[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 20th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 ET - UTC (sec) : 68 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
182/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
8
183/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
9
Coasting Arc #1 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2017/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4237629
62 A = 6779649
87 meter
Y = 2155383
92 meter E =
0006208
Z = 4834081
84 I = 51
79834
XDOT = -5364
973308 Wp = 16
89896
YDOT = -4857
706130 meter/sec RA = 26
18793 deg
ZDOT = -2530
487308 TA = 97
97045
MA = 97
89999
Ha = 219
981 n
mi
Hp = 216
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13902984
32 X = -4284898
53
Y = 7071469
56 feet Y = 2107731
11 meter
Z = 15859848
55 Z = 4813381
97
XDOT = -17601
618464 XDOT = -5297
962460
YDOT = -15937
356069 feet/sec YDOT = -4917
325974 meter/sec
ZDOT = -8302
123714 ZDOT = -2556
386609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6340345
63 X = 1932537
35
Y = 14352802
74 feet Y = 4374734
28 meter
Z = 15768022
11 Z = 4806093
14
XDOT = -15776
121745 XDOT = -4808
561908
YDOT = 16238
412533 feet/sec YDOT = 4949
468140 meter/sec
ZDOT = -8415
551044 ZDOT = -2565
059958
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 17170
54373036
00016717 00000-0 10270-3 0 9004
2 25544 51
6419 26
5901 0005127 297
5205 62
5427 15
54088572 22113
Satellite: ISS
Catalog Number: 25544
Epoch time: 17170
54373036 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 26
5901 deg
Eccentricity:
0005127
Arg of perigee: 297
5205 deg
Mean anomaly: 62
5427 deg
Mean motion: 15
54088572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 291
Coasting Arc #2 (Orbit 2225)
---------------------------------------
Vector Time (GMT): 2017/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5428402
24 A = 6783193
00 meter
Y = -1181827
12 meter E =
0001990
Z = -3892660
08 I = 51
77964
XDOT = 4046
720435 Wp = 60
11652
YDOT = 5045
306458 meter/sec RA = 21
20708 deg
ZDOT = 4114
009068 TA = 252
96294
MA = 252
98475
Ha = 220
145 n
mi
Hp = 216
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17809718
64 X = 5460123
11
Y = -3877385
56 feet Y = -1120945
24 meter
Z = -12771194
47 Z = -3866213
40
XDOT = 13276
641847 XDOT = 3970
017696
YDOT = 16552
842709 feet/sec YDOT = 5090
130292 meter/sec
ZDOT = 13497
405079 ZDOT = 4133
481251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3259977
42 X = -993641
12
Y = -18015764
96 feet Y = -5491205
16 meter
Z = -12654183
71 Z = -3856995
20
XDOT = 15684
713394 XDOT = 4780
700642
YDOT = -12372
472600 feet/sec YDOT = -3771
129648 meter/sec
ZDOT = 13582
403510 ZDOT = 4139
916590
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 17171
50830583
00016717 00000-0 10270-3 0 9017
2 25544 51
6412 21
7810 0005072 300
8872 59
1781 15
54069463 22268
Satellite: ISS
Catalog Number: 25544
Epoch time: 17171
50830583 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 21
7810 deg
Eccentricity:
0005072
Arg of perigee: 300
8872 deg
Mean anomaly: 59
1781 deg
Mean motion: 15
54069463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2226
Checksum: 289
Coasting Arc #3 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2017/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6284646
92 A = 6786749
17 meter
Y = 255248
90 meter E =
0009103
Z = 2540760
63 I = 51
76063
XDOT = -2349
718480 Wp = 91
98200
YDOT = -5026
963080 meter/sec RA = 16
23589 deg
ZDOT = -5291
026650 TA = 59
53723
MA = 59
44735
Ha = 220
225 n
mi
Hp = 216
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20618920
33 X = -6299375
98
Y = 837430
77 feet Y = 184887
02 meter
Z = 8335828
85 Z = 2510195
72
XDOT = -7709
050131 XDOT = -2267
629559
YDOT = -16492
661025 feet/sec YDOT = -5052
779526 meter/sec
ZDOT = -17359
011318 ZDOT = -5302
242262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 481548
