[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 4th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7803 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 ET - UTC (sec) : 67 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
226/10:19:30
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 212
7
Coasting Arc #1 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2015/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4393040
07 A = 6784066
04 meter
Y = -4485300
79 meter E =
0014408
Z = 2551625
84 I = 51
48132
XDOT = 5186
679739 Wp = 72
39714
YDOT = -2076
231856 meter/sec RA = 206
72074 deg
ZDOT = 5259
831297 TA = 316
36834
MA = 316
48218
Ha = 219
843 n
mi
Hp = 213
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14412861
11 X = -4354952
47
Y = -14715553
76 feet Y = -4534213
65 meter
Z = 8371475
86 Z = 2530378
26
XDOT = 17016
665809 XDOT = 5183
961347
YDOT = -6811
784303 feet/sec YDOT = -2018
246120 meter/sec
ZDOT = 17256
664360 ZDOT = 5285
020156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1646954
40 X = -501991
70
Y = 20568816
75 feet Y = 6269375
34 meter
Z = 8280761
73 Z = 2523976
17
XDOT = -14718
394075 XDOT = -4486
166514
YDOT = -8196
653428 feet/sec YDOT = -2498
339965 meter/sec
ZDOT = 17365
434436 ZDOT = 5292
984416
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 15215
55920874
00016717 00000-0 10270-3 0 9001
2 25544 51
6401 207
5008 0001167 22
0623 338
0580 15
55010238 35411
Satellite: ISS
Catalog Number: 25544
Epoch time: 15215
55920874 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 207
5008 deg
Eccentricity:
0001167
Arg of perigee: 22
0623 deg
Mean anomaly: 338
0580 deg
Mean motion: 15
55010238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 266
Coasting Arc #2 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2015/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2792925
33 A = 6779774
80 meter
Y = 4626419
49 meter E =
0008373
Z = -4103122
19 I = 51
49536
XDOT = -6619
687741 Wp = 65
38110
YDOT = 622
696599 meter/sec RA = 201
72088 deg
ZDOT = -3806
504206 TA = 165
21915
MA = 165
19465
Ha = 219
941 n
mi
Hp = 213
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9163140
84 X = 2760915
17
Y = 15178541
63 feet Y = 4657472
76 meter
Z = -13461686
99 Z = -4089632
73
XDOT = -21718
135633 XDOT = -6607
668582
YDOT = 2042
967844 feet/sec YDOT = 548
738037 meter/sec
ZDOT = -12488
530858 ZDOT = -3838
631734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5121113
62 X = 1560915
43
Y = -17019549
11 feet Y = -5187558
57 meter
Z = -13404381
23 Z = -4085655
40
XDOT = 14728
307077 XDOT = 4489
187997
YDOT = 14369
475546 feet/sec YDOT = 4379
816146 meter/sec
ZDOT = -12626
938019 ZDOT = -3848
690708
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 15216
52320729
00016717 00000-0 10270-3 0 9013
2 25544 51
6399 202
6878 0001350 28
3388 331
7838 15
54982008 35563
Satellite: ISS
Catalog Number: 25544
Epoch time: 15216
52320729 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 202
6878 deg
Eccentricity:
0001350
Arg of perigee: 28
3388 deg
Mean anomaly: 331
7838 deg
Mean motion: 15
54982008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 320
Coasting Arc #3 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2015/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -822083
53 A = 6775962
80 meter
Y = -4438538
52 meter E =
0005528
Z = 5049490
15 I = 51
51272
XDOT = 7418
333575 Wp = 110
49292
YDOT = 709
628925 meter/sec RA = 196
71059 deg
ZDOT = 1827
993331 TA = 321
76808
MA = 321
80727
Ha = 219
895 n
mi
Hp = 213
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2697124
43 X = -796917
89
Y = -14562134
24 feet Y = -4447590
82 meter
Z = 16566568
73 Z = 5045557
85
XDOT = 24338
364748 XDOT = 7400
967374
YDOT = 2328
178889 feet/sec YDOT = 792
488526 meter/sec
ZDOT = 5997
353447 ZDOT = 1863
987587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8762201
32 X = -2670718
96
Y = 11962044
