[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 15th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14255 723 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 865 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
073/05:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
1
000/00:00:00
000 0
0 0
0 221
5
079/17:18:26
637 1
0 1
9 1
9
N/A 1
5 0
0 230
7
000/00:08:53
274 -0
6 -0
0 221
9
081/01:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
7
000/00:00:00
000 0
0 0
0 221
7
085/12:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
9
000/00:00:00
000 0
0 0
0 221
4
Coasting Arc #1 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2020/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4063546
67 A = 6791669
46 meter
Y = -1049794
44 meter E =
0006298
Z = 5336016
37 I = 51
98361
XDOT = 2413
941241 Wp = 38
54121
YDOT = -7262
301576 meter/sec RA = 110
81054 deg
ZDOT = 414
055797 TA = 47
55333
MA = 47
50009
Ha = 230
180 n
mi
Hp = 221
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13331846
02 X = -4077424
62
Y = -3444207
48 feet Y = -1095312
84 meter
Z = 17506615
38 Z = 5316243
87
XDOT = 7919
754729 XDOT = 2492
959804
YDOT = -23826
448741 feet/sec YDOT = -7234
865296 meter/sec
ZDOT = 1358
450776 ZDOT = 425
974491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12516021
58 X = -3814883
38
Y = -6009778
37 feet Y = -1831780
45 meter
Z = 17415913
22 Z = 5308370
35
XDOT = 11983
442490 XDOT = 3652
553271
YDOT = -20904
090065 feet/sec YDOT = -6371
566652 meter/sec
ZDOT = 1413
433450 ZDOT = 430
814515
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 20071
54914440
00016717 00000-0 10270-3 0 9008
2 25544 51
6410 111
5742 0005954 13
5438 346
5870 15
49242261 16878
Satellite: ISS
Catalog Number: 25544
Epoch time: 20071
54914440 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 111
5742 deg
Eccentricity:
0005954
Arg of perigee: 13
5438 deg
Mean anomaly: 346
5870 deg
Mean motion: 15
49242261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1687
Checksum: 290
Coasting Arc #2 (Orbit 1701)
---------------------------------------
Vector Time (GMT): 2020/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4124558
43 A = 6791727
88 meter
Y = 787724
23 meter E =
0017620
Z = -5352562
14 I = 51
99487
XDOT = -1845
627695 Wp = 69
03257
YDOT = 7414
862519 meter/sec RA = 105
88626 deg
ZDOT = -325
713328 TA = 197
83820
MA = 197
90013
Ha = 230
146 n
mi
Hp = 221
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13532015
84 X = 4141442
87
Y = 2584397
08 feet Y = 833941
80 meter
Z = -17560899
42 Z = -5332485
84
XDOT = -6055
208972 XDOT = -1926
823583
YDOT = 24326
976768 feet/sec YDOT = 7393
769367 meter/sec
ZDOT = -1068
613282 ZDOT = -334
876632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12968639
99 X = 3952841
47
Y = 4983518
06 feet Y = 1518976
30 meter
Z = -17468791
43 Z = -5324487
63
XDOT = -9938
196003 XDOT = -3029
162142
YDOT = 21907
146664 feet/sec YDOT = 6677
298303 meter/sec
ZDOT = -1110
976646 ZDOT = -338
625682
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 20072
51672563
00016717 00000-0 10270-3 0 9014
2 25544 51
6415 106
7862 0005908 16
6137 343
5205 15
49220277 17021
Satellite: ISS
Catalog Number: 25544
Epoch time: 20072
51672563 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 106
7862 deg
Eccentricity:
0005908
Arg of perigee: 16
6137 deg
Mean anomaly: 343
5205 deg
Mean motion: 15
49220277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1702
Checksum: 289
Coasting Arc #3 (Orbit 1712)
---------------------------------------
Vector Time (GMT): 2020/073/05:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3799039