79 X = 146776
07
Y = 20684339
26 feet Y = 6304586
61 meter
Z = 8200818
80 Z = 2499609
57
XDOT = -15114
420173 XDOT = -4606
875269
YDOT = 7274
757253 feet/sec YDOT = 2217
346011 meter/sec
ZDOT = -17407
546552 ZDOT = -5305
820189
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 17172
53718203
00016717 00000-0 10270-3 0 9026
2 25544 51
6407 16
6530 0005177 306
6346 53
4330 15
54105320 22428
Satellite: ISS
Catalog Number: 25544
Epoch time: 17172
53718203 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 16
6530 deg
Eccentricity:
0005177
Arg of perigee: 306
6346 deg
Mean anomaly: 53
4330 deg
Mean motion: 15
54105320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 268
Coasting Arc #4 (Orbit 2256)
---------------------------------------
Vector Time (GMT): 2017/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6691159
79 A = 6789176
70 meter
Y = 569682
35 meter E =
0011107
Z = -949548
90 I = 51
73536
XDOT = 424
812899 Wp = 11
40128
YDOT = 4850
912272 meter/sec RA = 11
26986 deg
ZDOT = 5926
273794 TA = 338
32701
MA = 338
37397
Ha = 220
367 n
mi
Hp = 216
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21952623
98 X = 6688904
62
Y = 1869036
58 feet Y = 644494
97 meter
Z = -3115317
93 Z = -917050
47
XDOT = 1393
743107 XDOT = 341
750017
YDOT = 15915
066508 feet/sec YDOT = 4855
197463 meter/sec
ZDOT = 19443
155492 ZDOT = 5928
136424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1869715
43 X = 569889
26
Y = -21972436
43 feet Y = -6697198
62 meter
Z = -2971936
16 Z = -905846
14
XDOT = 14314
610930 XDOT = 4363
093411
YDOT = -1402
289249 feet/sec YDOT = -427
417763 meter/sec
ZDOT = 19450
421633 ZDOT = 5928
488514
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 17173
50175399
00016717 00000-0 10270-3 0 9038
2 25544 51
6392 11
8445 0005077 307
6987 52
3705 15
54061177 22575
Satellite: ISS
Catalog Number: 25544
Epoch time: 17173
50175399 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 11
8445 deg
Eccentricity:
0005077
Arg of perigee: 307
6987 deg
Mean anomaly: 52
3705 deg
Mean motion: 15
54061177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2257
Checksum: 317
Coasting Arc #5 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2017/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6611020
80 A = 6789188
28 meter
Y = -1332742
25 meter E =
0005248
Z = -758082
84 I = 51
70374
XDOT = 1598
274582 Wp = 147
32089
YDOT = -4554
320560 meter/sec RA = 6
30529 deg
ZDOT = -5954
948048 TA = 40
86193
MA = 40
82260
Ha = 220
462 n
mi
Hp = 216
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21689700
79 X = -6591943
98
Y = -4372513
93 feet Y = -1406564
37 meter
Z = -2487148
43 Z = -790151
10
XDOT = 5243
683011 XDOT = 1678
009678
YDOT = -14941
996589 feet/sec YDOT = -4536
000738 meter/sec
ZDOT = -19537
231127 ZDOT = -5946
991212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4000234
68 X = -1219271
53
Y = 21744818
50 feet Y = 6627820
68 meter
Z = -2628478
01 Z = -801160
10
XDOT = -13448
053124 XDOT = -4098
966592
YDOT = -4822
374908 feet/sec YDOT = -1469
859872 meter/sec
ZDOT = -19501
196060 ZDOT = -5943
964559
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 17174
53062682
00016717 00000-0 10270-3 0 9043
2 25544 51
6394 6
7154 0005119 312
9129 47
1593 15
54082155 22735
Satellite: ISS
Catalog Number: 25544
Epoch time: 17174
53062682 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 6
7154 deg
Eccentricity:
0005119
Arg of perigee: 312
9129 deg
Mean anomaly: 47
1593 deg
Mean motion: 15
54082155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 302
Coasting Arc #6 (Orbit 2288)
---------------------------------------
Vector Time (GMT): 2017/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6023690
14 A = 6786982
67 meter
Y = 2015092
13 meter E =
0012172
Z = 2370047
38 I = 51
66296
XDOT = -3521
249040 Wp = 52
68918
YDOT = 4177
994946 meter/sec RA = 1