59 feet Y = 3646031
19 meter
Z = 16550370
11 Z = 5044552
81
XDOT = -13956
948375 XDOT = -4254
077865
YDOT = -18751
483211 feet/sec YDOT = -5715
452083 meter/sec
ZDOT = 6152
200996 ZDOT = 1875
190864
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 15217
55146255
00016717 00000-0 10270-3 0 9028
2 25544 51
6398 197
5551 0001386 24
5311 335
5908 15
55004075 35723
Satellite: ISS
Catalog Number: 25544
Epoch time: 15217
55146255 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 197
5551 deg
Eccentricity:
0001386
Arg of perigee: 24
5311 deg
Mean anomaly: 335
5908 deg
Mean motion: 15
55004075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 305
Coasting Arc #4 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2015/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1321789
04 A = 6774860
84 meter
Y = 4025409
46 meter E =
0015527
Z = -5299972
66 I = 51
53994
XDOT = -7412
649617 Wp = 88
69592
YDOT = -1877
941779 meter/sec RA = 191
69345 deg
ZDOT = 423
776960 TA = 185
34796
MA = 185
36456
Ha = 219
938 n
mi
Hp = 212
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4336578
21 X = -1340958
83
Y = 13206723
93 feet Y = 4010521
15 meter
Z = -17388361
76 Z = -5306440
17
XDOT = -24319
716590 XDOT = -7393
157628
YDOT = -6161
226310 feet/sec YDOT = -1960
725908 meter/sec
ZDOT = 1390
344358 ZDOT = 387
815396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12448483
38 X = 3794297
73
Y = -6104625
82 feet Y = -1860689
95 meter
Z = -17416871
05 Z = -5308662
30
XDOT = 11972
220669 XDOT = 3649
132860
YDOT = 20901
045427 feet/sec YDOT = 6370
638646 meter/sec
ZDOT = 1235
813312 ZDOT = 376
675897
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 15218
51544444
00016717 00000-0 10270-3 0 9038
2 25544 51
6399 192
7426 0001430 30
6803 329
4434 15
55002615 35876
Satellite: ISS
Catalog Number: 25544
Epoch time: 15218
51544444 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 192
7426 deg
Eccentricity:
0001430
Arg of perigee: 30
6803 deg
Mean anomaly: 329
4434 deg
Mean motion: 15
55002615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 298
Coasting Arc #5 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2015/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3384303
88 A = 6776933
48 meter
Y = -3414708
85 meter E =
0008639
Z = 4772096
33 I = 51
57850
XDOT = 6612
378398 Wp = 56
32847
YDOT = 2871
910907 meter/sec RA = 186
68059 deg
ZDOT = -2626
275193 TA = 59
62039
MA = 59
53501
Ha = 219
794 n
mi
Hp = 212
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11103359
19 X = 3399055
58
Y = -11203113
01 feet Y = -3376780
92 meter
Z = 15656484
04 Z = 4788572
28
XDOT = 21694
154849 XDOT = 6592
529909
YDOT = 9422
279879 feet/sec YDOT = 2945
743920 meter/sec
ZDOT = -8616
388429 ZDOT = -2594
201975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15701592
11 X = -4785845
28
Y = 100015
62 feet Y = 30484
76 meter
Z = 15727994
81 Z = 4793892
82
XDOT = -8652
790082 XDOT = -2637
370417
YDOT = -20917
924528 feet/sec YDOT = -6375
783396 meter/sec
ZDOT = -8478
746555 ZDOT = -2584
321950
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 15219
54368301
00016717 00000-0 10270-3 0 9049
2 25544 51
6398 187
6096 0001451 28
8363 331
2870 15
55032282 36031
Satellite: ISS
Catalog Number: 25544
Epoch time: 15219
54368301 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 187
6096 deg
Eccentricity:
0001451
Arg of perigee: 28
8363 deg
Mean anomaly: 331
2870 deg
Mean motion: 15
55032282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 304
Coasting Arc #6 (Orbit 3617)
---------------------------------------
Vector Time (GMT): 2015/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5095712
81 A = 6781186
17 meter
Y = 2687968
00 meter E =
0006195
Z = -3581623
98 I = 51
62444
XDOT = -5053
198213 Wp = 85
58966
YDOT = -3668
456772 meter/sec RA = 181
68079 deg
ZDOT = 4443
339183 TA = 232
07514
MA = 232
13116
Ha = 219
908 n
mi
Hp = 212
