[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 1st 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 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
212/23:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 212
2
216/02:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
4
219/05:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
3
221/12:26:04
909 -0
5 0
8 0
8
N/A 0
6 -0
0 222
8
000/00:02:05
819 0
0 -0
0 213
0
225/21:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 213
4
Coasting Arc #1 (Orbit 2863)
---------------------------------------
Vector Time (GMT): 2017/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6763381
54 A = 6788985
58 meter
Y = -511068
40 meter E =
0017130
Z = 88219
21 I = 51
67606
XDOT = 447
762463 Wp = 118
58990
YDOT = 4735
672301 meter/sec RA = 176
26777 deg
ZDOT = -6015
419729 TA = 60
46023
MA = 60
28956
Ha = 223
067 n
mi
Hp = 212
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22189572
00 X = 6768165
26
Y = -1676733
61 feet Y = -435408
93 meter
Z = 289433
09 Z = 121084
96
XDOT = 1469
036953 XDOT = 423
993377
YDOT = 15536
982615 feet/sec YDOT = 4740
546799 meter/sec
ZDOT = -19735
629033 ZDOT = -6013
302217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15105932
23 X = -4604288
14
Y = -16336891
38 feet Y = -4979484
49 meter
Z = 434860
77 Z = 132545
56
XDOT = 9983
921852 XDOT = 3043
099380
YDOT = -9807
783415 feet/sec YDOT = -2989
412385 meter/sec
ZDOT = -19726
932798 ZDOT = -6012
769117
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 17212
53246702
00016717 00000-0 10270-3 0 9009
2 25544 51
6375 177
2693 0006113 86
4382 273
7470 15
54244337 28644
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
53246702 = yrday
fracday
Element set: 900
Inclination: 51
6375 deg
RA of node: 177
2693 deg
Eccentricity:
0006113
Arg of perigee: 86
4382 deg
Mean anomaly: 273
7470 deg
Mean motion: 15
54244337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2864
Checksum: 307
Coasting Arc #2 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2660820
23 A = 6779405
60 meter
Y = 4060984
45 meter E =
0017151
Z = -4747873
11 I = 51
65958
XDOT = -7012
758947 Wp = 103
61018
YDOT = -1416
199232 meter/sec RA = 173
89711 deg
ZDOT = 2723
141683 TA = 193
33831
MA = 193
38371
Ha = 223
066 n
mi
Hp = 212
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8729725
17 X = -2682970
82
Y = 13323439
81 feet Y = 4031105
70 meter
Z = -15577011
52 Z = -4760852
08
XDOT = -23007
739328 XDOT = -7009
629015
YDOT = -4646
322941 feet/sec YDOT = -1494
603278 meter/sec
ZDOT = 8934
191874 ZDOT = 2689
083683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15824935
39 X = -4823440
31
Y = -1218153
65 feet Y = -371293
23 meter
Z = -15634991
50 Z = -4765545
41
XDOT = -7022
382949 XDOT = -2140
422323
YDOT = -21330
147659 feet/sec YDOT = -6501
429006 meter/sec
ZDOT = 8783
754462 ZDOT = 2677
288360
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 17212
98254884
00016717 00000-0 10270-3 0 9019
2 25544 51
6376 175
0224 0006150 93
0001 267
1855 15
54240316 28719
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
98254884 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 175
0224 deg
Eccentricity:
0006150
Arg of perigee: 93
0001 deg
Mean anomaly: 267
1855 deg
Mean motion: 15
54240316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 292
Coasting Arc #3 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2017/213/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4233255
34 A = 6783182
28 meter
Y = -3794910
35 meter E =
0017732