49 A = 6791903
57 meter
Y = 1966313
08 meter E =
0016497
Z = -5288926
24 I = 52
00082
XDOT = -2367
631346 Wp = 78
06020
YDOT = 7206
437345 meter/sec RA = 102
36825 deg
ZDOT = 984
438420 TA = 201
30519
MA = 201
37396
Ha = 230
085 n
mi
Hp = 221
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12464040
31 X = 3802459
74
Y = 6451158
39 feet Y = 2008815
27 meter
Z = -17352120
22 Z = -5270463
94
XDOT = -7767
819378 XDOT = -2452
821710
YDOT = 23643
167142 feet/sec YDOT = 7179
484569 meter/sec
ZDOT = 3229
784844 ZDOT = 972
729863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10908976
50 X = -3325056
04
Y = 8994138
42 feet Y = 2741413
39 meter
Z = -17267470
21 Z = -5263124
92
XDOT = -17963
076369 XDOT = -5475
145677
YDOT = -15727
812747 feet/sec YDOT = -4793
837325 meter/sec
ZDOT = 3175
732481 ZDOT = 967
963260
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 20073
22628431
00016717 00000-0 10270-3 0 9029
2 25544 51
6405 103
2720 0005634 19
8214 340
3154 15
49251689 17133
Satellite: ISS
Catalog Number: 25544
Epoch time: 20073
22628431 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 103
2720 deg
Eccentricity:
0005634
Arg of perigee: 19
8214 deg
Mean anomaly: 340
3154 deg
Mean motion: 15
49251689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1713
Checksum: 276
Coasting Arc #4 (Orbit 1728)
---------------------------------------
Vector Time (GMT): 2020/074/05:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3915983
49 A = 6792031
33 meter
Y = -1752067
68 meter E =
0009139
Z = 5262094
62 I = 52
00834
XDOT = 1820
240286 Wp = 36
71392
YDOT = -7364
383650 meter/sec RA = 97
44366 deg
ZDOT = -1089
347048 TA = 63
72373
MA = 63
62985
Ha = 230
329 n
mi
Hp = 221
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12847714
88 X = -3921660
48
Y = -5748253
54 feet Y = -1795890
38 meter
Z = 17264089
95 Z = 5243058
70
XDOT = 5971
916949 XDOT = 1907
747120
YDOT = -24161
363681 feet/sec YDOT = -7343
539221 meter/sec
ZDOT = -3573
973255 ZDOT = -1080
292031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10248400
90 X = 3123712
60
Y = -9802186
29 feet Y = -2987706
38 meter
Z = 17176798
91 Z = 5235488
31
XDOT = 19347
344564 XDOT = 5897
070623
YDOT = 13991
872490 feet/sec YDOT = 4264
722735 meter/sec
ZDOT = -3532
069095 ZDOT = -1076
574660
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 20074
25836746
00016717 00000-0 10270-3 0 9034
2 25544 51
6417 98
1636 0005757 23
5809 336
5604 15
49230577 17299
Satellite: ISS
Catalog Number: 25544
Epoch time: 20074
25836746 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 98
1636 deg
Eccentricity:
0005757
Arg of perigee: 23
5809 deg
Mean anomaly: 336
5604 deg
Mean motion: 15
49230577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1729
Checksum: 327
Coasting Arc #5 (Orbit 1743)
---------------------------------------
Vector Time (GMT): 2020/075/05:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4045267
44 A = 6792009
01 meter
Y = 1500177
57 meter E =
0016889
Z = -5259467
65 I = 52
01207
XDOT = -1246
052440 Wp = 79
97579
YDOT = 7454
621579 meter/sec RA = 92
52205 deg
ZDOT = 1173
977305 TA = 201
21905
MA = 201
28918
Ha = 230
260 n
mi
Hp = 221
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13271874
82 X = 4053738
72
Y = 4921842
43 feet Y = 1545461
74 meter
Z = -17255471
30 Z = -5239796
93
XDOT = -4088
098558 XDOT = -1335
022089
YDOT = 24457
419879 feet/sec YDOT = 7440
189931 meter/sec
ZDOT = 3851
631577 ZDOT = 1167
708053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9463350
31 X = -2884429
17
Y = 10673215
43 feet Y = 3253196
06 meter
Z = -17165254
