[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 15th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
135/07:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
1
Coasting Arc #1 (Orbit 3956)
---------------------------------------
Vector Time (GMT): 2016/134/09:28:33
804
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4746320
09 A = 6787751
16 meter
Y = 4778018
50 meter E =
0015021
Z = 788654
05 I = 51
37026
XDOT = -2925
797059 Wp = 124
50396
YDOT = 3896
259317 meter/sec RA = 230
56033 deg
ZDOT = -5924
788832 TA = 46
93381
MA = 46
80816
Ha = 220
889 n
mi
Hp = 213
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15571916
29 X = 4688707
37
Y = 15675913
72 feet Y = 4830772
86 meter
Z = 2587447
68 Z = 811570
77
XDOT = -9599
071716 XDOT = -2940
368351
YDOT = 12783
003009 feet/sec YDOT = 3863
459773 meter/sec
ZDOT = -19438
283570 ZDOT = -5939
036988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18654166
29 X = 5685789
89
Y = 11820327
45 feet Y = 3602835
81 meter
Z = 2686200
32 Z = 818753
86
XDOT = -5528
987390 XDOT = -1685
235356
YDOT = 13209
080010 feet/sec YDOT = 4026
127587 meter/sec
ZDOT = -19500
865626 ZDOT = -5943
863843
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 16134
42860402
00016717 00000-0 10270-3 0 9008
2 25544 51
6399 231
4325 0001724 108
6422 251
4918 15
54574644 39571
Satellite: ISS
Catalog Number: 25544
Epoch time: 16134
42860402 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 231
4325 deg
Eccentricity:
0001724
Arg of perigee: 108
6422 deg
Mean anomaly: 251
4918 deg
Mean motion: 15
54574644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3957
Checksum: 303
Coasting Arc #2 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2016/135/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3690880
99 A = 6776229
78 meter
Y = 2218443
56 meter E =
0016317
Z = -5246251
89 I = 51
35102
XDOT = -4776
335312 Wp = 97
80267
YDOT = -5923
363472 meter/sec RA = 225
95967 deg
ZDOT = 855
632634 TA = 180
42272
MA = 180
42410
Ha = 220
910 n
mi
Hp = 213
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12109189
60 X = -3689929
70
Y = 7278358
13 feet Y = 2177175
06 meter
Z = -17212112
49 Z = -5264179
02
XDOT = -15670
391444 XDOT = -4713
900110
YDOT = -19433
607190 feet/sec YDOT = -5976
426547 meter/sec
ZDOT = 2807
193682 ZDOT = 832
581839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13497929
99 X = -4114169
06
Y = 3835615
37 feet Y = 1169095
56 meter
Z = -17290394
07 Z = -5270112
11
XDOT = -9695
206201 XDOT = -2955
098850
YDOT = -21912
754823 feet/sec YDOT = -6679
007670 meter/sec
ZDOT = 2708
038956 ZDOT = 825
410274
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 16135
32857121
00016717 00000-0 10270-3 0 9013
2 25544 51
6397 226
9443 0001817 106
4066 253
7287 15
54593931 39712
Satellite: ISS
Catalog Number: 25544
Epoch time: 16135
32857121 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 226
9443 deg
Eccentricity:
0001817
Arg of perigee: 106
4066 deg
Mean anomaly: 253
7287 deg
Mean motion: 15
54593931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 319
Coasting Arc #3 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2016/136/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4881010
36 A = 6778736
73 meter
Y = -681118
51 meter E =
0009450
Z = 4647915
35 I = 51
38206
XDOT = 3592
649187 Wp = 72
23220
YDOT = 6145
341705 meter/sec RA = 220
93787 deg
ZDOT = -2864
624585 TA = 46
34961
MA = 46
27129
Ha = 220
825 n
mi
Hp = 213
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16013813
51 X = 4865686
29
Y = -2234640
78 feet Y = -626621
51 meter
Z = 15249066
11 Z = 4671589
03
XDOT = 11786
906782 XDOT = 3537
578643
YDOT = 20161
882234 feet/sec YDOT = 6185
209198 meter/sec
ZDOT = -9398
374623 ZDOT = -2847
305987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15971055
55 X = 4867977
73
Y = 1791470
82 feet Y = 546040
31 meter
Z = 15352064
25 Z = 4679309
18
XDOT = 6596
