[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 4th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16466 6302 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
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
132/16:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
0
000/00:00:00
000 0
0 0
0 222
6
132/22:30:00
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
135/18:45:00
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
6
Coasting Arc #1 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2020/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1986160
75 A = 6791238
11 meter
Y = -3743993
79 meter E =
0001173
Z = 5305483
61 I = 51
46461
XDOT = 6925
707236 Wp = 108
14420
YDOT = 3264
593066 meter/sec RA = 203
51380 deg
ZDOT = -289
242344 TA = 344
62018
MA = 344
62375
Ha = 227
956 n
mi
Hp = 222
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6516275
41 X = 2002108
33
Y = -12283444
20 feet Y = -3721693
96 meter
Z = 17406442
30 Z = 5315170
43
XDOT = 22722
136602 XDOT = 6890
091842
YDOT = 10710
607171 feet/sec YDOT = 3341
842116 meter/sec
ZDOT = -948
957822 ZDOT = -255
686161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3448574
35 X = -1051125
46
Y = -13412649
44 feet Y = -4088175
55 meter
Z = 17450995
67 Z = 5319063
48
XDOT = 23087
327237 XDOT = 7037
017342
YDOT = -6969
182725 feet/sec YDOT = -2124
206894 meter/sec
ZDOT = -795
041468 ZDOT = -242
328639
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
54797763
00016717 00000-0 10270-3 0 9005
2 25544 51
6437 204
4619 0001576 237
9201 122
1797 15
49376176 25248
Satellite: ISS
Catalog Number: 25544
Epoch time: 20125
54797763 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 204
4619 deg
Eccentricity:
0001576
Arg of perigee: 237
9201 deg
Mean anomaly: 122
1797 deg
Mean motion: 15
49376176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 317
Coasting Arc #2 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2020/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1807461
96 A = 6791402
21 meter
Y = 3847814
37 meter E =
0013523
Z = -5308040
45 I = 51
49504
XDOT = -7125
357377 Wp = 96
27003
YDOT = -2752
753554 meter/sec RA = 198
55443 deg
ZDOT = 430
307569 TA = 177
85441
MA = 177
84860
Ha = 228
093 n
mi
Hp = 222
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5929993
32 X = -1824571
23
Y = 12624062
88 feet Y = 3827506
41 meter
Z = -17414830
87 Z = -5316862
06
XDOT = -23377
156748 XDOT = -7096
135916
YDOT = -9031
343681 feet/sec YDOT = -2832
270988 meter/sec
ZDOT = 1411
770240 ZDOT = 395
765826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4340104
12 X = 1322863
74
Y = 13201514
72 feet Y = 4023821
69 meter
Z = -17455418
19 Z = -5320411
46
XDOT = -22313
392936 XDOT = -6801
122167
YDOT = 8995
006042 feet/sec YDOT = 2741
677842 meter/sec
ZDOT = 1253
299281 ZDOT = 382
005621
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
51548904
00016717 00000-0 10270-3 0 9015
2 25544 51
6427 199
6743 0001420 244
9109 115
1894 15
49333755 25395
Satellite: ISS
Catalog Number: 25544
Epoch time: 20126
51548904 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 199
6743 deg
Eccentricity:
0001420
Arg of perigee: 244
9109 deg
Mean anomaly: 115
1894 deg
Mean motion: 15
49333755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 314
Coasting Arc #3 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2020/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1618431
44 A = 6791316
88 meter
Y = -3935195
21 meter E =
0001339
Z = 5292049
20 I = 51
52719
XDOT = 7306
484756 Wp = 69
63611
YDOT = 2234
