[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 11th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
223/13:37:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 222
5
231/17:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
2
234/09:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
1
Coasting Arc #1 (Orbit 42)
---------------------------------------
Vector Time (GMT): 2020/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2559284
85 A = 6795943
35 meter
Y = -4563157
04 meter E =
0009129
Z = -4346971
31 I = 52
02122
XDOT = 3904
631587 Wp = 61
60972
YDOT = 5552
546566 meter/sec RA = 78
84650 deg
ZDOT = -3531
248571 TA = 172
55943
MA = 172
54588
Ha = 228
918 n
mi
Hp = 222
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8396603
85 X = 2631236
15
Y = -14970987
67 feet Y = -4534134
88 meter
Z = -14261716
91 Z = -4334364
77
XDOT = 12810
471087 XDOT = 3859
403789
YDOT = 18217
016293 feet/sec YDOT = 5595
958146 meter/sec
ZDOT = -11585
461192 ZDOT = -3512
391278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16279719
50 X = -4962058
50
Y = 5591686
69 feet Y = 1704346
10 meter
Z = -14203301
37 Z = -4329166
26
XDOT = 2815
690799 XDOT = 858
222555
YDOT = -20997
864291 feet/sec YDOT = -6400
149036 meter/sec
ZDOT = -11498
624347 ZDOT = -3504
780701
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 20223
52255796
00016717 00000-0 10270-3 0 9007
2 25544 51
6430 79
5579 0001362 2
1659 357
9497 15
49154858 439
Satellite: ISS
Catalog Number: 25544
Epoch time: 20223
52255796 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 79
5579 deg
Eccentricity:
0001362
Arg of perigee: 2
1659 deg
Mean anomaly: 357
9497 deg
Mean motion: 15
49154858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 43
Checksum: 320
Coasting Arc #2 (Orbit 43)
---------------------------------------
Vector Time (GMT): 2020/223/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3483194
48 A = 6793001
05 meter
Y = -2853733
62 meter E =
0013618
Z = -5098449
14 I = 52
00845
XDOT = 2876
123755 Wp = 71
37796
YDOT = 6839
266521 meter/sec RA = 78
50208 deg
ZDOT = -1863
032721 TA = 180
62080
MA = 180
62249
Ha = 228
962 n
mi
Hp = 222
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11427803
40 X = 3539612
05
Y = -9362643
10 feet Y = -2814466
47 meter
Z = -16727195
35 Z = -5081392
33
XDOT = 9436
101559 XDOT = 2808
480742
YDOT = 22438
538455 feet/sec YDOT = 6871
051222 meter/sec
ZDOT = -6112
312078 ZDOT = -1849
225878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13778426
25 X = -4199664
32
Y = 5571516
55 feet Y = 1698198
25 meter
Z = -16648303
64 Z = -5074402
95
XDOT = -2082
247223 XDOT = -634
668953
YDOT = -23225
551331 feet/sec YDOT = -7079
148046 meter/sec
ZDOT = -6048
855222 ZDOT = -1843
691072
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 20223
58706702
00016717 00000-0 10270-3 0 9012
2 25544 51
6405 79
2367 0001233 10
5659 349
5517 15
49156187 441
Satellite: ISS
Catalog Number: 25544
Epoch time: 20223
58706702 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 79
2367 deg
Eccentricity:
0001233
Arg of perigee: 10
5659 deg
Mean anomaly: 349
5517 deg
Mean motion: 15
49156187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 44
Checksum: 297
Coasting Arc #3 (Orbit 59)
---------------------------------------
Vector Time (GMT): 2020/224/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3250805
01 A = 6793036
54 meter
Y = 3078771
54 meter E =
0005087
Z = 5105082
56 I = 52
00000
XDOT = -3421
359618 Wp = 110
74431
YDOT = -6614
593273 meter/sec RA = 73
57974 deg
ZDOT = 1807
275954 TA = 321
82316
MA = 321
85918
Ha = 229
198 n
mi
Hp = 222
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10665370
77 X = -3309788
56
Y = 10100956
49 feet Y = 3042088
72 meter
Z = 16748958
52 Z = 5089148
38
XDOT = -11224