Z = 3684879
57 I = 51
70463
XDOT = 5885
386547 Wp = 89
15935
YDOT = 2336
108579 meter/sec RA = 168
90864 deg
ZDOT = -4337
103271 TA = 46
97139
MA = 46
82299
Ha = 223
004 n
mi
Hp = 212
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13888633
00 X = 4257477
23
Y = -12450493
28 feet Y = -3747435
97 meter
Z = 12089499
90 Z = 3705501
87
XDOT = 19309
010982 XDOT = 5879
893488
YDOT = 7664
398225 feet/sec YDOT = 2401
892475 meter/sec
ZDOT = -14229
341440 ZDOT = -4308
527359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17636575
36 X = 5375628
17
Y = 5884978
66 feet Y = 1793741
50 meter
Z = 12181262
37 Z = 3712848
77
XDOT = 3317
459891 XDOT = 1011
161775
YDOT = 19373
315194 feet/sec YDOT = 5904
986471 meter/sec
ZDOT = -14103
264999 ZDOT = -4298
675172
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 17214
01130449
00016717 00000-0 10270-3 0 9026
2 25544 51
6377 169
8919 0006123 96
9685 263
2165 15
54229427 28870
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
01130449 = yrday
fracday
Element set: 902
Inclination: 51
6377 deg
RA of node: 169
8919 deg
Eccentricity:
0006123
Arg of perigee: 96
9685 deg
Mean anomaly: 263
2165 deg
Mean motion: 15
54229427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 330
Coasting Arc #4 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2017/214/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5411586
47 A = 6786723
60 meter
Y = 3415396
41 meter E =
0010671
Z = -2263543
27 I = 51
74968
XDOT = -4308
815952 Wp = 73
24499
YDOT = -3230
822632 meter/sec RA = 163
93472 deg
ZDOT = 5450
704878 TA = 261
62728
MA = 261
74826
Ha = 223
023 n
mi
Hp = 212
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17754548
78 X = -5438381
07
Y = 11205368
79 feet Y = 3354730
68 meter
Z = -7426323
05 Z = -2289895
69
XDOT = -14136
535277 XDOT = -4298
844374
YDOT = -10599
811784 feet/sec YDOT = -3278
951298 meter/sec
ZDOT = 17882
890021 ZDOT = 5429
798237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18640054
74 X = -5681488
69
Y = -9569748
28 feet Y = -2916859
28 meter
Z = -7543397
32 Z = -2299227
50
XDOT = 1200
739710 XDOT = 365
985464
YDOT = -16300
765614 feet/sec YDOT = -4968
473359 meter/sec
ZDOT = 17790
854377 ZDOT = 5422
652414
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 17214
97575923
00016717 00000-0 10270-3 0 9032
2 25544 51
6389 165
0837 0006173 99
5196 260
6654 15
54251675 29023
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
97575923 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 165
0837 deg
Eccentricity:
0006173
Arg of perigee: 99
5196 deg
Mean anomaly: 260
6654 deg
Mean motion: 15
54251675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 339
Coasting Arc #5 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2017/215/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6144562
73 A = 6788813
19 meter
Y = -2817251
85 meter E =
0018767
Z = 539435
06 I = 51
78692
XDOT = 2429
406175 Wp = 121
26537
YDOT = 4123
043858 meter/sec RA = 158
97092 deg
ZDOT = -5995
506753 TA = 52
92378
MA = 52
75235
Ha = 223
008 n
mi
Hp = 212
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20159326
55 X = 6172989
03
Y = -9242952
27 feet Y = -2748380
27 meter
Z = 1769800
07 Z = 569351
93
XDOT = 7970
492699 XDOT = 2412
243504
YDOT = 13527
046779 feet/sec YDOT = 4150
115530 meter/sec
ZDOT = -19670
297745 ZDOT = -5983
747037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18403969
62 X = 5609529
94
Y = 12354630
70 feet Y = 3765691
44 meter
Z = 1902579
44 Z = 579906
21
XDOT = -6403
784218 XDOT = -1951
873430
YDOT = 12628
