[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 30th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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
270/16:51:50
146 -1
0 1
5 1
5
N/A -0
9 -0
1 220
7
000/00:03:40
293 -0
5 -0
0 215
8
274/01:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
6
277/10:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 215
1
283/16:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
4
285/09:32:06
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
1
Coasting Arc #1 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2017/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2350450
21 A = 6788873
53 meter
Y = 6356133
57 meter E =
0007266
Z = -354077
06 I = 51
30942
XDOT = -4607
206511 Wp = 128
77093
YDOT = 1376
006537 meter/sec RA = 247
30776 deg
ZDOT = -5970
175330 TA = 55
06205
MA = 54
99381
Ha = 220
686 n
mi
Hp = 215
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7711450
81 X = 2280919
49
Y = 20853456
59 feet Y = 6382029
11 meter
Z = -1161670
16 Z = -342828
53
XDOT = -15115
506926 XDOT = -4593
250473
YDOT = 4514
457142 feet/sec YDOT = 1324
563205 meter/sec
ZDOT = -19587
189403 ZDOT = -5992
522149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9717669
18 X = -2961945
57
Y = -20000280
38 feet Y = -6096085
46 meter
Z = -1112786
29 Z = -339177
26
XDOT = 13016
167379 XDOT = 3967
327817
YDOT = -5245
605786 feet/sec YDOT = -1598
860643 meter/sec
ZDOT = -19686
280867 ZDOT = -6000
378408
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 17270
53152472
00016717 00000-0 10270-3 0 9003
2 25544 51
6383 248
1268 0004361 331
9720 28
1198 15
54267279 37667
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
53152472 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 248
1268 deg
Eccentricity:
0004361
Arg of perigee: 331
9720 deg
Mean anomaly: 28
1198 deg
Mean motion: 15
54267279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 314
Coasting Arc #2 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/270/16:53:40
293
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2413826
91 A = 6779764
19 meter
Y = 4119967
43 meter E =
0010532
Z = -4822610
03 I = 51
28212
XDOT = -4614
613968 Wp = 49
49693
YDOT = -5594
307623 meter/sec RA = 246
30311 deg
ZDOT = -2466
356395 TA = 196
11333
MA = 196
14685
Ha = 220
667 n
mi
Hp = 215
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7919379
62 X = -2436291
97
Y = 13516953
52 feet Y = 4092848
41 meter
Z = -15822211
39 Z = -4834390
64
XDOT = -15139
809607 XDOT = -4539
733491
YDOT = -18354
027635 feet/sec YDOT = -5645
492881 meter/sec
ZDOT = -8091
720457 ZDOT = -2488
590704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11815488
07 X = -3601360
76
Y = -10205286
63 feet Y = -3110571
37 meter
Z = -15874928
21 Z = -4838678
12
XDOT = 20108
184815 XDOT = 6128
974732
YDOT = -10525
839174 feet/sec YDOT = -3208
275780 meter/sec
ZDOT = -8189
333712 ZDOT = -2496
108915
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 17270
72441677
00016717 00000-0 10270-3 0 9013
2 25544 51
6414 247
1662 0004525 317
0297 43
0502 15
54010954 37699
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
72441677 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 247
1662 deg
Eccentricity:
0004525
Arg of perigee: 317
0297 deg
Mean anomaly: 43
0502 deg
Mean motion: 15
54010954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 296
Coasting Arc #3 (Orbit 3784)
---------------------------------------
Vector Time (GMT): 2017/271/16:53:40
293
