[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 10th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
225/21:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
3
226/16:31:37
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
3
228/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
5
Coasting Arc #1 (Orbit 3004)
---------------------------------------
Vector Time (GMT): 2017/221/13:04:32
527
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4919367
35 A = 6780271
03 meter
Y = 68424
15 meter E =
0013731
Z = 4658041
14 I = 51
91045
XDOT = 2698
535394 Wp = 117
32228
YDOT = -6556
702708 meter/sec RA = 131
29280 deg
ZDOT = 2933
481361 TA = 303
55102
MA = 303
68208
Ha = 223
012 n
mi
Hp = 212
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16139656
67 X = -4942392
92
Y = 224488
69 feet Y = 13283
76 meter
Z = 15282287
20 Z = 4634088
91
XDOT = 8853
462579 XDOT = 2757
404479
YDOT = -21511
491825 feet/sec YDOT = -6526
196654 meter/sec
ZDOT = 9624
282679 ZDOT = 2946
732826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14632309
54 X = 4459927
95
Y = 7047342
25 feet Y = 2148029
92 meter
Z = 15176221
51 Z = 4625712
32
XDOT = -16954
367723 XDOT = -5167
691282
YDOT = 14257
369992 feet/sec YDOT = 4345
646374 meter/sec
ZDOT = 9683
906470 ZDOT = 2951
654692
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 17221
59831780
00016717 00000-0 10270-3 0 9001
2 25544 51
6424 132
0687 0005425 120
3426 239
8263 15
54117886 30052
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
59831780 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 132
0687 deg
Eccentricity:
0005425
Arg of perigee: 120
3426 deg
Mean anomaly: 239
8263 deg
Mean motion: 15
54117886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3005
Checksum: 297
Coasting Arc #2 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2017/222/13:04:32
527
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4045984
43 A = 6777716
44 meter
Y = 1449259
55 meter E =
0018464
Z = -5256643
15 I = 51
92240
XDOT = -3768
595797 Wp = 92
90464
YDOT = 6572
914792 meter/sec RA = 126
31575 deg
ZDOT = -1092
709418 TA = 166
67217
MA = 166
62333
Ha = 222
753 n
mi
Hp = 213
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13274227
14 X = 4055011
50
Y = 4754788
54 feet Y = 1494554
83 meter
Z = -17246204
58 Z = -5236967
45
XDOT = -12364
159439 XDOT = -3836
508022
YDOT = 21564
681076 feet/sec YDOT = 6530
392040 meter/sec
ZDOT = -3585
004653 ZDOT = -1111
180911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10031597
42 X = -3057630
89
Y = -10058357
12 feet Y = -3065787
25 meter
Z = -17159288
97 Z = -5230151
28
XDOT = 19695
359847 XDOT = 6003
145681
YDOT = -13409
586624 feet/sec YDOT = -4087
242003 meter/sec
ZDOT = -3667
755191 ZDOT = -1117
931782
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 17222
56284924
00016717 00000-0 10270-3 0 9012
2 25544 51
6418 127
2613 0005286 124
1922 235
9733 15
54147418 30208
Satellite: ISS
Catalog Number: 25544
Epoch time: 17222
56284924 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 127
2613 deg
Eccentricity:
0005286
Arg of perigee: 124
1922 deg
Mean anomaly: 235
9733 deg
Mean motion: 15
54147418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 294
Coasting Arc #3 (Orbit 3035)
---------------------------------------
Vector Time (GMT): 2017/223/13:04:32
527
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3037694
06 A = 6777442
99 meter
Y = -2960186
42 meter E =
0007040
Z = 5280071
49 I = 51
94067
XDOT = 4517
991110 Wp = 104
10400
YDOT = -6145
399998 meter/sec RA = 121
33609 deg
ZDOT = -846
789702 TA = 353
94757