373903 feet/sec YDOT = 3849
128366 meter/sec
ZDOT = -19618
851144 ZDOT = -5979
825829
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 17216
00450939
00016717 00000-0 10270-3 0 9048
2 25544 51
6381 159
9541 0006096 103
6726 256
5106 15
54258253 29181
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
00450939 = yrday
fracday
Element set: 904
Inclination: 51
6381 deg
RA of node: 159
9541 deg
Eccentricity:
0006096
Arg of perigee: 103
6726 deg
Mean anomaly: 256
5106 deg
Mean motion: 15
54258253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2918
Checksum: 313
Coasting Arc #6 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2017/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 847417
93 A = 6777144
88 meter
Y = 4160104
82 meter E =
0020548
Z = -5300378
14 I = 51
75409
XDOT = -7259
315957 Wp = 97
54968
YDOT = 2330
322235 meter/sec RA = 158
24288 deg
ZDOT = 667
977104 TA = 178
83329
MA = 178
82849
Ha = 222
952 n
mi
Hp = 212
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2780242
56 X = 826581
85
Y = 13648637
87 feet Y = 4169465
05 meter
Z = -17389692
05 Z = -5296312
05
XDOT = -23816
653403 XDOT = -7288
079373
YDOT = 7645
414158 feet/sec YDOT = 2248
982765 meter/sec
ZDOT = 2191
525932 ZDOT = 632
644345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1573303
77 X = 479542
99
Y = 13861622
43 feet Y = 4225022
52 meter
Z = -17372293
84 Z = -5295075
16
XDOT = -23442
551030 XDOT = -7145
289554
YDOT = 5212
642947 feet/sec YDOT = 1588
813570 meter/sec
ZDOT = 2034
848146 ZDOT = 620
221715
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 17216
13310209
00016717 00000-0 10270-3 0 9058
2 25544 51
6400 159
3160 0005915 102
8605 257
3209 15
54247010 29205
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
13310209 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 159
3160 deg
Eccentricity:
0005915
Arg of perigee: 102
8605 deg
Mean anomaly: 257
3209 deg
Mean motion: 15
54247010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 267
Coasting Arc #7 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2017/217/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 898480
52 A = 6779000
67 meter
Y = -4687676
79 meter E =
0012068
Z = 4804334
56 I = 51
79193
XDOT = 7107
836650 Wp = 81
18220
YDOT = -1299
408024 meter/sec RA = 153
25279 deg
ZDOT = -2589
777178 TA = 34
28530
MA = 34
20746
Ha = 222
819 n
mi
Hp = 212
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2947770
73 X = 927495
86
Y = -15379517
04 feet Y = -4677467
41 meter
Z = 15762252
50 Z = 4808769
24
XDOT = 23319
674047 XDOT = 7134
418371
YDOT = -4263
149686 feet/sec YDOT = -1219
774591 meter/sec
ZDOT = -8496
644286 ZDOT = -2555
185578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4045423
69 X = 1233045
14
Y = -15106726
32 feet Y = -4604530
18 meter
Z = 15782549
46 Z = 4810521
08
XDOT = 22536
206588 XDOT = 6869
035768
YDOT = -2706
816900 feet/sec YDOT = -825
037791 meter/sec
ZDOT = -8343
370845 ZDOT = -2543
059433
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 17217
16184816
00016717 00000-0 10270-3 0 9066
2 25544 51
6410 154
1864 0005813 106
4184 253
7604 15
54295615 29369
Satellite: ISS
Catalog Number: 25544
Epoch time: 17217
16184816 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 154
1864 deg
Eccentricity:
0005813
Arg of perigee: 106
4184 deg
Mean anomaly: 253
7604 deg
Mean motion: 15
54295615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 309
Coasting Arc #8 (Orbit 2950)
---------------------------------------
Vector Time (GMT): 2017/218/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2460587