933131 XDOT = -3355
917628
YDOT = -21701
421499 feet/sec YDOT = -6652
487521 meter/sec
ZDOT = 5929
383052 ZDOT = 1790
815129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13152110
77 X = 4008763
36
Y = -6727974
88 feet Y = -2050686
74 meter
Z = 16675233
23 Z = 5082611
09
XDOT = 4335
995925 XDOT = 1321
611558
YDOT = 23010
637138 feet/sec YDOT = 7013
642200 meter/sec
ZDOT = 5853
677638 ZDOT = 1784
200944
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 20224
61920733
00016717 00000-0 10270-3 0 9020
2 25544 51
6403 74
1299 0001278 15
1137 345
0051 15
49115738 607
Satellite: ISS
Catalog Number: 25544
Epoch time: 20224
61920733 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 74
1299 deg
Eccentricity:
0001278
Arg of perigee: 15
1137 deg
Mean anomaly: 345
0051 deg
Mean motion: 15
49115738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 60
Checksum: 271
Coasting Arc #4 (Orbit 74)
---------------------------------------
Vector Time (GMT): 2020/225/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3019970
41 A = 6792844
55 meter
Y = -3290206
31 meter E =
0014007
Z = -5130927
00 I = 51
98875
XDOT = 3933
073700 Wp = 73
11806
YDOT = 6325
654497 meter/sec RA = 68
65656 deg
ZDOT = -1741
367603 TA = 180
08800
MA = 180
08825
Ha = 229
029 n
mi
Hp = 222
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9908039
40 X = 3081460
98
Y = -10794640
12 feet Y = -3256090
75 meter
Z = -16833750
00 Z = -5116108
09
XDOT = 12903
785105 XDOT = 3870
504536
YDOT = 20753
459636 feet/sec YDOT = 6369
287187 meter/sec
ZDOT = -5713
148305 ZDOT = -1722
414015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12483988
26 X = -3805119
62
Y = 7819731
72 feet Y = 2383454
23 meter
Z = -16765156
49 Z = -5110019
70
XDOT = -6534
043950 XDOT = -1991
576596
YDOT = -22493
329492 feet/sec YDOT = -6855
966829 meter/sec
ZDOT = -5625
934207 ZDOT = -1714
784746
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 20225
58683648
00016717 00000-0 10270-3 0 9039
2 25544 51
6400 69
3423 0001146 23
1609 336
9593 15
49157844 756
Satellite: ISS
Catalog Number: 25544
Epoch time: 20225
58683648 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 69
3423 deg
Eccentricity:
0001146
Arg of perigee: 23
1609 deg
Mean anomaly: 336
9593 deg
Mean motion: 15
49157844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 75
Checksum: 309
Coasting Arc #5 (Orbit 90)
---------------------------------------
Vector Time (GMT): 2020/226/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2762570
74 A = 6792855
23 meter
Y = 3477623
79 meter E =
0004940
Z = 5136219
16 I = 51
97561
XDOT = -4437
629827 Wp = 110
65647
YDOT = -6016
481836 meter/sec RA = 63
73223 deg
ZDOT = 1683
802341 TA = 323
13044
MA = 323
16439
Ha = 229
206 n
mi
Hp = 222
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9063552
30 X = -2826201
86
Y = 11409526
86 feet Y = 3446374
60 meter
Z = 16851112
73 Z = 5122645
48
XDOT = -14559
152975 XDOT = -4378
200794
YDOT = -19739
113634 feet/sec YDOT = -6065
774413 meter/sec
ZDOT = 5524
285895 ZDOT = 1662
390166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11678212
05 X = 3559519
03
Y = -8835114
88 feet Y = -2692943
01 meter
Z = 16788251
60 Z = 5117059
09
XDOT = 8712
615281 XDOT = 2655
605138
YDOT = 21844
878649 feet/sec YDOT = 6658
319012 meter/sec
ZDOT = 5425
717181 ZDOT = 1653
758597
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 20226
61897460
00016717 00000-0 10270-3 0 9044
2 25544 51
6405 64
2350 0001227 22
4783 337
6421 15
49126826 911
Satellite: ISS
Catalog Number: 25544
Epoch time: 20226
61897460 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 64
2350 deg
Eccentricity:
0001227
Arg of perigee: 22
4783 deg
Mean anomaly: 337
6421 deg
Mean motion: 15
49126826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 91
