[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 27th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
182/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
8
183/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
9
Coasting Arc #1 (Orbit 2320)
---------------------------------------
Vector Time (GMT): 2017/177/13:23:19
736
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6252152
92 A = 6786817
26 meter
Y = 970944
44 meter E =
0012679
Z = 2434096
17 I = 51
59689
XDOT = -2819
352646 Wp = 54
40496
YDOT = 4729
855934 meter/sec RA = 351
07215 deg
ZDOT = 5342
662198 TA = 332
86466
MA = 332
93087
Ha = 220
629 n
mi
Hp = 215
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20512312
73 X = 6229007
40
Y = 3185513
27 feet Y = 1040730
51 meter
Z = 7985879
81 Z = 2464410
73
XDOT = -9249
844639 XDOT = -2897
985304
YDOT = 15517
900047 feet/sec YDOT = 4697
887623 meter/sec
ZDOT = 17528
419285 ZDOT = 5328
776494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5699614
71 X = -1737242
56
Y = -19906388
13 feet Y = -6067467
10 meter
Z = 8119534
99 Z = 2474834
26
XDOT = 16565
490311 XDOT = 5049
161447
YDOT = 2397
407514 feet/sec YDOT = 730
729810 meter/sec
ZDOT = 17466
179675 ZDOT = 5323
691565
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17177
61722135
00016717 00000-0 10270-3 0 9007
2 25544 51
6396 351
3261 0004725 322
6265 37
4559 15
54099774 23219
Satellite: ISS
Catalog Number: 25544
Epoch time: 17177
61722135 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 351
3261 deg
Eccentricity:
0004725
Arg of perigee: 322
6265 deg
Mean anomaly: 37
4559 deg
Mean motion: 15
54099774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2321
Checksum: 310
Coasting Arc #2 (Orbit 2335)
---------------------------------------
Vector Time (GMT): 2017/178/13:23:19
736
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5323927
03 A = 6783178
40 meter
Y = -1795913
65 meter E =
0006641
Z = -3808051
34 I = 51
55319
XDOT = 4528
684411 Wp = 31
49855
YDOT = -4545
237907 meter/sec RA = 346
08774 deg
ZDOT = -4185
610924 TA = 194
25540
MA = 194
27415
Ha = 220
912 n
mi
Hp = 215
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17466952
19 X = -5284951
56
Y = -5892105
16 feet Y = -1855231
05 meter
Z = -12493606
76 Z = -3833818
53
XDOT = 14857
888489 XDOT = 4599
505253
YDOT = -14912
197856 feet/sec YDOT = -4494
198625 meter/sec
ZDOT = -13732
319304 ZDOT = -4163
440774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2265384
62 X = 690489
23
Y = 18216273
24 feet Y = 5552320
08 meter
Z = -12607020
01 Z = -3842619
70
XDOT = -18605
837784 XDOT = -5671
059357
YDOT = -7126
628824 feet/sec YDOT = -2172
196466 meter/sec
ZDOT = -13633
547339 ZDOT = -4155
505229
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17178
58177938
00016717 00000-0 10270-3 0 9010
2 25544 51
6401 346
5185 0004780 328
3833 31
7032 15
54093837 23365
Satellite: ISS
Catalog Number: 25544
Epoch time: 17178
58177938 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 346
5185 deg
Eccentricity:
0004780
Arg of perigee: 328
3833 deg
Mean anomaly: 31
7032 deg
Mean motion: 15
54093837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2336
Checksum: 319
Coasting Arc #3 (Orbit 2351)
---------------------------------------
Vector Time (GMT): 2017/179/13:23:19
736
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4021271
97 A = 6779573
67 meter
Y = 2636397
81 meter E =
0004065
Z = 4775532
78 I = 51
50977
XDOT = -5860
318163 Wp = 81
41356
YDOT = 4203
587240 meter/sec RA = 341
09061 deg
ZDOT = 2612
766773 TA = 342
78331
MA = 342
