[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 1st 2021
- spaceflight nasa gov will be taken offline in the next 30 days *
- *
- Current information about the International Space Station can be *
- found at www nasa gov/station *
- *
- Predicted ISS and visiting vehicle sightings opportunities can be *
- found at spotthestation nasa gov *
- *
- Updated ISS trajectory information will be made available as a CCSDS *
- Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
- system *
- Included in the OEM are a sequence of events with ISS maneuver *
- details (in the comment section), predicted post-maneuver state *
- vectors, predicted coasting state vectors at 4-minute intervals, *
- and ISS ballistic details *
- *
- OEMs will be provided in xml and txt formats *
- Links to the OEMs and more details to follow *
- *
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 497 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
029/19:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 223
3
036/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 223
2
040/05:21:30
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
9
040/13:27:30
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
9
Coasting Arc #1 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2021/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3101003
46 A = 6803654
06 meter
Y = -5871793
88 meter E =
0008972
Z = -1459469
51 I = 51
35236
XDOT = 4919
369861 Wp = 22
03527
YDOT = 1173
049836 meter/sec RA = 307
96191 deg
ZDOT = 5752
648510 TA = 322
01118
MA = 322
07443
Ha = 228
700 n
mi
Hp = 223
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10173895
87 X = 3173522
20
Y = -19264415
63 feet Y = -5836710
68 meter
Z = -4788285
81 Z = -1444230
73
XDOT = 16139
664899 XDOT = 4877
944750
YDOT = 3848
588700 feet/sec YDOT = 1227
829880 meter/sec
ZDOT = 18873
518735 ZDOT = 5776
443494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21461264
33 X = 6541393
37
Y = -3835917
33 feet Y = -1169187
60 meter
Z = -4717352
98 Z = -1437849
19
XDOT = 6556
109113 XDOT = 1998
302058
YDOT = 13414
802355 feet/sec YDOT = 4088
831758 meter/sec
ZDOT = 18983
879791 ZDOT = 5786
286560
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 21029
50280694
00016717 00000-0 10270-3 0 9005
2 25544 51
6449 308
6780 0002387 312
3847 47
7101 15
48914549 27099
Satellite: ISS
Catalog Number: 25544
Epoch time: 21029
50280694 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 308
6780 deg
Eccentricity:
0002387
Arg of perigee: 312
3847 deg
Mean anomaly: 47
7101 deg
Mean motion: 15
48914549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2709
Checksum: 318
Coasting Arc #2 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2021/029/19:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2817192
76 A = 6792792
94 meter
Y = -3271488
77 meter E =
0012798
Z = -5255499
96 I = 51
30797
XDOT = 5040
323019 Wp = 91
78632
YDOT = -5693
358075 meter/sec RA = 306
42057 deg
ZDOT = 843
600763 TA = 186
32716
MA = 186
34333
Ha = 228
686 n
mi
Hp = 223
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9242758
40 X = -2754873
28
Y = -10733230
86 feet Y = -3302643
99 meter
Z = -17242453
94 Z = -5269033
07
XDOT = 16536
492843 XDOT = 5099
515696
YDOT = -18678
996308 feet/sec YDOT = -5636
662618 meter/sec
ZDOT = 2767
719039 ZDOT = 868
227361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13847611
82 X = -4220752
08
Y = 2590252
45 feet Y = 789508
95 meter
Z = -17305123
07 Z = -5274601
51
XDOT = -7823
888435 XDOT = -2384
721195
YDOT = -22601
848565 feet/sec YDOT = -6889
043443 meter/sec
ZDOT = 2882
196949 ZDOT = 878
493630
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 21029
82539880
00016717 00000-0 10270-3 0 9015
2 25544 51
6430 307