932359 meter/sec RA = 193
59737 deg
ZDOT = -572
011462 TA = 25
83909
MA = 25
83240
Ha = 227
954 n
mi
Hp = 222
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5309814
42 X = 1636609
44
Y = -12910745
43 feet Y = -3916995
25 meter
Z = 17362366
13 Z = 5299955
10
XDOT = 23971
406681 XDOT = 7283
728601
YDOT = 7332
455245 feet/sec YDOT = 2316
511449 meter/sec
ZDOT = -1876
678024 ZDOT = -536
573967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5211917
72 X = -1588592
52
Y = -12901643
18 feet Y = -3932420
84 meter
Z = 17398757
18 Z = 5303141
19
XDOT = 21423
933496 XDOT = 6530
014929
YDOT = -10968
761176 feet/sec YDOT = -3343
278406 meter/sec
ZDOT = -1714
063660 ZDOT = -522
446604
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
54749850
00016717 00000-0 10270-3 0 9023
2 25544 51
6424 194
5674 0001452 247
5042 112
5954 15
49373672 25557
Satellite: ISS
Catalog Number: 25544
Epoch time: 20127
54749850 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 194
5674 deg
Eccentricity:
0001452
Arg of perigee: 247
5042 deg
Mean anomaly: 112
5954 deg
Mean motion: 15
49373672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2555
Checksum: 314
Coasting Arc #4 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2020/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1429447
53 A = 6791505
13 meter
Y = 4028976
11 meter E =
0013341
Z = -5288828
38 I = 51
55912
XDOT = -7425
518676 Wp = 97
88611
YDOT = -1699
960624 meter/sec RA = 188
64197 deg
ZDOT = 711
688426 TA = 178
93606
MA = 178
93322
Ha = 228
076 n
mi
Hp = 222
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4689788
47 X = -1448703
87
Y = 13218425
56 feet Y = 4012883
64 meter
Z = -17351799
15 Z = -5295818
77
XDOT = -24361
937915 XDOT = -7409
414376
YDOT = -5577
298634 feet/sec YDOT = -1782
908052 meter/sec
ZDOT = 2334
935780 ZDOT = 675
656451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6089419
50 X = 1856055
06
Y = 12590530
56 feet Y = 3837593
72 meter
Z = -17383996
50 Z = -5298642
13
XDOT = -20288
247034 XDOT = -6183
857696
YDOT = 12809
080177 feet/sec YDOT = 3904
207638 meter/sec
ZDOT = 2169
557289 ZDOT = 661
281062
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
51500848
00016717 00000-0 10270-3 0 9034
2 25544 51
6412 189
7793 0001382 252
6059 107
4940 15
49331683 25700
Satellite: ISS
Catalog Number: 25544
Epoch time: 20128
51500848 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 189
7793 deg
Eccentricity:
0001382
Arg of perigee: 252
6059 deg
Mean anomaly: 107
4940 deg
Mean motion: 15
49331683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 308
Coasting Arc #5 (Orbit 2585)
---------------------------------------
Vector Time (GMT): 2020/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1235021
62 A = 6791436
64 meter
Y = -4104511
13 meter E =
0001978
Z = 5266811
56 I = 51
59304
XDOT = 7524
555678 Wp = 49
39645
YDOT = 1164
639031 meter/sec RA = 183
68884 deg
ZDOT = -855
351197 TA = 48
80235
MA = 48
78530
Ha = 227
954 n
mi
Hp = 222
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4051908
20 X = 1255244
06
Y = -13466243
85 feet Y = -4090587
62 meter
Z = 17279565
48 Z = 5272859
68
XDOT = 24686
862461 XDOT = 7515
127980
YDOT = 3820
994196 feet/sec YDOT = 1248
731326 meter/sec
ZDOT = -2806
270333 ZDOT = -818
821965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6926737
12 X = -2111269
48
Y = -12198921
27 feet Y = -3718231
20 meter
Z = 17307446
36 Z = 5275309
65
XDOT = 19053
381569 XDOT = 5807
470702
YDOT = -14569
156684 feet/sec YDOT = -4440
678957 meter/sec
ZDOT = -2638
569545 ZDOT = -804
235997
