[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 19th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
353/08:43:02
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
6
361/06:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 215
4
362/01:04:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 215
4
364/11:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 215
2
Coasting Arc #1 (Orbit 1042)
---------------------------------------
Vector Time (GMT): 2017/352/14:05:06
902
Vector Time (MET): N/A
Weight (LBS) : 923966
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4146903
97 A = 6784370
09 meter
Y = -4166124
15 meter E =
0009535
Z = 3379724
64 I = 51
51812
XDOT = 5782
897362 Wp = 93
46411
YDOT = -1993
566619 meter/sec RA = 197
93586 deg
ZDOT = 4626
302036 TA = 306
08508
MA = 306
17334
Ha = 219
876 n
mi
Hp = 215
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13605327
97 X = -4116426
11
Y = -13668386
32 feet Y = -4212327
65 meter
Z = 11088335
44 Z = 3359653
77
XDOT = 18972
760374 XDOT = 5782
287818
YDOT = -6540
572898 feet/sec YDOT = -1928
902257 meter/sec
ZDOT = 15178
156286 ZDOT = 4654
391901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5715072
85 X = 1741954
20
Y = -18472253
88 feet Y = -5630342
98 meter
Z = 10999758
89 Z = 3352726
51
XDOT = 13236
154201 XDOT = 4034
379800
YDOT = 13231
103689 feet/sec YDOT = 4032
840405 meter/sec
ZDOT = 15303
213527 ZDOT = 4664
419483
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 17352
64420480
00016717 00000-0 10270-3 0 9003
2 25544 51
6357 198
7788 0003099 256
7529 103
3278 15
54194944 10432
Satellite: ISS
Catalog Number: 25544
Epoch time: 17352
64420480 = yrday
fracday
Element set: 900
Inclination: 51
6357 deg
RA of node: 198
7788 deg
Eccentricity:
0003099
Arg of perigee: 256
7529 deg
Mean anomaly: 103
3278 deg
Mean motion: 15
54194944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1043
Checksum: 329
Coasting Arc #2 (Orbit 1054)
---------------------------------------
Vector Time (GMT): 2017/353/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 939197
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1718507
64 A = 6779197
37 meter
Y = -4407003
59 meter E =
0004988
Z = 4854811
91 I = 51
52944
XDOT = 7274
662156 Wp = 139
25302
YDOT = -162
681221 meter/sec RA = 194
05720 deg
ZDOT = 2422
302415 TA = 286
92713
MA = 286
98181
Ha = 219
905 n
mi
Hp = 215
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5638148
43 X = -1692681
89
Y = -14458673
18 feet Y = -4426077
28 meter
Z = 15927860
59 Z = 4846526
15
XDOT = 23867
001824 XDOT = 7264
174289
YDOT = -533
731040 feet/sec YDOT = -81
389902 meter/sec
ZDOT = 7947
186401 ZDOT = 2457
614950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13430499
16 X = 4093616
14
Y = 7849551
66 feet Y = 2392543
34 meter
Z = 15891662
02 Z = 4843778
58
XDOT = -17857
043645 XDOT = -5442
826903
YDOT = 14112
212188 feet/sec YDOT = 4301
402275 meter/sec
ZDOT = 8104
092062 ZDOT = 2470
127260
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 17353
41578779
00016717 00000-0 10270-3 0 9015
2 25544 51
6399 194
9356 0002853 266
1535 93
9291 15
54188586 10553
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
41578779 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 194
9356 deg
Eccentricity:
0002853
Arg of perigee: 266
1535 deg
Mean anomaly: 93
9291 deg
Mean motion: 15
54188586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1055
Checksum: 352
Coasting Arc #3 (Orbit 1069)
---------------------------------------
Vector Time (GMT): 2017/354/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 939197
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -82774
31 A = 6777199
52 meter
Y = 4242891
66 meter E =
0011786
Z = -5294315
64 I = 51
55450
XDOT = -7601
104901 Wp = 84
60621
YDOT = -794
644613 meter/sec RA = 189
05211 deg
ZDOT = -517
903154 TA = 180