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3342689
50 A = 6777807
49 meter
Y = -2668709
32 meter E =
0002114
Z = 5257669
92 I = 51
28907
XDOT = 4119
606227 Wp = 353
76522
YDOT = 6435
573488 meter/sec RA = 241
28200 deg
ZDOT = 649
545755 TA = 90
01533
MA = 89
99111
Ha = 220
596 n
mi
Hp = 215
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10966829
07 X = 3346743
89
Y = -8755608
01 feet Y = -2631306
05 meter
Z = 17249573
21 Z = 5273917
83
XDOT = 13515
768461 XDOT = 4044
180552
YDOT = 21114
086246 feet/sec YDOT = 6481
220050 meter/sec
ZDOT = 2131
055626 ZDOT = 669
374030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6780445
24 X = 2066679
71
Y = 12184358
89 feet Y = 3713792
59 meter
Z = 17321857
53 Z = 5279702
18
XDOT = -22214
663649 XDOT = -6771
029480
YDOT = 9218
790391 feet/sec YDOT = 2809
887311 meter/sec
ZDOT = 2217
921472 ZDOT = 676
022465
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 17271
75333944
00016717 00000-0 10270-3 0 9025
2 25544 51
6407 242
0382 0004521 319
5887 40
4930 15
54022078 37856
Satellite: ISS
Catalog Number: 25544
Epoch time: 17271
75333944 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 242
0382 deg
Eccentricity:
0004521
Arg of perigee: 319
5887 deg
Mean anomaly: 40
4930 deg
Mean motion: 15
54022078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3785
Checksum: 305
Coasting Arc #4 (Orbit 3799)
---------------------------------------
Vector Time (GMT): 2017/272/16:53:40
293
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4226183
28 A = 6778151
38 meter
Y = 1147007
67 meter E =
0011227
Z = -5183127
58 I = 51
30698
XDOT = -3344
512397 Wp = 83
10208
YDOT = -6781
083201 meter/sec RA = 236
26011 deg
ZDOT = 1230
018938 TA = 198
74907
MA = 198
79045
Ha = 220
788 n
mi
Hp = 215
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13865430
71 X = -4213518
08
Y = 3763148
52 feet Y = 1099818
03 meter
Z = -17005011
74 Z = -5203626
51
XDOT = -10972
809701 XDOT = -3274
410813
YDOT = -22247
648296 feet/sec YDOT = -6818
091765 meter/sec
ZDOT = 4035
495202 ZDOT = 1213
943015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1611386
51 X = -491150
61
Y = -14167403
72 feet Y = -4318224
66 meter
Z = -17095905
51 Z = -5210832
00
XDOT = 22636
065968 XDOT = 6899
472907
YDOT = -7345
251347 feet/sec YDOT = -2238
832610 meter/sec
ZDOT = 3965
265561 ZDOT = 1208
612943
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 17272
71795086
00016717 00000-0 10270-3 0 9032
2 25544 51
6408 237
2310 0004612 322
7213 37
3619 15
54020117 38003
Satellite: ISS
Catalog Number: 25544
Epoch time: 17272
71795086 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 237
2310 deg
Eccentricity:
0004612
Arg of perigee: 322
7213 deg
Mean anomaly: 37
3619 deg
Mean motion: 15
54020117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3800
Checksum: 279
Coasting Arc #5 (Orbit 3815)
---------------------------------------
Vector Time (GMT): 2017/273/16:53:40
293
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4988853
02 A = 6780521
09 meter
Y = 364397
63 meter E =
0009004
Z = 4576891
03 I = 51
33482
XDOT = 2277
693083 Wp = 34
33854
YDOT = 6676
931422 meter/sec RA = 231
24280 deg
ZDOT = -3004
102422 TA = 85
82995
MA = 85
72705
Ha = 220
818 n
mi
Hp = 215
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16367628
03 X = 4962175
06
Y = 1195530
27 feet Y = 420037
62 meter
Z = 15016046
68 Z = 4601060
61
XDOT = 7472
746334 XDOT = 2217
453097
YDOT = 21905
942987 feet/sec YDOT = 6702
065057 meter/sec
ZDOT = -9855
979075 ZDOT = -2993
