[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 26th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16491 3871 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
116/01:51:40
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 222
4
116/05:12:17
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 222
4
117/03:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 222
5
130/00:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
8
Coasting Arc #1 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2020/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3653715
34 A = 6791767
41 meter
Y = -2368311
27 meter E =
0004802
Z = 5210624
80 I = 51
24875
XDOT = 2995
877081 Wp = 144
40616
YDOT = 6971
807754 meter/sec RA = 253
20640 deg
ZDOT = 1063
739277 TA = 295
31508
MA = 295
36481
Ha = 228
431 n
mi
Hp = 222
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11987255
04 X = 3654616
25
Y = -7770050
11 feet Y = -2327447
83 meter
Z = 17095225
72 Z = 5228375
61
XDOT = 9828
993047 XDOT = 2912
526472
YDOT = 22873
385020 feet/sec YDOT = 7004
843732 meter/sec
ZDOT = 3489
958259 ZDOT = 1078
089948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5932587
07 X = 1808252
54
Y = -12887203
69 feet Y = -3928019
68 meter
Z = 17176702
14 Z = 5235458
81
XDOT = 19515
738850 XDOT = 5948
397201
YDOT = 13741
748068 feet/sec YDOT = 4188
484811 meter/sec
ZDOT = 3555
444399 ZDOT = 1083
699453
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 20115
55025535
00016717 00000-0 10270-3 0 9006
2 25544 51
6412 253
9365 0001875 191
5864 168
5243 15
49322413 23692
Satellite: ISS
Catalog Number: 25544
Epoch time: 20115
55025535 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 253
9365 deg
Eccentricity:
0001875
Arg of perigee: 191
5864 deg
Mean anomaly: 168
5243 deg
Mean motion: 15
49322413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2369
Checksum: 302
Coasting Arc #2 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2020/116/01:51:40
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2537183
66 A = 6793817
89 meter
Y = -4166677
62 meter E =
0008114
Z = 4725005
93 I = 51
26221
XDOT = 4337
836317 Wp = 128
05006
YDOT = 5710
734757 meter/sec RA = 250
35017 deg
ZDOT = 2698
551473 TA = 295
06743
MA = 295
15162
Ha = 228
383 n
mi
Hp = 222
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8324093
38 X = 2560636
33
Y = -13670202
16 feet Y = -4138173
99 meter
Z = 15501987
96 Z = 4737387
68
XDOT = 14231
746447 XDOT = 4260
546536
YDOT = 18736
006420 feet/sec YDOT = 5758
811320 meter/sec
ZDOT = 8853
515332 ZDOT = 2719
435755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7865553
34 X = 2397420
66
Y = 13875497
36 feet Y = 4229251
60 meter
Z = 15558927
73 Z = 4742361
17
XDOT = -22270
398271 XDOT = -6788
017393
YDOT = 2559
936638 feet/sec YDOT = 780
268687 meter/sec
ZDOT = 8949
015818 ZDOT = 2727
660021
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 20116
13077586
00016717 00000-0 10270-3 0 9015
2 25544 51
6418 251
0687 0001497 198
2885 161
8211 15
49332646 23781
Satellite: ISS
Catalog Number: 25544
Epoch time: 20116
13077586 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 251
0687 deg
Eccentricity:
0001497
Arg of perigee: 198
2885 deg
Mean anomaly: 161
8211 deg
Mean motion: 15
49332646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 320
Coasting Arc #3 (Orbit 2379)
---------------------------------------
Vector Time (GMT): 2020/116/05:12:17
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4632325
57 A = 6794379
56 meter
Y = 1987561
90 meter E =
0007606
Z = 4550526
93 I = 51
26751