0786 0001976 308
7596 51
3377 15
48929001 27142
Satellite: ISS
Catalog Number: 25544
Epoch time: 21029
82539880 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 307
0786 deg
Eccentricity:
0001976
Arg of perigee: 308
7596 deg
Mean anomaly: 51
3377 deg
Mean motion: 15
48929001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 321
Coasting Arc #3 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2021/030/19:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3093988
43 A = 6792898
81 meter
Y = 3003068
15 meter E =
0003394
Z = 5248064
19 I = 51
28756
XDOT = -4527
369525 Wp = 26
83884
YDOT = 6123
938650 meter/sec RA = 301
45192 deg
ZDOT = -831
975551 TA = 71
17971
MA = 71
14290
Ha = 228
731 n
mi
Hp = 223
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10150880
67 X = 3034686
02
Y = 9852585
81 feet Y = 3037335
70 meter
Z = 17218058
37 Z = 5262949
08
XDOT = -14853
574556 XDOT = -4591
471670
YDOT = 20091
662237 feet/sec YDOT = 6072
951936 meter/sec
ZDOT = -2729
578580 ZDOT = -854
122593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13466508
97 X = 4104591
93
Y = -4048149
74 feet Y = -1233876
04 meter
Z = 17287017
65 Z = 5269082
98
XDOT = 10170
861825 XDOT = 3100
078684
YDOT = 21693
819699 feet/sec YDOT = 6612
276244 meter/sec
ZDOT = -2832
544761 ZDOT = -863
359643
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 21030
85769251
00016717 00000-0 10270-3 0 9028
2 25544 51
6418 301
9725 0001909 315
0189 45
0806 15
48887255 27308
Satellite: ISS
Catalog Number: 25544
Epoch time: 21030
85769251 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 301
9725 deg
Eccentricity:
0001909
Arg of perigee: 315
0189 deg
Mean anomaly: 45
0806 deg
Mean motion: 15
48887255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 310
Coasting Arc #4 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2021/031/19:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3360067
21 A = 6792744
22 meter
Y = -2709214
49 meter E =
0013042
Z = -5256521
04 I = 51
27107
XDOT = 3964
053736 Wp = 90
83195
YDOT = -6492
492352 meter/sec RA = 296
48405 deg
ZDOT = 813
911927 TA = 186
99707
MA = 187
01530
Ha = 228
762 n
mi
Hp = 223
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11023842
56 X = -3303989
83
Y = -8888498
99 feet Y = -2746475
67 meter
Z = -17245803
93 Z = -5272706
22
XDOT = 13005
425642 XDOT = 4032
406754
YDOT = -21300
827928 feet/sec YDOT = -6447
781255 meter/sec
ZDOT = 2670
314721 ZDOT = 833
333213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12949074
32 X = -3946877
85
Y = 5500836
53 feet Y = 1676654
97 meter
Z = -17320812
45 Z = -5279383
64
XDOT = -12384
759330 XDOT = -3774
874644
YDOT = -20477
620195 feet/sec YDOT = -6241
578635 meter/sec
ZDOT = 2760
622755 ZDOT = 841
437816
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 21031
82546306
00016717 00000-0 10270-3 0 9031
2 25544 51
6420 297
1875 0001928 316
3532 43
7465 15
48938588 27458
Satellite: ISS
Catalog Number: 25544
Epoch time: 21031
82546306 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 297
1875 deg
Eccentricity:
0001928
Arg of perigee: 316
3532 deg
Mean anomaly: 43
7465 deg
Mean motion: 15
48938588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 323
Coasting Arc #5 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2021/032/19:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3581565
94 A = 6792837
77 meter
Y = 2398601
77 meter E =
0003527
Z = 5248897
67 I = 51
25694
XDOT = -3385
207420 Wp = 27
15278
YDOT = 6825
275632 meter/sec RA = 291
51236 deg
ZDOT = -805
781185 TA = 70
61621
MA = 70
57809
Ha = 228
751 n
mi
Hp = 223
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11750544
43 X = 3528982
37
Y = 7869428
36 feet Y = 2438359
50 meter
Z = 17220792
88 Z = 5266167
31
XDOT = -11106
