[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 13th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 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
There are no maneuvers
Coasting Arc #1 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2020/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6168348
50 A = 6800022
67 meter
Y = -960508
55 meter E =
0007072
Z = -2693907
24 I = 51
73002
XDOT = 3002
885988 Wp = 49
09264
YDOT = 4760
021149 meter/sec RA = 11
05262 deg
ZDOT = 5192
083078 TA = 280
59822
MA = 280
67787
Ha = 229
010 n
mi
Hp = 221
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20237363
85 X = 6191716
12
Y = -3151274
77 feet Y = -891398
68 meter
Z = -8838278
35 Z = -2663887
40
XDOT = 9851
988148 XDOT = 2924
214850
YDOT = 15616
867286 feet/sec YDOT = 4793
161019 meter/sec
ZDOT = 17034
393300 ZDOT = 5206
479352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 287170
74 X = 87529
64
Y = -20538326
25 feet Y = -6260081
84 meter
Z = -8700073
59 Z = -2651782
43
XDOT = 15528
391419 XDOT = 4733
053705
YDOT = -7007
609007 feet/sec YDOT = -2135
919225 meter/sec
ZDOT = 17100
239284 ZDOT = 5212
152934
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 20164
50534843
00016717 00000-0 10270-3 0 9002
2 25544 51
6430 11
6483 0002140 38
9086 321
2218 15
49440635 31289
Satellite: ISS
Catalog Number: 25544
Epoch time: 20164
50534843 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 11
6483 deg
Eccentricity:
0002140
Arg of perigee: 38
9086 deg
Mean anomaly: 321
2218 deg
Mean motion: 15
49440635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 275
Coasting Arc #2 (Orbit 3143)
---------------------------------------
Vector Time (GMT): 2020/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6154787
17 A = 6800244
20 meter
Y = 1357412
02 meter E =
0014809
Z = 2538038
61 I = 51
69768
XDOT = -3190
698723 Wp = 96
08937
YDOT = -4539
268887 meter/sec RA = 6
10796 deg
ZDOT = -5284
764854 TA = 55
48615
MA = 55
34641
Ha = 229
004 n
mi
Hp = 221
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20192871
30 X = -6181837
01
Y = 4453451
51 feet Y = 1288433
25 meter
Z = 8326898
34 Z = 2508075
65
XDOT = -10468
171665 XDOT = -3114
031877
YDOT = -14892
614458 feet/sec YDOT = -4574
520246 meter/sec
ZDOT = -17338
467368 ZDOT = -5300
078294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1360730
83 X = 414750
76
Y = 20688457
90 feet Y = 6305841
97 meter
Z = 8188933
93 Z = 2495987
06
XDOT = -14771
002282 XDOT = -4502
201496
YDOT = 7895
225630 feet/sec YDOT = 2406
464772 meter/sec
ZDOT = -17408
545995 ZDOT = -5306
124819
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 20165
53729673
00016717 00000-0 10270-3 0 9014
2 25544 51
6428 6
5403 0002323 40
0167 320
1154 15
49482732 31447
Satellite: ISS
Catalog Number: 25544
Epoch time: 20165
53729673 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 6
5403 deg
Eccentricity:
0002323
Arg of perigee: 40
0167 deg
Mean anomaly: 320
1154 deg
Mean motion: 15
49482732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 275
Coasting Arc #3 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2020/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6096567
16 A = 6800609
07 meter
Y = -1790303
27 meter E =
0007785
Z = -2419606
47 I = 51
66302
XDOT = 3382
661404 Wp = 46
54331
YDOT = 4303
888018 meter/sec RA = 1
16066 deg
ZDOT = 5354
679622 TA = 286
47538
MA = 286
56091
Ha = 229
087 n
mi
Hp = 221
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20001860
76 X = 6127886
81
Y = -5873698
41 feet Y = -1721951
71 meter
Z = -7938341
44 Z = -2389915
90
XDOT = 11097
970485 XDOT = 3308
272697
YDOT = 14120
367513 feet/sec YDOT = 4341