44096
MA = 180
44200
Ha = 219
777 n
mi
Hp = 215
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -271569
27 X = -104496
24
Y = 13920248
22 feet Y = 4241845
16 meter
Z = -17369801
98 Z = -5294770
01
XDOT = -24938
008205 XDOT = -7589
138334
YDOT = -2607
101749 feet/sec YDOT = -879
578396 meter/sec
ZDOT = -1699
157329 ZDOT = -554
797841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8640349
32 X = -2633578
47
Y = -10913335
45 feet Y = -3326384
65 meter
Z = -17372407
84 Z = -5295109
91
XDOT = 20212
329283 XDOT = 6160
717966
YDOT = -13036
523113 feet/sec YDOT = -3973
532245 meter/sec
ZDOT = -1862
986147 ZDOT = -567
838178
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 17354
38027658
00016717 00000-0 10270-3 0 9028
2 25544 51
6392 190
1275 0002943 271
5377 88
5439 15
54218820 10704
Satellite: ISS
Catalog Number: 25544
Epoch time: 17354
38027658 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 190
1275 deg
Eccentricity:
0002943
Arg of perigee: 271
5377 deg
Mean anomaly: 88
5439 deg
Mean motion: 15
54218820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1070
Checksum: 316
Coasting Arc #4 (Orbit 1085)
---------------------------------------
Vector Time (GMT): 2017/355/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 939197
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1914239
38 A = 6777651
46 meter
Y = -3962171
33 meter E =
0002858
Z = 5155058
48 I = 51
58946
XDOT = 7344
907938 Wp = 11
31604
YDOT = 1666
934887 meter/sec RA = 184
04716 deg
ZDOT = -1443
318341 TA = 92
59809
MA = 92
56537
Ha = 219
609 n
mi
Hp = 215
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6280312
92 X = 1933362
60
Y = -12999249
79 feet Y = -3940658
61 meter
Z = 16912921
52 Z = 5164403
24
XDOT = 24097
466989 XDOT = 7332
732821
YDOT = 5468
946481 feet/sec YDOT = 1749
002744 meter/sec
ZDOT = -4735
296394 ZDOT = -1407
668694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3629787
43 X = 1106359
21
Y = 13922014
60 feet Y = 4243430
05 meter
Z = 16954996
09 Z = 5167882
81
XDOT = -20982
618298 XDOT = -6395
502057
YDOT = 11056
359024 feet/sec YDOT = 3369
978231 meter/sec
ZDOT = -4577
094079 ZDOT = -1395
098275
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 17355
40905929
00016717 00000-0 10270-3 0 9039
2 25544 51
6398 184
9985 0003131 274
7712 85
3083 15
54246071 10863
Satellite: ISS
Catalog Number: 25544
Epoch time: 17355
40905929 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 184
9985 deg
Eccentricity:
0003131
Arg of perigee: 274
7712 deg
Mean anomaly: 85
3083 deg
Mean motion: 15
54246071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1086
Checksum: 326
Coasting Arc #5 (Orbit 1100)
---------------------------------------
Vector Time (GMT): 2017/356/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 939197
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3610253
43 A = 6780472
28 meter
Y = 3602779
41 meter E =
0006506
Z = -4474400
36 I = 51
63176
XDOT = -6486
407987 Wp = 115
83022
YDOT = -2465
264760 meter/sec RA = 179
04848 deg
ZDOT = 3249
562591 TA = 186
91128
MA = 186
92025
Ha = 219
720 n
mi
Hp = 215
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11844663
50 X = -3628538
11
Y = 11820142
42 feet Y = 3562305
26 meter
Z = -14679791
21 Z = -4491981
79
XDOT = -21280
866099 XDOT = -6474
143295
YDOT = -8088
138975 feet/sec YDOT = -2537
731928 meter/sec
ZDOT = 10661
294591 ZDOT = 3218
083467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1115750
49 X = 340080
75
Y = -16626843
29 feet Y = -5067861
83 meter
Z = -14758430
59 Z = -4498369
64
XDOT = 20208
373194 XDOT = 6159
512150
YDOT = -7980
627379 feet/sec YDOT = -2432
495225 meter/sec
ZDOT = 10521
713516 ZDOT = 3207
018280
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 17356
37353931
00016717 00000-0 10270-3 0 9047
2 25544 51
6400 180
1893 0003128 280
2317 79
8483 15
54226522 11011