323558 XDOT = -3457
364218
YDOT = 22392
636588 feet/sec YDOT = 6787
016333 meter/sec
ZDOT = -2643
639057 ZDOT = -822
400148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12270898
03 X = 3740169
72
Y = -6831153
91 feet Y = -2082135
71 meter
Z = 17300846
87 Z = 5273298
13
XDOT = 14485
310684 XDOT = 4415
122696
YDOT = 19101
748816 feet/sec YDOT = 5822
213039 meter/sec
ZDOT = -2720
932917 ZDOT = -829
340353
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 21032
85775124
00016717 00000-0 10270-3 0 9048
2 25544 51
6419 292
0807 0001963 320
8936 39
2072 15
48901557 27610
Satellite: ISS
Catalog Number: 25544
Epoch time: 21032
85775124 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 292
0807 deg
Eccentricity:
0001963
Arg of perigee: 320
8936 deg
Mean anomaly: 39
2072 deg
Mean motion: 15
48901557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 312
Coasting Arc #6 (Orbit 2775)
---------------------------------------
Vector Time (GMT): 2021/033/19:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3788642
08 A = 6792678
84 meter
Y = -2065792
53 meter E =
0013211
Z = -5257372
29 I = 51
24663
XDOT = 2768
248152 Wp = 89
55690
YDOT = -7087
819328 meter/sec RA = 286
54153 deg
ZDOT = 791
976412 TA = 188
06079
MA = 188
08204
Ha = 228
815 n
mi
Hp = 223
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12429928
09 X = -3739723
40
Y = -6777534
55 feet Y = -2107886
42 meter
Z = -17248596
75 Z = -5275656
80
XDOT = 9082
178975 XDOT = 2843
453681
YDOT = -23254
000419 feet/sec YDOT = -7056
442267 meter/sec
ZDOT = 2598
347809 ZDOT = 805
605975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11464641
59 X = -3494422
76
Y = 8128246
84 feet Y = 2477489
64 meter
Z = -17333371
66 Z = -5283211
68
XDOT = -16389
485075 XDOT = -4995
515051
YDOT = -17453
480197 feet/sec YDOT = -5319
820764 meter/sec
ZDOT = 2661
759736 ZDOT = 811
304368
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 21033
82551504
00016717 00000-0 10270-3 0 9051
2 25544 51
6429 287
2949 0002035 324
1429 35
9584 15
48955185 27762
Satellite: ISS
Catalog Number: 25544
Epoch time: 21033
82551504 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 287
2949 deg
Eccentricity:
0002035
Arg of perigee: 324
1429 deg
Mean anomaly: 35
9584 deg
Mean motion: 15
48955185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2776
Checksum: 327
Coasting Arc #7 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2021/034/19:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3948964
12 A = 6792748
76 meter
Y = 1725881
78 meter E =
0003844
Z = 5249371
14 I = 51
23816
XDOT = -2143
217731 Wp = 28
30755
YDOT = 7313
078317 meter/sec RA = 281
56840 deg
ZDOT = -788
534138 TA = 69
29793
MA = 69
25672
Ha = 228
820 n
mi
Hp = 223
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12955919
02 X = 3903873
28
Y = 5662341
80 feet Y = 1769789
84 meter
Z = 17222346
25 Z = 5268443
81
XDOT = -7031
554235 XDOT = -2221
005335
YDOT = 23993
039097 feet/sec YDOT = 7288
676370 meter/sec
ZDOT = -2587
054258 ZDOT = -799
133825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10532167
37 X = 3210204
62
Y = -9270230
94 feet Y = -2825566
39 meter
Z = 17310789
45 Z = 5276328
62
XDOT = 18150
400562 XDOT = 5532
242091
YDOT = 15676
365157 feet/sec YDOT = 4778
156100 meter/sec
ZDOT = -2636
398224 ZDOT = -803
574179
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 21034
85779578
00016717 00000-0 10270-3 0 9069
2 25544 51
6430 282
1883 0002074 331
1668 28
9367 15
48927056 27926
Satellite: ISS
Catalog Number: 25544
Epoch time: 21034
85779578 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 282
1883 deg
Eccentricity:
0002074
Arg of perigee: 331
1668 deg
Mean anomaly: 28
9367 deg
Mean motion: 15
48927056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 339