Checksum: 289
Coasting Arc #6 (Orbit 105)
---------------------------------------
Vector Time (GMT): 2020/227/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2509762
11 A = 6792668
13 meter
Y = -3651820
68 meter E =
0014481
Z = -5161334
18 I = 51
96014
XDOT = 4897
772112 Wp = 74
48075
YDOT = 5649
209078 meter/sec RA = 58
80758 deg
ZDOT = -1615
415871 TA = 179
96543
MA = 179
96533
Ha = 229
112 n
mi
Hp = 222
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8234127
67 X = 2575481
86
Y = -11981038
97 feet Y = -3623386
85 meter
Z = -16933511
10 Z = -5148983
55
XDOT = 16068
806142 XDOT = 4842
083631
YDOT = 18534
150520 feet/sec YDOT = 5703
668220 meter/sec
ZDOT = -5299
920837 ZDOT = -1591
759484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10846675
76 X = -3306066
77
Y = 9779096
34 feet Y = 2980668
56 meter
Z = -16876280
73 Z = -5143890
37
XDOT = -10774
636041 XDOT = -3284
109065
YDOT = -20909
186084 feet/sec YDOT = -6373
119918 meter/sec
ZDOT = -5190
980941 ZDOT = -1582
210991
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 20227
58660080
00016717 00000-0 10270-3 0 9058
2 25544 51
6413 59
4477 0001244 36
2414 323
8820 15
49168594 1064
Satellite: ISS
Catalog Number: 25544
Epoch time: 20227
58660080 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 59
4477 deg
Eccentricity:
0001244
Arg of perigee: 36
2414 deg
Mean anomaly: 323
8820 deg
Mean motion: 15
49168594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 106
Checksum: 296
Coasting Arc #7 (Orbit 121)
---------------------------------------
Vector Time (GMT): 2020/228/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2233885
00 A = 6792671
09 meter
Y = 3799339
50 meter E =
0004937
Z = 5165064
00 I = 51
94010
XDOT = -5348
480139 Wp = 110
15707
YDOT = -5263
314226 meter/sec RA = 53
88103 deg
ZDOT = 1555
538622 TA = 324
88722
MA = 324
91975
Ha = 229
255 n
mi
Hp = 222
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7329019
02 X = -2301292
86
Y = 12465024
60 feet Y = 3773981
29 meter
Z = 16945748
04 Z = 5154049
41
XDOT = -17547
507019 XDOT = -5296
782476
YDOT = -17268
091293 feet/sec YDOT = -5322
835817 meter/sec
ZDOT = 5103
473168 ZDOT = 1529
683339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9893495
34 X = 3015537
38
Y = -10627253
67 feet Y = -3239186
92 meter
Z = 16894672
66 Z = 5149496
23
XDOT = 12794
358634 XDOT = 3899
720512
YDOT = 19849
829248 feet/sec YDOT = 6050
227955 meter/sec
ZDOT = 4984
366680 ZDOT = 1519
234964
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 20228
61873626
00016717 00000-0 10270-3 0 9066
2 25544 51
6400 54
3404 0001241 36
7695 323
3540 15
49141386 1229
Satellite: ISS
Catalog Number: 25544
Epoch time: 20228
61873626 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 54
3404 deg
Eccentricity:
0001241
Arg of perigee: 36
7695 deg
Mean anomaly: 323
3540 deg
Mean motion: 15
49141386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 122
Checksum: 279
Coasting Arc #8 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2020/229/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1963979
43 A = 6792515
43 meter
Y = -3935899
30 meter E =
0014738
Z = -5189012
05 I = 51
92025
XDOT = 5745
589843 Wp = 76
00651
YDOT = 4825
946669 meter/sec RA = 48
95470 deg
ZDOT = -1485
950247 TA = 179
70615
MA = 179
70528
Ha = 229
129 n
mi
Hp = 222
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6443502
08 X = 2033050
63
Y = -12913055
45 feet Y = -3913550
12 meter
Z = -17024317
74 Z = -5179304
51
XDOT = 18850
360376 XDOT = 5698
415394
YDOT = 15833
158362 feet/sec YDOT = 4889
934295 meter/sec
ZDOT = -4875
164853 ZDOT = -1458
155207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8927310
85 X = -2721044
35
Y = 11406172
42 feet Y = 3476601
35 meter
Z = -16979265
77 Z = -5175280
21
XDOT = -14643
