[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 24th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13864 993 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
146/12:14:26
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
2
148/20:33:33
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
3
149/04:45:00
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
2
149/15:17:02
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 222
2
152/12:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 222
0
Coasting Arc #1 (Orbit 2802)
---------------------------------------
Vector Time (GMT): 2020/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2052256
75 A = 6793762
18 meter
Y = -4415296
37 meter E =
0008091
Z = 4734765
95 I = 51
98014
XDOT = 4815
738838 Wp = 51
89924
YDOT = -5257
305054 meter/sec RA = 114
56119 deg
ZDOT = -2807
111999 TA = 65
85566
MA = 65
77107
Ha = 228
383 n
mi
Hp = 222
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6733125
81 X = -2025730
23
Y = -14485880
47 feet Y = -4438098
45 meter
Z = 15534009
03 Z = 4724860
59
XDOT = 15799
668103 XDOT = 4887
805239
YDOT = -17248
376161 feet/sec YDOT = -5203
048730 meter/sec
ZDOT = -9209
685035 ZDOT = -2783
544255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15955971
96 X = -4863380
25
Y = -1410709
29 feet Y = -429984
19 meter
Z = 15488641
35 Z = 4720937
88
XDOT = -6982
757453 XDOT = -2128
344472
YDOT = -21237
197523 feet/sec YDOT = -6473
097805 meter/sec
ZDOT = -9101
041138 ZDOT = -2773
997339
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 20143
54347066
00016717 00000-0 10270-3 0 9002
2 25544 51
6384 115
3987 0001605 336
0011 24
1064 15
49380891 28037
Satellite: ISS
Catalog Number: 25544
Epoch time: 20143
54347066 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 115
3987 deg
Eccentricity:
0001605
Arg of perigee: 336
0011 deg
Mean anomaly: 24
1064 deg
Mean motion: 15
49380891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2803
Checksum: 283
Coasting Arc #2 (Orbit 2817)
---------------------------------------
Vector Time (GMT): 2020/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2337435
59 A = 6794044
97 meter
Y = 4340615
86 meter E =
0009534
Z = -4683881
64 I = 51
99494
XDOT = -4404
029682 Wp = 102
17015
YDOT = 5530
045550 meter/sec RA = 109
63555 deg
ZDOT = 2930
068253 TA = 196
88689
MA = 196
91865
Ha = 228
410 n
mi
Hp = 222
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7668751
95 X = 2311475
78
Y = 14240865
68 feet Y = 4366610
26 meter
Z = -15367065
73 Z = -4672589
53
XDOT = -14448
916279 XDOT = -4479
773784
YDOT = 18143
194061 feet/sec YDOT = 5480
372617 meter/sec
ZDOT = 9613
084818 ZDOT = 2908
491708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16222177
27 X = 4944519
63
Y = 201376
59 feet Y = 61379
58 meter
Z = -15315323
48 Z = -4668110
60
XDOT = 8719
426359 XDOT = 2657
681154
YDOT = 20359
522345 feet/sec YDOT = 6205
582411 meter/sec
ZDOT = 9513
562213 ZDOT = 2899
733763
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 20144
51096002
00016717 00000-0 10270-3 0 9012
2 25544 51
6395 110
6103 0001633 340
4182 19
6905 15
49364111 28182
Satellite: ISS
Catalog Number: 25544
Epoch time: 20144
51096002 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 110
6103 deg
Eccentricity:
0001633
Arg of perigee: 340
4182 deg
Mean anomaly: 19
6905 deg
Mean motion: 15
49364111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2818
Checksum: 268
Coasting Arc #3 (Orbit 2833)
---------------------------------------
Vector Time (GMT): 2020/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2602073
40 A = 6794249
09 meter
Y = -4258563
51 meter E =
0008931
Z = 4606665
53 I = 52
00721
XDOT = 3995
130105 Wp = 55
15321
YDOT = -5772
517945 meter/sec RA = 104
71064 deg
ZDOT = -3070
496887 TA = 65