Coasting Arc #8 (Orbit 2806)
---------------------------------------
Vector Time (GMT): 2021/035/19:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4093106
92 A = 6792637
90 meter
Y = -1364428
62 meter E =
0013497
Z = -5258128
16 I = 51
23236
XDOT = 1491
616280 Wp = 88
71026
YDOT = -7462
945663 meter/sec RA = 276
59685 deg
ZDOT = 777
468814 TA = 188
76738
MA = 188
79098
Ha = 228
913 n
mi
Hp = 222
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13428828
47 X = -4052004
68
Y = -4476471
84 feet Y = -1409970
78 meter
Z = -17251076
63 Z = -5277910
75
XDOT = 4893
754200 XDOT = 1571
181918
YDOT = -24484
729865 feet/sec YDOT = -7445
820469 meter/sec
ZDOT = 2550
750703 ZDOT = 784
907497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9477775
46 X = -2888825
96
Y = 10361951
70 feet Y = 3158322
88 meter
Z = -17342825
85 Z = -5286093
32
XDOT = -19665
048695 XDOT = -5993
906842
YDOT = -13670
960487 feet/sec YDOT = -4166
908756 meter/sec
ZDOT = 2585
418425 ZDOT = 788
035536
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 21035
82555546
00016717 00000-0 10270-3 0 9075
2 25544 51
6428 277
4029 0002052 332
9504 27
1539 15
48965028 28076
Satellite: ISS
Catalog Number: 25544
Epoch time: 21035
82555546 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 277
4029 deg
Eccentricity:
0002052
Arg of perigee: 332
9504 deg
Mean anomaly: 27
1539 deg
Mean motion: 15
48965028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2807
Checksum: 315
Coasting Arc #9 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2021/036/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4188030
93 A = 6793351
01 meter
Y = -1583132
37 meter E =
0003067
Z = 5106603
41 I = 51
23304
XDOT = 886
567671 Wp = 96
32489
YDOT = 7444
917543 meter/sec RA = 272
95119 deg
ZDOT = 1579
802775 TA = 338
33502
MA = 338
34799
Ha = 228
917 n
mi
Hp = 223
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13740258
97 X = 4180618
20
Y = -5194003
83 feet Y = -1536340
41 meter
Z = 16753948
20 Z = 5126928
83
XDOT = 2908
686584 XDOT = 795
576789
YDOT = 24425
582491 feet/sec YDOT = 7454
322963 meter/sec
ZDOT = 5183
079970 ZDOT = 1583
888571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14483133
11 X = 4414458
97
Y = 1685690
88 feet Y = 513798
58 meter
Z = 16848278
08 Z = 5135355
16
XDOT = -8608
864382 XDOT = -2623
981864
YDOT = 21935
830384 feet/sec YDOT = 6686
041101 meter/sec
ZDOT = 5201
890098 ZDOT = 1585
536102
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 21036
59976195
00016717 00000-0 10270-3 0 9088
2 25544 51
6436 273
5777 0002651 338
8813 21
2227 15
48931948 28191
Satellite: ISS
Catalog Number: 25544
Epoch time: 21036
59976195 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 273
5777 deg
Eccentricity:
0002651
Arg of perigee: 338
8813 deg
Mean anomaly: 21
2227 deg
Mean motion: 15
48931948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2819
Checksum: 343
Coasting Arc #10 (Orbit 2833)
---------------------------------------
Vector Time (GMT): 2021/037/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4040496
77 A = 6793265
45 meter
Y = 1948373
06 meter E =
0013389
Z = -5113611
97 I = 51
23191
XDOT = -1529
444807 Wp = 66
26052
YDOT = -7326
756556 meter/sec RA = 267
97683 deg
ZDOT = -1581
152438 TA = 188
35580
MA = 188
37812
Ha = 229
039 n
mi
Hp = 222
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13256223
00 X = -4037145
26
Y = 6392300
05 feet Y = 1903208
33 meter
Z = -16776942
14 Z = -5133230
49
XDOT = -5017
863540 XDOT = -1439
720926
YDOT = -24037
915209 feet/sec YDOT = -7343
358145 meter/sec
ZDOT = -5187
508000 ZDOT = -1588
364217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14611755
91 X = -4453663
20
Y = -147905
87 feet Y = -45081
71 meter
Z = -16868000