612826 XDOT = 2010
647589
YDOT = 21307
876444 feet/sec YDOT = 6494
640740 meter/sec
ZDOT = -9324
152090 ZDOT = -2842
001557
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 16136
35709557
00016717 00000-0 10270-3 0 9027
2 25544 51
6394 221
8123 0001878 109
2384 250
8972 15
54570963 39875
Satellite: ISS
Catalog Number: 25544
Epoch time: 16136
35709557 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 221
8123 deg
Eccentricity:
0001878
Arg of perigee: 109
2384 deg
Mean anomaly: 250
8972 deg
Mean motion: 15
54570963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 336
Coasting Arc #4 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2016/137/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5769680
00 A = 6782634
51 meter
Y = -737372
37 meter E =
0006935
Z = -3495812
32 I = 51
42113
XDOT = -1976
403984 Wp = 99
66004
YDOT = -5872
329845 meter/sec RA = 215
93010 deg
ZDOT = 4507
128642 TA = 219
12063
MA = 219
17079
Ha = 220
850 n
mi
Hp = 213
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18929396
32 X = -5744024
37
Y = -2419200
68 feet Y = -801749
30 meter
Z = -11469200
53 Z = -3523777
97
XDOT = -6484
265041 XDOT = -1932
485150
YDOT = -19266
174031 feet/sec YDOT = -5894
185766 meter/sec
ZDOT = 14787
167461 ZDOT = 4497
634313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17780708
72 X = -5419560
02
Y = -6724658
32 feet Y = -2049675
86 meter
Z = -11590621
45 Z = -3532821
42
XDOT = -2425
294858 XDOT = -739
229873
YDOT = -18968
570506 feet/sec YDOT = -5781
620290 meter/sec
ZDOT = 14746
891917 ZDOT = 4494
852656
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 16137
32132757
00016717 00000-0 10270-3 0 9038
2 25544 51
6402 217
0031 0001830 111
3364 248
7984 15
54611226 40026
Satellite: ISS
Catalog Number: 25544
Epoch time: 16137
32132757 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 217
0031 deg
Eccentricity:
0001830
Arg of perigee: 111
3364 deg
Mean anomaly: 248
7984 deg
Mean motion: 15
54611226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 268
Coasting Arc #5 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2016/138/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6206719
40 A = 6786353
59 meter
Y = 1982340
61 meter E =
0015688
Z = 1870919
84 I = 51
45995
XDOT = 30
604365 Wp = 113
76691
YDOT = 5230
796225 meter/sec RA = 210
93526 deg
ZDOT = -5612
730501 TA = 45
57118
MA = 45
44290
Ha = 220
762 n
mi
Hp = 213
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20363252
61 X = 6175002
82
Y = 6503742
17 feet Y = 2051570
93 meter
Z = 6138188
45 Z = 1900993
92
XDOT = 100
408022 XDOT = -
625388
YDOT = 17161
404939 feet/sec YDOT = 5230
963900 meter/sec
ZDOT = -18414
470148 ZDOT = -5612
657636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18449429
90 X = 5623386
23
Y = 10722013
11 feet Y = 3268069
59 meter
Z = 6268576
23 Z = 1910662
04
XDOT = -2693
883611 XDOT = -821
095725
YDOT = 15460
075980 feet/sec YDOT = 4712
231159 meter/sec
ZDOT = -18415
030326 ZDOT = -5612
901243
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 16138
34983457
00016717 00000-0 10270-3 0 9043
2 25544 51
6400 211
8720 0001736 117
2802 242
8528 15
54620734 40188
Satellite: ISS
Catalog Number: 25544
Epoch time: 16138
34983457 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 211
8720 deg
Eccentricity:
0001736
Arg of perigee: 117
2802 deg
Mean anomaly: 242
8528 deg
Mean motion: 15
54620734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 295
Coasting Arc #6 (Orbit 4032)
---------------------------------------
Vector Time (GMT): 2016/139/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6113964
00 A = 6787839
15 meter
Y = -2936437
92 meter E =
0012629
Z = -44155
32 I = 51
49474
XDOT = 2038
903842 Wp = 52
84062
YDOT = -4317
518897 meter/sec RA = 205
95098 deg
ZDOT = 6001
120772 TA = 306
68274
MA = 306
79872
Ha = 220
771 n
mi
Hp = 213
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20058936
99 X = -6080459