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16718217
89 X = -5107993
58
Y = 8818792
65 feet Y = 2630915
82 meter
Z = -11750734
85 Z = -3606407
49
XDOT = -16578
734295 XDOT = -5033
384948
YDOT = -12035
619330 feet/sec YDOT = -3724
854281 meter/sec
ZDOT = 14577
884459 ZDOT = 4418
839996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18082465
35 X = 5511535
44
Y = 5269154
65 feet Y = 1606038
34 meter
Z = -11857914
62 Z = -3614292
37
XDOT = 3959
906806 XDOT = 1206
979594
YDOT = 18929
191233 feet/sec YDOT = 5769
617488 meter/sec
ZDOT = 14472
975494 ZDOT = 4411
362930
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 15220
50764887
00016717 00000-0 10270-3 0 9057
2 25544 51
6398 182
7974 0001528 32
5802 327
5445 15
55023283 36180
Satellite: ISS
Catalog Number: 25544
Epoch time: 15220
50764887 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 182
7974 deg
Eccentricity:
0001528
Arg of perigee: 32
5802 deg
Mean anomaly: 327
5445 deg
Mean motion: 15
55023283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3618
Checksum: 321
Coasting Arc #7 (Orbit 3633)
---------------------------------------
Vector Time (GMT): 2015/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6266235
96 A = 6785138
46 meter
Y = -1818466
54 meter E =
0014332
Z = 1839625
47 I = 51
67018
XDOT = 2914
545341 Wp = 107
77226
YDOT = 4301
313954 meter/sec RA = 176
69696 deg
ZDOT = -5643
952230 TA = 51
98920
MA = 51
85988
Ha = 219
879 n
mi
Hp = 212
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20558516
92 X = 6277168
67
Y = -5966097
57 feet Y = -1748332
30 meter
Z = 6035516
64 Z = 1870091
75
XDOT = 9562
156630 XDOT = 2893
646256
YDOT = 14111
922422 feet/sec YDOT = 4333
789634 meter/sec
ZDOT = -18516
903643 ZDOT = -5629
844741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19045957
02 X = -5805207
70
Y = -9689863
78 feet Y = -2953470
48 meter
Z = 6167046
33 Z = 1879715
72
XDOT = 1888
882314 XDOT = 575
731329
YDOT = -15524
610884 feet/sec YDOT = -4731
901397 meter/sec
ZDOT = -18456
845399 ZDOT = -5625
646478
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 15221
53587058
00016717 00000-0 10270-3 0 9065
2 25544 51
6403 177
6638 0001527 34
4706 325
6546 15
55055731 36342
Satellite: ISS
Catalog Number: 25544
Epoch time: 15221
53587058 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 177
6638 deg
Eccentricity:
0001527
Arg of perigee: 34
4706 deg
Mean anomaly: 325
6546 deg
Mean motion: 15
55055731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3634
Checksum: 311
Coasting Arc #8 (Orbit 3649)
---------------------------------------
Vector Time (GMT): 2015/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6722749
88 A = 6786570
23 meter
Y = 867571
72 meter E =
0013762
Z = 138112
39 I = 51
70682
XDOT = -479
601181 Wp = 46
01621
YDOT = -4732
329860 meter/sec RA = 171
72484 deg
ZDOT = 6018
657923 TA = 315
47107
MA = 315
58158
Ha = 219
868 n
mi
Hp = 212
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22056266
01 X = -6732622
51
Y = 2846363
91 feet Y = 792338
31 meter
Z = 453124
65 Z = 105431
15
XDOT = -1573
494689 XDOT = -455
883400
YDOT = -15526
016601 feet/sec YDOT = -4737
560638 meter/sec
ZDOT = 19746
253028 ZDOT = 6016
385619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18255380
04 X = 5564239
84
Y = 12705495
51 feet Y = 3872635
03 meter
Z = 312190
57 Z = 95155
68
XDOT = -8240
312052 XDOT = -2511
647113
YDOT = 11312
308527 feet/sec YDOT = 3447
991639 meter/sec
ZDOT = 19737
243019 ZDOT = 6015
911672
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 15222
56408268
00016717 00000-0 10270-3 0 9075
2 25544 51
6403 172
5306 0001477 38
5156 321
6102 15
55077752 36505
Satellite: ISS
Catalog Number: 25544
Epoch time: 15222
56408268 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 172
5306 deg
Eccentricity:
0001477
Arg of perigee: 38
5156 deg
Mean anomaly: 321
6102 deg
Mean motion: 15
55077752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3650