45597
MA = 65
36291
Ha = 228
456 n
mi
Hp = 222
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8536986
23 X = -2576636
30
Y = -13971665
07 feet Y = -4287520
26 meter
Z = 15113732
07 Z = 4594086
62
XDOT = 13107
382233 XDOT = 4074
298081
YDOT = -18938
707170 feet/sec YDOT = -5727
398408 meter/sec
ZDOT = -10073
808686 ZDOT = -3050
898514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16397864
46 X = -4998069
09
Y = 968082
00 feet Y = 295071
39 meter
Z = 15056072
33 Z = 4589090
85
XDOT = -10339
134052 XDOT = -3151
368059
YDOT = -19393
809766 feet/sec YDOT = -5911
233217 meter/sec
ZDOT = -9983
349625 ZDOT = -3042
924966
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 20145
54294623
00016717 00000-0 10270-3 0 9026
2 25544 51
6406 105
5025 0001748 343
5172 16
5921 15
49391749 28340
Satellite: ISS
Catalog Number: 25544
Epoch time: 20145
54294623 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 105
5025 deg
Eccentricity:
0001748
Arg of perigee: 343
5172 deg
Mean anomaly: 16
5921 deg
Mean motion: 15
49391749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2834
Checksum: 300
Coasting Arc #4 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2020/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2889886
18 A = 6794561
16 meter
Y = 4146239
31 meter E =
0008838
Z = -4549651
52 I = 52
01532
XDOT = -3558
876336 Wp = 100
52814
YDOT = 5977
053601 meter/sec RA = 99
78680 deg
ZDOT = 3190
207351 TA = 201
38385
MA = 201
42080
Ha = 228
498 n
mi
Hp = 222
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9481253
88 X = 2865406
70
Y = 13603147
35 feet Y = 4178419
97 meter
Z = -14926678
22 Z = -4535672
22
XDOT = -11676
103464 XDOT = -3640
945342
YDOT = 19609
755910 feet/sec YDOT = 5936
796296 meter/sec
ZDOT = 10466
559549 ZDOT = 3172
721264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16485025
43 X = 5024635
75
Y = -2256842
11 feet Y = -687885
47 meter
Z = -14862574
33 Z = -4530112
65
XDOT = 11850
471659 XDOT = 3612
023762
YDOT = 18245
180485 feet/sec YDOT = 5561
131012 meter/sec
ZDOT = 10385
785145 ZDOT = 3165
587312
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 20146
51043295
00016717 00000-0 10270-3 0 9032
2 25544 51
6405 100
7144 0001796 348
2456 11
8652 15
49369673 28494
Satellite: ISS
Catalog Number: 25544
Epoch time: 20146
51043295 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 100
7144 deg
Eccentricity:
0001796
Arg of perigee: 348
2456 deg
Mean anomaly: 11
8652 deg
Mean motion: 15
49369673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 310
Coasting Arc #5 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2020/146/12:14:26
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -994201
27 A = 6803123
17 meter
Y = 6720249
94 meter E =
0012733
Z = -204094
95 I = 52
04410
XDOT = -4689
523813 Wp = 37
56584
YDOT = -516
727068 meter/sec RA = 99
75821 deg
ZDOT = 6037
143153 TA = 320
25151
MA = 320
34474
Ha = 228
466 n
mi
Hp = 222
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3261815
20 X = -1068283
83
Y = 22048064
10 feet Y = 6708717
88 meter
Z = -669602
84 Z = -209103
22
XDOT = -15385
576814 XDOT = -4712
722297
YDOT = -1695
298781 feet/sec YDOT = -569
299395 meter/sec
ZDOT = 19806
900109 ZDOT = 6014
306665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18868922
68 X = 5751247
63
Y = 11861215
84 feet Y = 3615298
59 meter
Z = -693002
49 Z = -211227
16
XDOT = -6936
496594 XDOT = -2114
244162
YDOT = 12147
299754 feet/sec YDOT = 3702
496965 meter/sec
ZDOT = 19701
849711 ZDOT = 6005
123792
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 20146
51043293
00016717 00000-0 10270-3 0 9041
2 25544 51
6405 100
7145 0001729 349
3958 10
7155 15
49388627 28496
Satellite: ISS
Catalog Number: 25544
Epoch time: 20146
51043293 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 100