12
Y = -9633982
69 feet Y = -3004621
00 meter
Z = -144866
54 Z = -73774
58
XDOT = 6689
317068 XDOT = 2057
880552
YDOT = -14165
088245 feet/sec YDOT = -4294
612527 meter/sec
ZDOT = 19688
716444 ZDOT = 6011
071427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17750429
64 X = -5410330
96
Y = -13418018
08 feet Y = -4089811
91 meter
Z = -273130
66 Z = -83250
22
XDOT = 8260
716295 XDOT = 2517
866327
YDOT = -11287
379052 feet/sec YDOT = -3440
393135 meter/sec
ZDOT = 19732
693897 ZDOT = 6014
525100
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 16139
31405196
00016717 00000-0 10270-3 0 9051
2 25544 51
6417 207
0622 0001761 116
0673 244
0661 15
54639571 40333
Satellite: ISS
Catalog Number: 25544
Epoch time: 16139
31405196 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 207
0622 deg
Eccentricity:
0001761
Arg of perigee: 116
0673 deg
Mean anomaly: 244
0661 deg
Mean motion: 15
54639571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4033
Checksum: 288
Coasting Arc #7 (Orbit 4048)
---------------------------------------
Vector Time (GMT): 2016/140/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5423333
10 A = 6786404
60 meter
Y = 3639174
99 meter E =
0009011
Z = -1833330
50 I = 51
51851
XDOT = -4069
155167 Wp = 137
44356
YDOT = 3237
050497 meter/sec RA = 200
96926 deg
ZDOT = -5634
466099 TA = 62
75306
MA = 62
66129
Ha = 220
782 n
mi
Hp = 213
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17793087
61 X = 5391141
55
Y = 11939550
49 feet Y = 3699642
38 meter
Z = -6014863
84 Z = -1807062
89
XDOT = -13350
246612 XDOT = -4077
679940
YDOT = 10620
244413 feet/sec YDOT = 3191
499016 meter/sec
ZDOT = -18485
781166 ZDOT = -5654
253997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15371478
21 X = 4685226
56
Y = 14973911
73 feet Y = 4564048
29 meter
Z = -5901274
84 Z = -1798708
57
XDOT = -13844
853370 XDOT = -4219
911307
YDOT = 6922
948552 feet/sec YDOT = 2110
114719 meter/sec
ZDOT = -18572
348831 ZDOT = -5660
851924
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 16140
34254335
00016717 00000-0 10270-3 0 9064
2 25544 51
6409 201
9317 0001764 118
0999 242
0333 15
54661245 40498
Satellite: ISS
Catalog Number: 25544
Epoch time: 16140
34254335 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 201
9317 deg
Eccentricity:
0001764
Arg of perigee: 118
0999 deg
Mean anomaly: 242
0333 deg
Mean motion: 15
54661245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4049
Checksum: 296
Coasting Arc #8 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2016/141/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4203591
30 A = 6782733
08 meter
Y = -4049706
14 meter E =
0013839
Z = 3443983
82 I = 51
53715
XDOT = 5791
665188 Wp = 94
90286
YDOT = -2114
243550 meter/sec RA = 195
98151 deg
ZDOT = 4566
002551 TA = 305
56268
MA = 305
69161
Ha = 220
709 n
mi
Hp = 213
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13791310
03 X = -4174723
76
Y = -13286437
45 feet Y = -4096552
25 meter
Z = 11299159
52 Z = 3423633
35
XDOT = 19001
526206 XDOT = 5792
696638
YDOT = -6936
494585 feet/sec YDOT = -2049
471752 meter/sec
ZDOT = 14980
323329 ZDOT = 4594
139955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11491780
59 X = -3502694
72
Y = -15383275
90 feet Y = -4688822
49 meter
Z = 11211354
07 Z = 3417220
72
XDOT = 18665
627064 XDOT = 5689
283129
YDOT = -2895
771426 feet/sec YDOT = -882
631131 meter/sec
ZDOT = 15103
016493 ZDOT = 4603
399427
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 16141
37102713
00016717 00000-0 10270-3 0 9071
2 25544 51
6413 196
8013 0001738 127
0524 233
0788 15
54693135 40658
Satellite: ISS
Catalog Number: 25544
Epoch time: 16141
37102713 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 196
8013 deg
Eccentricity:
0001738
Arg of perigee: 127
0524 deg
Mean anomaly: 233
0788 deg
Mean motion: 15
54693135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4065
Checksum: 293
Coasting Arc #9 (Orbit 4079)