Satellite: ISS
Catalog Number: 25544
Epoch time: 17356
37353931 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 180
1893 deg
Eccentricity:
0003128
Arg of perigee: 280
2317 deg
Mean anomaly: 79
8483 deg
Mean motion: 15
54226522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1101
Checksum: 292
Coasting Arc #6 (Orbit 1116)
---------------------------------------
Vector Time (GMT): 2017/357/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 939197
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5026316
63 A = 6784270
19 meter
Y = -3140283
03 meter E =
0009653
Z = 3293890
87 I = 51
67723
XDOT = 5114
259214 Wp = 87
02324
YDOT = 3220
204095 meter/sec RA = 174
06237 deg
ZDOT = -4721
643464 TA = 54
71819
MA = 54
62792
Ha = 219
710 n
mi
Hp = 215
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16490540
12 X = 5045058
60
Y = -10302765
83 feet Y = -3083970
77 meter
Z = 10806728
57 Z = 3318352
21
XDOT = 16779
065664 XDOT = 5100
805138
YDOT = 10564
974066 feet/sec YDOT = 3277
320372 meter/sec
ZDOT = -15490
956248 ZDOT = -4696
832641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5317022
37 X = -1620628
42
Y = 18639815
41 feet Y = 5681415
74 meter
Z = 10915898
24 Z = 3327165
78
XDOT = -18255
576423 XDOT = -5564
299694
YDOT = 3823
753507 feet/sec YDOT = 1165
480069 meter/sec
ZDOT = -15381
100293 ZDOT = -4688
159369
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 17357
40231149
00016717 00000-0 10270-3 0 9059
2 25544 51
6397 175
0601 0003082 287
1415 72
9400 15
54253917 11178
Satellite: ISS
Catalog Number: 25544
Epoch time: 17357
40231149 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 175
0601 deg
Eccentricity:
0003082
Arg of perigee: 287
1415 deg
Mean anomaly: 72
9400 deg
Mean motion: 15
54253917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1117
Checksum: 291
Coasting Arc #7 (Orbit 1131)
---------------------------------------
Vector Time (GMT): 2017/358/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 939197
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6015594
11 A = 6787666
83 meter
Y = 2585386
49 meter E =
0006959
Z = -1773952
69 I = 51
72018
XDOT = -3353
349144 Wp = 13
30616
YDOT = -3915
451519 meter/sec RA = 169
08879 deg
ZDOT = 5676
030462 TA = 327
23519
MA = 327
27832
Ha = 219
774 n
mi
Hp = 215
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19736201
14 X = -6035440
59
Y = 8482239
15 feet Y = 2518005
15 meter
Z = -5820054
74 Z = -1803222
37
XDOT = -11001
801655 XDOT = -3336
887417
YDOT = -12845
969552 feet/sec YDOT = -3952
859271 meter/sec
ZDOT = 18622
147185 ZDOT = 5659
780812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8635228
42 X = 2632017
62
Y = -19630663
66 feet Y = -5983426
28 meter
Z = -5950540
17 Z = -1813724
64
XDOT = 15462
740591 XDOT = 4713
043332
YDOT = 1189
462083 feet/sec YDOT = 362
548043 meter/sec
ZDOT = 18550
433270 ZDOT = 5654
172061
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 17358
36678173
00016717 00000-0 10270-3 0 9068
2 25544 51
6392 170
2515 0003203 289
4637 70
6169 15
54219452 11320
Satellite: ISS
Catalog Number: 25544
Epoch time: 17358
36678173 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 170
2515 deg
Eccentricity:
0003203
Arg of perigee: 289
4637 deg
Mean anomaly: 70
6169 deg
Mean motion: 15
54219452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1132
Checksum: 312
Coasting Arc #8 (Orbit 1147)
---------------------------------------
Vector Time (GMT): 2017/359/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 939197
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6517440
45 A = 6789083
32 meter
Y = -1882752
08 meter E =
0009425
Z = 35630
67 I = 51
75750
XDOT = 1351
957978 Wp = 141
75361
YDOT = 4550
070607 meter/sec RA = 164
12427 deg
ZDOT = -6022
336910 TA = 37
86323
MA = 37
79698
Ha = 219
874 n
mi
Hp = 215
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21382678