004674 XDOT = -4463
187825
YDOT = -18526
845306 feet/sec YDOT = -5646
982449 meter/sec
ZDOT = -4747
082616 ZDOT = -1446
910781
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 20229
58636149
00016717 00000-0 10270-3 0 9071
2 25544 51
6413 49
5539 0001194 44
1089 316
0156 15
49174411 1378
Satellite: ISS
Catalog Number: 25544
Epoch time: 20229
58636149 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 49
5539 deg
Eccentricity:
0001194
Arg of perigee: 44
1089 deg
Mean anomaly: 316
0156 deg
Mean motion: 15
49174411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 303
Coasting Arc #9 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2020/230/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1675337
54 A = 6792461
72 meter
Y = 4042596
60 meter E =
0004690
Z = 5191552
07 I = 51
89719
XDOT = -6130
518544 Wp = 110
09018
YDOT = -4372
428279 meter/sec RA = 44
02430 deg
ZDOT = 1423
797351 TA = 326
23825
MA = 326
26811
Ha = 229
193 n
mi
Hp = 222
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5496514
25 X = -1745635
56
Y = 13263112
19 feet Y = 4023468
45 meter
Z = 17032651
14 Z = 5183243
59
XDOT = -20113
249817 XDOT = -6088
084945
YDOT = -14345
237136 feet/sec YDOT = -4440
746931 meter/sec
ZDOT = 4671
251151 ZDOT = 1394
121219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7859263
56 X = 2395503
53
Y = -12069267
36 feet Y = -3678712
69 meter
Z = 16994051
32 Z = 5179786
84
XDOT = 16425
863321 XDOT = 5006
603140
YDOT = 17093
000986 feet/sec YDOT = 5209
946701 meter/sec
ZDOT = 4534
461759 ZDOT = 1382
103944
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 20230
61849398
00016717 00000-0 10270-3 0 9080
2 25544 51
6415 44
4455 0001168 40
5722 319
5515 15
49167662 1531
Satellite: ISS
Catalog Number: 25544
Epoch time: 20230
61849398 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 44
4455 deg
Eccentricity:
0001168
Arg of perigee: 40
5722 deg
Mean anomaly: 319
5515 deg
Mean motion: 15
49167662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 305
Coasting Arc #10 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2020/231/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1395014
35 A = 6792367
07 meter
Y = -4139876
16 meter E =
0015061
Z = -5214469
28 I = 51
87269
XDOT = 6453
651048 Wp = 77
04073
YDOT = 3876
979386 meter/sec RA = 39
09461 deg
ZDOT = -1351
490773 TA = 179
97926
MA = 179
97920
Ha = 229
167 n
mi
Hp = 222
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4576818
74 X = 1466532
29
Y = -13582270
88 feet Y = -4123876
10 meter
Z = -17107838
84 Z = -5207519
42
XDOT = 21173
395827 XDOT = 6416
382464
YDOT = 12719
748642 feet/sec YDOT = 3948
940380 meter/sec
ZDOT = -4434
024846 ZDOT = -1320
232658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6793784
43 X = -2070745
49
Y = 12663927
52 feet Y = 3859965
11 meter
Z = -17075506
86 Z = -5204614
49
XDOT = -17987
329878 XDOT = -5482
538147
YDOT = -15433
923371 feet/sec YDOT = -4704
259843 meter/sec
ZDOT = -4289
907858 ZDOT = -1307
563915
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 20231
58611635
00016717 00000-0 10270-3 0 9099
2 25544 51
6423 39
6588 0001294 48
4625 311
6636 15
49181620 1685
Satellite: ISS
Catalog Number: 25544
Epoch time: 20231
58611635 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 39
6588 deg
Eccentricity:
0001294
Arg of perigee: 48
4625 deg
Mean anomaly: 311
6636 deg
Mean motion: 15
49181620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 168
Checksum: 308
Coasting Arc #11 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2020/231/17:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3266996
30 A = 6791937
36 meter
Y = 2717447
46 meter E =
0004317
Z = 5295643
44 I = 51
86952
XDOT = -5586
134924 Wp = 53
74201
YDOT = -5187
337421 meter/sec RA = 38
26500 deg
ZDOT = -781
405420 TA = 43