79709
Ha = 220
827 n
mi
Hp = 215
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13193149
51 X = 3968295
29
Y = 8649599
13 feet Y = 2681069
74 meter
Z = 15667758
45 Z = 4794938
22
XDOT = -19226
765625 XDOT = -5919
579619
YDOT = 13791
296718 feet/sec YDOT = 4137
721590 meter/sec
ZDOT = 8572
069464 ZDOT = 2584
155960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1819455
52 X = 554570
04
Y = -15584881
77 feet Y = -4750271
96 meter
Z = 15752918
97 Z = 4801489
70
XDOT = 19868
214303 XDOT = 6055
831720
YDOT = 10859
824497 feet/sec YDOT = 3310
074507 meter/sec
ZDOT = 8444
940096 ZDOT = 2574
017741
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17179
61063834
00016717 00000-0 10270-3 0 9025
2 25544 51
6399 341
3900 0004789 330
2205 29
8674 15
54116684 23527
Satellite: ISS
Catalog Number: 25544
Epoch time: 17179
61063834 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 341
3900 deg
Eccentricity:
0004789
Arg of perigee: 330
2205 deg
Mean anomaly: 29
8674 deg
Mean motion: 15
54116684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2352
Checksum: 316
Coasting Arc #4 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2017/180/13:23:19
736
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2497485
57 A = 6777588
41 meter
Y = -3478231
57 meter E =
0013804
Z = -5265068
90 I = 51
47312
XDOT = 6695
487925 Wp = 64
75063
YDOT = -3638
335607 meter/sec RA = 336
08445 deg
ZDOT = -768
247981 TA = 197
85830
MA = 197
90685
Ha = 221
078 n
mi
Hp = 215
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8193850
29 X = -2432830
57
Y = -11411520
90 feet Y = -3505798
21 meter
Z = -17273848
11 Z = -5277044
05
XDOT = 21966
823902 XDOT = 6739
406867
YDOT = -11936
796611 feet/sec YDOT = -3563
216492 meter/sec
ZDOT = -2520
498624 ZDOT = -735
617303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6330063
28 X = -1929403
29
Y = 12469417
00 feet Y = 3800678
30 meter
Z = -17326042
79 Z = -5280977
84
XDOT = -19899
096343 XDOT = -6065
244565
YDOT = -13421
794290 feet/sec YDOT = -4090
962900 meter/sec
ZDOT = -2375
744958 ZDOT = -724
127063
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17180
57519348
00016717 00000-0 10270-3 0 9039
2 25544 51
6406 336
5832 0004801 335
4231 24
6692 15
54108981 23677
Satellite: ISS
Catalog Number: 25544
Epoch time: 17180
57519348 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 336
5832 deg
Eccentricity:
0004801
Arg of perigee: 335
4231 deg
Mean anomaly: 24
6692 deg
Mean motion: 15
54108981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2367
Checksum: 310
Coasting Arc #5 (Orbit 2382)
---------------------------------------
Vector Time (GMT): 2017/181/13:23:19
736
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 852082
68 A = 6777975
80 meter
Y = 4263679
36 meter E =
0007053
Z = 5199334
17 I = 51
44533
XDOT = -7032
592801 Wp = 13
70258
YDOT = 2829
649117 meter/sec RA = 331
07155 deg
ZDOT = -1160
868304 TA = 87
49893
MA = 87
41819
Ha = 221
288 n
mi
Hp = 215
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2795546
84 X = 779086
11
Y = 13988449
35 feet Y = 4272799
38 meter
Z = 17058182
97 Z = 5203296
33
XDOT = -23072
811026 XDOT = -7058
073114
YDOT = 9283
625711 feet/sec YDOT = 2750
863515 meter/sec
ZDOT = -3808
623046 ZDOT = -1195
091916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10970990
53 X = 3343957
91
Y = -9086256
96 feet Y = -2769491
12 meter
Z = 17074855
92 Z = 5204416
09
XDOT = 18567
821745 XDOT = 5659
472068
YDOT = 14933
833423 feet/sec YDOT = 4551
832427 meter/sec
ZDOT = -3960
240336 ZDOT = -1207
081254