64 X = 6537836
43
Y = -6177008
14 feet Y = -1809755
57 meter
Z = 116898
52 Z = 67339
61
XDOT = 4435
557672 XDOT = 1330
230745
YDOT = 14928
053171 feet/sec YDOT = 4565
067947 meter/sec
ZDOT = -19758
323194 ZDOT = -6015
822101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11108168
52 X = -3385769
76
Y = 19285486
54 feet Y = 5878216
30 meter
Z = 258150
48 Z = 78684
27
XDOT = -12239
279792 XDOT = -3730
532481
YDOT = -6768
768873 feet/sec YDOT = -2063
120753 meter/sec
ZDOT = -19729
973157 ZDOT = -6013
695818
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 17359
39554448
00016717 00000-0 10270-3 0 9071
2 25544 51
6399 165
1221 0003169 290
7934 69
2879 15
54212005 11486
Satellite: ISS
Catalog Number: 25544
Epoch time: 17359
39554448 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 165
1221 deg
Eccentricity:
0003169
Arg of perigee: 290
7934 deg
Mean anomaly: 69
2879 deg
Mean motion: 15
54212005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1148
Checksum: 331
Coasting Arc #9 (Orbit 1163)
---------------------------------------
Vector Time (GMT): 2017/360/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 939197
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6483609
86 A = 6787760
80 meter
Y = 1045919
06 meter E =
0012208
Z = 1687865
44 I = 51
78351
XDOT = 675
031500 Wp = 52
09801
YDOT = -5071
950910 meter/sec RA = 159
16096 deg
ZDOT = 5715
124174 TA = 326
37251
MA = 326
44993
Ha = 219
869 n
mi
Hp = 215
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21271685
90 X = -6503022
52
Y = 3431492
99 feet Y = 973306
28 meter
Z = 5537616
27 Z = 1656323
10
XDOT = 2214
670274 XDOT = 703
936093
YDOT = -16640
258891 feet/sec YDOT = -5064
240892 meter/sec
ZDOT = 18750
407394 ZDOT = 5718
473227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12661237
55 X = 3859145
20
Y = -17478221
56 feet Y = -5327361
93 meter
Z = 5397202
41 Z = 1645067
29
XDOT = 8996
007195 XDOT = 2741
982993
YDOT = 12333
210322 feet/sec YDOT = 3759
162506 meter/sec
ZDOT = 18765
992047 ZDOT = 5719
874376
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 17360
42429860
00016717 00000-0 10270-3 0 9087
2 25544 51
6386 159
9917 0003222 295
7368 64
3452 15
54274463 11648
Satellite: ISS
Catalog Number: 25544
Epoch time: 17360
42429860 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 159
9917 deg
Eccentricity:
0003222
Arg of perigee: 295
7368 deg
Mean anomaly: 64
3452 deg
Mean motion: 15
54274463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1164
Checksum: 329
Coasting Arc #10 (Orbit 1177)
---------------------------------------
Vector Time (GMT): 2017/361/06:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 939197
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 928537
92 A = 6778879
30 meter
Y = -4658055
01 meter E =
0006195
Z = 4835854
11 I = 51
78346
XDOT = 7142
768138 Wp = 32
86755
YDOT = -1199
617469 meter/sec RA = 154
56366 deg
ZDOT = -2520
410845 TA = 81
89553
MA = 81
82526
Ha = 219
835 n
mi
Hp = 215
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3046384
27 X = 957066
36
Y = -15282332
71 feet Y = -4647512
18 meter
Z = 15865663
08 Z = 4840433
72
XDOT = 23434
278669 XDOT = 7167
894620
YDOT = -3935
752850 feet/sec YDOT = -1119
601537 meter/sec
ZDOT = -8269
064453 ZDOT = -2485
652569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1404734
91 X = 428163
20
Y = 15498060
48 feet Y = 4723808
84 meter
Z = 15886669
13 Z = 4842256
75
XDOT = -20349
446315 XDOT = -6202
511237
YDOT = 10184
375631 feet/sec YDOT = 3104
197692 meter/sec
ZDOT = -8114
311384 ZDOT = -2473
242110
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 17361
32445664
00016717 00000-0 10270-3 0 9098
2 25544 51
6399 155
5054 0003282 300
8902 59
1928 15
54300205 11783
Satellite: ISS
Catalog Number: 25544
Epoch time: 17361
32445664 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 155