---------------------------------------
Vector Time (GMT): 2016/142/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2510702
45 A = 6778667
73 meter
Y = 4251762
51 meter E =
0011401
Z = -4655069
32 I = 51
55491
XDOT = -7023
026100 Wp = 77
75668
YDOT = 979
570748 meter/sec RA = 190
98339 deg
ZDOT = -2896
795865 TA = 163
38972
MA = 163
35234
Ha = 220
687 n
mi
Hp = 213
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8237212
76 X = 2485584
33
Y = 13949352
07 feet Y = 4279698
72 meter
Z = -15272537
15 Z = -4642933
45
XDOT = -23041
424213 XDOT = -7019
386283
YDOT = 3213
814790 feet/sec YDOT = 901
055140 meter/sec
ZDOT = -9503
923441 ZDOT = -2930
903715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6189023
38 X = 1886414
33
Y = 15023966
36 feet Y = 4579304
95 meter
Z = -15220476
76 Z = -4639201
32
XDOT = -22106
763002 XDOT = -6738
141363
YDOT = -659
771580 feet/sec YDOT = -201
098378 meter/sec
ZDOT = -9652
404819 ZDOT = -2942
052989
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 16142
33522650
00016717 00000-0 10270-3 0 9085
2 25544 51
6418 191
9916 0001682 127
1791 232
9516 15
54661232 40803
Satellite: ISS
Catalog Number: 25544
Epoch time: 16142
33522650 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 191
9916 deg
Eccentricity:
0001682
Arg of perigee: 127
1791 deg
Mean anomaly: 232
9516 deg
Mean motion: 15
54661232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4080
Checksum: 302
Coasting Arc #10 (Orbit 4095)
---------------------------------------
Vector Time (GMT): 2016/143/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -549312
94 A = 6775920
36 meter
Y = -4244525
33 meter E =
0005106
Z = 5249810
04 I = 51
57777
XDOT = 7622
012143 Wp = 123
60603
YDOT = 100
024213 meter/sec RA = 185
97617 deg
ZDOT = 875
017734 TA = 318
00445
MA = 318
04359
Ha = 220
605 n
mi
Hp = 213
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1802207
82 X = -527310
54
Y = -13925608
05 feet Y = -4250545
52 meter
Z = 17223786
22 Z = 5247194
66
XDOT = 25006
601520 XDOT = 7616
076627
YDOT = 328
163427 feet/sec YDOT = 185
225364 meter/sec
ZDOT = 2870
793090 ZDOT = 912
029809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -82131
83 X = -25033
78
Y = -14054569
58 feet Y = -4283832
81 meter
Z = 17213124
43 Z = 5246560
33
XDOT = 23706
804472 XDOT = 7225
834003
YDOT = 3588
139325 feet/sec YDOT = 1093
664866 meter/sec
ZDOT = 3031
744510 ZDOT = 924
075727
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 16143
36369612
00016717 00000-0 10270-3 0 9097
2 25544 51
6415 186
8604 0001652 127
4515 232
6788 15
54715146 40960
Satellite: ISS
Catalog Number: 25544
Epoch time: 16143
36369612 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 186
8604 deg
Eccentricity:
0001652
Arg of perigee: 127
4515 deg
Mean anomaly: 232
6788 deg
Mean motion: 15
54715146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4096
Checksum: 321
Coasting Arc #11 (Orbit 4110)
---------------------------------------
Vector Time (GMT): 2016/144/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1505432
22 A = 6776164
09 meter
Y = 4094336
55 meter E =
0015628
Z = -5199047
95 I = 51
61024
XDOT = -7466
270867 Wp = 102
86147
YDOT = -1132
508565 meter/sec RA = 180
96866 deg
ZDOT = 1269
881807 TA = 179
35400
MA = 179
35198
Ha = 220
610 n
mi
Hp = 213
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4939082
10 X = -1525849
11
Y = 13432862
68 feet Y = 4077388
13 meter
Z = -17057243
92 Z = -5206410
28
XDOT = -24495
639329 XDOT = -7459
220594
YDOT = -3715
579282 feet/sec YDOT = -1215
962072 meter/sec
ZDOT = 4166
278894 ZDOT = 1233
628994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6319159
97 X = -1926079
96
Y = 12797948
53 feet Y = 3900814
71 meter
Z = -17089957
07 Z = -5209018
91
XDOT = -23010
207931 XDOT = -7013
511377
YDOT = -6007
636912 feet/sec YDOT = -1831
127731 meter/sec
ZDOT = 4008
780394 ZDOT = 1221
876264
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 16144