7145 deg
Eccentricity:
0001729
Arg of perigee: 349
3958 deg
Mean anomaly: 10
7155 deg
Mean motion: 15
49388627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 311
Coasting Arc #6 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2020/147/12:14:26
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 532477
06 A = 6803168
33 meter
Y = -6777463
60 meter E =
0010820
Z = 52412
09 I = 52
04960
XDOT = 4700
335401 Wp = 128
24118
YDOT = 316
104845 meter/sec RA = 94
83676 deg
ZDOT = -6039
615639 TA = 51
19866
MA = 51
10207
Ha = 228
495 n
mi
Hp = 222
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1746971
98 X = 607970
51
Y = -22235772
96 feet Y = -6771086
96 meter
Z = 171955
67 Z = 55180
87
XDOT = 15421
047905 XDOT = 4725
788376
YDOT = 1037
089388 feet/sec YDOT = 368
810682 meter/sec
ZDOT = -19815
011939 ZDOT = -6016
721294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19828113
80 X = -6043609
09
Y = -10213849
96 feet Y = -3113181
47 meter
Z = 185070
43 Z = 56409
47
XDOT = 6229
666600 XDOT = 1898
802380
YDOT = -12497
008263 feet/sec YDOT = -3809
088119 meter/sec
ZDOT = -19709
675952 ZDOT = -6007
509230
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 20147
54241869
00016717 00000-0 10270-3 0 9055
2 25544 51
6414 95
6071 0001771 351
1017 9
0101 15
49378804 28656
Satellite: ISS
Catalog Number: 25544
Epoch time: 20147
54241869 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 95
6071 deg
Eccentricity:
0001771
Arg of perigee: 351
1017 deg
Mean anomaly: 9
0101 deg
Mean motion: 15
49378804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 295
Coasting Arc #7 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2020/148/12:14:26
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -40142
30 A = 6803131
98 meter
Y = 6795692
53 meter E =
0013336
Z = 64353
11 I = 52
05145
XDOT = -4711
745593 Wp = 40
08238
YDOT = -91
524908 meter/sec RA = 89
91533 deg
ZDOT = 6041
755378 TA = 320
60565
MA = 320
70256
Ha = 228
510 n
mi
Hp = 222
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -131700
47 X = -116443
36
Y = 22295579
18 feet Y = 6794817
00 meter
Z = 211132
25 Z = 63973
88
XDOT = -15458
482918 XDOT = -4739
719318
YDOT = -300
278569 feet/sec YDOT = -144
372380 meter/sec
ZDOT = 19822
032079 ZDOT = 6018
799613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20654761
37 X = 6295571
27
Y = 8395946
94 feet Y = 2559084
63 meter
Z = 208998
93 Z = 63702
87
XDOT = -5451
055561 XDOT = -1661
481735
YDOT = 12862
828038 feet/sec YDOT = 3920
589986 meter/sec
ZDOT = 19716
393254 ZDOT = 6009
556664
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 20148
57440220
00016717 00000-0 10270-3 0 9062
2 25544 51
6416 90
4998 0001777 353
2531 6
8595 15
49392452 28814
Satellite: ISS
Catalog Number: 25544
Epoch time: 20148
57440220 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 90
4998 deg
Eccentricity:
0001777
Arg of perigee: 353
2531 deg
Mean anomaly: 6
8595 deg
Mean motion: 15
49392452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 320
Coasting Arc #8 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2020/148/20:33:33
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3083808
31 A = 6797274
75 meter
Y = -4746463
18 meter E =
0011606
Z = 3756156
03 I = 52
03004
XDOT = 3184
322228 Wp = 76
54808
YDOT = -5483
653351 meter/sec RA = 88
17945 deg
ZDOT = -4301
316234 TA = 58
91328
MA = 58
79944
Ha = 228
514 n
mi
Hp = 222
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10117481
32 X = -3048747
98
Y = -15572385
77 feet Y = -4780753
07 meter
Z = 12323346
55 Z = 3741260
53
XDOT = 10447
251404 XDOT = 3266
298699
YDOT = -17990
988683 feet/sec YDOT = -5447
584967 meter/sec
ZDOT = -14111
929901 ZDOT = -4285
649811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13519086
33 X = 4120617
51