XDOT = -5
098477 Wp = 73
28856
YDOT = 7026
925617 meter/sec RA = 249
61502 deg
ZDOT = -3057
593195 TA = 47
50578
MA = 47
44154
Ha = 228
217 n
mi
Hp = 222
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15197918
54 X = 4587651
52
Y = 6520872
38 feet Y = 2039113
97 meter
Z = 14929550
30 Z = 4572920
90
XDOT = -16
727288 XDOT = -68
822955
YDOT = 23054
217902 feet/sec YDOT = 7026
512366 meter/sec
ZDOT = -10031
473736 ZDOT = -3057
772576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -720167
07 X = -219506
92
Y = 16428827
43 feet Y = 5007506
60 meter
Z = 15032131
10 Z = 4581793
56
XDOT = -20327
001662 XDOT = -6195
670107
YDOT = 8307
738841 feet/sec YDOT = 2532
198799 meter/sec
ZDOT = -10032
592375 ZDOT = -3057
934156
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 20116
25977917
00016717 00000-0 10270-3 0 9026
2 25544 51
6434 250
4312 0001358 205
3896 154
7188 15
49355547 23807
Satellite: ISS
Catalog Number: 25544
Epoch time: 20116
25977917 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 250
4312 deg
Eccentricity:
0001358
Arg of perigee: 205
3896 deg
Mean anomaly: 154
7188 deg
Mean motion: 15
49355547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2380
Checksum: 317
Coasting Arc #4 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2020/117/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2837183
85 A = 6803434
79 meter
Y = 6176144
41 meter E =
0012721
Z = -34657
84 I = 51
30871
XDOT = -4362
540946 Wp = 141
08129
YDOT = 1977
282372 meter/sec RA = 245
09300 deg
ZDOT = -5980
157682 TA = 39
29303
MA = 39
20078
Ha = 228
485 n
mi
Hp = 222
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9308345
95 X = 2768077
85
Y = 20262940
96 feet Y = 6207485
42 meter
Z = -113706
81 Z = -21043
27
XDOT = -14312
798379 XDOT = -4355
278591
YDOT = 6487
146889 feet/sec YDOT = 1928
538189 meter/sec
ZDOT = -19619
939900 ZDOT = -6001
331838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21502541
99 X = -6553974
80
Y = 5906186
75 feet Y = 1800205
72 meter
Z = -51538
97 Z = -15709
08
XDOT = -3674
691374 XDOT = -1120
045931
YDOT = -13474
055499 feet/sec YDOT = -4106
892116 meter/sec
ZDOT = -19717
100562 ZDOT = -6009
772251
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 20117
16281290
00016717 00000-0 10270-3 0 9030
2 25544 51
6435 245
9620 0001532 201
5992 158
5093 15
49288840 23941
Satellite: ISS
Catalog Number: 25544
Epoch time: 20117
16281290 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 245
9620 deg
Eccentricity:
0001532
Arg of perigee: 201
5992 deg
Mean anomaly: 158
5093 deg
Mean motion: 15
49288840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 305
Coasting Arc #5 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2020/118/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3292443
06 A = 6803344
91 meter
Y = -5946272
27 meter E =
0011030
Z = 134231
87 I = 51
32445
XDOT = 4248
768904 Wp = 48
84779
YDOT = -2210
481401 meter/sec RA = 240
12099 deg
ZDOT = 5978
150524 TA = 312
60146
MA = 312
69444
Ha = 228
375 n
mi
Hp = 222
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10801978
55 X = -3226357
41
Y = -19508767
29 feet Y = -5982721
21 meter
Z = 440393
27 Z = 118398
41
XDOT = 13939
530525 XDOT = 4244
132532
YDOT = -7252
235567 feet/sec YDOT = -2162
994913 meter/sec
ZDOT = 19613
354736 ZDOT = 5998
778289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20868232
73 X = 6360637
33
Y = -7864483
92 feet Y = -2397094
70 meter
Z = 368026
56 Z = 112174
50
XDOT = 4601
109463 XDOT = 1402
418164
YDOT = 13189
021131 feet/sec YDOT = 4020
013641 meter/sec
ZDOT = 19708
