083888
49
XDOT = 4743
140676 XDOT = 1475
974383
YDOT = -16789
911325 feet/sec YDOT = -5101
228361 meter/sec
ZDOT = 18137
067525 ZDOT = 5535
275006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9474744
92 X = 2887902
25
Y = -18944011
75 feet Y = -5774134
78 meter
Z = 6803659
77 Z = 2073755
50
XDOT = 10665
866165 XDOT = 3250
956007
YDOT = 11883
411295 feet/sec YDOT = 3622
063763 meter/sec
ZDOT = 18168
684654 ZDOT = 5537
815082
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 16076
24308019
00016717 00000-0 10270-3 0 9149
2 25544 51
6393 161
5610 0002049 298
9758 61
1189 15
54096278 30525
Satellite: ISS
Catalog Number: 25544
Epoch time: 16076
24308019 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 161
5610 deg
Eccentricity:
0002049
Arg of perigee: 298
9758 deg
Mean anomaly: 61
1189 deg
Mean motion: 15
54096278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3052
Checksum: 318
Coasting Arc #16 (Orbit 3066)
---------------------------------------
Vector Time (GMT): 2016/077/04:23:20
227
Vector Time (MET): N/A
Weight (LBS) : 890089
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5756258
51 A = 6784158
27 meter
Y = 486164
71 meter E =
0003901
Z = -3561861
70 I = 51
78668
XDOT = -3220
321293 Wp = 65
44048
YDOT = 5316
324786 meter/sec RA = 155
78654 deg
ZDOT = -4480
941232 TA = 156
47068
MA = 156
45283
Ha = 220
552 n
mi
Hp = 215
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18885362
56 X = 5767696
10
Y = 1595028
57 feet Y = 550598
62 meter
Z = -11685897
95 Z = -3533871
77
XDOT = -10565
358574 XDOT = -3257
764144
YDOT = 17442
010452 feet/sec YDOT = 5280
103220 meter/sec
ZDOT = -14701
250762 ZDOT = -4496
676056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10815067
33 X = -3296432
52
Y = 15654387
87 feet Y = 4771457
42 meter
Z = -11564415
47 Z = -3524833
84
XDOT = -8778
826958 XDOT = -2675
786457
YDOT = -16970
812452 feet/sec YDOT = -5172
703635 meter/sec
ZDOT = -14770
419682 ZDOT = -4502
023919
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 16077
20763993
00016717 00000-0 10270-3 0 9153
2 25544 51
6387 156
7524 0002001 307
8240 52
2731 15
54096337 30678
Satellite: ISS
Catalog Number: 25544
Epoch time: 16077
20763993 = yrday
fracday
Element set: 915
Inclination: 51
6387 deg
RA of node: 156
7524 deg
Eccentricity:
0002001
Arg of perigee: 307
8240 deg
Mean anomaly: 52
2731 deg
Mean motion: 15
54096337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3067
Checksum: 305
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