33467 deg
ZDOT = 5385
514738 TA = 333
77818
MA = 333
83976
Ha = 220
444 n
mi
Hp = 215
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19762762
91 X = 5989196
67
Y = 6611194
65 feet Y = 2082259
84 meter
Z = 7775746
01 Z = 2399225
06
XDOT = -11552
654332 XDOT = -3593
866855
YDOT = 13707
332501 feet/sec YDOT = 4138
211003 meter/sec
ZDOT = 17669
011608 ZDOT = 5368
234002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5930821
23 X = 1807714
31
Y = -19927023
56 feet Y = -6073756
78 meter
Z = 7904176
77 Z = 2409193
08
XDOT = 12648
564778 XDOT = 3855
282544
YDOT = 10757
577639 feet/sec YDOT = 3278
909664 meter/sec
ZDOT = 17591
882332 ZDOT = 5362
005735
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 17175
55949644
00016717 00000-0 10270-3 0 9059
2 25544 51
6383 1
5855 0004954 315
3690 44
7063 15
54089696 22899
Satellite: ISS
Catalog Number: 25544
Epoch time: 17175
55949644 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 1
5855 deg
Eccentricity:
0004954
Arg of perigee: 315
3690 deg
Mean anomaly: 44
7063 deg
Mean motion: 15
54089696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2289
Checksum: 342
Coasting Arc #7 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2017/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4987220
76 A = 6783363
29 meter
Y = -2662862
56 meter E =
0005894
Z = -3755347
91 I = 51
61787
XDOT = 5183
466858 Wp = 27
69322
YDOT = -3706
117581 meter/sec RA = 356
35488 deg
ZDOT = -4253
438460 TA = 197
20433
MA = 197
22432
Ha = 220
711 n
mi
Hp = 215
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16362272
83 X = -4938831
80
Y = -8736425
71 feet Y = -2718361
88 meter
Z = -12320695
24 Z = -3779456
96
XDOT = 17006
124861 XDOT = 5245
185319
YDOT = -12159
178416 feet/sec YDOT = -3647
806774 meter/sec
ZDOT = -13954
850591 ZDOT = -4228
109699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7886774
44 X = -2403888
85
Y = 16710074
39 feet Y = 5093230
68 meter
Z = -12426618
22 Z = -3787633
23
XDOT = -11806
930071 XDOT = -3598
752286
YDOT = -15872
400206 feet/sec YDOT = -4837
907583 meter/sec
ZDOT = -13842
282458 ZDOT = -4219
127693
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 17176
52406162
00016717 00000-0 10270-3 0 9061
2 25544 51
6378 356
7775 0004897 321
3270 38
7532 15
54091032 23045
Satellite: ISS
Catalog Number: 25544
Epoch time: 17176
52406162 = yrday
fracday
Element set: 906
Inclination: 51
6378 deg
RA of node: 356
7775 deg
Eccentricity:
0004897
Arg of perigee: 321
3270 deg
Mean anomaly: 38
7532 deg
Mean motion: 15
54091032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 310
Coasting Arc #8 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2017/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3575934
13 A = 6779847
70 meter
Y = 3263030
49 meter E =
0003677
Z = 4743398
20 I = 51
57387
XDOT = -6453
428499 Wp = 82
94093
YDOT = 3146
388422 meter/sec RA = 351
36193 deg
ZDOT = 2699
299084 TA = 340
35878
MA = 340
37294
Ha = 220
734 n
mi
Hp = 215
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11732067
34 X = 3516139
48
Y = 10705480
60 feet Y = 3302684
01 meter
Z = 15562330
06 Z = 4760623
99
XDOT = -21172
665679 XDOT = -6501
244319
YDOT = 10322
796660 feet/sec YDOT = 3073
954080 meter/sec
ZDOT = 8855
968124 ZDOT = 2667
835014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9882455
81 X = 3012172
53
Y = -12338268
33 feet Y = -3760704
19 meter
Z = 15637744
01 Z = 4766384
37
XDOT = 10858
210164 XDOT = 3309
582458
YDOT = 19749
949498 feet/sec YDOT = 6019
784607 meter/sec
ZDOT = 8716
426937 ZDOT = 2656
766930
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 17177
55292812
00016717 00000-0 10270-3 0 9071
2 25544 51
6382 351
6481 0005002 323
3108 36
7701 15
54072168 23202
Satellite: ISS
Catalog Number: 25544
Epoch time: 17177
55292812 = yrday
fracday
Element set: 907
Inclination: 51
6382 deg
RA of node: 351
6481 deg
Eccentricity:
0005002