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
54701439
00016717 00000-0 10270-3 0 9048
2 25544 51
6415 184
6719 0001370 258
9296 101
1700 15
49375277 25863
Satellite: ISS
Catalog Number: 25544
Epoch time: 20129
54701439 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 184
6719 deg
Eccentricity:
0001370
Arg of perigee: 258
9296 deg
Mean anomaly: 101
1700 deg
Mean motion: 15
49375277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2586
Checksum: 315
Coasting Arc #6 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2020/130/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6603910
82 A = 6802749
72 meter
Y = 1076336
91 meter E =
0008457
Z = -1204315
10 I = 51
64855
XDOT = -1811
935153 Wp = 149
65838
YDOT = 4597
287140 meter/sec RA = 181
06966 deg
ZDOT = -5852
177932 TA = 43
39648
MA = 43
32993
Ha = 228
083 n
mi
Hp = 222
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21666374
10 X = 6597234
06
Y = 3531289
07 feet Y = 1150149
33 meter
Z = -3951165
02 Z = -1172251
45
XDOT = -5944
669136 XDOT = -1834
781708
YDOT = 15082
963058 feet/sec YDOT = 4576
897637 meter/sec
ZDOT = -19200
058833 ZDOT = -5861
034781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14410049
00 X = -4392182
93
Y = 16594996
19 feet Y = 5058154
84 meter
Z = -3803953
65 Z = -1159445
07
XDOT = -8561
338305 XDOT = -2609
495915
YDOT = -11824
958877 feet/sec YDOT = -3604
247466 meter/sec
ZDOT = -19240
855151 ZDOT = -5864
612650
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
06301813
00016717 00000-0 10270-3 0 9050
2 25544 51
6419 182
1195 0001394 271
4083 88
6908 15
49328268 25944
Satellite: ISS
Catalog Number: 25544
Epoch time: 20130
06301813 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 182
1195 deg
Eccentricity:
0001394
Arg of perigee: 271
4083 deg
Mean anomaly: 88
6908 deg
Mean motion: 15
49328268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 308
Coasting Arc #7 (Orbit 2609)
---------------------------------------
Vector Time (GMT): 2020/131/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6641703
00 A = 6802489
08 meter
Y = -590170
39 meter E =
0012678
Z = 1313538
44 I = 51
68019
XDOT = 1578
072605 Wp = 55
71920
YDOT = -4721
048741 meter/sec RA = 176
12117 deg
ZDOT = 5824
878849 TA = 318
54271
MA = 318
63882
Ha = 228
001 n
mi
Hp = 222
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21790364
17 X = -6640990
41
Y = -1936254
57 feet Y = -664438
81 meter
Z = 4309509
32 Z = 1281276
92
XDOT = 5177
403560 XDOT = 1602
453222
YDOT = -15489
005056 feet/sec YDOT = -4703
265979 meter/sec
ZDOT = 19110
494910 ZDOT = 5832
603258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12816108
04 X = 3906349
73
Y = -17764331
25 feet Y = -5414568
17 meter
Z = 4161349
89 Z = 1268379
45
XDOT = 9436
947387 XDOT = 2876
381564
YDOT = 11319
794026 feet/sec YDOT = 3450
273219 meter/sec
ZDOT = 19146
103872 ZDOT = 5835
732460
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 20131
09502147
00016717 00000-0 10270-3 0 9068
2 25544 51
6403 177
0110 0001355 276
9738 83
1258 15
49381230 26106
Satellite: ISS
Catalog Number: 25544
Epoch time: 20131
09502147 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 177
0110 deg
Eccentricity:
0001355
Arg of perigee: 276
9738 deg
Mean anomaly: 83
1258 deg
Mean motion: 15
49381230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2610
Checksum: 278
Coasting Arc #8 (Orbit 2624)
---------------------------------------
Vector Time (GMT): 2020/132/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6640761
91 A = 6802444
75 meter
Y = 128966
53 meter E =
0007561
Z = -1451863
54 I = 51
71272