026353 ZDOT = 6007
006432
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 20118
19484432
00016717 00000-0 10270-3 0 9048
2 25544 51
6440 240
8544 0001314 210
2721 149
8353 15
49317595 24102
Satellite: ISS
Catalog Number: 25544
Epoch time: 20118
19484432 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 240
8544 deg
Eccentricity:
0001314
Arg of perigee: 210
2721 deg
Mean anomaly: 149
8353 deg
Mean motion: 15
49317595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 284
Coasting Arc #6 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2020/119/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3702594
05 A = 6803418
18 meter
Y = 5693775
31 meter E =
0012094
Z = -268595
05 I = 51
34155
XDOT = -4140
916038 Wp = 143
13821
YDOT = 2417
983305 meter/sec RA = 235
15161 deg
ZDOT = -5975
246116 TA = 39
76245
MA = 39
67388
Ha = 228
439 n
mi
Hp = 222
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12147618
27 X = 3639954
08
Y = 18680365
18 feet Y = 5734830
12 meter
Z = -881217
34 Z = -250760
86
XDOT = -13585
682539 XDOT = -4138
622248
YDOT = 7933
016091 feet/sec YDOT = 2371
689865 meter/sec
ZDOT = -19603
825840 ZDOT = -5995
355545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20080628
31 X = -6120575
51
Y = 9665720
20 feet Y = 2946111
52 meter
Z = -799647
75 Z = -243732
63
XDOT = -5442
458398 XDOT = -1658
861320
YDOT = -12891
410973 feet/sec YDOT = -3929
302065 meter/sec
ZDOT = -19696
135912 ZDOT = -6003
382226
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 20119
16237318
00016717 00000-0 10270-3 0 9056
2 25544 51
6434 236
0672 0001420 208
5245 151
5828 15
49285752 24255
Satellite: ISS
Catalog Number: 25544
Epoch time: 20119
16237318 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 236
0672 deg
Eccentricity:
0001420
Arg of perigee: 208
5245 deg
Mean anomaly: 151
5828 deg
Mean motion: 15
49285752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 295
Coasting Arc #7 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2020/120/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4115362
14 A = 6803269
03 meter
Y = -5397998
47 meter E =
0011374
Z = 369826
49 I = 51
36109
XDOT = 4010
474388 Wp = 50
04665
YDOT = -2640
714436 meter/sec RA = 230
18231 deg
ZDOT = 5968
663783 TA = 313
94721
MA = 314
04100
Ha = 228
271 n
mi
Hp = 222
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13501844
30 X = -4056490
68
Y = -17709968
74 feet Y = -5443690
23 meter
Z = 1213341
50 Z = 349978
15
XDOT = 13157
724371 XDOT = 4010
713032
YDOT = -8663
761273 feet/sec YDOT = -2595
865537 meter/sec
ZDOT = 19582
230258 ZDOT = 5988
145622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19097177
95 X = 5820819
84
Y = -11465285
54 feet Y = -3494619
03 meter
Z = 1122502
52 Z = 342138
77
XDOT = 6330
890925 XDOT = 1929
655554
YDOT = 12511
012421 feet/sec YDOT = 3813
356586 meter/sec
ZDOT = 19671
677352 ZDOT = 5995
927257
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 20120
19440042
00016717 00000-0 10270-3 0 9062
2 25544 51
6429 230
9598 0001314 221
4015 138
7035 15
49328715 24412
Satellite: ISS
Catalog Number: 25544
Epoch time: 20120
19440042 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 230
9598 deg
Eccentricity:
0001314
Arg of perigee: 221
4015 deg
Mean anomaly: 138
7035 deg
Mean motion: 15
49328715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 278
Coasting Arc #8 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2020/121/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4480396
09 A = 6803341
76 meter
Y = 5086801
35 meter E =
0011332
Z = -505004
98 I = 51
38376