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17181
60404942
00016717 00000-0 10270-3 0 9048
2 25544 51
6413 331
4538 0004852 340
5272 19
5695 15
54079544 23836
Satellite: ISS
Catalog Number: 25544
Epoch time: 17181
60404942 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 331
4538 deg
Eccentricity:
0004852
Arg of perigee: 340
5272 deg
Mean anomaly: 19
5695 deg
Mean motion: 15
54079544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2383
Checksum: 308
Coasting Arc #6 (Orbit 2397)
---------------------------------------
Vector Time (GMT): 2017/182/13:23:19
736
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 720944
10 A = 6780394
40 meter
Y = -4921325
03 meter E =
0008281
Z = -4614608
15 I = 51
42512
XDOT = 6845
257594 Wp = 81
62191
YDOT = -1764
082822 meter/sec RA = 326
06274 deg
ZDOT = 2956
513195 TA = 217
92298
MA = 217
98133
Ha = 221
324 n
mi
Hp = 215
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2365302
16 X = 798337
49
Y = -16146079
48 feet Y = -4912829
84 meter
Z = -15139790
53 Z = -4610918
46
XDOT = 22458
194205 XDOT = 6850
114039
YDOT = -5787
673300 feet/sec YDOT = -1687
507592 meter/sec
ZDOT = 9699
846441 ZDOT = 2989
776878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15241226
68 X = -4645525
89
Y = 5875100
73 feet Y = 1790730
70 meter
Z = -15122565
75 Z = -4609358
04
XDOT = -15710
201473 XDOT = -4788
469409
YDOT = -15457
718819 feet/sec YDOT = -4711
512696 meter/sec
ZDOT = 9847
011676 ZDOT = 3001
369159
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17182
56859819
00016717 00000-0 10270-3 0 9052
2 25544 51
6408 326
6470 0004847 343
2271 16
8721 15
54105809 23984
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
56859819 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 326
6470 deg
Eccentricity:
0004847
Arg of perigee: 343
2271 deg
Mean anomaly: 16
8721 deg
Mean motion: 15
54105809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2398
Checksum: 330
Coasting Arc #7 (Orbit 2402)
---------------------------------------
Vector Time (GMT): 2017/182/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3752768
34 A = 6778172
12 meter
Y = -2361919
38 meter E =
0014511
Z = -5138939
45 I = 51
40815
XDOT = 5354
943604 Wp = 57
80354
YDOT = -5269
359574 meter/sec RA = 324
53243 deg
ZDOT = -1484
149180 TA = 197
81438
MA = 197
86530
Ha = 221
502 n
mi
Hp = 214
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12312232
08 X = -3701115
44
Y = -7749079
33 feet Y = -2403596
15 meter
Z = -16860037
56 Z = -5157043
93
XDOT = 17568
712610 XDOT = 5420
678228
YDOT = -17287
925113 feet/sec YDOT = -5209
109296 meter/sec
ZDOT = -4869
255840 ZDOT = -1457
977366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13534465
85 X = 4125305
19
Y = -5076580
90 feet Y = -1547341
86 meter
Z = -16939501
66 Z = -5163160
11
XDOT = 2838
112546 XDOT = 865
056704
YDOT = 23474
449756 feet/sec YDOT = 7155
012286 meter/sec
ZDOT = -4752
730050 ZDOT = -1448
632119
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17182
89011336
00016717 00000-0 10270-3 0 9063
2 25544 51
6397 325
0478 0005150 346
6900 13
4116 15
54088569 24037
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
89011336 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 325
0478 deg
Eccentricity:
0005150
Arg of perigee: 346
6900 deg
Mean anomaly: 13
4116 deg
Mean motion: 15
54088569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2403
Checksum: 304
Coasting Arc #8 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2017/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5009981
52 A = 6789265
14 meter
Y = 4546644
84 meter E =