Y = 12797463
92 feet Y = 3900667
00 meter
Z = 12255069
11 Z = 3735345
06
XDOT = -5173
557868 XDOT = -1576
900438
YDOT = 18953
249686 feet/sec YDOT = 5776
950504 meter/sec
ZDOT = -14039
513735 ZDOT = -4279
243787
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 20148
89689563
00016717 00000-0 10270-3 0 9073
2 25544 51
6399 88
9000 0001551 349
2896 10
8221 15
49383567 28862
Satellite: ISS
Catalog Number: 25544
Epoch time: 20148
89689563 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 88
9000 deg
Eccentricity:
0001551
Arg of perigee: 349
2896 deg
Mean anomaly: 10
8221 deg
Mean motion: 15
49383567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 349
Coasting Arc #9 (Orbit 2890)
---------------------------------------
Vector Time (GMT): 2020/149/04:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3424203
53 A = 6794137
97 meter
Y = -3587076
31 meter E =
0010862
Z = -4654922
38 I = 52
02223
XDOT = 2731
681183 Wp = 62
10489
YDOT = 6490
344938 meter/sec RA = 86
54902 deg
ZDOT = -2992
392826 TA = 178
15063
MA = 178
14661
Ha = 228
546 n
mi
Hp = 222
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11234263
54 X = 3486671
68
Y = -11768623
05 feet Y = -3548434
45 meter
Z = -15272055
04 Z = -4638137
78
XDOT = 8962
208606 XDOT = 2673
436491
YDOT = 21293
782606 feet/sec YDOT = 6520
567321 meter/sec
ZDOT = -9817
561766 ZDOT = -2979
263915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16325287
42 X = 4975947
60
Y = -744301
77 feet Y = -226863
18 meter
Z = -15194598
92 Z = -4631313
75
XDOT = -8146
973418 XDOT = -2483
197498
YDOT = 20475
873789 feet/sec YDOT = 6241
046331 meter/sec
ZDOT = -9757
517701 ZDOT = -2974
091395
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 20149
21939061
00016717 00000-0 10270-3 0 9082
2 25544 51
6430 87
3066 0001590 358
5739 1
5406 15
49383229 28918
Satellite: ISS
Catalog Number: 25544
Epoch time: 20149
21939061 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 87
3066 deg
Eccentricity:
0001590
Arg of perigee: 358
5739 deg
Mean anomaly: 1
5406 deg
Mean motion: 15
49383229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2891
Checksum: 314
Coasting Arc #10 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2020/149/15:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1373154
15 A = 6802867
62 meter
Y = -6593370
22 meter E =
0012467
Z = 921414
52 I = 52
05127
XDOT = 4487
406081 Wp = 118
61938
YDOT = -1773
747003 meter/sec RA = 84
36030 deg
ZDOT = -5949
891016 TA = 51
48255
MA = 51
37084
Ha = 228
605 n
mi
Hp = 222
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4505098
90 X = -1303798
76
Y = -21631792
05 feet Y = -6608338
14 meter
Z = 3023013
52 Z = 914911
82
XDOT = 14722
460897 XDOT = 4535
808210
YDOT = -5819
379932 feet/sec YDOT = -1723
294165 meter/sec
ZDOT = -19520
639816 ZDOT = -5927
975706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17696602
75 X = -5393924
52
Y = 13237760
80 feet Y = 4034869
49 meter
Z = 2993475
26 Z = 912411
26
XDOT = -10584
230900 XDOT = -3226
073578
YDOT = -9716
620861 feet/sec YDOT = -2961
626038 meter/sec
ZDOT = -19419
673077 ZDOT = -5919
116354
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 20149
67088333
00016717 00000-0 10270-3 0 9090
2 25544 51
6442 85
0744 0001746 358
9031 1
2115 15
49362866 28986
Satellite: ISS
Catalog Number: 25544
Epoch time: 20149
67088333 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 85
0744 deg
Eccentricity:
0001746
Arg of perigee: 358
9031 deg
Mean anomaly: 1
2115 deg
Mean motion: 15
49362866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 320
Coasting Arc #11 (Orbit 2912)
---------------------------------------
Vector Time (GMT): 2020/150/15:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1849022
07 A = 6802814
10 meter
Y = 6490799
56 meter E =
0011794