XDOT = -1354
533136 Wp = 150
21383
YDOT = 4832
149773 meter/sec RA = 171
17637 deg
ZDOT = -5785
701036 TA = 45
57321
MA = 45
51136
Ha = 228
059 n
mi
Hp = 222
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21787276
60 X = 6645878
58
Y = 423118
55 feet Y = 203257
04 meter
Z = -4763331
82 Z = -1419592
65
XDOT = -4444
006351 XDOT = -1380
363180
YDOT = 15853
509755 feet/sec YDOT = 4816
858706 meter/sec
ZDOT = -18981
958780 ZDOT = -5792
343017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11194948
80 X = -3412220
39
Y = 18733068
38 feet Y = 5709839
24 meter
Z = -4615089
54 Z = -1406679
29
XDOT = -10255
482358 XDOT = -3125
871023
YDOT = -10796
522701 feet/sec YDOT = -3290
780119 meter/sec
ZDOT = -19012
607238 ZDOT = -5795
042686
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 20132
06252689
00016717 00000-0 10270-3 0 9070
2 25544 51
6399 172
2231 0001438 279
5476 80
5512 15
49340995 26254
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
06252689 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 172
2231 deg
Eccentricity:
0001438
Arg of perigee: 279
5476 deg
Mean anomaly: 80
5512 deg
Mean motion: 15
49340995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2625
Checksum: 318
Coasting Arc #9 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2020/132/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3852226
31 A = 6796622
26 meter
Y = -3986480
63 meter E =
0009915
Z = 3925550
36 I = 51
71308
XDOT = 6189
639323 Wp = 77
48476
YDOT = 1966
368184 meter/sec RA = 168
00392 deg
ZDOT = -4066
360043 TA = 55
10164
MA = 55
00849
Ha = 227
994 n
mi
Hp = 222
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12638537
75 X = 3877449
86
Y = -13079004
69 feet Y = -3943261
73 meter
Z = 12879102
22 Z = 3944323
83
XDOT = 20307
215627 XDOT = 6186
942913
YDOT = 6451
339187 feet/sec YDOT = 2035
570544 meter/sec
ZDOT = -13341
076257 ZDOT = -4036
299387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16451488
95 X = -5014413
83
Y = -7609825
61 feet Y = -2319474
85 meter
Z = 12965467
19 Z = 3951874
40
XDOT = -1095
443895 XDOT = -333
891299
YDOT = -20186
667929 feet/sec YDOT = -6152
896385 meter/sec
ZDOT = -13203
024019 ZDOT = -4024
281721
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 20132
70752970
00016717 00000-0 10270-3 0 9080
2 25544 51
6382 169
0300 0001238 285
0918 75
0095 15
49366105 26355
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
70752970 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 169
0300 deg
Eccentricity:
0001238
Arg of perigee: 285
0918 deg
Mean anomaly: 75
0095 deg
Mean motion: 15
49366105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2635
Checksum: 299
Coasting Arc #10 (Orbit 2638)
---------------------------------------
Vector Time (GMT): 2020/132/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6432419
25 A = 6801361
07 meter
Y = 254311
64 meter E =
0005211
Z = -2188831
73 I = 51
74143
XDOT = -2058
062552 Wp = 148
00744
YDOT = 4930
868077 meter/sec RA = 166
71109 deg
ZDOT = -5485
521274 TA = 56
19532
MA = 56
14571
Ha = 228
076 n
mi
Hp = 222
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21103737
68 X = 6439729
51
Y = 834355
78 feet Y = 326284
66 meter
Z = -7181206
47 Z = -2157567
67
XDOT = -6752
173726 XDOT = -2086
402420
YDOT = 16177
388704 feet/sec YDOT = 4907
695541 meter/sec
ZDOT = -17997
117040 ZDOT = -5495
586823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19261577
11 X = -5870928
70
Y = 8780539
63 feet Y = 2676308
48 meter
Z = -7037569
96 Z = -2145051
33
XDOT = -724
853855 XDOT = -220
935455
YDOT = -16024