64 A = 6782641
61 meter
Y = 5048096
09 meter E =
0012196
Z = -3816578
80 I = 51
83235
XDOT = -6395
051667 Wp = 107
14222
YDOT = 61
484053 meter/sec RA = 148
27412 deg
ZDOT = 4211
887294 TA = 207
21966
MA = 207
28364
Ha = 222
889 n
mi
Hp = 212
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8072794
11 X = -2498315
19
Y = 16561995
04 feet Y = 5020369
35 meter
Z = -12521583
98 Z = -3828622
75
XDOT = -20981
140641 XDOT = -6415
722808
YDOT = 201
719333 feet/sec YDOT = -10
145535 meter/sec
ZDOT = 13818
527866 ZDOT = 4180
772490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8994107
05 X = -2741403
83
Y = 16038068
83 feet Y = 4888403
38 meter
Z = -12575616
74 Z = -3833047
98
XDOT = -19874
263481 XDOT = -6057
675509
YDOT = -437
665899 feet/sec YDOT = -133
400566 meter/sec
ZDOT = 13680
799534 ZDOT = 4169
907698
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 17218
12629660
00016717 00000-0 10270-3 0 9075
2 25544 51
6406 149
3785 0006022 109
2318 250
9487 15
54289437 29515
Satellite: ISS
Catalog Number: 25544
Epoch time: 17218
12629660 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 149
3785 deg
Eccentricity:
0006022
Arg of perigee: 109
2318 deg
Mean anomaly: 250
9487 deg
Mean motion: 15
54289437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2951
Checksum: 324
Coasting Arc #9 (Orbit 2966)
---------------------------------------
Vector Time (GMT): 2017/219/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3759030
95 A = 6786426
20 meter
Y = -5118077
12 meter E =
0019704
Z = 2367105
26 I = 51
87233
XDOT = 5275
236001 Wp = 108
16628
YDOT = 1360
157017 meter/sec RA = 143
30789 deg
ZDOT = -5405
516760 TA = 45
47300
MA = 45
31220
Ha = 222
825 n
mi
Hp = 212
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12332778
72 X = 3804485
27
Y = -16791591
59 feet Y = -5075787
00 meter
Z = 7766093
38 Z = 2385475
34
XDOT = 17307
204727 XDOT = 5285
891115
YDOT = 4462
457405 feet/sec YDOT = 1419
208032 meter/sec
ZDOT = -17734
635040 ZDOT = -5379
865900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13013914
64 X = 3966641
18
Y = -16229965
43 feet Y = -4946893
46 meter
Z = 7848148
39 Z = 2392115
63
XDOT = 16024
602039 XDOT = 4884
298701
YDOT = 4279
925477 feet/sec YDOT = 1304
521285 meter/sec
ZDOT = -17621
281030 ZDOT = -5370
966458
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 17219
15503780
00016717 00000-0 10270-3 0 9084
2 25544 51
6407 144
2496 0005940 111
5907 248
5879 15
54293591 29678
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
15503780 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 144
2496 deg
Eccentricity:
0005940
Arg of perigee: 111
5907 deg
Mean anomaly: 248
5879 deg
Mean motion: 15
54293591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2967
Checksum: 336
Coasting Arc #10 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2017/219/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -125148
36 A = 6778787
20 meter
Y = -4708744
04 meter E =
0011786
Z = 4865228
48 I = 51
84907
XDOT = 6747
082336 Wp = 83
76398
YDOT = -2718
448930 meter/sec RA = 142
70614 deg
ZDOT = -2451
124767 TA = 30
22778
MA = 30
15984
Ha = 222
959 n
mi
Hp = 212
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -410591
74 X = -96117
05
Y = -15448635
31 feet Y = -4709981
35 meter
Z = 15962035
70 Z = 4864690
94
XDOT = 22136
096903 XDOT = 6788
885415
YDOT = -8918
795703 feet/sec YDOT = -2642
764665 meter/sec
ZDOT = -8041
747922 ZDOT = -2418
248749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10587924