Z = -805044
56 I = 52
04661
XDOT = -4370
183570 Wp = 33
61479
YDOT = 1979
419156 meter/sec RA = 79
43784 deg
ZDOT = 5973
219529 TA = 317
74603
MA = 317
83685
Ha = 228
576 n
mi
Hp = 222
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6066345
39 X = 1780213
04
Y = 21295274
14 feet Y = 6511092
00 meter
Z = -2641222
31 Z = -796229
11
XDOT = -14337
872606 XDOT = -4421
007623
YDOT = 6494
157336 feet/sec YDOT = 1930
263764 meter/sec
ZDOT = 19597
176931 ZDOT = 5951
867738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16481305
92 X = 5023502
05
Y = -14794135
01 feet Y = -4509252
35 meter
Z = -2601043
33 Z = -792798
01
XDOT = 11096
862735 XDOT = 3382
323762
YDOT = 8964
209865 feet/sec YDOT = 2732
291167 meter/sec
ZDOT = 19498
785498 ZDOT = 5943
229820
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 20150
63836400
00016717 00000-0 10270-3 0 9106
2 25544 51
6437 80
2857 0001912 359
1946
9201 15
49409680 29131
Satellite: ISS
Catalog Number: 25544
Epoch time: 20150
63836400 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 80
2857 deg
Eccentricity:
0001912
Arg of perigee: 359
1946 deg
Mean anomaly:
9201 deg
Mean motion: 15
49409680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2913
Checksum: 291
Coasting Arc #12 (Orbit 2928)
---------------------------------------
Vector Time (GMT): 2020/151/15:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2290825
64 A = 6803053
36 meter
Y = -6367120
09 meter E =
0012203
Z = 650959
81 I = 52
03951
XDOT = 4256
474709 Wp = 121
07827
YDOT = -2152
123851 meter/sec RA = 74
51607 deg
ZDOT = -5994
208789 TA = 51
94571
MA = 51
83566
Ha = 228
670 n
mi
Hp = 222
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7515832
14 X = -2222618
34
Y = -20889501
60 feet Y = -6392356
42 meter
Z = 2135694
90 Z = 639996
89
XDOT = 13964
812039 XDOT = 4309
340475
YDOT = -7060
773790 feet/sec YDOT = -2104
228720 meter/sec
ZDOT = -19666
039335 ZDOT = -5973
404323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15207303
63 X = -4635186
15
Y = 16180489
60 feet Y = 4931813
23 meter
Z = 2085635
40 Z = 635701
67
XDOT = -11505
034713 XDOT = -3506
734580
YDOT = -8257
237875 feet/sec YDOT = -2516
806104 meter/sec
ZDOT = -19570
152290 ZDOT = -5964
982418
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 20151
67034524
00016717 00000-0 10270-3 0 9119
2 25544 51
6436 75
1784 0001775 4
5032 355
6134 15
49360851 29294
Satellite: ISS
Catalog Number: 25544
Epoch time: 20151
67034524 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 75
1784 deg
Eccentricity:
0001775
Arg of perigee: 4
5032 deg
Mean anomaly: 355
6134 deg
Mean motion: 15
49360851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2929
Checksum: 297
Coasting Arc #13 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2020/152/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3941987
66 A = 6791047
73 meter
Y = 1392895
06 meter E =
0003207
Z = 5349381
62 I = 51
99104
XDOT = -2584
607607 Wp = 51
35275
YDOT = -7214
121054 meter/sec RA = 70
14742 deg
ZDOT = -24
209622 TA = 38
88852
MA = 38
86545
Ha = 228
706 n
mi
Hp = 221
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12933030
39 X = -3983254
77
Y = 4569865
69 feet Y = 1348581
71 meter
Z = 17550464
62 Z = 5330132
82
XDOT = -8479
683750 XDOT = -2503
627472
YDOT = -23668
376163 feet/sec YDOT = -7242
571186 meter/sec
ZDOT = -79
427894 ZDOT = -36
568664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1654184
58 X = 504195
46
Y = 13730096
04 feet Y = 4184933
27 meter
Z = 17461783
77 Z = 5322351
69
XDOT = -23937
453301 XDOT = -7296
135766
YDOT = 3064
931999 feet/sec YDOT = 934
191273 meter/sec
ZDOT = -135
847148 ZDOT = -41
406211
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 20152
57332489
00016717 00000-0 10270-3 0 9121
2 25544 51
6433 70
7082 0001913 3