298774 meter/sec
ZDOT = 17567
846530 ZDOT = 5370
931094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3149762
96 X = -960047
75
Y = -20659282
74 feet Y = -6296949
38 meter
Z = -7801606
37 Z = -2377929
62
XDOT = 13951
553231 XDOT = 4252
433425
YDOT = -8769
119592 feet/sec YDOT = -2672
827652 meter/sec
ZDOT = 17642
253768 ZDOT = 5377
358948
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 20166
50475026
00016717 00000-0 10270-3 0 9023
2 25544 51
6410 1
7514 0002148 49
2425 310
8911 15
49438426 31595
Satellite: ISS
Catalog Number: 25544
Epoch time: 20166
50475026 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 1
7514 deg
Eccentricity:
0002148
Arg of perigee: 49
2425 deg
Mean anomaly: 310
8911 deg
Mean motion: 15
49438426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 282
Coasting Arc #4 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2020/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6022645
49 A = 6800785
60 meter
Y = 2190491
32 meter E =
0014922
Z = 2258088
19 I = 51
63101
XDOT = -3533
637234 Wp = 100
90959
YDOT = -4080
885824 meter/sec RA = 356
21134 deg
ZDOT = -5438
179794 TA = 54
01136
MA = 53
87309
Ha = 228
971 n
mi
Hp = 221
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19759335
59 X = -6057661
12
Y = 7186651
32 feet Y = 2122945
74 meter
Z = 7408425
80 Z = 2228747
69
XDOT = -11593
298012 XDOT = -3461
325304
YDOT = -13388
733018 feet/sec YDOT = -4119
996469 meter/sec
ZDOT = -17841
797226 ZDOT = -5455
169743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4837290
93 X = 1474406
27
Y = 20510097
34 feet Y = 6251477
67 meter
Z = 7273279
64 Z = 2216895
63
XDOT = -13136
007692 XDOT = -4003
855144
YDOT = 9485
724262 feet/sec YDOT = 2891
248755 meter/sec
ZDOT = -17919
613199 ZDOT = -5461
898103
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 20167
53669693
00016717 00000-0 10270-3 0 9033
2 25544 51
6417 356
6431 0002136 45
6438 314
4887 15
49487269 31752
Satellite: ISS
Catalog Number: 25544
Epoch time: 20167
53669693 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 356
6431 deg
Eccentricity:
0002136
Arg of perigee: 45
6438 deg
Mean anomaly: 314
4887 deg
Mean motion: 15
49487269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 339
Coasting Arc #5 (Orbit 3189)
---------------------------------------
Vector Time (GMT): 2020/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5899981
18 A = 6801131
03 meter
Y = -2619116
47 meter E =
0008549
Z = -2134662
37 I = 51
59731
XDOT = 3689
547116 Wp = 44
87268
YDOT = 3844
016915 meter/sec RA = 351
25889 deg
ZDOT = 5500
508646 TA = 291
50912
MA = 291
60024
Ha = 229
129 n
mi
Hp = 221
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19356893
63 X = 5939199
44
Y = -8592901
80 feet Y = -2552919
10 meter
Z = -7003485
45 Z = -2105907
53
XDOT = 12104
813374 XDOT = 3619
569511
YDOT = 12611
604051 feet/sec YDOT = 3884
884032 meter/sec
ZDOT = 18046
288208 ZDOT = 5518
261678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6628826
91 X = -2020466
44
Y = -20159960
32 feet Y = -6144755
90 meter
Z = -6871008
28 Z = -2094283
32
XDOT = 12267
378412 XDOT = 3739
096940
YDOT = -10189
890920 feet/sec YDOT = -3105
878752 meter/sec
ZDOT = 18127
627070 ZDOT = 5525
300731
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 20168
50414832
00016717 00000-0 10270-3 0 9045
2 25544 51
6407 351
8535 0002162 57
7499 302
3861 15
49442652 31905
Satellite: ISS
Catalog Number: 25544
Epoch time: 20168
50414832 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 351
8535 deg
Eccentricity:
0002162
Arg of perigee: 57
7499 deg
Mean anomaly: 302
3861 deg
Mean motion: 15
49442652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3190