0009502
Z = 531591
80 I = 51
42829
XDOT = -3573
598356 Wp = 111
11174
YDOT = -3230
947866 meter/sec RA = 321
36830 deg
ZDOT = -5962
492284 TA = 63
13806
MA = 63
04096
Ha = 221
427 n
mi
Hp = 214
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16436947
23 X = -5063033
15
Y = 14916813
78 feet Y = 4490323
15 meter
Z = 1744067
57 Z = 507126
44
XDOT = -11724
404055 XDOT = -3508
240628
YDOT = -10600
222658 feet/sec YDOT = -3270
544303 meter/sec
ZDOT = -19561
982558 ZDOT = -5979
693237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17511688
61 X = 5337562
69
Y = 13652588
18 feet Y = 4161308
88 meter
Z = 1635217
77 Z = 498414
38
XDOT = -7465
516193 XDOT = -2275
489336
YDOT = 11962
529498 feet/sec YDOT = 3646
178991 meter/sec
ZDOT = -19637
292775 ZDOT = -5985
446838
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17183
53314596
00016717 00000-0 10270-3 0 9070
2 25544 51
6392 321
8378 0004912 346
7706 13
3317 15
54113488 24137
Satellite: ISS
Catalog Number: 25544
Epoch time: 17183
53314596 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 321
8378 deg
Eccentricity:
0004912
Arg of perigee: 346
7706 deg
Mean anomaly: 13
3317 deg
Mean motion: 15
54113488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2413
Checksum: 311
Coasting Arc #9 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2017/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5426018
15 A = 6788749
98 meter
Y = -3895958
94 meter E =
0016272
Z = 1155806
89 I = 51
40366
XDOT = 2005
957026 Wp = 41
66369
YDOT = 4540
340731 meter/sec RA = 316
38265 deg
ZDOT = 5851
808213 TA = 330
93660
MA = 331
02708
Ha = 221
478 n
mi
Hp = 214
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17801896
80 X = 5463566
17
Y = -12782017
51 feet Y = -3835071
69 meter
Z = 3792017
37 Z = 1182255
62
XDOT = 6581
223838 XDOT = 1926
611447
YDOT = 14896
131007 feet/sec YDOT = 4562
328468 meter/sec
ZDOT = 19198
845843 ZDOT = 5861
360267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15896619
03 X = -4845289
48
Y = -15055905
46 feet Y = -4589039
98 meter
Z = 3909489
90 Z = 1191612
52
XDOT = 12320
157620 XDOT = 3755
184043
YDOT = -7982
761322 feet/sec YDOT = -2433
145651 meter/sec
ZDOT = 19240
149353 ZDOT = 5864
397523
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17184
56199380
00016717 00000-0 10270-3 0 9087
2 25544 51
6410 316
7090 0004893 351
4848 8
6221 15
54122769 24290
Satellite: ISS
Catalog Number: 25544
Epoch time: 17184
56199380 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 316
7090 deg
Eccentricity:
0004893
Arg of perigee: 351
4848 deg
Mean anomaly: 8
6221 deg
Mean motion: 15
54122769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 321
Coasting Arc #10 (Orbit 2443)
---------------------------------------
Vector Time (GMT): 2017/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5487023
10 A = 6786060
63 meter
Y = 2899100
22 meter E =
0004491
Z = -2752506
09 I = 51
37146
XDOT = -439
020675 Wp = 54
98906
YDOT = -5685
192594 meter/sec RA = 311
39136 deg
ZDOT = -5116
220683 TA = 156
27591
MA = 156
25519
Ha = 221
660 n
mi
Hp = 214
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18002044
29 X = -5505663
47
Y = 9511483
65 feet Y = 2837636
69 meter
Z = -9030531
79 Z = -2779205
30
XDOT = -1440
356545 XDOT = -350
562641
YDOT = -18652
206673 feet/sec YDOT = -5689
606842 meter/sec
ZDOT = -16785
500930 ZDOT = -5118
139104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12985656
66 X = 3958028
15
Y = 15612894
65 feet Y = 4758810
29 meter
Z = -9148916
11 Z = -2788589
63
XDOT = -16846
673352 XDOT = -5134
866038