184942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3399850
27 X = -1036274
36
Y = 15954508
47 feet Y = 4862934
18 meter
Z = 15122991
62 Z = 4609487
85
XDOT = -21563
716835 XDOT = -6572
620891
YDOT = 4733
691741 feet/sec YDOT = 1442
829243 meter/sec
ZDOT = -9808
550366 ZDOT = -2989
646151
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 17273
74686146
00016717 00000-0 10270-3 0 9043
2 25544 51
6413 232
1027 0004759 326
7128 33
3724 15
54058911 38162
Satellite: ISS
Catalog Number: 25544
Epoch time: 17273
74686146 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 232
1027 deg
Eccentricity:
0004759
Arg of perigee: 326
7128 deg
Mean anomaly: 33
3724 deg
Mean motion: 15
54058911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3816
Checksum: 309
Coasting Arc #6 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2017/274/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3502425
11 A = 6788979
64 meter
Y = -5663233
20 meter E =
0014185
Z = 1278958
90 I = 51
36945
XDOT = 4738
208604 Wp = 42
07058
YDOT = -1610
982349 meter/sec RA = 229
43569 deg
ZDOT = 5814
996419 TA = 331
90200
MA = 331
97848
Ha = 220
875 n
mi
Hp = 215
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11490896
04 X = -3445049
60
Y = -18580161
41 feet Y = -5702078
78 meter
Z = 4196059
39 Z = 1262085
02
XDOT = 15545
303818 XDOT = 4727
624364
YDOT = -5285
375161 feet/sec YDOT = -1558
055109 meter/sec
ZDOT = 19078
072242 ZDOT = 5837
987702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20034729
29 X = -6106585
49
Y = -8745728
04 feet Y = -2665697
91 meter
Z = 4122119
32 Z = 1256421
97
XDOT = 9049
604144 XDOT = 2758
319343
YDOT = -11647
996689 feet/sec YDOT = -3550
309391 meter/sec
ZDOT = 19180
069635 ZDOT = 5846
085225
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 17274
13270288
00016717 00000-0 10270-3 0 9054
2 25544 51
6407 230
1745 0004167 326
3860 33
7028 15
54020231 38224
Satellite: ISS
Catalog Number: 25544
Epoch time: 17274
13270288 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 230
1745 deg
Eccentricity:
0004167
Arg of perigee: 326
3860 deg
Mean anomaly: 33
7028 deg
Mean motion: 15
54020231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 282
Coasting Arc #7 (Orbit 3836)
---------------------------------------
Vector Time (GMT): 2017/275/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2511352
18 A = 6786259
35 meter
Y = 5633501
55 meter E =
0002296
Z = -2833585
78 I = 51
38199
XDOT = -5753
140156 Wp = 57
56822
YDOT = 20
001067 meter/sec RA = 224
44396 deg
ZDOT = -5060
931410 TA = 154
72816
MA = 154
71693
Ha = 220
944 n
mi
Hp = 215
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8239344
44 X = 2461934
45
Y = 18482616
63 feet Y = 5661308
58 meter
Z = -9296541
28 Z = -2821507
01
XDOT = -18875
131744 XDOT = -5728
352600
YDOT = 65
620298 feet/sec YDOT = -44
196435 meter/sec
ZDOT = -16604
105677 ZDOT = -5088
818291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17508818
50 X = 5336687
88
Y = 10193766
14 feet Y = 3107059
92 meter
Z = -9243808
78 Z = -2817512
92
XDOT = -14476
408255 XDOT = -4412
409236
YDOT = 9701
340444 feet/sec YDOT = 2956
968567 meter/sec
ZDOT = -16727
572973 ZDOT = -5098
564242
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 17275
09729952
00016717 00000-0 10270-3 0 9068
2 25544 51
6402 225
3673 0004146 328
5847 31
5058 15
54026902 38377
Satellite: ISS
Catalog Number: 25544
Epoch time: 17275
09729952 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 225
3673 deg
Eccentricity:
0004146