72339
MA = 43
68920
Ha = 229
144 n
mi
Hp = 222
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10718491
79 X = -3322863
37
Y = 8915510
03 feet Y = 2680601
08 meter
Z = 17374158
27 Z = 5279638
42
XDOT = -18327
214317 XDOT = -5523
917867
YDOT = -17018
823561 feet/sec YDOT = -5249
457683 meter/sec
ZDOT = -2563
666076 ZDOT = -808
389002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 40534
63 X = 12354
96
Y = -14033489
84 feet Y = -4277407
70 meter
Z = 17300094
82 Z = 5273068
90
XDOT = 23761
456560 XDOT = 7242
491960
YDOT = -3256
922869 feet/sec YDOT = -992
710090 meter/sec
ZDOT = -2687
967466 ZDOT = -819
292484
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 20231
77963831
00016717 00000-0 10270-3 0 9100
2 25544 51
6447 38
7026 0001137 34
9808 325
1416 15
49206298 1716
Satellite: ISS
Catalog Number: 25544
Epoch time: 20231
77963831 = yrday
fracday
Element set: 910
Inclination: 51
6447 deg
RA of node: 38
7026 deg
Eccentricity:
0001137
Arg of perigee: 34
9808 deg
Mean anomaly: 325
1416 deg
Mean motion: 15
49206298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 171
Checksum: 300
Coasting Arc #12 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2020/232/17:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3085459
27 A = 6792111
12 meter
Y = -2951028
87 meter E =
0015122
Z = -5295575
14 I = 51
84125
XDOT = 5961
725464 Wp = 92
51782
YDOT = 4717
087464 meter/sec RA = 33
33335 deg
ZDOT = 846
374459 TA = 185
56336
MA = 185
58018
Ha = 229
134 n
mi
Hp = 222
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10122897
87 X = 3143951
51
Y = -9681853
24 feet Y = -2916198
03 meter
Z = -17373934
18 Z = -5280445
46
XDOT = 19559
466746 XDOT = 5904
423388
YDOT = 15476
008740 feet/sec YDOT = 4783
435351 meter/sec
ZDOT = 2776
819090 ZDOT = 875
194307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1171337
45 X = 357023
65
Y = 14045206
99 feet Y = 4280979
09 meter
Z = -17303903
07 Z = -5274229
66
XDOT = -23263
972603 XDOT = -7090
858849
YDOT = 5518
998973 feet/sec YDOT = 1682
190887 meter/sec
ZDOT = 2909
618351 ZDOT = 886
851674
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 20232
74726155
00016717 00000-0 10270-3 0 9115
2 25544 51
6436 33
9159 0001224 39
6195 320
5045 15
49164107 1861
Satellite: ISS
Catalog Number: 25544
Epoch time: 20232
74726155 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 33
9159 deg
Eccentricity:
0001224
Arg of perigee: 39
6195 deg
Mean anomaly: 320
5045 deg
Mean motion: 15
49164107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 186
Checksum: 290
Coasting Arc #13 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2020/233/17:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2887481
63 A = 6792034
58 meter
Y = 3154448
51 meter E =
0004615
Z = 5273856
05 I = 51
81324
XDOT = -6317
527749 Wp = 53
74127
YDOT = -4238
689729 meter/sec RA = 28
39890 deg
ZDOT = -920
393270 TA = 45
06702
MA = 45
02959
Ha = 229
158 n
mi
Hp = 222
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9473364
94 X = -2948157
89
Y = 10349240
52 feet Y = 3121819
51 meter
Z = 17302677
34 Z = 5259682
62
XDOT = -20726
797077 XDOT = -6265
189265
YDOT = -13906
462366 feet/sec YDOT = -4309
044228 meter/sec
ZDOT = -3019
662959 ZDOT = -950
953509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2338190
71 X = -712680
53
Y = -13915849
90 feet Y = -4241551
05 meter
Z = 17237054
60 Z = 5253854
24
XDOT = 22642
439785 XDOT = 6901
415646
YDOT = -7732
422278 feet/sec YDOT = -2356
842310 meter/sec
ZDOT = -3160
513895 ZDOT = -963
324635
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 20233
77938982
00016717 00000-0 10270-3 0 9123
2 25544 51
6443 28
8092 0001118 40
7790 319
3444 15
49202249 2022
Satellite: ISS
Catalog Number: 25544
Epoch time: 20233
77938982 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 28