YDOT = 4177
922965 feet/sec YDOT = 1273
430920 meter/sec
ZDOT = -16792
901619 ZDOT = -5118
476413
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 17185
52653649
00016717 00000-0 10270-3 0 9098
2 25544 51
6406 311
9012 0004974 355
6144 4
4964 15
54118825 24444
Satellite: ISS
Catalog Number: 25544
Epoch time: 17185
52653649 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 311
9012 deg
Eccentricity:
0004974
Arg of perigee: 355
6144 deg
Mean anomaly: 4
4964 deg
Mean motion: 15
54118825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2444
Checksum: 316
Coasting Arc #11 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2017/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5198065
85 A = 6782232
83 meter
Y = -1607494
78 meter E =
0010531
Z = 4038250
73 I = 51
33849
XDOT = -983
987923 Wp = 75
43769
YDOT = 6553
109768 meter/sec RA = 306
38921 deg
ZDOT = 3869
302391 TA = 334
31362
MA = 334
36589
Ha = 221
524 n
mi
Hp = 214
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17054021
81 X = 5196039
13
Y = -5273933
00 feet Y = -1549378
32 meter
Z = 13248854
11 Z = 4063496
18
XDOT = -3228
306834 XDOT = -1075
988537
YDOT = 21499
703962 feet/sec YDOT = 6541
591254 meter/sec
ZDOT = 12694
561651 ZDOT = 3864
299857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8903543
04 X = -2713799
92
Y = -15375567
19 feet Y = -4686472
88 meter
Z = 13360577
06 Z = 4072303
89
XDOT = 20578
643001 XDOT = 6272
370387
YDOT = -889
219503 feet/sec YDOT = -271
034105 meter/sec
ZDOT = 12671
261168 ZDOT = 3862
200404
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 17186
55537829
00016717 00000-0 10270-3 0 9105
2 25544 51
6410 306
7727 0004929 358
2715 1
8419 15
54146449 24604
Satellite: ISS
Catalog Number: 25544
Epoch time: 17186
55537829 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 306
7727 deg
Eccentricity:
0004929
Arg of perigee: 358
2715 deg
Mean anomaly: 1
8419 deg
Mean motion: 15
54146449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2460
Checksum: 323
Coasting Arc #12 (Orbit 2474)
---------------------------------------
Vector Time (GMT): 2017/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4672151
36 A = 6778991
63 meter
Y = 86668
32 meter E =
0014701
Z = -4924390
24 I = 51
30969
XDOT = 2197
939044 Wp = 54
72055
YDOT = -6995
674384 meter/sec RA = 301
37602 deg
ZDOT = -2204
820741 TA = 193
61151
MA = 193
65119
Ha = 221
820 n
mi
Hp = 214
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15328580
57 X = -4648853
07
Y = 284344
87 feet Y = 34552
09 meter
Z = -16156135
95 Z = -4947029
43
XDOT = 7211
086102 XDOT = 2286
713062
YDOT = -22951
687610 feet/sec YDOT = -6970
598875 meter/sec
ZDOT = -7233
663848 ZDOT = -2193
929195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3904825
20 X = 1190190
72
Y = 14715956
93 feet Y = 4485423
67 meter
Z = -16256073
17 Z = -4954851
10
XDOT = -22947
915093 XDOT = -6994
524520
YDOT = -1860
208156 feet/sec YDOT = -566
991446 meter/sec
ZDOT = -7184
298850 ZDOT = -2189
774289
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 17187
51991702
00016717 00000-0 10270-3 0 9117
2 25544 51
6419 301
9655 0005017 1
7383 358
3786 15
54114160 24758
Satellite: ISS
Catalog Number: 25544
Epoch time: 17187
51991702 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 301
9655 deg
Eccentricity:
0005017
Arg of perigee: 1
7383 deg
Mean anomaly: 358
3786 deg
Mean motion: 15
54114160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2475
Checksum: 309
Coasting Arc #13 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2017/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3948757