Arg of perigee: 328
5847 deg
Mean anomaly: 31
5058 deg
Mean motion: 15
54026902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3837
Checksum: 319
Coasting Arc #8 (Orbit 3852)
---------------------------------------
Vector Time (GMT): 2017/276/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1256234
76 A = 6782432
62 meter
Y = -5258861
94 meter E =
0008470
Z = 4086674
46 I = 51
39442
XDOT = 6506
424274 Wp = 81
58663
YDOT = 1412
002616 meter/sec RA = 219
44423 deg
ZDOT = 3811
509444 TA = 328
91131
MA = 328
96141
Ha = 220
948 n
mi
Hp = 215
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4121505
13 X = -1217186
58
Y = -17253484
06 feet Y = -5272691
17 meter
Z = 13407724
61 Z = 4080667
54
XDOT = 21346
536332 XDOT = 6471
636760
YDOT = 4632
554515 feet/sec YDOT = 1484
567867 meter/sec
ZDOT = 12504
952244 ZDOT = 3843
031142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13664196
33 X = -4164847
04
Y = -11342549
42 feet Y = -3457209
06 meter
Z = 13381812
56 Z = 4078776
47
XDOT = 19007
852124 XDOT = 5793
593327
YDOT = -7959
256921 feet/sec YDOT = -2425
981509 meter/sec
ZDOT = 12644
337154 ZDOT = 3853
993965
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 17276
12619462
00016717 00000-0 10270-3 0 9078
2 25544 51
6410 220
2389 0004142 331
6701 28
4226 15
54071413 38531
Satellite: ISS
Catalog Number: 25544
Epoch time: 17276
12619462 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 220
2389 deg
Eccentricity:
0004142
Arg of perigee: 331
6701 deg
Mean anomaly: 28
4226 deg
Mean motion: 15
54071413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3853
Checksum: 283
Coasting Arc #9 (Orbit 3867)
---------------------------------------
Vector Time (GMT): 2017/277/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -208398
44 A = 6779243
69 meter
Y = 4643130
45 meter E =
0012428
Z = -4946381
86 I = 51
40971
XDOT = -6865
856920 Wp = 54
28213
YDOT = -2615
311092 meter/sec RA = 214
43679 deg
ZDOT = -2162
424127 TA = 194
52413
MA = 194
55988
Ha = 221
124 n
mi
Hp = 215
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -683721
93 X = -236276
36
Y = 15233367
62 feet Y = 4640643
45 meter
Z = -16228286
94 Z = -4947462
55
XDOT = -22525
777295 XDOT = -6825
597436
YDOT = -8580
416970 feet/sec YDOT = -2691
864983 meter/sec
ZDOT = -7094
567346 ZDOT = -2195
678485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8831685
04 X = 2691897
60
Y = 12423750
53 feet Y = 3786759
16 meter
Z = -16233669
44 Z = -4948022
45
XDOT = -22142
017066 XDOT = -6748
886802
YDOT = 6263
879431 feet/sec YDOT = 1909
230451 meter/sec
ZDOT = -7241
483037 ZDOT = -2207
204030
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 17277
09077884
00016717 00000-0 10270-3 0 9082
2 25544 51
6414 215
4317 0004291 335
1356 24
9589 15
54035589 38685
Satellite: ISS
Catalog Number: 25544
Epoch time: 17277
09077884 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 215
4317 deg
Eccentricity:
0004291
Arg of perigee: 335
1356 deg
Mean anomaly: 24
9589 deg
Mean motion: 15
54035589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3868
Checksum: 341
Coasting Arc #10 (Orbit 3873)
---------------------------------------
Vector Time (GMT): 2017/277/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 612910
87 A = 6780157
87 meter
Y = 4847861
32 meter E =
0011847
Z = -4711529
93 I = 51
42126
XDOT = -6915
223890 Wp = 47
88293
YDOT = -1804
428883 meter/sec RA = 212
51880 deg
ZDOT = -2752
898682 TA = 194
72554
MA = 194
76007
Ha = 221
334 n
mi
Hp = 215