19 X = -3227199
29
Y = -11259623
91 feet Y = -3431933
37 meter
Z = 15960333
12 Z = 4864709
53
XDOT = 9950
519773 XDOT = 3032
918427
YDOT = -20578
569263 feet/sec YDOT = -6272
347911 meter/sec
ZDOT = -7895
821739 ZDOT = -2406
646466
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 17219
28363025
00016717 00000-0 10270-3 0 9095
2 25544 51
6398 143
6092 0006152 110
8192 249
3620 15
54291775 29693
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
28363025 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 143
6092 deg
Eccentricity:
0006152
Arg of perigee: 110
8192 deg
Mean anomaly: 249
3620 deg
Mean motion: 15
54291775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 322
Coasting Arc #11 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2017/220/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1358209
41 A = 6782414
71 meter
Y = 5381497
88 meter E =
0012583
Z = -3911882
64 I = 51
88742
XDOT = -6313
217701 Wp = 110
34420
YDOT = 1386
282567 meter/sec RA = 137
73052 deg
ZDOT = 4105
466542 TA = 202
58416
MA = 202
63959
Ha = 222
907 n
mi
Hp = 212
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4456067
62 X = -1399284
19
Y = 17655832
94 feet Y = 5366079
83 meter
Z = -12834260
62 Z = -3918579
97
XDOT = -20712
656500 XDOT = -6348
192199
YDOT = 4548
171150 feet/sec YDOT = 1315
488280 meter/sec
ZDOT = 13469
378420 ZDOT = 4074
714594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8652343
86 X = 2637234
41
Y = 15998124
72 feet Y = 4876228
41 meter
Z = -12864687
03 Z = -3921156
61
XDOT = -11151
864567 XDOT = -3399
088320
YDOT = 16735
978688 feet/sec YDOT = 5101
126304 meter/sec
ZDOT = 13333
031119 ZDOT = 4063
907885
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 17220
24807244
00016717 00000-0 10270-3 0 9101
2 25544 51
6409 138
8013 0006057 114
1358 246
0429 15
54268613 29843
Satellite: ISS
Catalog Number: 25544
Epoch time: 17220
24807244 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 138
8013 deg
Eccentricity:
0006057
Arg of perigee: 114
1358 deg
Mean anomaly: 246
0429 deg
Mean motion: 15
54268613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 298
Coasting Arc #12 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2017/221/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 917506
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2641739
48 A = 6786171
26 meter
Y = -5724027
37 meter E =
0019683
Z = 2485512
85 I = 51
92284
XDOT = 5506
872572 Wp = 108
49593
YDOT = 209
620313 meter/sec RA = 132
76630 deg
ZDOT = -5341
828842 TA = 43
73262
MA = 43
57686
Ha = 222
837 n
mi
Hp = 212
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8667124
27 X = 2693477
56
Y = -18779617
35 feet Y = -5694196
34 meter
Z = 8154569
73 Z = 2498471
06
XDOT = 18067
167231 XDOT = 5530
066734
YDOT = 687
730685 feet/sec YDOT = 271
331549 meter/sec
ZDOT = -17525
685177 ZDOT = -5315
022360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6610323
20 X = -2014826
51
Y = -19574066
52 feet Y = -5966175
48 meter
Z = 8212772
10 Z = 2503252
94
XDOT = 12275
276708 XDOT = 3741
504341
YDOT = -11487
858897 feet/sec YDOT = -3501
499392 meter/sec
ZDOT = -17407
024477 ZDOT = -5305
661061
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
27680581
00016717 00000-0 10270-3 0 9119
2 25544 51
6400 133
6715 0006071 116
4447 243
7329 15
54301652 30000
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
27680581 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 133
6715 deg
Eccentricity:
0006071
Arg of perigee: 116
4447 deg
Mean anomaly: 243
7329 deg
Mean motion: 15