Checksum: 304
Coasting Arc #6 (Orbit 3205)
---------------------------------------
Vector Time (GMT): 2020/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5765416
22 A = 6801300
91 meter
Y = 3011048
60 meter E =
0015199
Z = 1966348
60 I = 51
56485
XDOT = -3806
088885 Wp = 105
32263
YDOT = -3626
130996 meter/sec RA = 346
30511 deg
ZDOT = -5574
844104 TA = 52
99693
MA = 52
85793
Ha = 229
040 n
mi
Hp = 221
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18915407
53 X = -5808209
61
Y = 9878768
37 feet Y = 2946336
03 meter
Z = 6451274
95 Z = 1938238
82
XDOT = -12487
168257 XDOT = -3738
177964
YDOT = -11896
755235 feet/sec YDOT = -3668
312814 meter/sec
ZDOT = -18290
170944 ZDOT = -5593
168332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8292616
60 X = 2527589
54
Y = 19704561
74 feet Y = 6005950
42 meter
Z = 6321741
18 Z = 1926866
71
XDOT = -11433
718721 XDOT = -3484
997466
YDOT = 10741
255189 feet/sec YDOT = 3273
934582 meter/sec
ZDOT = -18374
149061 ZDOT = -5600
440634
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 20169
53609135
00016717 00000-0 10270-3 0 9052
2 25544 51
6405 346
7452 0002173 55
6480 304
4876 15
49484340 32060
Satellite: ISS
Catalog Number: 25544
Epoch time: 20169
53609135 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 346
7452 deg
Eccentricity:
0002173
Arg of perigee: 55
6480 deg
Mean anomaly: 304
4876 deg
Mean motion: 15
49484340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3206
Checksum: 306
Coasting Arc #7 (Orbit 3220)
---------------------------------------
Vector Time (GMT): 2020/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5577928
42 A = 6801608
25 meter
Y = -3424932
80 meter E =
0009364
Z = -1839115
95 I = 51
53233
XDOT = 3931
271911 Wp = 45
22340
YDOT = 3393
021432 meter/sec RA = 341
34876 deg
ZDOT = 5628
686920 TA = 294
56527
MA = 294
66283
Ha = 229
203 n
mi
Hp = 221
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18300290
10 X = 5624745
90
Y = -11236656
17 feet Y = -3362294
34 meter
Z = -6033844
97 Z = -1811907
26
XDOT = 12897
873723 XDOT = 3865
696849
YDOT = 11131
960079 feet/sec YDOT = 3436
616079 meter/sec
ZDOT = 18466
820603 ZDOT = 5647
624944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10025375
29 X = -3055734
39
Y = -19030309
15 feet Y = -5800438
23 meter
Z = -5908428
62 Z = -1800889
04
XDOT = 10549
163612 XDOT = 3215
385069
YDOT = -11292
777715 feet/sec YDOT = -3442
038648 meter/sec
ZDOT = 18553
636434 ZDOT = 5655
148385
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 20170
50354125
00016717 00000-0 10270-3 0 9068
2 25544 51
6397 341
9562 0002257 69
3302 290
8090 15
49444122 32214
Satellite: ISS
Catalog Number: 25544
Epoch time: 20170
50354125 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 341
9562 deg
Eccentricity:
0002257
Arg of perigee: 69
3302 deg
Mean anomaly: 290
8090 deg
Mean motion: 15
49444122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3221
Checksum: 286
Coasting Arc #8 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2020/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5382497
23 A = 6801779
80 meter
Y = 3798636
44 meter E =
0015371
Z = 1665840
20 I = 51
50181
XDOT = -4020
770645 Wp = 110
06114
YDOT = -3184
213556 meter/sec RA = 336
39052 deg
ZDOT = -5692
851731 TA = 51
68457
MA = 51
54647
Ha = 229
091 n
mi
Hp = 221
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17659111
66 X = -5432666
41
Y = 12462717
97 feet Y = 3738164
69 meter
Z = 5465354
98 Z = 1639572
89
XDOT = -13191
504741 XDOT = -3957
212252
YDOT = -10446
894869 feet/sec YDOT = -3228
820204 meter/sec
ZDOT = -18677
335077 ZDOT = -5712