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2010862
43 X = 581541
79
Y = 15905056
82 feet Y = 4854539
26 meter
Z = -15457775
36 Z = -4708629
43
XDOT = -22687
742422 XDOT = -6881
159955
YDOT = -5920
042268 feet/sec YDOT = -1881
569555 meter/sec
ZDOT = -9031
819823 ZDOT = -2786
408061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1125483
42 X = -343047
35
Y = -16003918
85 feet Y = -4877994
47 meter
Z = -15445552
36 Z = -4707804
36
XDOT = 21051
892858 XDOT = 6416
616943
YDOT = 7389
747137 feet/sec YDOT = 2252
394927 meter/sec
ZDOT = -9179
974327 ZDOT = -2798
056175
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 17277
47661093
00016717 00000-0 10270-3 0 9096
2 25544 51
6393 213
5102 0004678 341
8085 18
2899 15
54058584 38741
Satellite: ISS
Catalog Number: 25544
Epoch time: 17277
47661093 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 213
5102 deg
Eccentricity:
0004678
Arg of perigee: 341
8085 deg
Mean anomaly: 18
2899 deg
Mean motion: 15
54058584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3874
Checksum: 341
Coasting Arc #11 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2017/278/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 987945
81 A = 6777767
32 meter
Y = -4189195
36 meter E =
0003165
Z = 5233850
26 I = 51
44185
XDOT = 7064
892480 Wp = 33
23709
YDOT = 2835
762516 meter/sec RA = 207
50928 deg
ZDOT = 938
508354 TA = 47
77437
MA = 47
74751
Ha = 221
285 n
mi
Hp = 215
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3241292
03 X = 1009293
21
Y = -13744079
26 feet Y = -4178027
40 meter
Z = 17171424
75 Z = 5238701
89
XDOT = 23178
781104 XDOT = 7028
098265
YDOT = 9303
682796 feet/sec YDOT = 2914
561366 meter/sec
ZDOT = 3079
095649 ZDOT = 972
738174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3738562
16 X = -1139513
75
Y = 13589415
17 feet Y = 4142053
74 meter
Z = 17193442
50 Z = 5240561
27
XDOT = -21728
993862 XDOT = -6622
997329
YDOT = -10055
212903 feet/sec YDOT = -3064
828893 meter/sec
ZDOT = 3230
322976 ZDOT = 984
602443
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 17278
50548821
00016717 00000-0 10270-3 0 9106
2 25544 51
6393 208
3828 0004740 344
0397 16
0606 15
54093547 38907
Satellite: ISS
Catalog Number: 25544
Epoch time: 17278
50548821 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 208
3828 deg
Eccentricity:
0004740
Arg of perigee: 344
0397 deg
Mean anomaly: 16
0606 deg
Mean motion: 15
54093547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 317
Coasting Arc #12 (Orbit 3904)
---------------------------------------
Vector Time (GMT): 2017/279/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2610689
40 A = 6777790
06 meter
Y = 3433955
70 meter E =
0013629
Z = -5239068
63 I = 51
47166
XDOT = -6686
097329 Wp = 78
56636
YDOT = -3607
056580 meter/sec RA = 202
49723 deg
ZDOT = 972
305432 TA = 200
74505
MA = 200
80042
Ha = 221
451 n
mi
Hp = 214
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8565253
92 X = -2623445
44
Y = 11266258
86 feet Y = 3404689
21 meter
Z = -17188545
36 Z = -5251782
21
XDOT = -21936
014859 XDOT = -6649
988410
YDOT = -11834
175131 feet/sec YDOT = -3681
623066 meter/sec
ZDOT = 3189
978450 ZDOT = 939
913965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8758038
41 X = 2669450
11
Y = -11028830
54 feet Y = -3361587
55 meter
Z = -17245286
75 Z = -5256363
40
XDOT = 20819
466302 XDOT = 6345
773329
YDOT = 11792
921950 feet/sec YDOT = 3594
482610 meter/sec
ZDOT = 3046
976310 ZDOT = 928
718379
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 17279
47005459