74 Z = -5141366
63
XDOT = 6263
929907 XDOT = 1909
245836
YDOT = -22668
042483 feet/sec YDOT = -6909
219349 meter/sec
ZDOT = -5220
841086 ZDOT = -1591
312363
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 21037
56751645
00016717 00000-0 10270-3 0 9098
2 25544 51
6429 268
7900 0002747 339
5835 20
5205 15
48967863 28345
Satellite: ISS
Catalog Number: 25544
Epoch time: 21037
56751645 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 268
7900 deg
Eccentricity:
0002747
Arg of perigee: 339
5835 deg
Mean anomaly: 20
5205 deg
Mean motion: 15
48967863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2834
Checksum: 337
Coasting Arc #11 (Orbit 2849)
---------------------------------------
Vector Time (GMT): 2021/038/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3849726
85 A = 6793359
40 meter
Y = -2288107
08 meter E =
0003399
Z = 5105305
83 I = 51
23412
XDOT = 2163
087390 Wp = 93
06347
YDOT = 7177
905502 meter/sec RA = 263
00362 deg
ZDOT = 1584
807073 TA = 341
54781
MA = 341
56014
Ha = 229
059 n
mi
Hp = 223
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12630337
43 X = 3850228
99
Y = -7506912
99 feet Y = -2245054
18 meter
Z = 16749691
04 Z = 5124006
92
XDOT = 7096
743405 XDOT = 2074
963197
YDOT = 23549
558735 feet/sec YDOT = 7201
601869 meter/sec
ZDOT = 5199
498270 ZDOT = 1595
100674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14527979
54 X = 4428128
16
Y = -1378907
35 feet Y = -420290
96 meter
Z = 16836500
26 Z = 5131765
28
XDOT = -3879
861346 XDOT = -1182
581738
YDOT = 23233
903657 feet/sec YDOT = 7081
693835 meter/sec
ZDOT = 5247
154119 ZDOT = 1599
332575
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 21038
59978699
00016717 00000-0 10270-3 0 9104
2 25544 51
6427 263
6842 0002726 346
5054 13
6022 15
48934036 28504
Satellite: ISS
Catalog Number: 25544
Epoch time: 21038
59978699 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 263
6842 deg
Eccentricity:
0002726
Arg of perigee: 346
5054 deg
Mean anomaly: 13
6022 deg
Mean motion: 15
48934036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2850
Checksum: 322
Coasting Arc #12 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2021/039/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3642093
16 A = 6793283
35 meter
Y = 2619083
90 meter E =
0013784
Z = -5113742
70 I = 51
23724
XDOT = -2773
129630 Wp = 66
74353
YDOT = -6951
187272 meter/sec RA = 258
03039 deg
ZDOT = -1583
171590 TA = 187
85355
MA = 187
87515
Ha = 229
190 n
mi
Hp = 222
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11949124
54 X = -3646270
96
Y = 8592794
94 feet Y = 2578332
34 meter
Z = -16777371
05 Z = -5131444
03
XDOT = -9098
194324 XDOT = -2687
503314
YDOT = -22805
732521 feet/sec YDOT = -6981
719542 meter/sec
ZDOT = -5194
132513 ZDOT = -1596
434432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14333419
36 X = -4368826
22
Y = 2899424
14 feet Y = 883744
48 meter
Z = -16859546
57 Z = -5138789
80
XDOT = 1442
738587 XDOT = 439
746721
YDOT = -23464
384412 feet/sec YDOT = -7151
944369 meter/sec
ZDOT = -5255
594628 ZDOT = -1601
905243
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 21039
56753644
00016717 00000-0 10270-3 0 9114
2 25544 51
6404 258
8973 0002686 348
4863 11
6225 15
48965973 28657
Satellite: ISS
Catalog Number: 25544
Epoch time: 21039
56753644 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 258
8973 deg
Eccentricity:
0002686
Arg of perigee: 348
4863 deg
Mean anomaly: 11
6225 deg
Mean motion: 15
48965973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 345
Coasting Arc #13 (Orbit 2875)
---------------------------------------
Vector Time (GMT): 2021/040/05:21:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2598941
35 A = 6795479
65 meter
Y = -4324251
47 meter E =
0007557
Z = 4546362