0758 357
0404 15
49434462 29438
Satellite: ISS
Catalog Number: 25544
Epoch time: 20152
57332489 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 70
7082 deg
Eccentricity:
0001913
Arg of perigee: 3
0758 deg
Mean anomaly: 357
0404 deg
Mean motion: 15
49434462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 293
Coasting Arc #14 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2020/153/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3885512
24 A = 6791126
71 meter
Y = -1573977
38 meter E =
0015295
Z = -5355805
15 I = 51
97976
XDOT = 3078
382761 Wp = 83
81825
YDOT = 7000
616402 meter/sec RA = 65
22089 deg
ZDOT = 177
972120 TA = 187
86208
MA = 187
88608
Ha = 228
701 n
mi
Hp = 222
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12747743
58 X = 3928839
79
Y = -5163967
79 feet Y = -1530284
04 meter
Z = -17571539
20 Z = -5336825
62
XDOT = 10099
680975 XDOT = 2999
006503
YDOT = 22967
901583 feet/sec YDOT = 7034
597233 meter/sec
ZDOT = 583
898033 ZDOT = 192
733696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2509141
59 X = -764786
36
Y = -13636037
27 feet Y = -4156264
16 meter
Z = -17484084
64 Z = -5329149
00
XDOT = 23520
059298 XDOT = 7168
914074
YDOT = -5154
462170 feet/sec YDOT = -1571
080070 meter/sec
ZDOT = 651
371079 ZDOT = 198
537905
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 20153
54080359
00016717 00000-0 10270-3 0 9136
2 25544 51
6445 65
9195 0002030 11
4599 348
6597 15
49415937 29580
Satellite: ISS
Catalog Number: 25544
Epoch time: 20153
54080359 = yrday
fracday
Element set: 913
Inclination: 51
6445 deg
RA of node: 65
9195 deg
Eccentricity:
0002030
Arg of perigee: 11
4599 deg
Mean anomaly: 348
6597 deg
Mean motion: 15
49415937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 330
Coasting Arc #15 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2020/154/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3817070
14 A = 6791078
36 meter
Y = 1737712
75 meter E =
0003946
Z = 5338900
50 I = 51
96438
XDOT = -3561
875662 Wp = 47
06926
YDOT = -6776
843372 meter/sec RA = 60
29417 deg
ZDOT = -338
069198 TA = 46
15787
MA = 46
12526
Ha = 228
805 n
mi
Hp = 221
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12523196
01 X = -3862151
70
Y = 5701157
32 feet Y = 1694774
90 meter
Z = 17516077
76 Z = 5320249
15
XDOT = -11685
943773 XDOT = -3484
188094
YDOT = -22233
738097 feet/sec YDOT = -6816
240386 meter/sec
ZDOT = -1109
150911 ZDOT = -355
183659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3312421
26 X = 1009626
00
Y = 13467196
22 feet Y = 4104801
41 meter
Z = 17430120
62 Z = 5312700
76
XDOT = -23002
298695 XDOT = -7011
100642
YDOT = 7206
400892 feet/sec YDOT = 2196
510992 meter/sec
ZDOT = -1187
447864 ZDOT = -361
934109
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 20154
57277780
00016717 00000-0 10270-3 0 9147
2 25544 51
6442 60
8122 0001992 11
8381 348
2816 15
49438611 29742
Satellite: ISS
Catalog Number: 25544
Epoch time: 20154
57277780 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 60
8122 deg
Eccentricity:
0001992
Arg of perigee: 11
8381 deg
Mean anomaly: 348
2816 deg
Mean motion: 15
49438611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 313
Coasting Arc #16 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2020/155/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3752394
57 A = 6791188
27 meter
Y = -1919509
07 meter E =
0015191
Z = -5337974
30 I = 51
94733
XDOT = 4016
604694 Wp = 86
23405
YDOT = 6491
779008 meter/sec RA = 55
36649 deg
ZDOT = 491
284382 TA = 188
43132
MA = 188
45688
Ha = 228
725 n
mi
Hp = 221
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12311005
82 X = 3799509
39
Y = -6297601
92 feet Y = -1877282
97 meter
Z = -17513039
06 Z = -5319632
21
XDOT = 13177
836924 XDOT = 3941
326759
YDOT = 21298
487560 feet/sec YDOT = 6536