00016717 00000-0 10270-3 0 9119
2 25544 51
6397 203
5746 0004702 348
0132 12
0908 15
54076833 39053
Satellite: ISS
Catalog Number: 25544
Epoch time: 17279
47005459 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 203
5746 deg
Eccentricity:
0004702
Arg of perigee: 348
0132 deg
Mean anomaly: 12
0908 deg
Mean motion: 15
54076833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3905
Checksum: 306
Coasting Arc #13 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2017/280/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147780
76 A = 6780000
88 meter
Y = -2601486
05 meter E =
0010400
Z = 4688295
05 I = 51
51041
XDOT = 5796
018732 Wp = 37
79160
YDOT = 4165
163980 meter/sec RA = 197
49106 deg
ZDOT = -2805
229764 TA = 80
12860
MA = 80
01121
Ha = 221
459 n
mi
Hp = 214
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13608204
59 X = 4153789
03
Y = -8535059
21 feet Y = -2555068
63 meter
Z = 15381545
45 Z = 4708459
02
XDOT = 19015
809489 XDOT = 5762
638729
YDOT = 13665
236154 feet/sec YDOT = 4229
792075 meter/sec
ZDOT = -9203
509725 ZDOT = -2777
155385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13593542
90 X = -4143311
88
Y = 8395259
43 feet Y = 2558875
07 meter
Z = 15471186
73 Z = 4715617
72
XDOT = -18322
893361 XDOT = -5584
817896
YDOT = -12867
535781 feet/sec YDOT = -3922
024906 meter/sec
ZDOT = -9079
685681 ZDOT = -2767
488195
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 17280
49891442
00016717 00000-0 10270-3 0 9129
2 25544 51
6402 198
4467 0004752 351
8456 8
2619 15
54092154 39216
Satellite: ISS
Catalog Number: 25544
Epoch time: 17280
49891442 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 198
4467 deg
Eccentricity:
0004752
Arg of perigee: 351
8456 deg
Mean anomaly: 8
2619 deg
Mean motion: 15
54092154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 319
Coasting Arc #14 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2017/281/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5413717
83 A = 6783563
70 meter
Y = 1789754
36 meter E =
0006425
Z = -3676240
17 I = 51
55316
XDOT = -4429
167239 Wp = 55
56652
YDOT = -4508
077001 meter/sec RA = 192
49503 deg
ZDOT = 4336
735509 TA = 260
65368
MA = 260
72634
Ha = 221
573 n
mi
Hp = 214
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17761541
42 X = -5415471
17
Y = 5871897
51 feet Y = 1729204
35 meter
Z = -12061155
41 Z = -3702543
38
XDOT = -14531
388581 XDOT = -4399
493782
YDOT = -14790
278876 feet/sec YDOT = -4557
440679 meter/sec
ZDOT = 14228
134871 ZDOT = 4315
291935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17640631
94 X = 5376864
61
Y = -5994151
64 feet Y = -1827017
42 meter
Z = -12177900
27 Z = -3711824
00
XDOT = 14290
170160 XDOT = 4355
643865
YDOT = 13400
321032 feet/sec YDOT = 4084
417851 meter/sec
ZDOT = 14133
714300 ZDOT = 4307
956119
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 17281
46346180
00016717 00000-0 10270-3 0 9132
2 25544 51
6395 193
6389 0004804 355
7974 4
3138 15
54101777 39364
Satellite: ISS
Catalog Number: 25544
Epoch time: 17281
46346180 = yrday
fracday
Element set: 913
Inclination: 51
6395 deg
RA of node: 193
6389 deg
Eccentricity:
0004804
Arg of perigee: 355
7974 deg
Mean anomaly: 4
3138 deg
Mean motion: 15
54101777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 330
Coasting Arc #15 (Orbit 3951)
---------------------------------------
Vector Time (GMT): 2017/282/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6326911
93 A = 6787131
52 meter
Y = -963990
31 meter E =
0013103
Z = 2249167