35 Z = -5231969
53
XDOT = -20496
167740 XDOT = -6247
231927
YDOT = -12057
411066 feet/sec YDOT = -3675
098893 meter/sec
ZDOT = 3822
486494 ZDOT = 1165
093884
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 20075
22594236
00016717 00000-0 10270-3 0 9048
2 25544 51
6421 93
3769 0005790 27
4958 332
6497 15
49262971 17440
Satellite: ISS
Catalog Number: 25544
Epoch time: 20075
22594236 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 93
3769 deg
Eccentricity:
0005790
Arg of perigee: 27
4958 deg
Mean anomaly: 332
6497 deg
Mean motion: 15
49262971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1744
Checksum: 332
Coasting Arc #6 (Orbit 1759)
---------------------------------------
Vector Time (GMT): 2020/076/05:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4139736
00 A = 6792131
13 meter
Y = -1272330
43 meter E =
0009795
Z = 5228115
23 I = 52
01267
XDOT = 685
153215 Wp = 41
10296
YDOT = -7525
451284 meter/sec RA = 87
59858 deg
ZDOT = -1280
361097 TA = 61
18343
MA = 61
08512
Ha = 230
462 n
mi
Hp = 221
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13581811
02 X = -4150595
73
Y = -4174312
44 feet Y = -1318684
42 meter
Z = 17152609
03 Z = 5207979
86
XDOT = 2247
878003 XDOT = 775
473318
YDOT = -24689
800801 feet/sec YDOT = -7517
284451 meter/sec
ZDOT = -4200
659767 ZDOT = -1276
813266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8685461
90 X = 2647328
79
Y = -11384780
02 feet Y = -3470080
95 meter
Z = 17060246
39 Z = 5199963
10
XDOT = 21518
708719 XDOT = 6558
902418
YDOT = 10104
696462 feet/sec YDOT = 3079
911482 meter/sec
ZDOT = -4183
982041 ZDOT = -1275
277726
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 20076
25802236
00016717 00000-0 10270-3 0 9055
2 25544 51
6421 88
2692 0005827 30
8953 329
2539 15
49249459 17605
Satellite: ISS
Catalog Number: 25544
Epoch time: 20076
25802236 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 88
2692 deg
Eccentricity:
0005827
Arg of perigee: 30
8953 deg
Mean anomaly: 329
2539 deg
Mean motion: 15
49249459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1760
Checksum: 324
Coasting Arc #7 (Orbit 1774)
---------------------------------------
Vector Time (GMT): 2020/077/05:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4241677
82 A = 6792152
21 meter
Y = 1003785
26 meter E =
0017075
Z = -5223150
36 I = 52
01112
XDOT = -107
617180 Wp = 82
27332
YDOT = 7524
906112 meter/sec RA = 82
67718 deg
ZDOT = 1364
785542 TA = 200
77768
MA = 200
84718
Ha = 230
365 n
mi
Hp = 221
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13916265
81 X = 4255508
72
Y = 3293258
72 feet Y = 1051295
86 meter
Z = -17136320
08 Z = -5202512
65
XDOT = -353
074737 XDOT = -198
384168
YDOT = 24688
012179 feet/sec YDOT = 7523
195200 meter/sec
ZDOT = 4477
642853 ZDOT = 1364
042057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7768474
77 X = -2367831
11
Y = 12140631
75 feet Y = 3700464
56 meter
Z = -17041635
30 Z = -5194290
44
XDOT = -22272
367983 XDOT = -6788
617761
YDOT = -7999
658088 feet/sec YDOT = -2438
295785 meter/sec
ZDOT = 4473
820494 ZDOT = 1363
620487
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 20077
22559558
00016717 00000-0 10270-3 0 9060
2 25544 51
6428 83
4827 0005795 34
4953 325
6572 15
49270671 17756
Satellite: ISS
Catalog Number: 25544
Epoch time: 20077
22559558 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 83
4827 deg
Eccentricity:
0005795
Arg of perigee: 34
4953 deg
Mean anomaly: 325
6572 deg
Mean motion: 15
49270671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1775
Checksum: 340
Coasting Arc #8 (Orbit 1790)
---------------------------------------