MA = 353
95607
Ha = 222
744 n
mi
Hp = 213
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9966187
85 X = -3030014
38
Y = -9711897
72 feet Y = -2994112
86 meter
Z = 17323069
18 Z = 5265334
25
XDOT = 14822
805479 XDOT = 4590
488051
YDOT = -20162
073485 feet/sec YDOT = -6094
471423 meter/sec
ZDOT = -2778
181436 ZDOT = -824
666681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5135481
60 X = 1565294
79
Y = 13019774
56 feet Y = 3968427
29 meter
Z = 17258241
00 Z = 5260311
86
XDOT = -20925
165246 XDOT = -6377
990367
YDOT = 11802
008879 feet/sec YDOT = 3597
252306 meter/sec
ZDOT = -2679
310804 ZDOT = -816
653933
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 17223
59167973
00016717 00000-0 10270-3 0 9021
2 25544 51
6421 122
1328 0005171 129
5136 230
6474 15
54169111 30363
Satellite: ISS
Catalog Number: 25544
Epoch time: 17223
59167973 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 122
1328 deg
Eccentricity:
0005171
Arg of perigee: 129
5136 deg
Mean anomaly: 230
6474 deg
Mean motion: 15
54169111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3036
Checksum: 288
Coasting Arc #4 (Orbit 3050)
---------------------------------------
Vector Time (GMT): 2017/224/13:04:32
527
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2001148
85 A = 6779656
33 meter
Y = 4386576
91 meter E =
0016009
Z = -4781669
22 I = 51
96375
XDOT = -4932
289905 Wp = 116
11103
YDOT = 5194
405721 meter/sec RA = 116
35939 deg
ZDOT = 2701
179191 TA = 180
50282
MA = 180
50443
Ha = 222
603 n
mi
Hp = 213
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6565448
98 X = 1975175
06
Y = 14391656
52 feet Y = 4408809
71 meter
Z = -15687891
14 Z = -4772011
59
XDOT = -16182
053494 XDOT = -5003
129438
YDOT = 17042
013521 feet/sec YDOT = 5138
853509 meter/sec
ZDOT = 8862
136453 ZDOT = 2677
047621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -361247
98 X = -110108
39
Y = -15856045
45 feet Y = -4832922
65 meter
Z = -15645770
95 Z = -4768830
99
XDOT = 20541
397439 XDOT = 6261
017939
YDOT = -9105
897276 feet/sec YDOT = -2775
477490 meter/sec
ZDOT = 8754
497092 ZDOT = 2668
370714
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 17224
55620653
00016717 00000-0 10270-3 0 9038
2 25544 51
6419 117
3240 0005120 131
8193 228
3397 15
54149734 30516
Satellite: ISS
Catalog Number: 25544
Epoch time: 17224
55620653 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 117
3240 deg
Eccentricity:
0005120
Arg of perigee: 131
8193 deg
Mean anomaly: 228
3397 deg
Mean motion: 15
54149734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 288
Coasting Arc #5 (Orbit 3066)
---------------------------------------
Vector Time (GMT): 2017/225/13:04:32
527
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -976456
93 A = 6783218
39 meter
Y = -5553804
31 meter E =
0015338
Z = 3755077
51 I = 51
98888
XDOT = 5096
137973 Wp = 98
63510
YDOT = -3807
790042 meter/sec RA = 111
39252 deg
ZDOT = -4293
920630 TA = 36
65801
MA = 36
55317
Ha = 222
563 n
mi
Hp = 213
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3203598
85 X = -932520
48
Y = -18221142
74 feet Y = -5564477
95 meter
Z = 12319808
09 Z = 3750441
07
XDOT = 16719
612773 XDOT = 5159
196584
YDOT = -12492
749480 feet/sec YDOT = -3750
449095 meter/sec
ZDOT = -14087
666110 ZDOT = -4269
012042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3960683
29 X = -1207216
27
Y = 18085107
43 feet Y = 5512340
75 meter
Z = 12300107
18 Z = 3749072
67
XDOT = -19000
579729 XDOT = -5791
376702
YDOT = 5373
066674 feet/sec YDOT = 1637
710722 meter/sec
ZDOT = -13976
778239 ZDOT = -4260
122007
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 17225