229396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11606583
27 X = 3537686
58
Y = 18269098
47 feet Y = 5568421
21 meter
Z = 5344243
12 Z = 1628925
30
XDOT = -9725
713046 XDOT = -2964
397336
YDOT = 11705
484633 feet/sec YDOT = 3567
831716 meter/sec
ZDOT = -18766
187491 ZDOT = -5719
933947
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 20171
53548319
00016717 00000-0 10270-3 0 9073
2 25544 51
6399 336
8478 0002144 67
4530 292
6847 15
49473277 32372
Satellite: ISS
Catalog Number: 25544
Epoch time: 20171
53548319 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 336
8478 deg
Eccentricity:
0002144
Arg of perigee: 67
4530 deg
Mean anomaly: 292
6847 deg
Mean motion: 15
49473277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 339
Coasting Arc #9 (Orbit 3251)
---------------------------------------
Vector Time (GMT): 2020/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5132961
68 A = 6801992
68 meter
Y = -4185965
39 meter E =
0010189
Z = -1534158
51 I = 51
47362
XDOT = 4119
296315 Wp = 45
55610
YDOT = 2959
267749 meter/sec RA = 331
42974 deg
ZDOT = 5738
492194 TA = 297
67935
MA = 297
78270
Ha = 229
222 n
mi
Hp = 221
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16840425
45 X = 5186840
97
Y = -13733482
25 feet Y = -4128263
38 meter
Z = -5033328
45 Z = -1509094
55
XDOT = 13514
751689 XDOT = 4058
024402
YDOT = 9708
883692 feet/sec YDOT = 3004
988880 meter/sec
ZDOT = 18827
074128 ZDOT = 5758
353948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13214257
34 X = -4027705
64
Y = -17284161
82 feet Y = -5268212
52 meter
Z = -4917724
31 Z = -1498922
37
XDOT = 8852
130005 XDOT = 2698
129226
YDOT = -12121
109144 feet/sec YDOT = -3694
514067 meter/sec
ZDOT = 18918
170999 ZDOT = 5766
258520
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 20172
50292943
00016717 00000-0 10270-3 0 9081
2 25544 51
6415 332
0586 0002325 76
7711 283
3698 15
49456334 32527
Satellite: ISS
Catalog Number: 25544
Epoch time: 20172
50292943 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 332
0586 deg
Eccentricity:
0002325
Arg of perigee: 76
7711 deg
Mean anomaly: 283
3698 deg
Mean motion: 15
49456334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3252
Checksum: 312
Coasting Arc #10 (Orbit 3267)
---------------------------------------
Vector Time (GMT): 2020/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4880507
49 A = 6802187
18 meter
Y = 4530233
57 meter E =
0015529
Z = 1355335
04 I = 51
44416
XDOT = -4186
640244 Wp = 114
18327
YDOT = -2763
639717 meter/sec RA = 326
46752 deg
ZDOT = -5792
059136 TA = 51
04052
MA = 50
90225
Ha = 229
182 n
mi
Hp = 221
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16012163
69 X = -4937386
61
Y = 14862971
03 feet Y = 4475337
94 meter
Z = 4446637
26 Z = 1331490
32
XDOT = -13735
696340 XDOT = -4127
290818
YDOT = -9067
059440 feet/sec YDOT = -2810
124633 meter/sec
ZDOT = -19002
818689 ZDOT = -5812
252586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14649966
49 X = 4465309
79
Y = 16237059
48 feet Y = 4949055
73 meter
Z = 4336618
29 Z = 1321801
25
XDOT = -8063
060552 XDOT = -2457
620856
YDOT = 12416
621258 feet/sec YDOT = 3784
586160 meter/sec
ZDOT = -19095
458867 ZDOT = -5820
295863
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 20173
53486854
00016717 00000-0 10270-3 0 9092
2 25544 51
6404 326
9503 0002306 77
7934 282
3474 15
49464540 32689
Satellite: ISS
Catalog Number: 25544
Epoch time: 20173
53486854 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 326
9503 deg
Eccentricity:
0002306
Arg of perigee: 77
7934 deg
Mean anomaly: 282
3474 deg
Mean motion: 15
49464540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3268