32788345
00016717 00000-0 10270-3 0 9104
2 25544 51
6411 182
0514 0001715 128
2256 231
9051 15
54708638 41116
Satellite: ISS
Catalog Number: 25544
Epoch time: 16144
32788345 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 182
0514 deg
Eccentricity:
0001715
Arg of perigee: 128
2256 deg
Mean anomaly: 231
9051 deg
Mean motion: 15
54708638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4111
Checksum: 284
Coasting Arc #12 (Orbit 4126)
---------------------------------------
Vector Time (GMT): 2016/145/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3421590
13 A = 6779138
59 meter
Y = -3779275
76 meter E =
0009937
Z = 4461202
51 I = 51
65255
XDOT = 6611
872626 Wp = 77
52028
YDOT = 2122
774359 meter/sec RA = 175
96661 deg
ZDOT = -3264
552703 TA = 45
37226
MA = 45
29126
Ha = 220
543 n
mi
Hp = 213
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11225689
39 X = 3441925
77
Y = -12399198
70 feet Y = -3740900
01 meter
Z = 14636491
17 Z = 4477872
96
XDOT = 21692
495493 XDOT = 6603
501803
YDOT = 6964
482806 feet/sec YDOT = 2196
666241 meter/sec
ZDOT = -10710
474749 ZDOT = -3232
453607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12271591
58 X = 3740381
11
Y = -11270195
40 feet Y = -3435155
56 meter
Z = 14709651
26 Z = 4483501
70
XDOT = 20168
890141 XDOT = 6147
477715
YDOT = 8128
556812 feet/sec YDOT = 2477
584116 meter/sec
ZDOT = -10571
189958 ZDOT = -3222
098699
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 16145
35634290
00016717 00000-0 10270-3 0 9118
2 25544 51
6414 176
9197 0001709 130
1307 229
9996 15
54695178 41276
Satellite: ISS
Catalog Number: 25544
Epoch time: 16145
35634290 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 176
9197 deg
Eccentricity:
0001709
Arg of perigee: 130
1307 deg
Mean anomaly: 229
9996 deg
Mean motion: 15
54695178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4127
Checksum: 328
Coasting Arc #13 (Orbit 4141)
---------------------------------------
Vector Time (GMT): 2016/146/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4987667
86 A = 6783317
51 meter
Y = 3330425
96 meter E =
0005606
Z = -3174517
43 I = 51
69864
XDOT = -5107
062850 Wp = 92
80517
YDOT = -3051
485072 meter/sec RA = 170
97923 deg
ZDOT = 4829
748589 TA = 230
60136
MA = 230
65102
Ha = 220
520 n
mi
Hp = 213
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16363739
69 X = -5009118
25
Y = 10926594
34 feet Y = 3274530
92 meter
Z = -10415083
43 Z = -3198798
25
XDOT = -16755
455543 XDOT = -5096
021852
YDOT = -10011
433963 feet/sec YDOT = -3108
534399 meter/sec
ZDOT = 15845
631854 ZDOT = 4804
966045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17108579
81 X = -5214695
12
Y = 9603920
92 feet Y = 2927275
10 meter
Z = -10521292
86 Z = -3206890
06
XDOT = -15313
284128 XDOT = -4667
489002
YDOT = -10062
935390 feet/sec YDOT = -3067
182707 meter/sec
ZDOT = 15738
317781 ZDOT = 4797
039260
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 16146
32051603
00016717 00000-0 10270-3 0 9128
2 25544 51
6415 172
1098 0001501 132
8395 227
2884 15
54695794 41429
Satellite: ISS
Catalog Number: 25544
Epoch time: 16146
32051603 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 172
1098 deg
Eccentricity:
0001501
Arg of perigee: 132
8395 deg
Mean anomaly: 227
2884 deg
Mean motion: 15
54695794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4142
Checksum: 301
Coasting Arc #14 (Orbit 4157)
---------------------------------------
Vector Time (GMT): 2016/147/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6055684
35 A = 6786721
09 meter
Y = -2683016
64 meter E =
0015491
Z = 1444369
24 I = 51
74088
XDOT = 3133
076038 Wp = 120
71622
YDOT = 3930
248353 meter/sec RA = 166
00619 deg
ZDOT = -5796
688841 TA = 43
53967
MA = 43
41749
Ha = 220
542 n
mi
Hp = 213
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19867730
80 X = 6078220
28
Y = -8802548
02 feet Y = -2615172
08 meter
Z = 4738744