XDOT = -3887
678776 Wp = 145
93146
YDOT = 2839
985853 meter/sec RA = 225
21526 deg
ZDOT = -5959
191403 TA = 39
52475
MA = 39
44216
Ha = 228
328 n
mi
Hp = 222
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14699462
23 X = 4425634
01
Y = 16688980
82 feet Y = 5136598
17 meter
Z = -1656840
48 Z = -483373
59
XDOT = -12754
851626 XDOT = -3890
200970
YDOT = 9317
538888 feet/sec YDOT = 2796
497331 meter/sec
ZDOT = -19551
152898 ZDOT = -5978
082233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17993032
21 X = -5484276
22
Y = 13083022
45 feet Y = 3987705
24 meter
Z = -1557789
01 Z = -474814
09
XDOT = -7139
636623 XDOT = -2176
161243
YDOT = -12126
518235 feet/sec YDOT = -3696
162758 meter/sec
ZDOT = -19637
902179 ZDOT = -5985
632584
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 20121
16192583
00016717 00000-0 10270-3 0 9075
2 25544 51
6432 226
1722 0001465 221
3273 138
7767 15
49287733 24566
Satellite: ISS
Catalog Number: 25544
Epoch time: 20121
16192583 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 226
1722 deg
Eccentricity:
0001465
Arg of perigee: 221
3273 deg
Mean anomaly: 138
7767 deg
Mean motion: 15
49287733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 305
Coasting Arc #9 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2020/122/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4839926
80 A = 6803113
69 meter
Y = -4733871
83 meter E =
0011699
Z = 609065
59 I = 51
40807
XDOT = 3741
887380 Wp = 51
31451
YDOT = -3051
426313 meter/sec RA = 220
24815 deg
ZDOT = 5947
733947 TA = 315
26823
MA = 315
36252
Ha = 228
150 n
mi
Hp = 222
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15879024
93 X = -4789590
02
Y = -15531075
56 feet Y = -4787713
91 meter
Z = 1998246
70 Z = 585677
13
XDOT = 12276
533399 XDOT = 3746
840510
YDOT = -10011
241183 feet/sec YDOT = -3009
554455 meter/sec
ZDOT = 19513
562817 ZDOT = 5965
922475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16701205
85 X = 5090527
54
Y = -14657564
48 feet Y = -4467625
65 meter
Z = 1891099
43 Z = 576407
11
XDOT = 7983
028878 XDOT = 2433
227202
YDOT = 11655
920151 feet/sec YDOT = 3552
724462 meter/sec
ZDOT = 19597
101977 ZDOT = 5973
196682
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 20122
19394651
00016717 00000-0 10270-3 0 9080
2 25544 51
6432 221
0638 0001324 234
0031 126
0996 15
49351059 24728
Satellite: ISS
Catalog Number: 25544
Epoch time: 20122
19394651 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 221
0638 deg
Eccentricity:
0001324
Arg of perigee: 234
0031 deg
Mean anomaly: 126
0996 deg
Mean motion: 15
49351059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 282
Coasting Arc #10 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2020/123/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5150705
21 A = 6803193
30 meter
Y = 4373081
12 meter E =
0010495
Z = -745661
50 I = 51
43344
XDOT = -3604
663907 Wp = 147
50716
YDOT = 3242
464511 meter/sec RA = 215
28400 deg
ZDOT = -5930
987826 TA = 40
55758
MA = 40
47943
Ha = 228
260 n
mi
Hp = 222
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16898639
13 X = 5105043
31
Y = 14347379
01 feet Y = 4430424
68 meter
Z = -2446395
99 Z = -720752
14
XDOT = -11826
325155 XDOT = -3611
844823
YDOT = 10638
006927 feet/sec YDOT = 3202
114618 meter/sec
ZDOT = -19458
621475 ZDOT = -5948
515237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15325651
18 X = -4671258
48
Y = 16033752
83 feet Y = 4887087
86 meter
Z = -2332236
81 Z = -710865
78
XDOT = -8755
142096 XDOT = -2668
567311
YDOT = -11186
772028 feet/sec YDOT = -3409
728114 meter/sec
ZDOT = -19539