54301652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 273
Coasting Arc #13 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2017/221/12:27:07
819
Vector Time (MET): N/A
Weight (LBS) : 917421
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2682510
74 A = 6777424
37 meter
Y = 3262089
96 meter E =
0019616
Z = -5317502
99 I = 51
90039
XDOT = -5387
010359 Wp = 101
50748
YDOT = 5404
522300 meter/sec RA = 131
39626 deg
ZDOT = 595
950697 TA = 174
18218
MA = 174
15936
Ha = 222
791 n
mi
Hp = 212
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8800888
27 X = 2671663
15
Y = 10702394
88 feet Y = 3292026
90 meter
Z = -17445875
94 Z = -5304498
82
XDOT = -17673
918501 XDOT = -5449
939567
YDOT = 17731
372374 feet/sec YDOT = 5343
929235 meter/sec
ZDOT = 1955
218822 ZDOT = 569
629863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -948740
81 X = -289176
20
Y = -13895542
74 feet Y = -4235361
43 meter
Z = -17388768
23 Z = -5300096
56
XDOT = 23710
114093 XDOT = 7226
842775
YDOT = -3926
792828 feet/sec YDOT = -1196
886454 meter/sec
ZDOT = 1837
893418 ZDOT = 560
189914
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
53399028
00016717 00000-0 10270-3 0 9122
2 25544 51
6422 132
3902 0005307 120
5126 239
6551 15
54142568 30043
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
53399028 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 132
3902 deg
Eccentricity:
0005307
Arg of perigee: 120
5126 deg
Mean anomaly: 239
6551 deg
Mean motion: 15
54142568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 279
Coasting Arc #14 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2017/222/12:27:07
819
Vector Time (MET): N/A
Weight (LBS) : 917421
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1411641
06 A = 6779197
26 meter
Y = -4500358
95 meter E =
0010345
Z = 4860785
50 I = 51
92668
XDOT = 5718
310179 Wp = 86
76238
YDOT = -4478
208169 meter/sec RA = 126
41791 deg
ZDOT = -2480
367280 TA = 27
50282
MA = 27
44811
Ha = 222
737 n
mi
Hp = 212
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4631368
31 X = -1384822
86
Y = -14764957
18 feet Y = -4515994
80 meter
Z = 15947459
00 Z = 4853993
56
XDOT = 18760
860167 XDOT = 5780
009903
YDOT = -14692
284020 feet/sec YDOT = -4413
917218 meter/sec
ZDOT = -8137
687925 ZDOT = -2452
439984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4564548
11 X = -1391274
27
Y = 14817420
20 feet Y = 4516349
68 meter
Z = 15918038
22 Z = 4851818
05
XDOT = -22756
301233 XDOT = -6936
120616
YDOT = 1616
472989 feet/sec YDOT = 492
700967 meter/sec
ZDOT = -8013
370935 ZDOT = -2442
475461
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
56281955
00016717 00000-0 10270-3 0 9136
2 25544 51
6413 127
2623 0005171 124
3481 235
8161 15
54170389 30206
Satellite: ISS
Catalog Number: 25544
Epoch time: 17222
56281955 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 127
2623 deg
Eccentricity:
0005171
Arg of perigee: 124
3481 deg
Mean anomaly: 235
8161 deg
Mean motion: 15
54170389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 286
Coasting Arc #15 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2017/223/12:27:07
819
Vector Time (MET): N/A
Weight (LBS) : 917421
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 217302
57 A = 6782757
72 meter
Y = 5534969
54 meter E =
0011465
Z = -3927333
31 I = 51
95748
XDOT = -5666
420760 Wp = 116
35947
YDOT = 3124
716356 meter/sec RA = 121
44741 deg
ZDOT = 4094
563514 TA = 196
38381
MA = 196
42089
Ha = 222
638 n
mi
Hp = 213
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 712934
94 X = 174469