Vector Time (GMT): 2020/078/05:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4312036
61 A = 6792240
16 meter
Y = -764407
91 meter E =
0010413
Z = 5187240
63 I = 52
00662
XDOT = -452
165396 Wp = 44
84785
YDOT = -7508
133686 meter/sec RA = 77
75293 deg
ZDOT = -1473
318725 TA = 59
32094
MA = 59
21836
Ha = 230
551 n
mi
Hp = 220
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14147101
75 X = -4328364
56
Y = -2507899
98 feet Y = -812719
24 meter
Z = 17018505
99 Z = 5166255
14
XDOT = -1483
482269 XDOT = -361
017194
YDOT = -24632
984533 feet/sec YDOT = -7512
680543 meter/sec
ZDOT = -4833
722851 ZDOT = -1475
293428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6886097
82 X = 2098882
61
Y = -12738919
46 feet Y = -3882822
65 meter
Z = 16922209
80 Z = 5157889
55
XDOT = 22900
140645 XDOT = 6979
962869
YDOT = 5906
921720 feet/sec YDOT = 1800
429740 meter/sec
ZDOT = -4842
364837 ZDOT = -1475
952802
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 20078
25767087
00016717 00000-0 10270-3 0 9073
2 25544 51
6434 78
3746 0005892 37
1745 322
9812 15
49274697 17910
Satellite: ISS
Catalog Number: 25544
Epoch time: 20078
25767087 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 78
3746 deg
Eccentricity:
0005892
Arg of perigee: 37
1745 deg
Mean anomaly: 322
9812 deg
Mean motion: 15
49274697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1791
Checksum: 347
Coasting Arc #9 (Orbit 1805)
---------------------------------------
Vector Time (GMT): 2020/079/05:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4384752
56 A = 6792334
12 meter
Y = 482966
53 meter E =
0017280
Z = -5179343
61 I = 51
99837
XDOT = 1017
082829 Wp = 84
12951
YDOT = 7418
211240 meter/sec RA = 72
83070 deg
ZDOT = 1558
966504 TA = 200
82675
MA = 200
89724
Ha = 230
515 n
mi
Hp = 220
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14385671
13 X = 4404183
86
Y = 1584535
87 feet Y = 532108
31 meter
Z = -16992597
14 Z = -5157997
40
XDOT = 3336
885923 XDOT = 926
482175
YDOT = 24337
963385 feet/sec YDOT = 7429
078491 meter/sec
ZDOT = 5114
719501 ZDOT = 1563
686539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5856474
06 X = -1785053
29
Y = 13359636
89 feet Y = 4072017
32 meter
Z = -16894628
11 Z = -5149482
65
XDOT = -23234
998897 XDOT = -7082
027664
YDOT = -3716
397862 feet/sec YDOT = -1132
758068 meter/sec
ZDOT = 5135
957426 ZDOT = 1565
439823
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 20079
22524012
00016717 00000-0 10270-3 0 9081
2 25544 51
6432 73
5880 0005972 41
0302 319
1296 15
49275255 18068
Satellite: ISS
Catalog Number: 25544
Epoch time: 20079
22524012 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 73
5880 deg
Eccentricity:
0005972
Arg of perigee: 41
0302 deg
Mean anomaly: 319
1296 deg
Mean motion: 15
49275255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1806
Checksum: 293
Coasting Arc #10 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2020/079/17:22:53
274
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3721878
01 A = 6792702
78 meter
Y = -1985675
00 meter E =
0018187
Z = -5339464
28 I = 51
99030
XDOT = 2963
955264 Wp = 72
88371
YDOT = 7027
902145 meter/sec RA = 70
32766 deg
ZDOT = -543
889009 TA = 191
91539
MA = 191
95847
Ha = 230
655 n
mi
Hp = 221
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12210885
87 X = 3769741
40
Y = -6514681
75 feet Y = -1943787
04 meter
Z = -17517927
44 Z = -5321268
80
XDOT = 9724
262678 XDOT = 2887
788758
YDOT = 23057
421735 feet/sec YDOT = 7060
621290 meter/sec
ZDOT = -1784
412760 ZDOT = -529
676981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3701578
61 X = -1128241
16
Y = -13445031