Checksum: 325
Coasting Arc #11 (Orbit 3282)
---------------------------------------
Vector Time (GMT): 2020/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4572695
84 A = 6802345
24 meter
Y = -4880777
26 meter E =
0010949
Z = -1220448
54 I = 51
41851
XDOT = 4265
360318 Wp = 46
63270
YDOT = 2548
775203 meter/sec RA = 321
50398 deg
ZDOT = 5828
589395 TA = 300
09143
MA = 300
19994
Ha = 229
238 n
mi
Hp = 221
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15002282
94 X = 4632862
49
Y = -16013048
74 feet Y = -4829305
44 meter
Z = -4004096
25 Z = -1198091
23
XDOT = 13993
964299 XDOT = 4208
230410
YDOT = 8362
123369 feet/sec YDOT = 2596
152828 meter/sec
ZDOT = 19122
668620 ZDOT = 5849
170482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16073101
01 X = -4899081
19
Y = -14965207
41 feet Y = -4561395
22 meter
Z = -3900897
49 Z = -1188993
55
XDOT = 7216
526768 XDOT = 2199
597359
YDOT = -12724
532405 feet/sec YDOT = -3878
437477 meter/sec
ZDOT = 19217
112472 ZDOT = 5857
375881
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 20174
50231248
00016717 00000-0 10270-3 0 9107
2 25544 51
6417 322
1623 0002353 84
4450 275
6969 15
49455967 32838
Satellite: ISS
Catalog Number: 25544
Epoch time: 20174
50231248 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 322
1623 deg
Eccentricity:
0002353
Arg of perigee: 84
4450 deg
Mean anomaly: 275
6969 deg
Mean motion: 15
49455967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3283
Checksum: 309
Coasting Arc #12 (Orbit 3298)
---------------------------------------
Vector Time (GMT): 2020/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4267224
06 A = 6802500
73 meter
Y = 5186133
58 meter E =
0015355
Z = 1038146
60 I = 51
39342
XDOT = -4318
204413 Wp = 118
54751
YDOT = -2366
042783 meter/sec RA = 316
53792 deg
ZDOT = -5870
830849 TA = 50
17933
MA = 50
04429
Ha = 229
166 n
mi
Hp = 221
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14000078
92 X = -4329942
46
Y = 17014873
96 feet Y = 5138063
55 meter
Z = 3405992
79 Z = 1017267
06
XDOT = -14167
337314 XDOT = -4262
908887
YDOT = -7762
607556 feet/sec YDOT = -2414
021650 meter/sec
ZDOT = -19261
256067 ZDOT = -5891
672934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17308388
51 X = 5275596
82
Y = 13659257
69 feet Y = 4163341
74 meter
Z = 3309576
88 Z = 1008759
03
XDOT = -6468
458808 XDOT = -1971
586245
YDOT = 12934
975478 feet/sec YDOT = 3942
580526 meter/sec
ZDOT = -19356
919431 ZDOT = -5899
989042
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 20175
53425033
00016717 00000-0 10270-3 0 9119
2 25544 51
6417 317
0539 0002245 86
3955 273
7452 15
49462338 32991
Satellite: ISS
Catalog Number: 25544
Epoch time: 20175
53425033 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 317
0539 deg
Eccentricity:
0002245
Arg of perigee: 86
3955 deg
Mean anomaly: 273
7452 deg
Mean motion: 15
49462338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3299
Checksum: 314
Coasting Arc #13 (Orbit 3313)
---------------------------------------
Vector Time (GMT): 2020/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3908237
97 A = 6802608
92 meter
Y = -5489436
69 meter E =
0011752
Z = -899239
45 I = 51
37168
XDOT = 4381
866253 Wp = 47
68577
YDOT = 2162
856438 meter/sec RA = 311
57070 deg
ZDOT = 5898
377224 TA = 302
56599
MA = 302
67943
Ha = 229
227 n
mi
Hp = 221
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12822303
06 X = 3973699
95
Y = -18009962
88 feet Y = -5445365
80 meter
Z = -2950260
65 Z = -880097
06
XDOT = 14376
201618 XDOT = 4328
704370
YDOT = 7095
985690 feet/sec YDOT = 2211
559246 meter/sec
ZDOT = 19351
631311 ZDOT = 5919
533586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18489788