58503114
00016717 00000-0 10270-3 0 9045
2 25544 51
6412 112
1952 0005059 134
2147 225
9422 15
54176915 30679
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
58503114 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 112
1952 deg
Eccentricity:
0005059
Arg of perigee: 134
2147 deg
Mean anomaly: 225
9422 deg
Mean motion: 15
54176915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3067
Checksum: 288
Coasting Arc #6 (Orbit 3071)
---------------------------------------
Vector Time (GMT): 2017/225/21:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4494703
22 A = 6782211
85 meter
Y = -2970999
00 meter E =
0010702
Z = -4126992
64 I = 51
98881
XDOT = 828
562851 Wp = 100
80613
YDOT = 6575
991695 meter/sec RA = 109
75928 deg
ZDOT = -3842
012754 TA = 129
70890
MA = 129
61450
Ha = 222
737 n
mi
Hp = 213
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14746401
63 X = 4547638
47
Y = -9747372
03 feet Y = -2920440
28 meter
Z = -13540002
11 Z = -4105030
23
XDOT = 2718
382056 XDOT = 773
629320
YDOT = 21574
775902 feet/sec YDOT = 6584
950009 meter/sec
ZDOT = -12605
028721 ZDOT = -3838
121444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12092143
78 X = 3685685
42
Y = 12995550
51 feet Y = 3961043
80 meter
Z = -13442284
23 Z = -4097208
23
XDOT = -19853
815594 XDOT = -6051
442993
YDOT = 5487
590761 feet/sec YDOT = 1672
617664 meter/sec
ZDOT = -12588
785406 ZDOT = -3837
061792
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 17225
90654001
00016717 00000-0 10270-3 0 9054
2 25544 51
6410 110
5883 0005611 141
1259 219
0298 15
54130600 30729
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
90654001 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 110
5883 deg
Eccentricity:
0005611
Arg of perigee: 141
1259 deg
Mean anomaly: 219
0298 deg
Mean motion: 15
54130600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3072
Checksum: 267
Coasting Arc #7 (Orbit 3084)
---------------------------------------
Vector Time (GMT): 2017/226/16:31:37
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4388667
59 A = 6780526
01 meter
Y = 2412768
29 meter E =
0013665
Z = 4565168
69 I = 51
98786
XDOT = -569
872384 Wp = 123
92200
YDOT = -6981
733873 meter/sec RA = 105
76165 deg
ZDOT = 3128
010173 TA = 294
84147
MA = 294
98351
Ha = 222
650 n
mi
Hp = 213
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14398515
73 X = -4437496
90
Y = 7915906
45 feet Y = 2363418
24 meter
Z = 14977587
58 Z = 4543731
37
XDOT = -1869
660053 XDOT = -506
952718
YDOT = -22905
951027 feet/sec YDOT = -6987
754740 meter/sec
ZDOT = 10262
500566 ZDOT = 3125
394804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8515437
90 X = 2595505
47
Y = -14153172
48 feet Y = -4313886
97 meter
Z = 14882270
85 Z = 4536116
16
XDOT = 12204
666398 XDOT = 3719
982318
YDOT = 18172
206648 feet/sec YDOT = 5538
888586 meter/sec
ZDOT = 10251
981235 ZDOT = 3124
803880
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 17226
74245751
00016717 00000-0 10270-3 0 9066
2 25544 51
6372 106
4207 0005324 142
2432 217
9095 15
54151884 30859
Satellite: ISS
Catalog Number: 25544
Epoch time: 17226
74245751 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 106
4207 deg
Eccentricity:
0005324
Arg of perigee: 142
2432 deg
Mean anomaly: 217
9095 deg
Mean motion: 15
54151884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3085
Checksum: 299
Coasting Arc #8 (Orbit 3099)
---------------------------------------
Vector Time (GMT): 2017/227/16:31:37
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284121
75 A = 6777838
38 meter
Y = -671821
54 meter E =