37 feet Y = -4098045
56 meter
Z = -17434277
76 Z = -5313967
86
XDOT = 23634
609224 XDOT = 7203
828892
YDOT = -4261
426777 feet/sec YDOT = -1298
882882 meter/sec
ZDOT = -1719
581274 ZDOT = -524
128372
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 20079
74127953
00016717 00000-0 10270-3 0 9092
2 25544 51
6427 71
0371 0005069 32
9001 327
2464 15
48905567 18143
Satellite: ISS
Catalog Number: 25544
Epoch time: 20079
74127953 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 71
0371 deg
Eccentricity:
0005069
Arg of perigee: 32
9001 deg
Mean anomaly: 327
2464 deg
Mean motion: 15
48905567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 309
Coasting Arc #11 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2020/080/17:22:53
274
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3515498
32 A = 6792636
04 meter
Y = 2321201
51 meter E =
0006156
Z = 5323614
96 I = 51
97763
XDOT = -3585
748042 Wp = 61
62877
YDOT = -6749
585103 meter/sec RA = 65
40689 deg
ZDOT = 577
410731 TA = 22
89743
MA = 22
87000
Ha = 230
741 n
mi
Hp = 221
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11533787
13 X = -3567052
02
Y = 7615490
51 feet Y = 2281600
89 meter
Z = 17465928
34 Z = 5306412
94
XDOT = -11764
265229 XDOT = -3512
810373
YDOT = -22144
308082 feet/sec YDOT = -6789
275620 meter/sec
ZDOT = 1894
392163 ZDOT = 560
170584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5145879
10 X = 1568463
95
Y = 12934492
79 feet Y = 3942433
40 meter
Z = 17386817
38 Z = 5299501
94
XDOT = -23101
399792 XDOT = -7041
306657
YDOT = 6760
424269 feet/sec YDOT = 2060
577317 meter/sec
ZDOT = 1815
653279 ZDOT = 553
411119
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 20080
77359311
00016717 00000-0 10270-3 0 9104
2 25544 51
6424 65
9318 0004892 35
3310 324
8163 15
48925309 18309
Satellite: ISS
Catalog Number: 25544
Epoch time: 20080
77359311 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 65
9318 deg
Eccentricity:
0004892
Arg of perigee: 35
3310 deg
Mean anomaly: 324
8163 deg
Mean motion: 15
48925309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 297
Coasting Arc #12 (Orbit 1834)
---------------------------------------
Vector Time (GMT): 2020/081/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2855423
54 A = 6793358
04 meter
Y = 3351703
92 meter E =
0006867
Z = 5167165
12 I = 51
97309
XDOT = -4357
929099 Wp = 83
01547
YDOT = -6111
129233 meter/sec RA = 63
82977 deg
ZDOT = 1554
823109 TA = 352
05701
MA = 352
06788
Ha = 230
709 n
mi
Hp = 221
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9368187
47 X = -2917789
77
Y = 10996403
95 feet Y = 3319424
29 meter
Z = 16952641
48 Z = 5153143
07
XDOT = -14297
667647 XDOT = -4296
821072
YDOT = -20049
636592 feet/sec YDOT = -6159
520882 meter/sec
ZDOT = 5101
125687 ZDOT = 1533
803316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6457409
20 X = 1968218
32
Y = -13006574
66 feet Y = -3964403
96 meter
Z = 16888065
95 Z = 5147482
50
XDOT = 17910
563441 XDOT = 5459
139737
YDOT = 15394
808625 feet/sec YDOT = 4692
337669 meter/sec
ZDOT = 5005
000199 ZDOT = 1525
524061
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 20081
09619149
00016717 00000-0 10270-3 0 9119
2 25544 51
6402 64
3308 0004590 39
7669 320
3817 15
48907608 18351
Satellite: ISS
Catalog Number: 25544
Epoch time: 20081
09619149 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 64
3308 deg
Eccentricity:
0004590
Arg of perigee: 39
7669 deg
Mean anomaly: 320
3817 deg
Mean motion: 15
48907608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1835
Checksum: 314
Coasting Arc #13 (Orbit 1849)
---------------------------------------