Arg of perigee: 323
3108 deg
Mean anomaly: 36
7701 deg
Mean motion: 15
54072168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 287
Coasting Arc #9 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2017/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1939507
28 A = 6777684
95 meter
Y = -3827349
72 meter E =
0013274
Z = -5257664
56 I = 51
53571
XDOT = 7202
986425 Wp = 64
10285
YDOT = -2455
568178 meter/sec RA = 346
35965 deg
ZDOT = -865
606220 TA = 197
57519
MA = 197
62116
Ha = 220
919 n
mi
Hp = 215
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6363212
85 X = -1871025
88
Y = -12556921
65 feet Y = -3848655
09 meter
Z = -17249555
66 Z = -5266920
08
XDOT = 23631
845228 XDOT = 7234
114531
YDOT = -8056
326044 feet/sec YDOT = -2374
845353 meter/sec
ZDOT = -2839
915420 ZDOT = -830
541480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11975424
74 X = -3650109
46
Y = 7305505
28 feet Y = 2226718
01 meter
Z = -17289671
04 Z = -5269891
73
XDOT = -9524
716127 XDOT = -2903
133475
YDOT = -21997
555663 feet/sec YDOT = -6704
854966 meter/sec
ZDOT = -2684
620814 ZDOT = -818
272424
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 17178
51748759
00016717 00000-0 10270-3 0 9085
2 25544 51
6393 346
8403 0004774 329
1983 30
8889 15
54092411 23355
Satellite: ISS
Catalog Number: 25544
Epoch time: 17178
51748759 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 346
8403 deg
Eccentricity:
0004774
Arg of perigee: 329
1983 deg
Mean anomaly: 30
8889 deg
Mean motion: 15
54092411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 344
Coasting Arc #10 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2017/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 188165
06 A = 6777996
65 meter
Y = 4318755
52 meter E =
0006402
Z = 5220673
36 I = 51
50357
XDOT = -7421
320946 Wp = 8
96923
YDOT = 1613
809345 meter/sec RA = 341
35149 deg
ZDOT = -1061
155030 TA = 91
25130
MA = 91
17795
Ha = 221
121 n
mi
Hp = 215
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 617339
44 X = 114498
45
Y = 14169145
41 feet Y = 4320447
32 meter
Z = 17128193
43 Z = 5221408
88
XDOT = -24348
165832 XDOT = -7433
660913
YDOT = 5294
650083 feet/sec YDOT = 1530
750207 meter/sec
ZDOT = -3481
479758 ZDOT = -1097
234897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14043278
95 X = 4280391
42
Y = -1962040
20 feet Y = -598029
85 meter
Z = 17130601
69 Z = 5221407
40
XDOT = 7628
249394 XDOT = 2325
090415
YDOT = 22626
238705 feet/sec YDOT = 6896
477557 meter/sec
ZDOT = -3641
081638 ZDOT = -1109
801683
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 17179
54635005
00016717 00000-0 10270-3 0 9099
2 25544 51
6380 341
7112 0004728 332
9721 27
1185 15
54047004 23517
Satellite: ISS
Catalog Number: 25544
Epoch time: 17179
54635005 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 341
7112 deg
Eccentricity:
0004728
Arg of perigee: 332
9721 deg
Mean anomaly: 27
1185 deg
Mean motion: 15
54047004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 290
Coasting Arc #11 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2017/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1479303
38 A = 6780260
91 meter
Y = -4700384
73 meter E =
0007938
Z = -4663684
58 I = 51
48266
XDOT = 7079
848272 Wp = 83
78180
YDOT = -610
579207 meter/sec RA = 336
34600 deg
ZDOT = 2866
133077 TA = 214
75186
MA = 214
80374
Ha = 221
126 n
mi
Hp = 215
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4853357
56 X = 1554408
05
Y = -15421209
75 feet Y = -4683421
84 meter
Z = -15300802
43 Z = -4656316
62
XDOT = 23227
848660 XDOT = 7072
227608
YDOT = -2003
212623 feet/sec YDOT = -531
450388 meter/sec
ZDOT = 9403
323745 ZDOT = 2900
505902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15905771
11 X = -4848079
03
Y = -3065492
89 feet Y = -934362
23 meter
Z = -15267368
58 Z = -4653493
94
XDOT = -4993
210762 XDOT = -1521
930640
YDOT = -21597
922514 feet/sec YDOT = -6583