8092 deg
Eccentricity:
0001118
Arg of perigee: 40
7790 deg
Mean anomaly: 319
3444 deg
Mean motion: 15
49202249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 202
Checksum: 299
Coasting Arc #14 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2020/234/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5177236
50 A = 6802282
20 meter
Y = -4014945
59 meter E =
0006932
Z = -1824031
15 I = 51
82485
XDOT = 4251
286116 Wp = 128
44336
YDOT = -2919
459679 meter/sec RA = 25
14964 deg
ZDOT = -5659
260006 TA = 71
50533
MA = 71
43001
Ha = 229
136 n
mi
Hp = 222
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16985684
05 X = -5123095
44
Y = -13172393
67 feet Y = -4072538
50 meter
Z = -5984354
16 Z = -1849048
09
XDOT = 13947
789096 XDOT = 4311
105435
YDOT = -9578
279786 feet/sec YDOT = -2871
584494 meter/sec
ZDOT = -18567
126003 ZDOT = -5638
463859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5951483
54 X = -1814012
18
Y = 20620679
79 feet Y = 6285183
20 meter
Z = -6099616
49 Z = -1859163
11
XDOT = -12610
987301 XDOT = -3843
828929
YDOT = -9085
606018 feet/sec YDOT = -2769
292714 meter/sec
ZDOT = -18470
944874 ZDOT = -5629
943998
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 20234
42447038
00016717 00000-0 10270-3 0 9134
2 25544 51
6417 25
6171 0001507 36
0015 324
1236 15
49183157 2126
Satellite: ISS
Catalog Number: 25544
Epoch time: 20234
42447038 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 25
6171 deg
Eccentricity:
0001507
Arg of perigee: 36
0015 deg
Mean anomaly: 324
1236 deg
Mean motion: 15
49183157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 212
Checksum: 264
Coasting Arc #15 (Orbit 227)
---------------------------------------
Vector Time (GMT): 2020/235/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5467227
82 A = 6802239
15 meter
Y = 3577492
39 meter E =
0015258
Z = 1865417
94 I = 51
79322
XDOT = -4053
465436 Wp = 64
43510
YDOT = 3238
320758 meter/sec RA = 20
21198 deg
ZDOT = 5640
042272 TA = 316
01434
MA = 316
13566
Ha = 229
176 n
mi
Hp = 222
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17937099
14 X = 5417755
85
Y = 11737179
75 feet Y = 3638354
30 meter
Z = 6120137
60 Z = 1891855
01
XDOT = -13298
771114 XDOT = -4116
771862
YDOT = 10624
411936 feet/sec YDOT = 3192
638268 meter/sec
ZDOT = 18504
075696 ZDOT = 5620
198442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3904804
29 X = 1190184
35
Y = -21041562
21 feet Y = -6413468
16 meter
Z = 6241967
79 Z = 1902551
78
XDOT = 13455
584367 XDOT = 4101
262115
YDOT = 7987
217570 feet/sec YDOT = 2434
503915 meter/sec
ZDOT = 18412
279884 ZDOT = 5612
062909
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 20235
45659672
00016717 00000-0 10270-3 0 9148
2 25544 51
6414 20
5095 0001446 44
7928 315
3338 15
49177183 2287
Satellite: ISS
Catalog Number: 25544
Epoch time: 20235
45659672 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 20
5095 deg
Eccentricity:
0001446
Arg of perigee: 44
7928 deg
Mean anomaly: 315
3338 deg
Mean motion: 15
49177183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 228
Checksum: 309
Coasting Arc #16 (Orbit 242)
---------------------------------------
Vector Time (GMT): 2020/236/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5706574
26 A = 6802035
35 meter
Y = -3147064
10 meter E =
0006927
Z = -1944887
24 I = 51
76036
XDOT = 3847
618372 Wp = 125
85773
YDOT = -3525
789640 meter/sec RA = 15
27339 deg
ZDOT = -5602
252536 TA = 75
49466
MA = 75
41781
Ha = 229
219 n
mi
Hp = 221
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18722356
49 X = -5661511
63
Y = -10325013
46 feet Y = -3210627
20 meter
Z = -6380863
64 Z = -1972497
83
XDOT = 12623
419856 XDOT = 3913
971227
YDOT = -11567
551312 feet/sec YDOT = -3482
391992 meter/sec
ZDOT = -18380