20 I = 51
59765
XDOT = 2660
576409 Wp = 87
98105
YDOT = 4701
290354 meter/sec RA = 187
51163 deg
ZDOT = -5441
364249 TA = 66
98951
MA = 66
85136
Ha = 221
659 n
mi
Hp = 214
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20757585
06 X = 6326295
69
Y = -3162697
87 feet Y = -893241
76 meter
Z = 7379157
47 Z = 2279900
65
XDOT = 8728
925228 XDOT = 2634
239681
YDOT = 15424
180952 feet/sec YDOT = 4730
895117 meter/sec
ZDOT = -17852
244912 ZDOT = -5428
503976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20626217
96 X = -6286871
24
Y = 3661862
59 feet Y = 1116135
72 meter
Z = 7515441
13 Z = 2290706
46
XDOT = -8949
145282 XDOT = -2727
699482
YDOT = -13700
236736 feet/sec YDOT = -4175
832157 meter/sec
ZDOT = -17795
865496 ZDOT = -5424
179803
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 17282
49230423
00016717 00000-0 10270-3 0 9149
2 25544 51
6398 188
5106 0004774 358
9744 1
1398 15
54120155 39525
Satellite: ISS
Catalog Number: 25544
Epoch time: 17282
49230423 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 188
5106 deg
Eccentricity:
0004774
Arg of perigee: 358
9744 deg
Mean anomaly: 1
1398 deg
Mean motion: 15
54120155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3952
Checksum: 318
Coasting Arc #16 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2017/283/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6750182
26 A = 6789152
65 meter
Y = 190084
12 meter E =
0014732
Z = -617480
84 I = 51
63684
XDOT = -674
105509 Wp = 29
08412
YDOT = -4764
048631 meter/sec RA = 182
53761 deg
ZDOT = 5975
070336 TA = 324
24682
MA = 324
34538
Ha = 221
714 n
mi
Hp = 214
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22146267
25 X = -6748806
66
Y = 623635
55 feet Y = 114606
63 meter
Z = -2025855
77 Z = -650268
46
XDOT = -2211
632249 XDOT = -649
807093
YDOT = -15630
080809 feet/sec YDOT = -4771
450781 meter/sec
ZDOT = 19603
249133 ZDOT = 5971
854929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22087756
93 X = 6732348
31
Y = -1538574
01 feet Y = -468957
36 meter
Z = -2171163
19 Z = -661770
54
XDOT = 2872
572240 XDOT = 875
560019
YDOT = 13907
600345 feet/sec YDOT = 4239
036585 meter/sec
ZDOT = 19589
607904 ZDOT = 5970
912489
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 17283
45683454
00016717 00000-0 10270-3 0 9153
2 25544 51
6397 183
7023 0004840 1
8107 358
3062 15
54125617 39679
Satellite: ISS
Catalog Number: 25544
Epoch time: 17283
45683454 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 183
7023 deg
Eccentricity:
0004840
Arg of perigee: 1
8107 deg
Mean anomaly: 358
3062 deg
Mean motion: 15
54125617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 316
Coasting Arc #17 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2017/283/16:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1013799
75 A = 6777674
30 meter
Y = 4184113
82 meter E =
0015854
Z = -5248152
29 I = 51
60376
XDOT = -7570
352342 Wp = 65
64624
YDOT = 599
063951 meter/sec RA = 181
34968 deg
ZDOT = -980
728885 TA = 194
92462
MA = 194
97146
Ha = 221
717 n
mi
Hp = 214
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3326114
66 X = 992429
96
Y = 13727407
56 feet Y = 4195331
09 meter
Z = -17218347
40 Z = -5243279
57
XDOT = -24837
113983 XDOT = -7571
724596
YDOT = 1965
432910 feet/sec YDOT = 514
399387 meter/sec
ZDOT = -3217
614453 ZDOT = -1017
507375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13770778
49 X = -4197333
28
Y = 3255023
13 feet Y = 992131
05 meter
Z = -17197288
41 Z = -5241733
51
XDOT = -1395
536542 XDOT = -425
359538