046782 meter/sec
ZDOT = 9555
184739 ZDOT = 2912
420308
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 17180
51090448
00016717 00000-0 10270-3 0 9106
2 25544 51
6397 336
9039 0004760 335
5269 24
5657 15
54092201 23661
Satellite: ISS
Catalog Number: 25544
Epoch time: 17180
51090448 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 336
9039 deg
Eccentricity:
0004760
Arg of perigee: 335
5269 deg
Mean anomaly: 24
5657 deg
Mean motion: 15
54092201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 311
Coasting Arc #12 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2017/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2988252
92 A = 6784017
42 meter
Y = 4905388
17 meter E =
0011531
Z = 3605696
37 I = 51
46524
XDOT = -6257
252148 Wp = 63
17682
YDOT = -569
514453 meter/sec RA = 331
34561 deg
ZDOT = -4394
972826 TA = 74
00435
MA = 73
87735
Ha = 221
286 n
mi
Hp = 215
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9803979
39 X = -3060398
76
Y = 16093793
19 feet Y = 4871567
82 meter
Z = 11829712
51 Z = 3591005
61
XDOT = -20529
042481 XDOT = -6229
070156
YDOT = -1868
485738 feet/sec YDOT = -639
329375 meter/sec
ZDOT = -14419
202186 ZDOT = -4425
300017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17297872
82 X = 5272391
64
Y = 7580503
77 feet Y = 2310537
55 meter
Z = 11763921
44 Z = 3585643
26
XDOT = 1503
046461 XDOT = 458
128561
YDOT = 19236
285636 feet/sec YDOT = 5863
219862 meter/sec
ZDOT = -14552
968021 ZDOT = -4435
744653
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 17181
53976090
00016717 00000-0 10270-3 0 9116
2 25544 51
6393 331
7745 0004777 339
5143 20
5817 15
54081372 23826
Satellite: ISS
Catalog Number: 25544
Epoch time: 17181
53976090 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 331
7745 deg
Eccentricity:
0004777
Arg of perigee: 339
5143 deg
Mean anomaly: 20
5817 deg
Mean motion: 15
54081372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 316
Coasting Arc #13 (Orbit 2396)
---------------------------------------
Vector Time (GMT): 2017/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4164703
52 A = 6787409
05 meter
Y = -4879463
73 meter E =
0009639
Z = -2201870
53 I = 51
44931
XDOT = 5056
205771 Wp = 16
74300
YDOT = 1859
422890 meter/sec RA = 326
35480 deg
ZDOT = 5457
931149 TA = 318
73069
MA = 318
80351
Ha = 221
384 n
mi
Hp = 215
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13663725
44 X = 4229653
00
Y = -16008739
26 feet Y = -4832527
85 meter
Z = -7223984
66 Z = -2181482
40
XDOT = 16588
601610 XDOT = 5008
525573
YDOT = 6100
468798 feet/sec YDOT = 1915
697779 meter/sec
ZDOT = 17906
598257 ZDOT = 5482
376885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17931625
12 X = -5465559
34
Y = -11078780
28 feet Y = -3376812
23 meter
Z = -7133058
81 Z = -2174156
33
XDOT = 2682
064707 XDOT = 817
493323
YDOT = -15907
352233 feet/sec YDOT = -4848
560961 meter/sec
ZDOT = 18014
149671 ZDOT = 5490
712820
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 17182
50431111
00016717 00000-0 10270-3 0 9125
2 25544 51
6400 326
9672 0004808 343
8046 16
2952 15
54098283 23972
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
50431111 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 326
9672 deg
Eccentricity:
0004808
Arg of perigee: 343
8046 deg
Mean anomaly: 16
2952 deg
Mean motion: 15
54098283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2397
Checksum: 301
Coasting Arc #14 (Orbit 2402)
---------------------------------------
Vector Time (GMT): 2017/182/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3760234
34 A = 6778183
55 meter
Y = -2354547
86 meter E =
0014461
Z = -5136844
47 I = 51
40833
XDOT = 5348
309645 Wp = 57
82393
YDOT = -5273
522086 meter/sec RA = 324
53334 deg
ZDOT = -1493
377651 TA = 197
70311
MA = 197
75355
Ha = 221
485 n
mi
Hp = 214
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12336726
83 X = -3708673
49