136598 ZDOT = -5955
528835
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 20123
16146762
00016717 00000-0 10270-3 0 9097
2 25544 51
6424 216
2757 0001341 233
1038 126
9989 15
49297913 24878
Satellite: ISS
Catalog Number: 25544
Epoch time: 20123
16146762 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 216
2757 deg
Eccentricity:
0001341
Arg of perigee: 233
1038 deg
Mean anomaly: 126
9989 deg
Mean motion: 15
49297913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2487
Checksum: 319
Coasting Arc #11 (Orbit 2502)
---------------------------------------
Vector Time (GMT): 2020/124/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5449839
10 A = 6802951
25 meter
Y = -3971997
60 meter E =
0011984
Z = 850333
34 I = 51
46087
XDOT = 3441
582290 Wp = 53
39114
YDOT = -3444
950910 meter/sec RA = 210
32115 deg
ZDOT = 5914
473935 TA = 315
81228
MA = 315
90793
Ha = 228
095 n
mi
Hp = 222
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17880049
54 X = -5409148
45
Y = -13031488
19 feet Y = -4032714
08 meter
Z = 2789807
55 Z = 823958
85
XDOT = 11291
280479 XDOT = 3451
119741
YDOT = -11302
332382 feet/sec YDOT = -3406
411429 meter/sec
ZDOT = 19404
442045 ZDOT = 5931
214974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13774314
08 X = 4198410
93
Y = -17333325
21 feet Y = -5283197
52 meter
Z = 2668893
22 Z = 813478
65
XDOT = 9556
839374 XDOT = 2912
924641
YDOT = 10621
179234 feet/sec YDOT = 3237
335430 meter/sec
ZDOT = 19481
357188 ZDOT = 5937
917671
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 20124
19348550
00016717 00000-0 10270-3 0 9102
2 25544 51
6419 211
1680 0001345 241
1336 118
9679 15
49359305 25035
Satellite: ISS
Catalog Number: 25544
Epoch time: 20124
19348550 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 211
1680 deg
Eccentricity:
0001345
Arg of perigee: 241
1336 deg
Mean anomaly: 118
9679 deg
Mean motion: 15
49359305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2503
Checksum: 291
Coasting Arc #12 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2020/125/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5699973
11 A = 6802977
30 meter
Y = 3570708
26 meter E =
0009582
Z = -986795
98 I = 51
49074
XDOT = -3287
417336 Wp = 149
82147
YDOT = 3628
931375 meter/sec RA = 205
36084 deg
ZDOT = -5890
742939 TA = 40
86909
MA = 40
79728
Ha = 228
138 n
mi
Hp = 222
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18700699
19 X = 5664414
09
Y = 11714922
13 feet Y = 3634250
60 meter
Z = -3237519
61 Z = -959193
90
XDOT = -10785
489947 XDOT = -3299
138721
YDOT = 11905
942831 feet/sec YDOT = 3592
103600 meter/sec
ZDOT = -19326
584447 ZDOT = -5906
740512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12178503
60 X = -3712007
90
Y = 18423983
52 feet Y = 5615630
18 meter
Z = -3110942
81 Z = -948215
37
XDOT = -10291
724156 XDOT = -3136
917523
YDOT = -10059
670386 feet/sec YDOT = -3066
187534 meter/sec
ZDOT = -19400
095543 ZDOT = -5913
149122
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 20125
16100337
00016717 00000-0 10270-3 0 9110
2 25544 51
6425 206
3799 0001440 246
5006 113
5993 15
49314835 25183
Satellite: ISS
Catalog Number: 25544
Epoch time: 20125
16100337 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 206
3799 deg
Eccentricity:
0001440
Arg of perigee: 246
5006 deg
Mean anomaly: 113
5993 deg
Mean motion: 15
49314835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 287
Coasting Arc #13 (Orbit 2533)
---------------------------------------
Vector Time (GMT): 2020/126/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5931692
64 A = 6802760