0017201
Z = -5223346
34 I = 51
98845
XDOT = -399
511638 Wp = 96
81532
YDOT = 7534
122255 meter/sec RA = 100
78941 deg
ZDOT = -1302
358313 TA = 160
74901
MA = 160
68394
Ha = 222
604 n
mi
Hp = 213
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14055517
56 X = 4316688
18
Y = -2204138
91 feet Y = -623731
44 meter
Z = -17136963
05 Z = -5202456
40
XDOT = -1310
733719 XDOT = -477
404305
YDOT = 24718
248868 feet/sec YDOT = 7529
219131 meter/sec
ZDOT = -4272
829112 ZDOT = -1304
488131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10957960
96 X = -3339986
50
Y = 9246904
79 feet Y = 2818456
58 meter
Z = -17044328
92 Z = -5195111
45
XDOT = -11075
150436 XDOT = -3375
705853
YDOT = -20985
553373 feet/sec YDOT = -6396
396668 meter/sec
ZDOT = -4283
428691 ZDOT = -1305
589065
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 17227
70697683
00016717 00000-0 10270-3 0 9079
2 25544 51
6388 101
6124 0005529 143
3911 216
7620 15
54156694 31005
Satellite: ISS
Catalog Number: 25544
Epoch time: 17227
70697683 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 101
6124 deg
Eccentricity:
0005529
Arg of perigee: 143
3911 deg
Mean anomaly: 216
7620 deg
Mean motion: 15
54156694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3100
Checksum: 308
Coasting Arc #9 (Orbit 3111)
---------------------------------------
Vector Time (GMT): 2017/228/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4139094
31 A = 6779084
39 meter
Y = -2176794
33 meter E =
0014317
Z = -4919772
11 I = 52
00031
XDOT = 983
050161 Wp = 92
50110
YDOT = 7214
929640 meter/sec RA = 96
98395 deg
ZDOT = -2371
794776 TA = 154
39154
MA = 154
32056
Ha = 222
397 n
mi
Hp = 213
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13579705
74 X = 4187025
86
Y = -7141713
69 feet Y = -2130240
07 meter
Z = -16140984
62 Z = -4899549
43
XDOT = 3225
230186 XDOT = 913
818786
YDOT = 23671
029001 feet/sec YDOT = 7225
535725 meter/sec
ZDOT = -7781
478924 ZDOT = -2367
187465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14181204
85 X = -4322431
24
Y = -6099230
77 feet Y = -1859045
54 meter
Z = -16051064
77 Z = -4892364
54
XDOT = 15838
484684 XDOT = 4827
570132
YDOT = -16455
180033 feet/sec YDOT = -5015
538874 meter/sec
ZDOT = -7762
198574 ZDOT = -2365
918125
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 17228
47858916
00016717 00000-0 10270-3 0 9083
2 25544 51
6421 97
7704 0005020 145
3629 214
7851 15
54169473 31122
Satellite: ISS
Catalog Number: 25544
Epoch time: 17228
47858916 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 97
7704 deg
Eccentricity:
0005020
Arg of perigee: 145
3629 deg
Mean anomaly: 214
7851 deg
Mean motion: 15
54169473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3112
Checksum: 319
Coasting Arc #10 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2017/229/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4173842
63 A = 6777309
95 meter
Y = 401217
24 meter E =
0007419
Z = 5320451
43 I = 51
99730
XDOT = -110
465765 Wp = 136
49888
YDOT = -7656
455878 meter/sec RA = 92
01060 deg
ZDOT = 485
076183 TA = 308
86610
MA = 308
93228
Ha = 222
468 n
mi
Hp = 213
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13693709
41 X = -4203862
81
Y = 1316329
53 feet Y = 354374
51 meter
Z = 17455549
32 Z = 5300103
51
XDOT = -362
420488 XDOT = -27
197276
YDOT = -25119
605899 feet/sec YDOT = -7657
225611 meter/sec
ZDOT = 1591
457292 ZDOT = 484
741632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9910537
20 X = 3020731
74
Y = 9704258
94 feet Y = 2957858
12 meter
Z = 17365345
19 Z = 5292957
21
XDOT = -18252
026924 XDOT = -5563
217806
YDOT = 15759