57 X = -5635687
56
Y = -12141331
70 feet Y = -3700677
90 meter
Z = -2861824
56 Z = -872284
12
XDOT = 5659
710783 XDOT = 1725
079847
YDOT = -13157
618857 feet/sec YDOT = -4010
442228 meter/sec
ZDOT = 19448
760496 ZDOT = 5927
982199
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 20176
50169059
00016717 00000-0 10270-3 0 9121
2 25544 51
6432 312
2657 0002356 88
2265 271
9155 15
49460117 33145
Satellite: ISS
Catalog Number: 25544
Epoch time: 20176
50169059 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 312
2657 deg
Eccentricity:
0002356
Arg of perigee: 88
2265 deg
Mean anomaly: 271
9155 deg
Mean motion: 15
49460117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3314
Checksum: 300
Coasting Arc #14 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2020/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3557913
33 A = 6802718
41 meter
Y = 5746346
30 meter E =
0015127
Z = 712760
39 I = 51
34962
XDOT = -4425
151572 Wp = 122
08570
YDOT = -1993
974071 meter/sec RA = 306
60218 deg
ZDOT = -5928
757697 TA = 50
19667
MA = 50
06360
Ha = 229
188 n
mi
Hp = 221
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11672944
01 X = -3625368
39
Y = 18852842
19 feet Y = 5706181
90 meter
Z = 2338452
72 Z = 695314
81
XDOT = -14518
213820 XDOT = -4373
727424
YDOT = -6541
909682 feet/sec YDOT = -2043
170779 meter/sec
ZDOT = -19451
304780 ZDOT = -5950
128440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19473345
85 X = 5935475
81
Y = 10622932
81 feet Y = 3237869
92 meter
Z = 2257817
88 Z = 688182
89
XDOT = -4958
872150 XDOT = -1511
464231
YDOT = 13306
650091 feet/sec YDOT = 4055
866948 meter/sec
ZDOT = -19549
436678 ZDOT = -5958
668299
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 20177
53362504
00016717 00000-0 10270-3 0 9136
2 25544 51
6422 307
1580 0002340 91
7943 268
3475 15
49466107 33305
Satellite: ISS
Catalog Number: 25544
Epoch time: 20177
53362504 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 307
1580 deg
Eccentricity:
0002340
Arg of perigee: 91
7943 deg
Mean anomaly: 268
3475 deg
Mean motion: 15
49466107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3330
Checksum: 295
Coasting Arc #15 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2020/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3155309
05 A = 6802809
11 meter
Y = -5994258
15 meter E =
0012444
Z = -571365
18 I = 51
33114
XDOT = 4480
165973 Wp = 49
71955
YDOT = 1800
430885 meter/sec RA = 301
63217 deg
ZDOT = 5946
598586 TA = 304
10070
MA = 304
21871
Ha = 229
222 n
mi
Hp = 221
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10352063
80 X = 3224879
44
Y = -19666201
27 feet Y = -5958584
16 meter
Z = -1874557
68 Z = -555870
00
XDOT = 14698
707261 XDOT = 4430
815290
YDOT = 5906
925476 feet/sec YDOT = 1850
254541 meter/sec
ZDOT = 19509
837879 ZDOT = 5968
241554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20368071
88 X = -6208188
31
Y = -8906732
73 feet Y = -2714772
14 meter
Z = -1802893
14 Z = -549521
83
XDOT = 4183
450444 XDOT = 1275
115695
YDOT = -13471
273702 feet/sec YDOT = -4106
044225 meter/sec
ZDOT = 19609
238495 ZDOT = 5976
895893
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 20178
50106324
00016717 00000-0 10270-3 0 9141
2 25544 51
6426 302
3701 0002357 94
3940 265
7480 15
49458056 33452
Satellite: ISS
Catalog Number: 25544
Epoch time: 20178
50106324 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 302
3701 deg
Eccentricity:
0002357
Arg of perigee: 94
3940 deg
Mean anomaly: 265
7480 deg
Mean motion: 15
49458056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 297
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