Vector Time (GMT): 2020/082/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2539816
86 A = 6793395
12 meter
Y = -3622886
70 meter E =
0017672
Z = -5170761
39 I = 51
95865
XDOT = 4870
928042 Wp = 69
36286
YDOT = 5677
538247 meter/sec RA = 58
90794 deg
ZDOT = -1583
746459 TA = 185
38015
MA = 185
39916
Ha = 230
673 n
mi
Hp = 221
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8332732
48 X = 2605256
51
Y = -11886111
21 feet Y = -3594119
29 meter
Z = -16964440
24 Z = -5158264
83
XDOT = 15980
735045 XDOT = 4814
770937
YDOT = 18627
093986 feet/sec YDOT = 5731
694273 meter/sec
ZDOT = -5196
018565 ZDOT = -1560
222729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4998750
05 X = -1523619
01
Y = 13699535
38 feet Y = 4175618
39 meter
Z = -16906848
65 Z = -5153207
47
XDOT = -19377
069731 XDOT = -5906
130854
YDOT = -13356
849758 feet/sec YDOT = -4071
167806 meter/sec
ZDOT = -5088
383720 ZDOT = -1550
939358
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 20082
06398353
00016717 00000-0 10270-3 0 9129
2 25544 51
6415 59
5449 0004711 44
0967 316
0558 15
48910536 18507
Satellite: ISS
Catalog Number: 25544
Epoch time: 20082
06398353 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 59
5449 deg
Eccentricity:
0004711
Arg of perigee: 44
0967 deg
Mean anomaly: 316
0558 deg
Mean motion: 15
48910536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1850
Checksum: 310
Coasting Arc #14 (Orbit 1865)
---------------------------------------
Vector Time (GMT): 2020/083/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2189774
73 A = 6793347
63 meter
Y = 3843856
61 meter E =
0007400
Z = 5149030
02 I = 51
94072
XDOT = -5367
372004 Wp = 86
72238
YDOT = -5227
966067 meter/sec RA = 53
98359 deg
ZDOT = 1618
562685 TA = 347
71330
MA = 347
73133
Ha = 230
756 n
mi
Hp = 221
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7184300
28 X = -2257605
87
Y = 12611078
13 feet Y = 3818990
30 meter
Z = 16893143
12 Z = 5138227
91
XDOT = -17609
488203 XDOT = -5316
374392
YDOT = -17152
119642 feet/sec YDOT = -5287
702513 meter/sec
ZDOT = 5310
245029 ZDOT = 1592
614848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3455920
49 X = 1053364
56
Y = -14155958
09 feet Y = -4314736
03 meter
Z = 16843313
53 Z = 5133841
97
XDOT = 20725
521093 XDOT = 6317
138829
YDOT = 11242
998910 feet/sec YDOT = 3426
866068 meter/sec
ZDOT = 5191
468271 ZDOT = 1582
359529
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 20083
09629145
00016717 00000-0 10270-3 0 9130
2 25544 51
6418 54
4383 0004652 46
8991 313
2548 15
48931002 18668
Satellite: ISS
Catalog Number: 25544
Epoch time: 20083
09629145 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 54
4383 deg
Eccentricity:
0004652
Arg of perigee: 46
8991 deg
Mean anomaly: 313
2548 deg
Mean motion: 15
48931002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1866
Checksum: 312
Coasting Arc #15 (Orbit 1880)
---------------------------------------
Vector Time (GMT): 2020/084/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1831436
84 A = 6793462
47 meter
Y = -4050522
74 meter E =
0017837
Z = -5153128
14 I = 51
92013
XDOT = 5792
913234 Wp = 70
71648
YDOT = 4712
202629 meter/sec RA = 49
05981 deg
ZDOT = -1644
044753 TA = 183
42546
MA = 183
43769
Ha = 230
762 n
mi
Hp = 221
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6008651
07 X = 1901625
63
Y = -13289116
59 feet Y = -4029650
45 meter
Z = -16906588
40 Z = -5144060
87
XDOT = 19005
620848 XDOT = 5747
775222
YDOT = 15459
982379 feet/sec YDOT = 4776
730535 meter/sec
ZDOT = -5393
847615 ZDOT = -1616
015440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1887795
02 X = -575399
92