Checksum: 294
Coasting Arc #9 (Orbit 3664)
---------------------------------------
Vector Time (GMT): 2015/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6434050
64 A = 6784668
80 meter
Y = 218792
88 meter E =
0006335
Z = -2138917
32 I = 51
73303
XDOT = -1995
818366 Wp = 125
40165
YDOT = 4937
873467 meter/sec RA = 166
75407 deg
ZDOT = -5513
572860 TA = 78
27568
MA = 78
20461
Ha = 219
912 n
mi
Hp = 212
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21109090
03 X = 6441515
72
Y = 717824
41 feet Y = 290784
45 meter
Z = -7017445
27 Z = -2107644
41
XDOT = -6547
960519 XDOT = -2024
104164
YDOT = 16200
372268 feet/sec YDOT = 4915
396878 meter/sec
ZDOT = -18089
149802 ZDOT = -5523
336571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15442619
02 X = -4706910
28
Y = -14474354
04 feet Y = -4411783
11 meter
Z = -6882738
15 Z = -2097858
59
XDOT = 14454
924185 XDOT = 4405
860891
YDOT = -6823
864038 feet/sec YDOT = -2079
913759 meter/sec
ZDOT = -18132
030271 ZDOT = -5526
642826
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 15223
52802394
00016717 00000-0 10270-3 0 9081
2 25544 51
6415 167
7180 0001544 37
9332 322
1930 15
55088259 36653
Satellite: ISS
Catalog Number: 25544
Epoch time: 15223
52802394 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 167
7180 deg
Eccentricity:
0001544
Arg of perigee: 37
9332 deg
Mean anomaly: 322
1930 deg
Mean motion: 15
55088259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3665
Checksum: 308
Coasting Arc #10 (Orbit 3680)
---------------------------------------
Vector Time (GMT): 2015/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5442641
02 A = 6780460
24 meter
Y = -1359958
87 meter E =
0012491
Z = 3797761
41 I = 51
75034
XDOT = 4168
160253 Wp = 91
55155
YDOT = -4871
959139 meter/sec RA = 161
77552 deg
ZDOT = 4216
552560 TA = 313
99639
MA = 314
09929
Ha = 219
962 n
mi
Hp = 212
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17856433
79 X = -5445476
84
Y = -4461807
32 feet Y = -1420837
95 meter
Z = 12459847
14 Z = 3771315
77
XDOT = 13675
066447 XDOT = 4201
847890
YDOT = -15984
117910 feet/sec YDOT = -4825
159709 meter/sec
ZDOT = 13833
833859 ZDOT = 4236
882029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10814994
91 X = 3296410
45
Y = 14987233
39 feet Y = 4568108
74 meter
Z = 12346111
28 Z = 3763094
72
XDOT = -19601
846639 XDOT = -5974
642856
YDOT = 2642
646607 feet/sec YDOT = 805
478686 meter/sec
ZDOT = 13922
238115 ZDOT = 4243
498178
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 15224
55621857
00016717 00000-0 10270-3 0 9099
2 25544 51
6420 162
5852 0001461 42
8627 317
2640 15
55110093 36811
Satellite: ISS
Catalog Number: 25544
Epoch time: 15224
55621857 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 162
5852 deg
Eccentricity:
0001461
Arg of perigee: 42
8627 deg
Mean anomaly: 317
2640 deg
Mean motion: 15
55110093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3681
Checksum: 294
Coasting Arc #11 (Orbit 3695)
---------------------------------------
Vector Time (GMT): 2015/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3894803
26 A = 6776246
79 meter
Y = 2557860
34 meter E =
0013488
Z = -4932463
78 I = 51
76694
XDOT = -5805
882350 Wp = 70
35331
YDOT = 4444
995450 meter/sec RA = 156
78373 deg
ZDOT = -2280
057399 TA = 177
38003
MA = 177
37296
Ha = 219
879 n
mi
Hp = 212
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12778225
91 X = 3889870
71
Y = 8391930
24 feet Y = 2601386
97 meter
Z = -16182623
96 Z = -4913556
00
XDOT = -19048
170441 XDOT = -5844
080438
YDOT = 14583
318404 feet/sec YDOT = 4379
856662 meter/sec
ZDOT = -7480
503279 ZDOT = -2308
353441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4670699
85 X = -1423629
32
Y = -14646136
10 feet Y = -4464142
28 meter
Z = -16101556
73 Z = -4907754
49
XDOT = 22872
216943 XDOT = 6971
451724
YDOT = 1062
345174 feet/sec YDOT = 323
802809 meter/sec
ZDOT = -7603
180961 ZDOT = -2317
449557