80 meter
Y = -3132973
64 meter E =
0012255
Z = 1092941
74 I = 51
52072
XDOT = 3107
058212 Wp = 55
18799
YDOT = -3821
343417 meter/sec RA = 200
40118 deg
ZDOT = 5868
740272 TA = 316
66574
MA = 316
76205
Ha = 228
046 n
mi
Hp = 222
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19460933
85 X = -5901526
89
Y = -10278784
90 feet Y = -3199137
38 meter
Z = 3585766
86 Z = 1064200
80
XDOT = 10193
760537 XDOT = 3121
051338
YDOT = -12537
215936 feet/sec YDOT = -3786
519849 meter/sec
ZDOT = 19254
397218 ZDOT = 5883
867317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10429593
92 X = 3178940
23
Y = -19404457
91 feet Y = -5914478
77 meter
Z = 3453935
93 Z = 1052759
67
XDOT = 11042
669510 XDOT = 3365
805667
YDOT = 9399
135161 feet/sec YDOT = 2864
856397 meter/sec
ZDOT = 19323
922363 ZDOT = 5889
931536
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 20126
19301729
00016717 00000-0 10270-3 0 9123
2 25544 51
6419 201
2712 0001358 252
4641 107
6361 15
49360244 25340
Satellite: ISS
Catalog Number: 25544
Epoch time: 20126
19301729 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 201
2712 deg
Eccentricity:
0001358
Arg of perigee: 252
4641 deg
Mean anomaly: 107
6361 deg
Mean motion: 15
49360244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2534
Checksum: 277
Coasting Arc #14 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2020/127/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6115726
77 A = 6802712
90 meter
Y = 2702595
01 meter E =
0008721
Z = -1229538
35 I = 51
55093
XDOT = -2935
036372 Wp = 150
31196
YDOT = 3997
489017 meter/sec RA = 195
44552 deg
ZDOT = -5837
361461 TA = 43
04004
MA = 42
97187
Ha = 228
119 n
mi
Hp = 222
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20064720
37 X = 6091023
51
Y = 8866781
54 feet Y = 2770847
32 meter
Z = -4033918
48 Z = -1199889
98
XDOT = -9629
384422 XDOT = -2951
164283
YDOT = 13115
121448 feet/sec YDOT = 3964
577273 meter/sec
ZDOT = -19151
448364 ZDOT = -5851
658073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8676577
02 X = -2644620
68
Y = 20174457
45 feet Y = 6149174
63 meter
Z = -3897896
16 Z = -1188078
75
XDOT = -11732
000277 XDOT = -3575
913684
YDOT = -8742
081801 feet/sec YDOT = -2664
586533 meter/sec
ZDOT = -19217
173229 ZDOT = -5857
394400
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 20127
16053142
00016717 00000-0 10270-3 0 9135
2 25544 51
6406 196
4835 0001321 256
8643 103
2360 15
49331209 25493
Satellite: ISS
Catalog Number: 25544
Epoch time: 20127
16053142 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 196
4835 deg
Eccentricity:
0001321
Arg of perigee: 256
8643 deg
Mean anomaly: 103
2360 deg
Mean motion: 15
49331209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 282
Coasting Arc #15 (Orbit 2564)
---------------------------------------
Vector Time (GMT): 2020/128/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6276604
20 A = 6802557
53 meter
Y = -2238992
62 meter E =
0012431
Z = 1334960
78 I = 51
58225
XDOT = 2733
855802 Wp = 57
77309
YDOT = -4179
968243 meter/sec RA = 190
49068 deg
ZDOT = 5809
981359 TA = 316
74572
MA = 316
84326
Ha = 228
049 n
mi
Hp = 222
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20592533
46 X = -6257585
23
Y = -7345776
33 feet Y = -2309075
80 meter
Z = 4379792
57 Z = 1304516
97
XDOT = 8969
343183 XDOT = 2752
172128
YDOT = -13713
806572 feet/sec YDOT = -4149
294163 meter/sec
ZDOT = 19061
618631 ZDOT = 5823
305932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6793659
65 X = 2070707
46
Y = -20810172
28 feet Y = -6342940
51 meter
Z = 4240090
21 Z = 1292379