Y = 14510519
13 feet Y = 4422806
23 meter
Z = -16864705
84 Z = -5140362
34
XDOT = -21723
567678 XDOT = -6621
343428
YDOT = -8950
096472 feet/sec YDOT = -2727
989405 meter/sec
ZDOT = -5265
499509 ZDOT = -1604
924250
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 20084
06408101
00016717 00000-0 10270-3 0 9146
2 25544 51
6418 49
6529 0004724 51
3042 308
8530 15
48906699 18816
Satellite: ISS
Catalog Number: 25544
Epoch time: 20084
06408101 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 49
6529 deg
Eccentricity:
0004724
Arg of perigee: 51
3042 deg
Mean anomaly: 308
8530 deg
Mean motion: 15
48906699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1881
Checksum: 306
Coasting Arc #16 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2020/085/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1445325
80 A = 6793376
74 meter
Y = 4203301
53 meter E =
0007838
Z = 5130710
86 I = 51
89832
XDOT = -6200
860743 Wp = 91
09549
YDOT = -4182
980609 meter/sec RA = 44
13301 deg
ZDOT = 1677
735291 TA = 342
74274
MA = 342
76937
Ha = 230
768 n
mi
Hp = 221
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4741882
54 X = -1517142
92
Y = 13790359
36 feet Y = 4186737
89 meter
Z = 16833040
87 Z = 5123515
16
XDOT = -20344
031308 XDOT = -6161
774011
YDOT = -13723
689661 feet/sec YDOT = -4252
104309 meter/sec
ZDOT = 5504
380877 ZDOT = 1647
709444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 277366
82 X = 84541
41
Y = -14618574
31 feet Y = -4455741
45 meter
Z = 16799734
49 Z = 5120559
07
XDOT = 22594
469105 XDOT = 6886
794183
YDOT = 6605
211788 feet/sec YDOT = 2013
268553 meter/sec
ZDOT = 5366
851856 ZDOT = 1635
816446
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 20085
09638581
00016717 00000-0 10270-3 0 9158
2 25544 51
6428 44
5467 0004586 54
5155 305
6423 15
48940548 18972
Satellite: ISS
Catalog Number: 25544
Epoch time: 20085
09638581 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 44
5467 deg
Eccentricity:
0004586
Arg of perigee: 54
5155 deg
Mean anomaly: 305
6423 deg
Mean motion: 15
48940548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 334
Coasting Arc #17 (Orbit 1903)
---------------------------------------
Vector Time (GMT): 2020/085/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 577565
06 A = 6794372
46 meter
Y = -4662526
12 meter E =
0016828
Z = -4924049
77 I = 51
88889
XDOT = 6479
975353 Wp = 66
52295
YDOT = 3299
814629 meter/sec RA = 41
76311 deg
ZDOT = -2364
385209 TA = 180
33578
MA = 180
33692
Ha = 230
869 n
mi
Hp = 221
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1894898
50 X = 653578
07
Y = -15297001
71 feet Y = -4655642
90 meter
Z = -16155018
92 Z = -4921059
06
XDOT = 21259
761657 XDOT = 6454
079065
YDOT = 10826
163482 feet/sec YDOT = 3372
133271 meter/sec
ZDOT = -7757
169321 ZDOT = -2332
971326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1363825
92 X = -415694
14
Y = -15368225
25 feet Y = -4684235
06 meter
Z = -16140977
96 Z = -4919770
08
XDOT = 22033
003534 XDOT = 6715
659477
YDOT = 6041
111008 feet/sec YDOT = 1841
330635 meter/sec
ZDOT = -7613
219136 ZDOT = -2320
509193
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 20085
54802033
00016717 00000-0 10270-3 0 9164
2 25544 51
6421 42
3167 0005046 51
8450 308
3154 15
48913423 19040
Satellite: ISS
Catalog Number: 25544
Epoch time: 20085
54802033 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 42
3167 deg
Eccentricity:
0005046
Arg of perigee: 51
8450 deg
Mean anomaly: 308
3154 deg
Mean motion: 15
48913423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1904
Checksum: 278
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