YDOT = -23835
363306 feet/sec YDOT = -7265
018736 meter/sec
ZDOT = -3380
663625 ZDOT = -1030
426273
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 17283
71403971
00016717 00000-0 10270-3 0 9167
2 25544 51
6371 182
4174 0004684 2
5995 357
5182 15
54141890 39713
Satellite: ISS
Catalog Number: 25544
Epoch time: 17283
71403971 = yrday
fracday
Element set: 916
Inclination: 51
6371 deg
RA of node: 182
4174 deg
Eccentricity:
0004684
Arg of perigee: 2
5995 deg
Mean anomaly: 357
5182 deg
Mean motion: 15
54141890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 324
Coasting Arc #18 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2017/284/16:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 831109
53 A = 6777657
04 meter
Y = -4211499
00 meter E =
0007295
Z = 5242762
98 I = 51
63594
XDOT = 7603
799445 Wp = 28
99759
YDOT = 284
266355 meter/sec RA = 176
34811 deg
ZDOT = -970
234566 TA = 70
32507
MA = 70
24637
Ha = 221
784 n
mi
Hp = 214
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2726737
29 X = 852674
71
Y = -13817253
92 feet Y = -4202084
16 meter
Z = 17200665
95 Z = 5246852
87
XDOT = 24946
848574 XDOT = 7604
768565
YDOT = 932
632397 feet/sec YDOT = 369
302606 meter/sec
ZDOT = -3183
184273 ZDOT = -933
294776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13825713
57 X = 4214077
50
Y = 2561026
72 feet Y = 780600
94 meter
Z = 17219329
19 Z = 5248451
54
XDOT = -650
254382 XDOT = -198
197536
YDOT = 23962
389960 feet/sec YDOT = 7303
736460 meter/sec
ZDOT = -3019
507624 ZDOT = -920
345924
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 17284
74286229
00016717 00000-0 10270-3 0 9177
2 25544 51
6367 177
2882 0004654 6
5964 353
5249 15
54119219 39870
Satellite: ISS
Catalog Number: 25544
Epoch time: 17284
74286229 = yrday
fracday
Element set: 917
Inclination: 51
6367 deg
RA of node: 177
2882 deg
Eccentricity:
0004654
Arg of perigee: 6
5964 deg
Mean anomaly: 353
5249 deg
Mean motion: 15
54119219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 351
Coasting Arc #19 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2017/285/09:32:06
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3361562
99 A = 6779476
72 meter
Y = -3403079
81 meter E =
0007345
Z = 4797474
19 I = 51
66766
XDOT = 6620
941980 Wp = 81
70820
YDOT = -2888
482605 meter/sec RA = 172
88553 deg
ZDOT = 2587
966455 TA = 342
81418
MA = 342
83904
Ha = 221
871 n
mi
Hp = 214
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11028749
98 X = -3346563
07
Y = -11164960
01 feet Y = -3440587
01 meter
Z = 15739744
70 Z = 4781181
15
XDOT = 21722
250590 XDOT = 6640
178455
YDOT = -9476
648968 feet/sec YDOT = -2814
335038 meter/sec
ZDOT = 8490
703592 ZDOT = 2620
176179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7456678
35 X = 2272795
56
Y = 13890360
79 feet Y = 4233781
97 meter
Z = 15667962
43 Z = 4775594
95
XDOT = -22461
866188 XDOT = -6846
376814
YDOT = 2310
589181 feet/sec YDOT = 704
267583 meter/sec
ZDOT = 8633
837198 ZDOT = 2631
593578
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 17285
45017287
00016717 00000-0 10270-3 0 9183
2 25544 51
6391 173
7652 0004747 8
4308 351
6924 15
54183593 39986
Satellite: ISS
Catalog Number: 25544
Epoch time: 17285
45017287 = yrday
fracday
Element set: 918
Inclination: 51
6391 deg
RA of node: 173
7652 deg
Eccentricity:
0004747
Arg of perigee: 8
4308 deg
Mean anomaly: 351
6924 deg
Mean motion: 15
54183593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 343
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