50
XDOT = 12425
857341 XDOT = 3787
401318
YDOT = 7975
756020 feet/sec YDOT = 2431
010435 meter/sec
ZDOT = 19122
895732 ZDOT = 5828
658619
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 20128
19254445
00016717 00000-0 10270-3 0 9149
2 25544 51
6396 191
3753 0001381 257
5814 102
5182 15
49348869 25650
Satellite: ISS
Catalog Number: 25544
Epoch time: 20128
19254445 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 191
3753 deg
Eccentricity:
0001381
Arg of perigee: 257
5814 deg
Mean anomaly: 102
5182 deg
Mean motion: 15
49348869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2565
Checksum: 323
Coasting Arc #16 (Orbit 2579)
---------------------------------------
Vector Time (GMT): 2020/129/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6391686
89 A = 6802373
36 meter
Y = 1790209
87 meter E =
0007810
Z = -1470616
55 I = 51
61478
XDOT = -2540
927152 Wp = 150
94349
YDOT = 4347
005961 meter/sec RA = 185
53835 deg
ZDOT = -5771
414775 TA = 45
07565
MA = 45
01231
Ha = 228
059 n
mi
Hp = 222
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20970101
34 X = 6378336
74
Y = 5873391
96 feet Y = 1861611
73 meter
Z = -4824857
44 Z = -1439599
91
XDOT = -8336
375169 XDOT = -2561
313034
YDOT = 14261
830581 feet/sec YDOT = 4318
477956 meter/sec
ZDOT = -18935
087845 ZDOT = -5783
807034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4947017
03 X = -1507850
79
Y = 21239642
36 feet Y = 6473842
99 meter
Z = -4682493
76 Z = -1427224
10
XDOT = -13057
988044 XDOT = -3980
074756
YDOT = -7213
807633 feet/sec YDOT = -2198
768567 meter/sec
ZDOT = -18992
100782 ZDOT = -5788
792318
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 20129
16005532
00016717 00000-0 10270-3 0 9159
2 25544 51
6394 186
5865 0001343 266
8276 93
2720 15
49357056 25800
Satellite: ISS
Catalog Number: 25544
Epoch time: 20129
16005532 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 186
5865 deg
Eccentricity:
0001343
Arg of perigee: 266
8276 deg
Mean anomaly: 93
2720 deg
Mean motion: 15
49357056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2580
Checksum: 313
Coasting Arc #17 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2020/130/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6611001
79 A = 6802787
12 meter
Y = 1058203
28 meter E =
0008547
Z = -1181127
61 I = 51
64864
XDOT = -1778
759860 Wp = 149
62820
YDOT = 4602
639356 meter/sec RA = 181
07040 deg
ZDOT = -5858
206881 TA = 43
17102
MA = 43
10404
Ha = 228
092 n
mi
Hp = 222
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21689638
42 X = 6604414
64
Y = 3471795
55 feet Y = 1132095
50 meter
Z = -3875090
59 Z = -1149029
31
XDOT = -5835
826311 XDOT = -1801
639445
YDOT = 15100
522821 feet/sec YDOT = 4582
620659 meter/sec
ZDOT = -19219
838849 ZDOT = -5866
902654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14371408
33 X = -4380405
26
Y = 16645625
13 feet Y = 5073586
54 meter
Z = -3727719
56 Z = -1136208
92
XDOT = -8629
883143 XDOT = -2630
388382
YDOT = -11744
316035 feet/sec YDOT = -3579
667527 meter/sec
ZDOT = -19259
895630 ZDOT = -5870
416188
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 20130
06306405
00016717 00000-0 10270-3 0 9164
2 25544 51
6419 182
1197 0001394 270
1544 89
9447 15
49323178 25941
Satellite: ISS
Catalog Number: 25544
Epoch time: 20130
06306405 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 182
1197 deg
Eccentricity:
0001394
Arg of perigee: 270
1544 deg
Mean anomaly: 89
9447 deg
Mean motion: 15
49323178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 309
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