50 A = 6777270
24 meter
Y = 1561088
00 meter E =
0005413
Z = 5279436
88 I = 51
28859
XDOT = -3174
153991 Wp = 33
02479
YDOT = 6976
896207 meter/sec RA = 296
35321 deg
ZDOT = 315
405768 TA = 53
98000
MA = 53
92984
Ha = 221
751 n
mi
Hp = 214
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12955241
16 X = 3905362
77
Y = 5121679
78 feet Y = 1605002
31 meter
Z = 17320987
15 Z = 5298513
43
XDOT = -10413
891048 XDOT = -3253
467649
YDOT = 22890
079419 feet/sec YDOT = 6940
957151 meter/sec
ZDOT = 1034
795828 ZDOT = 299
795140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1677288
97 X = 511237
68
Y = -13723798
23 feet Y = -4183013
70 meter
Z = 17404899
80 Z = 5305013
46
XDOT = 23790
498452 XDOT = 7251
343928
YDOT = 4113
126825 feet/sec YDOT = 1253
681056 meter/sec
ZDOT = 964
616533 ZDOT = 294
015119
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 17188
54875254
00016717 00000-0 10270-3 0 9125
2 25544 51
6422 296
8364 0005140 5
8458 354
2754 15
54163396 24919
Satellite: ISS
Catalog Number: 25544
Epoch time: 17188
54875254 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 296
8364 deg
Eccentricity:
0005140
Arg of perigee: 5
8458 deg
Mean anomaly: 354
2754 deg
Mean motion: 15
54163396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 328
Coasting Arc #14 (Orbit 2505)
---------------------------------------
Vector Time (GMT): 2017/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3152306
88 A = 6778157
30 meter
Y = -3175796
06 meter E =
0014334
Z = -5102992
95 I = 51
27750
XDOT = 3878
017412 Wp = 80
91866
YDOT = -6407
801470 meter/sec RA = 291
33068 deg
ZDOT = 1598
313375 TA = 204
56248
MA = 204
63083
Ha = 221
976 n
mi
Hp = 213
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10342214
18 X = -3091772
40
Y = -10419278
41 feet Y = -3210708
11 meter
Z = -16742102
84 Z = -5118159
15
XDOT = 12723
154239 XDOT = 3941
619164
YDOT = -21022
970703 feet/sec YDOT = -6364
079453 meter/sec
ZDOT = 5243
810287 ZDOT = 1617
304998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7248187
24 X = -2209247
47
Y = 12679113
64 feet Y = 3864593
84 meter
Z = -16808468
81 Z = -5123221
29
XDOT = -22754
796665 XDOT = -6935
662024
YDOT = -5970
126218 feet/sec YDOT = -1819
694471 meter/sec
ZDOT = 5328
797741 ZDOT = 1624
217551
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 17189
51328629
00016717 00000-0 10270-3 0 9133
2 25544 51
6419 292
0302 0005176 10
7242 349
4020 15
54151684 25066
Satellite: ISS
Catalog Number: 25544
Epoch time: 17189
51328629 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 292
0302 deg
Eccentricity:
0005176
Arg of perigee: 10
7242 deg
Mean anomaly: 349
4020 deg
Mean motion: 15
54151684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2506
Checksum: 293
Coasting Arc #15 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2017/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2288924
67 A = 6781169
77 meter
Y = 4650334
20 meter E =
0013092
Z = 4368557
88 I = 51
27649
XDOT = -4371
320548 Wp = 51
22513
YDOT = 5327
826721 meter/sec RA = 286
31054 deg
ZDOT = -3366
204004 TA = 73
07939
MA = 72
93591
Ha = 222
090 n
mi
Hp = 213
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7509595
36 X = 2215533
24
Y = 15257001
98 feet Y = 4675519
57 meter
Z = 14332538
99 Z = 4379499
00
XDOT = -14341
602848 XDOT = -4414
221657
YDOT = 17479
746460 feet/sec YDOT = 5278
704222 meter/sec
ZDOT = -11043
976391 ZDOT = -3387
541763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12473132
83 X = 3801810
89
Y = -11499057
77 feet Y = -3504912
81 meter