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 15225
52014375
00016717 00000-0 10270-3 0 9100
2 25544 51
6426 157
7724 0001575 44
1010 316
0268 15
55120984 36967
Satellite: ISS
Catalog Number: 25544
Epoch time: 15225
52014375 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 157
7724 deg
Eccentricity:
0001575
Arg of perigee: 44
1010 deg
Mean anomaly: 316
0268 deg
Mean motion: 15
55120984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3696
Checksum: 291
Coasting Arc #12 (Orbit 3710)
---------------------------------------
Vector Time (GMT): 2015/226/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4776270
94 A = 6777642
19 meter
Y = -1528864
35 meter E =
0009468
Z = 4552629
46 I = 51
79827
XDOT = 4658
929254 Wp = 105
37794
YDOT = -5238
637148 meter/sec RA = 152
15437 deg
ZDOT = 3120
706935 TA = 313
41822
MA = 313
49698
Ha = 219
900 n
mi
Hp = 212
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15670180
26 X = -4780934
32
Y = -5015959
16 feet Y = -1582301
71 meter
Z = 14936448
36 Z = 4529416
48
XDOT = 15285
200963 XDOT = 4702
003804
YDOT = -17187
129751 feet/sec YDOT = -5186
297018 meter/sec
ZDOT = 10238
539814 ZDOT = 3143
443366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2563347
04 X = 781308
18
Y = 16343653
78 feet Y = 4981545
67 meter
Z = 14836647
81 Z = 4522210
25
XDOT = -20985
733528 XDOT = -6396
451579
YDOT = -6116
324619 feet/sec YDOT = -1864
255744 meter/sec
ZDOT = 10337
396926 ZDOT = 3150
838583
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 15226
48405901
00016717 00000-0 10270-3 0 9116
2 25544 51
6420 152
9602 0001371 46
6209 313
5058 15
55157917 37117
Satellite: ISS
Catalog Number: 25544
Epoch time: 15226
48405901 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 152
9602 deg
Eccentricity:
0001371
Arg of perigee: 46
6209 deg
Mean anomaly: 313
5058 deg
Mean motion: 15
55157917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3711
Checksum: 287
Coasting Arc #13 (Orbit 3725)
---------------------------------------
Vector Time (GMT): 2015/227/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3136060
81 A = 6774754
95 meter
Y = 2907187
76 meter E =
0015658
Z = -5268252
88 I = 51
81632
XDOT = -5955
441510 Wp = 79
70874
YDOT = 4722
705276 meter/sec RA = 147
15881 deg
ZDOT = -938
633795 TA = 181
31880
MA = 181
32293
Ha = 219
863 n
mi
Hp = 212
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10288913
42 X = 3128909
53
Y = 9538017
57 feet Y = 2942217
05 meter
Z = -17284294
22 Z = -5253036
31
XDOT = -19538
850098 XDOT = -6003
249883
YDOT = 15494
439883 feet/sec YDOT = 4655
840264 meter/sec
ZDOT = -3079
507203 ZDOT = -967
679897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3646711
18 X = 1111517
57
Y = -13630249
25 feet Y = -4154499
97 meter
Z = -17219179
67 Z = -5248405
96
XDOT = 21770
162357 XDOT = 6635
545486
YDOT = 9875
501830 feet/sec YDOT = 3010
052958 meter/sec
ZDOT = -3205
487683 ZDOT = -977
032646
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 15227
44796904
00016717 00000-0 10270-3 0 9120
2 25544 51
6422 148
1471 0001514 47
8478 312
2803 15
55131591 37260
Satellite: ISS
Catalog Number: 25544
Epoch time: 15227
44796904 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 148
1471 deg
Eccentricity:
0001514
Arg of perigee: 47
8478 deg
Mean anomaly: 312
2803 deg
Mean motion: 15
55131591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3726
Checksum: 304
Coasting Arc #14 (Orbit 3741)
---------------------------------------
Vector Time (GMT): 2015/228/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1269337
36 A = 6774962
98 meter
Y = -4170258
89 meter E =
0005871
Z = 5182907
93 I = 51
84401
XDOT = 6565
301751 Wp = 54
19689
YDOT = -3723
244370 meter/sec RA = 142
16192 deg
ZDOT = -1383
444086 TA = 49
08343
MA = 49
03260
Ha = 219
896 n
mi
Hp = 212
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4164492
64 X = -1247786
35
Y = -13681951
75 feet Y = -4184332