259425 feet/sec YDOT = -4884
194273 meter/sec
ZDOT = -18043
504364 ZDOT = -5499
660130
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 20132
96553052
00016717 00000-0 10270-3 0 9099
2 25544 51
6424 167
7550 0001441 281
7645 78
3343 15
49333624 26396
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
96553052 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 167
7550 deg
Eccentricity:
0001441
Arg of perigee: 281
7645 deg
Mean anomaly: 78
3343 deg
Mean motion: 15
49333624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2639
Checksum: 309
Coasting Arc #11 (Orbit 2654)
---------------------------------------
Vector Time (GMT): 2020/133/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6392939
49 A = 6801089
24 meter
Y = 204576
35 meter E =
0012816
Z = 2292475
85 I = 51
77322
XDOT = 1792
509621 Wp = 67
64807
YDOT = -5096
896382 meter/sec RA = 161
76882 deg
ZDOT = 5434
001432 TA = 317
78728
MA = 317
88589
Ha = 228
103 n
mi
Hp = 222
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20974210
92 X = -6405887
52
Y = 671182
26 feet Y = 133013
32 meter
Z = 7521246
23 Z = 2261390
02
XDOT = 5880
937076 XDOT = 1822
976135
YDOT = -16722
100990 feet/sec YDOT = -5076
681476 meter/sec
ZDOT = 17828
088689 ZDOT = 5442
782215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18294110
39 X = 5576044
85
Y = -10383738
01 feet Y = -3164963
34 meter
Z = 7378391
71 Z = 2248933
79
XDOT = 1931
179754 XDOT = 588
623589
YDOT = 16145
706759 feet/sec YDOT = 4921
211420 meter/sec
ZDOT = 17868
585884 ZDOT = 5446
344977
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 20133
99753093
00016717 00000-0 10270-3 0 9102
2 25544 51
6424 162
6464 0001456 295
9666 64
1334 15
49362755 26558
Satellite: ISS
Catalog Number: 25544
Epoch time: 20133
99753093 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 162
6464 deg
Eccentricity:
0001456
Arg of perigee: 295
9666 deg
Mean anomaly: 64
1334 deg
Mean motion: 15
49362755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2655
Checksum: 324
Coasting Arc #12 (Orbit 2669)
---------------------------------------
Vector Time (GMT): 2020/134/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6321927
47 A = 6800901
48 meter
Y = -632089
18 meter E =
0004296
Z = -2422783
92 I = 51
80303
XDOT = -1528
224012 Wp = 140
80256
YDOT = 5245
506617 meter/sec RA = 156
82989 deg
ZDOT = -5364
656426 TA = 66
15817
MA = 66
11315
Ha = 228
108 n
mi
Hp = 222
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20741231
87 X = 6340294
31
Y = -2073783
40 feet Y = -561289
98 meter
Z = -7948766
14 Z = -2392029
95
XDOT = -5013
858306 XDOT = -1560
708839
YDOT = 17209
667380 feet/sec YDOT = 5228
235762 meter/sec
ZDOT = -17600
578824 ZDOT = -5372
158375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17236727
41 X = -5253754
51
Y = 11816169
01 feet Y = 3601568
31 meter
Z = -7807402
81 Z = -2379696
38
XDOT = -3120
342677 XDOT = -951
080448
YDOT = -16185
408593 feet/sec YDOT = -4933
312539 meter/sec
ZDOT = -17635
210506 ZDOT = -5375
212162
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 20134
96503122
00016717 00000-0 10270-3 0 9117
2 25544 51
6415 157
8583 0001451 294
0384 66
0614 15
49337901 26702
Satellite: ISS
Catalog Number: 25544
Epoch time: 20134
96503122 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 157
8583 deg
Eccentricity:
0001451
Arg of perigee: 294
0384 deg
Mean anomaly: 66
0614 deg
Mean motion: 15
49337901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2670
Checksum: 293
Coasting Arc #13 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2020/135/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4964445