22 Z = 1473840
89
XDOT = 10279
120861 XDOT = 3117
052136
YDOT = 12894
515593 feet/sec YDOT = 3965
195449 meter/sec
ZDOT = -19018
008010 ZDOT = -5781
507600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20343212
74 X = 6200611
24
Y = -7558366
68 feet Y = -2303790
16 meter
Z = 4867449
44 Z = 1483598
59
XDOT = 9032
939461 XDOT = 2753
239948
YDOT = 12027
916736 feet/sec YDOT = 3666
109021 meter/sec
ZDOT = -18952
608994 ZDOT = -5776
755222
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 16147
34896357
00016717 00000-0 10270-3 0 9135
2 25544 51
6408 166
9790 0001676 135
9456 224
1831 15
54705983 41583
Satellite: ISS
Catalog Number: 25544
Epoch time: 16147
34896357 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 166
9790 deg
Eccentricity:
0001676
Arg of perigee: 135
9456 deg
Mean anomaly: 224
1831 deg
Mean motion: 15
54705983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4158
Checksum: 342
Coasting Arc #15 (Orbit 4173)
---------------------------------------
Vector Time (GMT): 2016/148/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6504816
22 A = 6787583
87 meter
Y = 1868545
81 meter E =
0012959
Z = 439481
06 I = 51
77529
XDOT = -930
693647 Wp = 56
44229
YDOT = -4680
366191 meter/sec RA = 161
04130 deg
ZDOT = 6003
953334 TA = 308
28916
MA = 308
40565
Ha = 220
497 n
mi
Hp = 213
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21341260
56 X = -6527362
13
Y = 6130399
65 feet Y = 1795678
53 meter
Z = 1441867
00 Z = 407827
57
XDOT = -3053
456846 XDOT = -907
452174
YDOT = -15355
532122 feet/sec YDOT = -4690
644382 meter/sec
ZDOT = 19698
009626 ZDOT = 5999
488296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21602649
14 X = -6584487
46
Y = 5170674
70 feet Y = 1576021
65 meter
Z = 1303785
22 Z = 397393
73
XDOT = -2114
196953 XDOT = -644
407231
YDOT = -13905
138157 feet/sec YDOT = -4238
286110 meter/sec
ZDOT = 19679
369200 ZDOT = 5998
271732
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 16148
37740455
00016717 00000-0 10270-3 0 9147
2 25544 51
6415 161
8477 0001501 137
1316 222
9954 15
54706665 41741
Satellite: ISS
Catalog Number: 25544
Epoch time: 16148
37740455 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 161
8477 deg
Eccentricity:
0001501
Arg of perigee: 137
1316 deg
Mean anomaly: 222
9954 deg
Mean motion: 15
54706665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4174
Checksum: 312
Coasting Arc #16 (Orbit 4188)
---------------------------------------
Vector Time (GMT): 2016/149/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6325693
88 A = 6785394
32 meter
Y = -818096
81 meter E =
0007470
Z = -2309217
65 I = 51
79791
XDOT = -1297
932736 Wp = 137
30894
YDOT = 5252
307778 meter/sec RA = 156
07697 deg
ZDOT = -5431
848416 TA = 68
36124
MA = 68
28170
Ha = 220
507 n
mi
Hp = 213
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20753588
83 X = 6345589
12
Y = -2684044
65 feet Y = -747247
29 meter
Z = -7576173
39 Z = -2278440
64
XDOT = -4258
309500 XDOT = -1330
183226
YDOT = 17231
980898 feet/sec YDOT = 5237
613493 meter/sec
ZDOT = -17821
024987 ZDOT = -5438
231429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20867886
20 X = 6360531
71
Y = -2112087
47 feet Y = -643764
26 meter
Z = -7442066
96 Z = -2268342
01
XDOT = -4769
356561 XDOT = -1453
699880
YDOT = 15588
232114 feet/sec YDOT = 4751
293148 meter/sec
ZDOT = -17849
700225 ZDOT = -5440
588629
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 16149
34156125
00016717 00000-0 10270-3 0 9151
2 25544 51
6412 157
0375 0001532 140
0094 220
1172 15
54730047 41891
Satellite: ISS
Catalog Number: 25544
Epoch time: 16149
34156125 = yrday
fracday
Element set: 915
Inclination: 51
6412 deg
RA of node: 157
0375 deg
Eccentricity:
0001532
Arg of perigee: 140
0094 deg
Mean anomaly: 220
1172 deg
Mean motion: 15
54730047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4189
Checksum: 276
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