67 meter
Z = 17004291
11 Z = 5176794
42
XDOT = 21539
703909 XDOT = 6613
168156
YDOT = -12215
368668 feet/sec YDOT = -3649
559290 meter/sec
ZDOT = -4538
858550 ZDOT = -1351
435236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9978381
61 X = -3041410
72
Y = 10288002
48 feet Y = 3135783
16 meter
Z = 16978622
56 Z = 5175084
16
XDOT = -20283
510856 XDOT = -6182
414109
YDOT = -12387
070435 feet/sec YDOT = -3775
579069 meter/sec
ZDOT = -4400
258372 ZDOT = -1341
198752
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 15228
47612942
00016717 00000-0 10270-3 0 9134
2 25544 51
6426 143
0145 0001537 50
1691 309
9597 15
55152006 37420
Satellite: ISS
Catalog Number: 25544
Epoch time: 15228
47612942 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 143
0145 deg
Eccentricity:
0001537
Arg of perigee: 50
1691 deg
Mean anomaly: 309
9597 deg
Mean motion: 15
55152006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3742
Checksum: 298
Coasting Arc #15 (Orbit 3756)
---------------------------------------
Vector Time (GMT): 2015/229/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -565413
88 A = 6778294
57 meter
Y = 5176649
35 meter E =
0009616
Z = -4348521
85 I = 51
87972
XDOT = -6442
078228 Wp = 103
09566
YDOT = 2230
070868 meter/sec RA = 137
17183 deg
ZDOT = 3496
763940 TA = 202
34307
MA = 202
38499
Ha = 219
836 n
mi
Hp = 212
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1855032
41 X = -602135
22
Y = 16983757
70 feet Y = 5170120
92 meter
Z = -14266803
98 Z = -4351358
00
XDOT = -21135
427258 XDOT = -6483
522348
YDOT = 7316
505472 feet/sec YDOT = 2157
799810 meter/sec
ZDOT = 11472
322638 ZDOT = 3465
369239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15647570
70 X = 4769379
55
Y = -6831488
79 feet Y = -2082237
78 meter
Z = -14279886
51 Z = -4352509
41
XDOT = 16318
109492 XDOT = 4973
759773
YDOT = 13709
759187 feet/sec YDOT = 4178
734600 meter/sec
ZDOT = 11336
604464 ZDOT = 3455
397041
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 15229
44002107
00016717 00000-0 10270-3 0 9149
2 25544 51
6425 138
2016 0001521 51
9365 308
1925 15
55162438 37574
Satellite: ISS
Catalog Number: 25544
Epoch time: 15229
44002107 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 138
2016 deg
Eccentricity:
0001521
Arg of perigee: 51
9365 deg
Mean anomaly: 308
1925 deg
Mean motion: 15
55162438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3757
Checksum: 287
Coasting Arc #16 (Orbit 3772)
---------------------------------------
Vector Time (GMT): 2015/230/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2212412
36 A = 6782829
47 meter
Y = -5745032
96 meter E =
0014497
Z = 2832916
35 I = 51
91809
XDOT = 5710
526594 Wp = 95
36691
YDOT = -332
844246 meter/sec RA = 132
19755 deg
ZDOT = -5113
616466 TA = 52
55462
MA = 52
42282
Ha = 219
816 n
mi
Hp = 212
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7258570
72 X = 2262729
18
Y = -18848533
32 feet Y = -5720010
78 meter
Z = 9294344
99 Z = 2843786
30
XDOT = 18735
323470 XDOT = 5738
663867
YDOT = -1092
008681 feet/sec YDOT = -268
828407 meter/sec
ZDOT = -16776
956911 ZDOT = -5085
807797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19893491
27 X = -6063536
14
Y = 3363310
04 feet Y = 1025136
90 meter
Z = 9342165
53 Z = 2847492
05
XDOT = -10260
260458 XDOT = -3127
327388
YDOT = -14228
930348 feet/sec YDOT = -4336
977970 meter/sec
ZDOT = -16657
004209 ZDOT = -5077
054883
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 15230
46816335
00016717 00000-0 10270-3 0 9150
2 25544 51
6428 133
0681 0001543 54
9537 305
1761 15
55181373 37738
Satellite: ISS
Catalog Number: 25544
Epoch time: 15230
46816335 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 133
0681 deg
Eccentricity:
0001543
Arg of perigee: 54
9537 deg
Mean anomaly: 305
1761 deg
Mean motion: 15
55181373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3773
Checksum: 302
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