Y = -7724894
54 feet Y = -2396308
63 meter
Z = -16853164
28 Z = -5154985
44
XDOT = 17546
947653 XDOT = 5414
136136
YDOT = -17301
581647 feet/sec YDOT = -5213
345478 meter/sec
ZDOT = -4899
532975 ZDOT = -1467
237840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13529927
98 X = 4123922
05
Y = -5110735
13 feet Y = -1557752
07 meter
Z = -16932790
85 Z = -5161114
65
XDOT = 2859
512253 XDOT = 871
579335
YDOT = 23465
783798 feet/sec YDOT = 7152
370902 meter/sec
ZDOT = -4783
147651 ZDOT = -1457
903404
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 17182
89012967
00016717 00000-0 10270-3 0 9132
2 25544 51
6398 325
0483 0005113 346
3262 13
7751 15
54087690 24033
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
89012967 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 325
0483 deg
Eccentricity:
0005113
Arg of perigee: 346
3262 deg
Mean anomaly: 13
7751 deg
Mean motion: 15
54087690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2403
Checksum: 309
Coasting Arc #15 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2017/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5004848
43 A = 6789264
07 meter
Y = 4551228
07 meter E =
0009512
Z = 540216
46 I = 51
42843
XDOT = -3582
794634 Wp = 111
31714
YDOT = -3222
606160 meter/sec RA = 321
36907 deg
ZDOT = -5961
536707 TA = 62
83902
MA = 62
74207
Ha = 221
410 n
mi
Hp = 214
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16420106
40 X = -5057993
59
Y = 14931850
63 feet Y = 4494963
26 meter
Z = 1772363
72 Z = 515775
81
XDOT = -11754
575571 XDOT = -3517
534144
YDOT = -10572
854855 feet/sec YDOT = -3262
305979 meter/sec
ZDOT = -19558
847465 ZDOT = -5978
782569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17523655
84 X = 5341210
30
Y = 13633604
73 feet Y = 4155522
72 meter
Z = 1663622
10 Z = 507072
02
XDOT = -7434
769439 XDOT = -2266
117725
YDOT = 11986
719266 feet/sec YDOT = 3653
552032 meter/sec
ZDOT = -19634
357483 ZDOT = -5984
552161
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 17183
53316262
00016717 00000-0 10270-3 0 9140
2 25544 51
6392 321
8383 0004876 346
3642 13
7379 15
54112603 24137
Satellite: ISS
Catalog Number: 25544
Epoch time: 17183
53316262 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 321
8383 deg
Eccentricity:
0004876
Arg of perigee: 346
3642 deg
Mean anomaly: 13
7379 deg
Mean motion: 15
54112603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2413
Checksum: 301
Coasting Arc #16 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2017/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5423135
82 A = 6788760
19 meter
Y = -3902581
87 meter E =
0016225
Z = 1147200
79 I = 51
40384
XDOT = 2016
112965 Wp = 41
59560
YDOT = 4532
976799 meter/sec RA = 316
38345 deg
ZDOT = 5853
973061 TA = 330
90923
MA = 330
99953
Ha = 221
461 n
mi
Hp = 214
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17792440
36 X = 5460799
92
Y = -12803746
28 feet Y = -3841726
21 meter
Z = 3763782
11 Z = 1173635
79
XDOT = 6614
543849 XDOT = 1936
838461
YDOT = 14871
971125 feet/sec YDOT = 4555
078504 meter/sec
ZDOT = 19205
948362 ZDOT = 5863
574621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15916219
04 X = -4851263
56
Y = -15042712
61 feet Y = -4585018
80 meter
Z = 3881195
33 Z = 1182988
34
XDOT = 12291
134352 XDOT = 3746
337750
YDOT = -8009
468031 feet/sec YDOT = -2441
285856 meter/sec
ZDOT = 19247
471767 ZDOT = 5866
629395
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 17184
56201084
00016717 00000-0 10270-3 0 9150
2 25544 51
6410 316
7096 0004858 351
0859 9
0207 15
54122236 24293
Satellite: ISS
Catalog Number: 25544
Epoch time: 17184
56201084 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 316
7096 deg
Eccentricity:
0004858
Arg of perigee: 351
0859 deg
Mean anomaly: 9
0207 deg
Mean motion: 15
54122236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 297
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