5054 deg
Eccentricity:
0003282
Arg of perigee: 300
8902 deg
Mean anomaly: 59
1928 deg
Mean motion: 15
54300205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1178
Checksum: 305
Coasting Arc #11 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2017/362/01:04:30
000
Vector Time (MET): N/A
Weight (LBS) : 924764
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3625183
24 A = 6777871
47 meter
Y = -2581317
67 meter E =
0002048
Z = 5111136
66 I = 51
79996
XDOT = 5774
940712 Wp = 129
13635
YDOT = -4754
633183 meter/sec RA = 150
79385 deg
ZDOT = 1693
015445 TA = 304
54032
MA = 304
55965
Ha = 220
034 n
mi
Hp = 215
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11893645
79 X = -3620876
22
Y = -8468889
98 feet Y = -2621833
14 meter
Z = 16768821
05 Z = 5093536
95
XDOT = 18946
655878 XDOT = 5819
455251
YDOT = -15599
190233 feet/sec YDOT = -4689
805042 meter/sec
ZDOT = 5554
512614 ZDOT = 1721
176190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3365546
30 X = -1025818
51
Y = 14298999
86 feet Y = 4358335
16 meter
Z = 16690894
77 Z = 5087384
72
XDOT = -20494
593346 XDOT = -6246
752052
YDOT = -11461
027690 feet/sec YDOT = -3493
321240 meter/sec
ZDOT = 5680
424679 ZDOT = 1731
393442
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 17362
09601784
00016717 00000-0 10270-3 0 9102
2 25544 51
6377 151
6570 0003209 302
5635 57
5207 15
54289820 11905
Satellite: ISS
Catalog Number: 25544
Epoch time: 17362
09601784 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 151
6570 deg
Eccentricity:
0003209
Arg of perigee: 302
5635 deg
Mean anomaly: 57
5207 deg
Mean motion: 15
54289820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1190
Checksum: 301
Coasting Arc #12 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2017/363/01:04:30
000
Vector Time (MET): N/A
Weight (LBS) : 924764
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2088363
71 A = 6776976
26 meter
Y = 3645563
36 meter E =
0012447
Z = -5328124
43 I = 51
82517
XDOT = -6455
025056 Wp = 83
42125
YDOT = 4113
767540 meter/sec RA = 145
80389 deg
ZDOT = 286
596599 TA = 189
29523
MA = 189
31829
Ha = 220
100 n
mi
Hp = 215
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6851586
98 X = 2073324
29
Y = 11960509
71 feet Y = 3668833
16 meter
Z = -17480723
19 Z = -5318016
05
XDOT = -21177
903727 XDOT = -6501
938708
YDOT = 13496
612663 feet/sec YDOT = 4041
320703 meter/sec
ZDOT = 940
277556 ZDOT = 255
126370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8297875
58 X = 2529192
48
Y = -11076807
44 feet Y = -3376210
91 meter
Z = -17436264
45 Z = -5314573
40
XDOT = 19878
275276 XDOT = 6058
898304
YDOT = 13642
568217 feet/sec YDOT = 4158
254792 meter/sec
ZDOT = 799
710752 ZDOT = 243
751837
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 17363
06046335
00016717 00000-0 10270-3 0 9116
2 25544 51
6379 146
8472 0003189 308
9219 51
1649 15
54265738 12058
Satellite: ISS
Catalog Number: 25544
Epoch time: 17363
06046335 = yrday
fracday
Element set: 911
Inclination: 51
6379 deg
RA of node: 146
8472 deg
Eccentricity:
0003189
Arg of perigee: 308
9219 deg
Mean anomaly: 51
1649 deg
Mean motion: 15
54265738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 318
Coasting Arc #13 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2017/364/01:04:30
000
Vector Time (MET): N/A
Weight (LBS) : 924764
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -496013
31 A = 6778536
67 meter
Y = -4607183
01 meter E =
0006462
Z = 4946581
35 I = 51
85701
XDOT = 6631
227869 Wp = 29
32433
YDOT = -3130
914404 meter/sec RA = 140
81829 deg
ZDOT = -2244
421857 TA = 82
55885
MA = 82
48543
Ha = 220
197 n
mi
Hp = 215
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1627340
26 X = -468485
79
Y = -15115429
82 feet Y = -4612576
31 meter
Z = 16228941
44 Z = 4944238
30
XDOT = 21755
996946 XDOT = 6676
648067
YDOT = -10272
028884 feet/sec YDOT = -3056