351506 feet/sec YDOT = 4803
450339 meter/sec
ZDOT = 1591
187899 ZDOT = 484
994072
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 17229
50740531
00016717 00000-0 10270-3 0 9092
2 25544 51
6421 92
6421 0005093 150
1408 210
0036 15
54167033 31282
Satellite: ISS
Catalog Number: 25544
Epoch time: 17229
50740531 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 92
6421 deg
Eccentricity:
0005093
Arg of perigee: 150
1408 deg
Mean anomaly: 210
0036 deg
Mean motion: 15
54167033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 268
Coasting Arc #11 (Orbit 3142)
---------------------------------------
Vector Time (GMT): 2017/230/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4134347
97 A = 6777932
72 meter
Y = 1440557
06 meter E =
0017186
Z = -5189204
83 I = 51
99973
XDOT = -760
111649 Wp = 114
33634
YDOT = 7475
391116 meter/sec RA = 87
03468 deg
ZDOT = 1466
552176 TA = 169
75066
MA = 169
71557
Ha = 222
189 n
mi
Hp = 213
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13564133
76 X = 4143138
25
Y = 4726237
07 feet Y = 1486839
40 meter
Z = -17024950
24 Z = -5169100
37
XDOT = -2493
804622 XDOT = -850
770644
YDOT = 24525
561403 feet/sec YDOT = 7466
384096 meter/sec
ZDOT = 4811
522887 ZDOT = 1462
639798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5437942
21 X = -1657484
79
Y = -13407790
33 feet Y = -4086694
49 meter
Z = -16936112
76 Z = -5162127
17
XDOT = 19155
185608 XDOT = 5838
500573
YDOT = -13836
049798 feet/sec YDOT = -4217
227978 meter/sec
ZDOT = 4792
993714 ZDOT = 1460
904484
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 17230
47191835
00016717 00000-0 10270-3 0 9109
2 25544 51
6422 87
8337 0004928 154
1455 205
9945 15
54175050 31434
Satellite: ISS
Catalog Number: 25544
Epoch time: 17230
47191835 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 87
8337 deg
Eccentricity:
0004928
Arg of perigee: 154
1455 deg
Mean anomaly: 205
9945 deg
Mean motion: 15
54175050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3143
Checksum: 307
Coasting Arc #12 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2017/231/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3979756
79 A = 6780621
50 meter
Y = -3144934
94 meter E =
0010321
Z = 4490316
94 I = 52
00632
XDOT = 1637
526994 Wp = 96
09700
YDOT = -6747
298421 meter/sec RA = 82
06388 deg
ZDOT = -3268
992524 TA = 26
64835
MA = 26
59534
Ha = 222
147 n
mi
Hp = 213
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13056944
86 X = -3966104
87
Y = -10318028
00 feet Y = -3189362
97 meter
Z = 14732010
96 Z = 4471018
02
XDOT = 5372
463891 XDOT = 1728
734237
YDOT = -22136
805842 feet/sec YDOT = -6728
476493 meter/sec
ZDOT = -10725
041090 ZDOT = -3260
816581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1169844
95 X = 356568
74
Y = 16675553
68 feet Y = 5082708
76 meter
Z = 14647014
37 Z = 4464409
98
XDOT = -18854
382093 XDOT = -5746
815662
YDOT = 10725
809890 feet/sec YDOT = 3269
226855 meter/sec
ZDOT = -10687
728980 ZDOT = -3257
619793
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 17231
50072821
00016717 00000-0 10270-3 0 9118
2 25544 51
6421 82
7048 0004746 158
0934 202
0422 15
54209825 31592
Satellite: ISS
Catalog Number: 25544
Epoch time: 17231
50072821 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 82
7048 deg
Eccentricity:
0004746
Arg of perigee: 158
0934 deg
Mean anomaly: 202
0422 deg
Mean motion: 15
54209825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 284
Coasting Arc #13 (Orbit 3173)
---------------------------------------
Vector Time (GMT): 2017/232/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3728721