274570 meter/sec
ZDOT = 1611
825401 ZDOT = 510
613784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4166824
87 X = -1270048
22
Y = -13297087
17 feet Y = -4052952
17 meter
Z = -17428489
16 Z = -5312203
50
XDOT = 22205
553547 XDOT = 6768
252721
YDOT = -9177
622875 feet/sec YDOT = -2797
339452 meter/sec
ZDOT = 1700
315434 ZDOT = 518
256144
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 20155
54025489
00016717 00000-0 10270-3 0 9153
2 25544 51
6447 56
0243 0002015 14
4665 345
6543 15
49420655 29892
Satellite: ISS
Catalog Number: 25544
Epoch time: 20155
54025489 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 56
0243 deg
Eccentricity:
0002015
Arg of perigee: 14
4665 deg
Mean anomaly: 345
6543 deg
Mean motion: 15
49420655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 309
Coasting Arc #17 (Orbit 3004)
---------------------------------------
Vector Time (GMT): 2020/156/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3678593
73 A = 6791176
54 meter
Y = 2081611
56 meter E =
0004591
Z = 5313080
65 I = 51
92828
XDOT = -4457
416702 Wp = 44
26782
YDOT = -6199
282112 meter/sec RA = 50
43719 deg
ZDOT = -653
804781 TA = 51
97444
MA = 51
93300
Ha = 228
823 n
mi
Hp = 221
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12068877
07 X = -3727405
78
Y = 6829434
25 feet Y = 2040201
12 meter
Z = 17431366
95 Z = 5295093
02
XDOT = -14624
070546 XDOT = -4384
587352
YDOT = -20338
852072 feet/sec YDOT = -6248
720797 meter/sec
ZDOT = -2145
028810 ZDOT = -675
281574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4956761
22 X = 1510820
82
Y = 13061927
54 feet Y = 3981275
52 meter
Z = 17348431
82 Z = 5287802
02
XDOT = -21320
005069 XDOT = -6498
337545
YDOT = 11085
667381 feet/sec YDOT = 3378
911418 meter/sec
ZDOT = -2243
403768 ZDOT = -683
789468
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 20156
57222618
00016717 00000-0 10270-3 0 9161
2 25544 51
6455 50
9168 0001989 14
8900 345
2308 15
49443206 30057
Satellite: ISS
Catalog Number: 25544
Epoch time: 20156
57222618 = yrday
fracday
Element set: 916
Inclination: 51
6455 deg
RA of node: 50
9168 deg
Eccentricity:
0001989
Arg of perigee: 14
8900 deg
Mean anomaly: 345
2308 deg
Mean motion: 15
49443206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3005
Checksum: 302
Coasting Arc #18 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2020/157/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3604775
91 A = 6791313
24 meter
Y = -2264426
54 meter E =
0015103
Z = -5304471
57 I = 51
90583
XDOT = 4860
875725 Wp = 88
23873
YDOT = 5851
262488 meter/sec RA = 45
50628 deg
ZDOT = 807
912205 TA = 189
45926
MA = 189
48774
Ha = 228
798 n
mi
Hp = 221
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11826692
62 X = 3655595
83
Y = -7429220
93 feet Y = -2223830
23 meter
Z = -17403121
94 Z = -5286837
79
XDOT = 15947
755004 XDOT = 4791
159485
YDOT = 19197
055406 feet/sec YDOT = 5905
230300 meter/sec
ZDOT = 2650
630594 ZDOT = 831
356444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5807008
83 X = -1769976
29
Y = -12812754
26 feet Y = -3905327
50 meter
Z = -17321795
87 Z = -5279683
38
XDOT = 20178
351626 XDOT = 6150
361576
YDOT = -12863
072417 feet/sec YDOT = -3920
664473 meter/sec
ZDOT = 2758
070636 ZDOT = 840
659930
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 20157
53969913
00016717 00000-0 10270-3 0 9175
2 25544 51
6451 46
1284 0002132 19
7903 340
3330 15
49427301 30203
Satellite: ISS
Catalog Number: 25544
Epoch time: 20157
53969913 = yrday
fracday
Element set: 917
Inclination: 51
6451 deg
RA of node: 46
1284 deg
Eccentricity:
0002132
Arg of perigee: 19
7903 deg
Mean anomaly: 340
3330 deg
Mean motion: 15
49427301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 282
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