093622 ZDOT = -5583
401154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1934230
36 X = -589553
41
Y = 21254436
26 feet Y = 6478352
17 meter
Z = -6508121
73 Z = -1983675
50
XDOT = -14171
344409 XDOT = -4319
425776
YDOT = -6873
248792 feet/sec YDOT = -2094
966232 meter/sec
ZDOT = -18292
867906 ZDOT = -5575
666138
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 20236
42421424
00016717 00000-0 10270-3 0 9159
2 25544 51
6411 15
7222 0001636 48
1113 312
0177 15
49198641 2431
Satellite: ISS
Catalog Number: 25544
Epoch time: 20236
42421424 = yrday
fracday
Element set: 915
Inclination: 51
6411 deg
RA of node: 15
7222 deg
Eccentricity:
0001636
Arg of perigee: 48
1113 deg
Mean anomaly: 312
0177 deg
Mean motion: 15
49198641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 243
Checksum: 264
Coasting Arc #17 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2020/237/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5922702
10 A = 6802037
13 meter
Y = 2672798
76 meter E =
0015313
Z = 1986348
42 I = 51
72664
XDOT = -3604
726646 Wp = 67
07747
YDOT = 3818
900892 meter/sec RA = 10
33189 deg
ZDOT = 5581
113688 TA = 314
78468
MA = 314
90913
Ha = 229
228 n
mi
Hp = 221
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19431437
33 X = 5882725
36
Y = 8769024
80 feet Y = 2738807
15 meter
Z = 6516891
14 Z = 2015021
36
XDOT = -11826
530992 XDOT = -3674
272601
YDOT = 12529
202402 feet/sec YDOT = 3778
201475 meter/sec
ZDOT = 18310
740446 ZDOT = 5563
434433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -141185
58 X = -43033
37
Y = -21277133
05 feet Y = -6485270
15 meter
Z = 6649067
51 Z = 2026635
78
XDOT = 14828
118907 XDOT = 4519
610643
YDOT = 5626
709713 feet/sec YDOT = 1715
021121 meter/sec
ZDOT = 18228
911133 ZDOT = 5556
172113
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 20237
45633945
00016717 00000-0 10270-3 0 9167
2 25544 51
6405 10
6152 0001444 57
4560 302
6730 15
49175973 2596
Satellite: ISS
Catalog Number: 25544
Epoch time: 20237
45633945 = yrday
fracday
Element set: 916
Inclination: 51
6405 deg
RA of node: 10
6152 deg
Eccentricity:
0001444
Arg of perigee: 57
4560 deg
Mean anomaly: 302
6730 deg
Mean motion: 15
49175973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 259
Checksum: 297
Coasting Arc #18 (Orbit 273)
---------------------------------------
Vector Time (GMT): 2020/238/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6088846
85 A = 6801787
64 meter
Y = -2214512
69 meter E =
0006808
Z = -2067227
33 I = 51
69411
XDOT = 3358
925726 Wp = 124
44349
YDOT = -4079
127032 meter/sec RA = 5
38840 deg
ZDOT = -5540
473541 TA = 78
34682
MA = 78
27042
Ha = 229
231 n
mi
Hp = 221
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19976531
67 X = -6053589
60
Y = -7265461
57 feet Y = -2282405
37 meter
Z = -6782241
89 Z = -2096718
86
XDOT = 11020
097526 XDOT = 3431
202472
YDOT = -13382
962703 feet/sec YDOT = -4041
160948 meter/sec
ZDOT = -18177
406631 ZDOT = -5523
981736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2097551
74 X = 639333
77
Y = 21108911
92 feet Y = 6433996
35 meter
Z = -6918212
83 Z = -2108671
27
XDOT = -15353
672025 XDOT = -4679
799233
YDOT = -4389
052041 feet/sec YDOT = -1337
783062 meter/sec
ZDOT = -18101
044308 ZDOT = -5517
198305
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 20238
42395383
00016717 00000-0 10270-3 0 9177
2 25544 51
6419 5
8275 0001618 55
9995 304
1309 15
49209696 2747
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
42395383 = yrday
fracday
Element set: 917
Inclination: 51
6419 deg
RA of node: 5
8275 deg
Eccentricity:
0001618
Arg of perigee: 55
9995 deg
Mean anomaly: 304
1309 deg
Mean motion: 15
49209696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 274
Checksum: 328
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