505309 meter/sec
ZDOT = -7363
588770 ZDOT = -2212
099325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13112031
90 X = -3996547
32
Y = 7714676
68 feet Y = 2351433
45 meter
Z = 16219167
00 Z = 4943602
10
XDOT = -17670
055379 XDOT = -5385
832880
YDOT = -14808
154652 feet/sec YDOT = -4513
525538 meter/sec
ZDOT = -7219
343225 ZDOT = -2200
455815
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 17364
08919903
00016717 00000-0 10270-3 0 9120
2 25544 51
6378 141
7182 0003194 314
4127 45
6764 15
54272991 12218
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
08919903 = yrday
fracday
Element set: 912
Inclination: 51
6378 deg
RA of node: 141
7182 deg
Eccentricity:
0003194
Arg of perigee: 314
4127 deg
Mean anomaly: 45
6764 deg
Mean motion: 15
54272991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 312
Coasting Arc #14 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 924764
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3425368
13 A = 6777123
54 meter
Y = -2508985
62 meter E =
0000615
Z = 5281632
77 I = 51
86318
XDOT = 5281
718715 Wp = 74
96444
YDOT = -5501
526573 meter/sec RA = 138
62778 deg
ZDOT = 812
056832 TA = 7
29964
MA = 7
29875
Ha = 220
197 n
mi
Hp = 215
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11238084
42 X = -3422712
99
Y = -8231580
12 feet Y = -2547276
13 meter
Z = 17328191
51 Z = 5264999
57
XDOT = 17328
473473 XDOT = 5338
901140
YDOT = -18049
627863 feet/sec YDOT = -5442
143139 meter/sec
ZDOT = 2664
228452 ZDOT = 837
852123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7316328
03 X = 2230016
78
Y = -11961263
40 feet Y = -3645793
08 meter
Z = 17254541
30 Z = 5259184
19
XDOT = 18476
709915 XDOT = 5631
701182
YDOT = 15311
186066 feet/sec YDOT = 4666
849513 meter/sec
ZDOT = 2779
780064 ZDOT = 847
276963
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 17364
53926899
00016717 00000-0 10270-3 0 9133
2 25544 51
6374 139
4696 0002915 308
6679 51
4213 15
54287091 12283
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
53926899 = yrday
fracday
Element set: 913
Inclination: 51
6374 deg
RA of node: 139
4696 deg
Eccentricity:
0002915
Arg of perigee: 308
6679 deg
Mean anomaly: 51
4213 deg
Mean motion: 15
54287091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1228
Checksum: 340
Coasting Arc #15 (Orbit 1242)
---------------------------------------
Vector Time (GMT): 2017/365/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 924764
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2049665
61 A = 6777273
97 meter
Y = 3799964
48 meter E =
0011916
Z = -5234355
86 I = 51
88921
XDOT = -5857
054341 Wp = 91
45698
YDOT = 4791
841183 meter/sec RA = 133
64337 deg
ZDOT = 1187
247485 TA = 189
89203
MA = 189
91551
Ha = 220
147 n
mi
Hp = 215
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6724624
70 X = 2032446
89
Y = 12467075
06 feet Y = 3822789
61 meter
Z = -17173083
53 Z = -5224440
61
XDOT = -19216
057548 XDOT = -5915
969735
YDOT = 15721
263725 feet/sec YDOT = 4726
014035 meter/sec
ZDOT = 3895
168915 ZDOT = 1158
653316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11756387
66 X = -3583346
96
Y = 7995666
04 feet Y = 2437079
01 meter
Z = -17129506
99 Z = -5221073
73
XDOT = -16902
594332 XDOT = -5151
910752
YDOT = -16796
248424 feet/sec YDOT = -5119
496520 meter/sec
ZDOT = 3767
237434 ZDOT = 1148
253970
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 17365
50370081
00016717 00000-0 10270-3 0 9148
2 25544 51
6387 134
6615 0002867 312
6031 47
4880 15
54306179 12439
Satellite: ISS
Catalog Number: 25544
Epoch time: 17365
50370081 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 134
6615 deg
Eccentricity:
0002867
Arg of perigee: 312
6031 deg
Mean anomaly: 47
4880 deg
Mean motion: 15
54306179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1243
Checksum: 301
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