36 A = 6794985
54 meter
Y = 1367531
42 meter E =
0008319
Z = -4442111
37 I = 51
80968
XDOT = -4441
069288 Wp = 62
53076
YDOT = 5258
125184 meter/sec RA = 152
66624 deg
ZDOT = -3345
608455 TA = 173
67867
MA = 173
66817
Ha = 228
125 n
mi
Hp = 222
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16287550
41 X = 4970361
48
Y = 4486651
64 feet Y = 1423080
79 meter
Z = -14573856
18 Z = -4417981
58
XDOT = -14570
437297 XDOT = -4483
286094
YDOT = 17251
066877 feet/sec YDOT = 5208
226186 meter/sec
ZDOT = -10976
405693 ZDOT = -3367
283564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12626823
28 X = -3848655
73
Y = -11366488
48 feet Y = -3464505
69 meter
Z = -14462983
74 Z = -4408317
44
XDOT = 19869
289882 XDOT = 6056
159556
YDOT = -7983
344794 feet/sec YDOT = -2433
323493 meter/sec
ZDOT = -11076
190894 ZDOT = -3376
022984
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 20135
80353233
00016717 00000-0 10270-3 0 9128
2 25544 51
6417 153
7081 0001287 305
8618 54
2412 15
49381745 26834
Satellite: ISS
Catalog Number: 25544
Epoch time: 20135
80353233 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 153
7081 deg
Eccentricity:
0001287
Arg of perigee: 305
8618 deg
Mean anomaly: 54
2412 deg
Mean motion: 15
49381745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 296
Coasting Arc #14 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2020/136/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4974305
10 A = 6794780
14 meter
Y = -1045182
24 meter E =
0007836
Z = 4504207
96 I = 51
83829
XDOT = 4110
836374 Wp = 109
04555
YDOT = -5600
679311 meter/sec RA = 147
72976 deg
ZDOT = 3233
178950 TA = 308
46564
MA = 308
53592
Ha = 228
276 n
mi
Hp = 222
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16319898
61 X = -4984126
75
Y = -3429075
59 feet Y = -1100863
66 meter
Z = 14777585
17 Z = 4480020
78
XDOT = 13486
995977 XDOT = 4157
454353
YDOT = -18374
932123 feet/sec YDOT = -5554
448558 meter/sec
ZDOT = 10607
542486 ZDOT = 3253
260684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13309462
58 X = 4056724
19
Y = 10209250
94 feet Y = 3111779
69 meter
Z = 14666426
79 Z = 4470326
88
XDOT = -19310
787484 XDOT = -5885
928025
YDOT = 9769
717637 feet/sec YDOT = 2977
809936 meter/sec
ZDOT = 10700
028955 ZDOT = 3261
368826
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 20136
83553098
00016717 00000-0 10270-3 0 9134
2 25544 51
6418 148
6005 0001314 305
9029 54
1999 15
49364945 26991
Satellite: ISS
Catalog Number: 25544
Epoch time: 20136
83553098 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 148
6005 deg
Eccentricity:
0001314
Arg of perigee: 305
9029 deg
Mean anomaly: 54
1999 deg
Mean motion: 15
49364945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 329
Coasting Arc #15 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2020/137/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4967490
37 A = 6794429
64 meter
Y = 747275
64 meter E =
0009261
Z = -4584244
99 I = 51
86622
XDOT = -3750
515219 Wp = 62
22951
YDOT = 5904
915382 meter/sec RA = 142
79500 deg
ZDOT = -3102
099295 TA = 176
75071
MA = 176
74469
Ha = 228
140 n
mi
Hp = 222
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16297540
58 X = 4981032
65
Y = 2451691
73 feet Y = 802901
63 meter
Z = -15040173
84 Z = -4560081
83
XDOT = -12304
839958 XDOT = -3801
198702
YDOT = 19373
081963 feet/sec YDOT = 5862
691237 meter/sec
ZDOT = -10177
491125 ZDOT = -3120
440674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13873026
23 X = -4228498
39
Y = -9082312
13 feet Y = -2768288
74 meter