74
Y = 18159348
89 feet Y = 5537159
94 meter
Z = -12884951
81 Z = -3926381
97
XDOT = -18590
619290 XDOT = -5720
830155
YDOT = 10251
694083 feet/sec YDOT = 3061
046508 meter/sec
ZDOT = 13433
607330 ZDOT = 4066
905891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9471495
97 X = 2886911
97
Y = -15512853
91 feet Y = -4728317
87 meter
Z = -12881550
34 Z = -3926296
54
XDOT = 20089
706971 XDOT = 6123
342685
YDOT = 1224
707119 feet/sec YDOT = 373
290730 meter/sec
ZDOT = 13310
670452 ZDOT = 4057
092354
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
52734498
00016717 00000-0 10270-3 0 9149
2 25544 51
6419 122
4540 0005107 128
8367 231
3243 15
54145007 30355
Satellite: ISS
Catalog Number: 25544
Epoch time: 17223
52734498 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 122
4540 deg
Eccentricity:
0005107
Arg of perigee: 128
8367 deg
Mean anomaly: 231
3243 deg
Mean motion: 15
54145007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 288
Coasting Arc #16 (Orbit 3050)
---------------------------------------
Vector Time (GMT): 2017/224/12:27:07
819
Vector Time (MET): N/A
Weight (LBS) : 917421
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 875223
97 A = 6786555
18 meter
Y = -6219036
94 meter E =
0018468
Z = 2546429
56 I = 51
98614
XDOT = 5351
909266 Wp = 111
63978
YDOT = -1431
408657 meter/sec RA = 116
48873 deg
ZDOT = -5311
204491 TA = 39
87555
MA = 39
74001
Ha = 222
691 n
mi
Hp = 213
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2871469
73 X = 932332
64
Y = -20403664
50 feet Y = -6208930
18 meter
Z = 8354427
68 Z = 2550820
02
XDOT = 17558
757434 XDOT = 5393
316894
YDOT = -4696
222628 feet/sec YDOT = -1371
328633 meter/sec
ZDOT = -17425
211586 ZDOT = -5285
106180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13456857
16 X = -4101650
06
Y = 15592535
78 feet Y = 4752604
91 meter
Z = 8374792
44 Z = 2552636
74
XDOT = -16249
377746 XDOT = -4952
810337
YDOT = -4684
346156 feet/sec YDOT = -1427
788708 meter/sec
ZDOT = -17309
419900 ZDOT = -5275
911186
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
55616792
00016717 00000-0 10270-3 0 9150
2 25544 51
6419 117
3253 0005249 131
6418 228
5185 15
54133025 30513
Satellite: ISS
Catalog Number: 25544
Epoch time: 17224
55616792 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 117
3253 deg
Eccentricity:
0005249
Arg of perigee: 131
6418 deg
Mean anomaly: 228
5185 deg
Mean motion: 15
54133025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 297
Coasting Arc #17 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2017/225/12:27:07
819
Vector Time (MET): N/A
Weight (LBS) : 917421
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1770833
01 A = 6788818
07 meter
Y = 6484562
72 meter E =
0010557
Z = -939118
50 I = 52
00733
XDOT = -4812
143554 Wp = 67
66108
YDOT = -461
073838 meter/sec RA = 111
53893 deg
ZDOT = 5947
382726 TA = 282
22714
MA = 282
34535
Ha = 222
513 n
mi
Hp = 213
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5809819
59 X = -1838651
74
Y = 21274812
07 feet Y = 6464380
84 meter
Z = -3081097
44 Z = -947885
51
XDOT = -15787
872551 XDOT = -4835
519369
YDOT = -1512
709443 feet/sec YDOT = -515
017039 meter/sec
ZDOT = 19512
410517 ZDOT = 5923
950188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16170366
87 X = 4928727
82
Y = -14988129
53 feet Y = -4568381
88 meter
Z = -3120897
67 Z = -951249
61
XDOT = 11611
854374 XDOT = 3539
293213
YDOT = 8524
941902 feet/sec YDOT = 2598
402292 meter/sec
ZDOT = 19408
700347 ZDOT = 5915
771866
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