07 A = 6784550
31 meter
Y = 4583799
23 meter E =
0007534
Z = -3343931
88 I = 52
01190
XDOT = -2520
091367 Wp = 124
29750
YDOT = 5486
121421 meter/sec RA = 77
10183 deg
ZDOT = 4713
625085 TA = 197
02654
MA = 197
05183
Ha = 222
047 n
mi
Hp = 213
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12233336
85 X = 3693429
54
Y = 15038711
38 feet Y = 4625298
94 meter
Z = -10970905
11 Z = -3325905
07
XDOT = -8268
016297 XDOT = -2604
147341
YDOT = 17999
086027 feet/sec YDOT = 5457
470137 meter/sec
ZDOT = 15464
649228 ZDOT = 4701
179268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2569815
09 X = 783279
64
Y = -19259889
33 feet Y = -5870414
27 meter
Z = -10891778
67 Z = -3319814
14
XDOT = 17456
370638 XDOT = 5320
701771
YDOT = -6378
230614 feet/sec YDOT = -1944
084691 meter/sec
ZDOT = 15408
615369 ZDOT = 4696
545965
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 17232
46523870
00016717 00000-0 10270-3 0 9120
2 25544 51
6405 77
8962 0004866 161
6744 198
4585 15
54166368 31745
Satellite: ISS
Catalog Number: 25544
Epoch time: 17232
46523870 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 77
8962 deg
Eccentricity:
0004866
Arg of perigee: 161
6744 deg
Mean anomaly: 198
4585 deg
Mean motion: 15
54166368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3174
Checksum: 339
Coasting Arc #14 (Orbit 3189)
---------------------------------------
Vector Time (GMT): 2017/233/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3303352
39 A = 6787808
31 meter
Y = -5633196
64 meter E =
0017368
Z = 1815461
63 I = 52
01534
XDOT = 3425
188383 Wp = 126
60531
YDOT = -3850
099001 meter/sec RA = 72
14997 deg
ZDOT = -5686
672036 TA = 33
52805
MA = 33
41825
Ha = 221
974 n
mi
Hp = 213
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10837770
30 X = -3248933
42
Y = -18481616
28 feet Y = -5669832
63 meter
Z = 5956238
94 Z = 1799547
70
XDOT = 11237
494694 XDOT = 3495
609142
YDOT = -12631
558403 feet/sec YDOT = -3811
402697 meter/sec
ZDOT = -18657
060487 ZDOT = -5669
862682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5705086
26 X = -1738910
29
Y = 20671321
87 feet Y = 6300618
91 meter
Z = 5886648
50 Z = 1794250
46
XDOT = -15470
109404 XDOT = -4715
289346
YDOT = 1047
995188 feet/sec YDOT = 319
428933 meter/sec
ZDOT = -18581
954664 ZDOT = -5663
779782
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 17233
49404665
00016717 00000-0 10270-3 0 9135
2 25544 51
6412 72
7672 0004776 165
4132 194
7160 15
54183652 31909
Satellite: ISS
Catalog Number: 25544
Epoch time: 17233
49404665 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 72
7672 deg
Eccentricity:
0004776
Arg of perigee: 165
4132 deg
Mean anomaly: 194
7160 deg
Mean motion: 15
54183652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3190
Checksum: 308
Coasting Arc #15 (Orbit 3204)
---------------------------------------
Vector Time (GMT): 2017/234/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2721870
79 A = 6789202
23 meter
Y = 6215705
07 meter E =
0009958
Z = -129047
16 I = 52
00784
XDOT = -4279
589240 Wp = 67
56843
YDOT = 1991
648507 meter/sec RA = 67
20240 deg
ZDOT = 6039
166545 TA = 291
04904
MA = 291
15551
Ha = 221
867 n
mi
Hp = 214
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8930022
28 X = 2652789
67
Y = 20392733
18 feet Y = 6245756
62 meter
Z = -423383
06 Z = -115993
57
XDOT = -14040
647113 XDOT = -4330
877086
YDOT = 6534
279880 feet/sec YDOT = 1943
504837 meter/sec
ZDOT = 19813
538534 ZDOT = 6018
253319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8074980
02 X = 2461253
91
Y = -20747251
48 feet Y = -6323762
25 meter
Z = -366567