Z = -14929105
81 Z = -4550391
45
XDOT = 18551
327346 XDOT = 5654
444575
YDOT = -11471
745809 feet/sec YDOT = -3496
588123 meter/sec
ZDOT = -10262
001536 ZDOT = -3127
858068
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 20137
80302684
00016717 00000-0 10270-3 0 9146
2 25544 51
6429 143
8123 0001407 314
3515 45
7519 15
49389248 27143
Satellite: ISS
Catalog Number: 25544
Epoch time: 20137
80302684 = yrday
fracday
Element set: 914
Inclination: 51
6429 deg
RA of node: 143
8123 deg
Eccentricity:
0001407
Arg of perigee: 314
3515 deg
Mean anomaly: 45
7519 deg
Mean motion: 15
49389248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 303
Coasting Arc #16 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2020/138/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4937338
16 A = 6794253
77 meter
Y = -442608
36 meter E =
0007257
Z = 4641700
43 I = 51
89074
XDOT = 3367
317102 Wp = 110
07406
YDOT = -6203
129414 meter/sec RA = 137
86182 deg
ZDOT = 2984
080372 TA = 310
23049
MA = 310
29396
Ha = 228
377 n
mi
Hp = 222
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16198616
00 X = -4954568
72
Y = -1452127
17 feet Y = -497917
80 meter
Z = 15228675
97 Z = 4617674
72
XDOT = 11047
628286 XDOT = 3421
937003
YDOT = -20351
474456 feet/sec YDOT = -6165
168446 meter/sec
ZDOT = 9790
289935 ZDOT = 3000
569919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14340011
62 X = 4370835
54
Y = 7887958
31 feet Y = 2404249
69 meter
Z = 15118220
33 Z = 4608033
56
XDOT = -17666
015510 XDOT = -5384
601527
YDOT = 13166
852122 feet/sec YDOT = 4013
256527 meter/sec
ZDOT = 9866
312142 ZDOT = 3007
251941
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 20138
83502282
00016717 00000-0 10270-3 0 9157
2 25544 51
6422 138
7045 0001343 319
7525 40
3525 15
49364096 27301
Satellite: ISS
Catalog Number: 25544
Epoch time: 20138
83502282 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 138
7045 deg
Eccentricity:
0001343
Arg of perigee: 319
7525 deg
Mean anomaly: 40
3525 deg
Mean motion: 15
49364096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 292
Coasting Arc #17 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2020/139/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4897529
08 A = 6793919
25 meter
Y = 161417
52 meter E =
0010097
Z = -4715796
23 I = 51
91398
XDOT = -2956
453753 Wp = 62
78497
YDOT = 6456
870937 meter/sec RA = 132
93085 deg
ZDOT = -2849
572726 TA = 178
97791
MA = 178
97584
Ha = 228
151 n
mi
Hp = 222
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16068008
79 X = 4918266
96
Y = 529585
05 feet Y = 216301
43 meter
Z = -15471772
41 Z = -4691955
31
XDOT = -9699
651419 XDOT = -3014
594921
YDOT = 21183
959766 feet/sec YDOT = 6423
484857 meter/sec
ZDOT = -9348
991883 ZDOT = -2864
074991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14711271
79 X = -4483995
64
Y = -6739436
80 feet Y = -2054180
34 meter
Z = -15362147
72 Z = -4682382
62
XDOT = 16584
013587 XDOT = 5054
807341
YDOT = -14739
145246 feet/sec YDOT = -4492
491471 meter/sec
ZDOT = -9415
902968 ZDOT = -2869
967225
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 20139
80251720
00016717 00000-0 10270-3 0 9164
2 25544 51
6422 133
9166 0001522 318
5892 41
5142 15
49388958 27452
Satellite: ISS
Catalog Number: 25544
Epoch time: 20139
80251720 = yrday
fracday
Element set: 916
Inclination: 51
6422 deg
RA of node: 133
9166 deg
Eccentricity:
0001522
Arg of perigee: 318
5892 deg
Mean anomaly: 41
5142 deg
Mean motion: 15
49388958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 310
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