52068435
00016717 00000-0 10270-3 0 9164
2 25544 51
6414 112
5167 0005093 135
7896 224
3664 15
54170069 30662
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
52068435 = yrday
fracday
Element set: 916
Inclination: 51
6414 deg
RA of node: 112
5167 deg
Eccentricity:
0005093
Arg of perigee: 135
7896 deg
Mean anomaly: 224
3664 deg
Mean motion: 15
54170069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 310
Coasting Arc #18 (Orbit 3071)
---------------------------------------
Vector Time (GMT): 2017/225/21:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 917421
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4373575
45 A = 6778026
84 meter
Y = -174430
57 meter E =
0016969
Z = -5189422
14 I = 51
97496
XDOT = -1432
029326 Wp = 95
53836
YDOT = 7378
075241 meter/sec RA = 109
72513 deg
ZDOT = -1460
580574 TA = 160
47958
MA = 160
41453
Ha = 222
625 n
mi
Hp = 213
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14349000
81 X = 4400408
48
Y = -572278
76 feet Y = -125372
35 meter
Z = -17025663
18 Z = -5168111
58
XDOT = -4698
258943 XDOT = -1507
331733
YDOT = 24206
283600 feet/sec YDOT = 7361
640241 meter/sec
ZDOT = -4791
931016 ZDOT = -1467
719960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3385374
59 X = 1031862
18
Y = 14070053
90 feet Y = 4288552
43 meter
Z = -16931253
82 Z = -5160646
16
XDOT = -23625
184120 XDOT = -7200
956120
YDOT = -98
773959 feet/sec YDOT = -30
106303 meter/sec
ZDOT = -4824
662956 ZDOT = -1470
557269
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
90649095
00016717 00000-0 10270-3 0 9174
2 25544 51
6411 110
5895 0005445 141
4314 218
7229 15
54143626 30725
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
90649095 = yrday
fracday
Element set: 917
Inclination: 51
6411 deg
RA of node: 110
5895 deg
Eccentricity:
0005445
Arg of perigee: 141
4314 deg
Mean anomaly: 218
7229 deg
Mean motion: 15
54143626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3072
Checksum: 303
Coasting Arc #19 (Orbit 3087)
---------------------------------------
Vector Time (GMT): 2017/226/21:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 917421
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3885095
69 A = 6777213
83 meter
Y = -1576702
05 meter E =
0006615
Z = 5319460
56 I = 51
98355
XDOT = 2310
157284 Wp = 121
80676
YDOT = -7301
836070 meter/sec RA = 104
74791 deg
ZDOT = -480
007826 TA = 332
72990
MA = 332
76462
Ha = 222
594 n
mi
Hp = 213
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12746376
94 X = -3893015
08
Y = -5172906
98 feet Y = -1620192
08 meter
Z = 17452298
44 Z = 5300568
82
XDOT = 7579
256180 XDOT = 2393
968286
YDOT = -23956
155084 feet/sec YDOT = -7275
533706 meter/sec
ZDOT = -1574
828824 ZDOT = -468
582236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2326832
80 X = 709218
64
Y = -13664560
36 feet Y = -4164958
00 meter
Z = 17368864
44 Z = 5294029
88
XDOT = 24024
378777 XDOT = 7322
630651
YDOT = 2167
326699 feet/sec YDOT = 660
601178 meter/sec
ZDOT = -1523
106080 ZDOT = -464
242733
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
93530432
00016717 00000-0 10270-3 0 9183
2 25544 51
6417 105
4601 0005372 145
1109 215
0397 15
54196725 30882
Satellite: ISS
Catalog Number: 25544
Epoch time: 17226
93530432 = yrday
fracday
Element set: 918
Inclination: 51
6417 deg
RA of node: 105
4601 deg
Eccentricity:
0005372
Arg of perigee: 145
1109 deg
Mean anomaly: 215
0397 deg
Mean motion: 15
54196725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3088
Checksum: 299
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