43 Z = -111729
75
XDOT = 13135
940235 XDOT = 4003
834584
YDOT = 4789
247622 feet/sec YDOT = 1459
762675 meter/sec
ZDOT = 19720
552397 ZDOT = 6010
824371
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 17234
45855135
00016717 00000-0 10270-3 0 9145
2 25544 51
6400 67
9575 0004775 169
5266 190
5987 15
54168579 32055
Satellite: ISS
Catalog Number: 25544
Epoch time: 17234
45855135 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 67
9575 deg
Eccentricity:
0004775
Arg of perigee: 169
5266 deg
Mean anomaly: 190
5987 deg
Mean motion: 15
54168579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3205
Checksum: 344
Coasting Arc #16 (Orbit 3220)
---------------------------------------
Vector Time (GMT): 2017/235/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1897107
43 A = 6788116
71 meter
Y = -6309260
12 meter E =
0012304
Z = -1609634
82 I = 51
98955
XDOT = 5059
606139 Wp = 153
69635
YDOT = -57
888418 meter/sec RA = 62
25628 deg
ZDOT = -5763
835904 TA = 43
83496
MA = 43
73737
Ha = 221
812 n
mi
Hp = 214
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6224105
73 X = -1818595
91
Y = -20699672
32 feet Y = -6330036
01 meter
Z = -5280954
14 Z = -1618659
06
XDOT = 16599
757673 XDOT = 5087
874897
YDOT = -189
922631 feet/sec YDOT = -1
150851 meter/sec
ZDOT = -18910
222781 ZDOT = -5739
189610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9905668
98 X = -3019247
91
Y = 19201063
91 feet Y = 5852484
28 meter
Z = -5319893
80 Z = -1621503
63
XDOT = -10775
516918 XDOT = -3284
377557
YDOT = -10743
228248 feet/sec YDOT = -3274
535970 meter/sec
ZDOT = -18801
017603 ZDOT = -5730
550165
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 17235
48735500
00016717 00000-0 10270-3 0 9153
2 25544 51
6390 62
8286 0004833 173
4740 186
6476 15
54161433 32211
Satellite: ISS
Catalog Number: 25544
Epoch time: 17235
48735500 = yrday
fracday
Element set: 915
Inclination: 51
6390 deg
RA of node: 62
8286 deg
Eccentricity:
0004833
Arg of perigee: 173
4740 deg
Mean anomaly: 186
6476 deg
Mean motion: 15
54161433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3221
Checksum: 308
Coasting Arc #17 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2017/236/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 897056
50 A = 6784938
17 meter
Y = 5944066
85 meter E =
0013519
Z = 3139568
09 I = 51
96314
XDOT = -5652
907788 Wp = 106
41720
YDOT = -1736
448616 meter/sec RA = 57
30197 deg
ZDOT = 4881
669611 TA = 289
58176
MA = 289
72767
Ha = 221
638 n
mi
Hp = 214
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2943098
74 X = 815271
38
Y = 19501531
65 feet Y = 5953641
33 meter
Z = 10300420
26 Z = 3143726
51
XDOT = -18546
285394 XDOT = -5656
782726
YDOT = -5697
009896 feet/sec YDOT = -1799
684524 meter/sec
ZDOT = 16015
976415 ZDOT = 4854
200579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11183395
30 X = 3408698
89
Y = -16234031
73 feet Y = -4948132
87 meter
Z = 10317853
83 Z = 3144881
85
XDOT = 8586
860130 XDOT = 2617
274968
YDOT = 16061
368953 feet/sec YDOT = 4895
505257 meter/sec
ZDOT = 15894
569222 ZDOT = 4844
664699
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 17236
51615598
00016717 00000-0 10270-3 0 9163
2 25544 51
6389 57
6987 0004904 179
3807 180
7353 15
54197664 32378
Satellite: ISS
Catalog Number: 25544
Epoch time: 17236
51615598 = yrday
fracday
Element set: 916
Inclination: 51
6389 deg
RA of node: 57
6987 deg
Eccentricity:
0004904
Arg of perigee: 179
3807 deg
Mean anomaly: 180
7353 deg
Mean motion: 15
54197664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 355
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