Z = 14380001
17 Z = 4383024
36
XDOT = 20011
360918 XDOT = 6099
462808
YDOT = 7715
693871 feet/sec YDOT = 2351
743492 meter/sec
ZDOT = -11139
114781 ZDOT = -3395
202185
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 17190
54211925
00016717 00000-0 10270-3 0 9149
2 25544 51
6420 286
9014 0005210 14
5507 345
5795 15
54131690 25224
Satellite: ISS
Catalog Number: 25544
Epoch time: 17190
54211925 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 286
9014 deg
Eccentricity:
0005210
Arg of perigee: 14
5507 deg
Mean anomaly: 345
5795 deg
Mean motion: 15
54131690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 287
Coasting Arc #16 (Orbit 2536)
---------------------------------------
Vector Time (GMT): 2017/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1463680
66 A = 6784947
50 meter
Y = -5796371
57 meter E =
0008380
Z = -3207091
93 I = 51
28085
XDOT = 4652
029338 Wp = 45
46514
YDOT = -3801
505139 meter/sec RA = 281
30044 deg
ZDOT = 4761
035810 TA = 277
24200
MA = 277
33726
Ha = 222
167 n
mi
Hp = 213
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4802101
89 X = -1383177
07
Y = -19016967
10 feet Y = -5812288
93 meter
Z = -10521955
14 Z = -3214007
10
XDOT = 15262
563444 XDOT = 4671
066582
YDOT = -12472
129720 feet/sec YDOT = -3749
377122 meter/sec
ZDOT = 15620
196227 ZDOT = 4783
679383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16671657
72 X = -5081521
27
Y = 10302394
45 feet Y = 3140169
83 meter
Z = -10551457
61 Z = -3216084
28
XDOT = -15745
444346 XDOT = -4799
211437
YDOT = -9424
062197 feet/sec YDOT = -2872
454158 meter/sec
ZDOT = 15720
819538 ZDOT = 4791
705795
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 17191
50664605
00016717 00000-0 10270-3 0 9154
2 25544 51
6419 282
0942 0005321 16
0275 344
1045 15
54125765 25376
Satellite: ISS
Catalog Number: 25544
Epoch time: 17191
50664605 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 282
0942 deg
Eccentricity:
0005321
Arg of perigee: 16
0275 deg
Mean anomaly: 344
1045 deg
Mean motion: 15
54125765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2537
Checksum: 294
Coasting Arc #17 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2017/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 623839
38 A = 6788127
34 meter
Y = 6545962
82 meter E =
0014527
Z = 1669654
71 I = 51
28503
XDOT = -4787
608459 Wp = 94
45754
YDOT = 1914
295688 meter/sec RA = 276
29976 deg
ZDOT = -5674
594236 TA = 67
15673
MA = 67
00339
Ha = 222
302 n
mi
Hp = 213
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2046717
12 X = 542484
10
Y = 21476255
96 feet Y = 6552483
95 meter
Z = 5477869
78 Z = 1672488
17
XDOT = -15707
376834 XDOT = -4781
094836
YDOT = 6280
497663 feet/sec YDOT = 1860
794418 meter/sec
ZDOT = -18617
435157 ZDOT = -5697
834570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19694581
76 X = 6002908
52
Y = -8798713
69 feet Y = -2681847
93 meter
Z = 5489240
88 Z = 1673120
62
XDOT = 10307
974984 XDOT = 3141
870775
YDOT = 11308
649177 feet/sec YDOT = 3446
876269 meter/sec
ZDOT = -18720
358463 ZDOT = -5705
965260
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 17192
53547405
00016717 00000-0 10270-3 0 9167
2 25544 51
6409 276
9660 0005340 21
6217 338
5160 15
54134383 25532
Satellite: ISS
Catalog Number: 25544
Epoch time: 17192
53547405 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 276
9660 deg
Eccentricity:
0005340
Arg of perigee: 21
6217 deg
Mean anomaly: 338
5160 deg
Mean motion: 15
54134383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 303
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