19 I = 51
25101
XDOT = 4109
412729 Wp = 96
48389
YDOT = 5696
676887 meter/sec RA = 254
68639 deg
ZDOT = 3063
964424 TA = 322
64885
MA = 322
70137
Ha = 229
048 n
mi
Hp = 222
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8526710
47 X = 2625020
39
Y = -14187176
74 feet Y = -4295042
66 meter
Z = 14915886
44 Z = 4559049
53
XDOT = 13482
325228 XDOT = 4030
522832
YDOT = 18689
884800 feet/sec YDOT = 5742
190037 meter/sec
ZDOT = 10052
376718 ZDOT = 3083
734393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2379243
61 X = 725193
45
Y = 16326625
86 feet Y = 4976355
56 meter
Z = 14974809
89 Z = 4564322
06
XDOT = -20994
639684 XDOT = -6399
166176
YDOT = -6260
377594 feet/sec YDOT = -1908
163091 meter/sec
ZDOT = 10144
068638 ZDOT = 3091
912121
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 21040
27721885
00016717 00000-0 10270-3 0 9127
2 25544 51
6412 255
3884 0002617 350
3071 9
8028 15
49002996 28766
Satellite: ISS
Catalog Number: 25544
Epoch time: 21040
27721885 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 255
3884 deg
Eccentricity:
0002617
Arg of perigee: 350
3071 deg
Mean anomaly: 9
8028 deg
Mean motion: 15
49002996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2876
Checksum: 307
Coasting Arc #14 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2021/040/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4053793
12 A = 6799837
75 meter
Y = 4398937
03 meter E =
0012253
Z = 3225007
58 I = 51
26815
XDOT = -2266
519030 Wp = 80
50025
YDOT = 5575
882233 meter/sec RA = 252
95884 deg
ZDOT = -4739
104932 TA = 62
03066
MA = 61
90670
Ha = 229
083 n
mi
Hp = 222
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13299846
19 X = 3988636
87
Y = 14432208
12 feet Y = 4443905
01 meter
Z = 10580733
52 Z = 3244540
61
XDOT = -7436
086055 XDOT = -2305
682718
YDOT = 18293
576879 feet/sec YDOT = 5550
317630 meter/sec
ZDOT = -15548
244527 ZDOT = -4750
209274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7752613
44 X = 2362996
58
Y = 17976256
62 feet Y = 5479163
02 meter
Z = 10671346
89 Z = 3252626
53
XDOT = -11619
732928 XDOT = -3541
694597
YDOT = 14305
568248 feet/sec YDOT = 4360
337202 meter/sec
ZDOT = -15599
829529 ZDOT = -4754
828040
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 21040
59980000
00016717 00000-0 10270-3 0 9139
2 25544 51
6407 253
7907 0002753 347
3445 12
7635 15
48994904 28811
Satellite: ISS
Catalog Number: 25544
Epoch time: 21040
59980000 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 253
7907 deg
Eccentricity:
0002753
Arg of perigee: 347
3445 deg
Mean anomaly: 12
7635 deg
Mean motion: 15
48994904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 314
Coasting Arc #15 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2021/041/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4426422
76 A = 6799843
78 meter
Y = -4019180
55 meter E =
0005376
Z = -3239263
74 I = 51
27817
XDOT = 1766
807949 Wp = 54
68786
YDOT = -5753
077850 meter/sec RA = 247
98585 deg
ZDOT = 4732
552861 TA = 267
68131
MA = 267
74287
Ha = 229
207 n
mi
Hp = 222
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14522384
37 X = -4365416
17
Y = -13186287
89 feet Y = -4068338
80 meter
Z = -10627505
70 Z = -3260616
71
XDOT = 5796
614006 XDOT = 1808
022125
YDOT = -18874
927331 feet/sec YDOT = -5733
089809 meter/sec
ZDOT = 15526
748233 ZDOT = 4741
234955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9610710
43 X = -2929344
54
Y = -17038080
35 feet Y = -5193206
89 meter
Z = -10726592
03 Z = -3269465
25
XDOT = 10054
523149 XDOT = 3064
618656
YDOT = -15454
309227 feet/sec YDOT = -4710
473452 meter/sec
ZDOT = 15567
077394 ZDOT = 4744
845190
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 21041
56754630
00016717 00000-0 10270-3 0 9146
2 25544 51
6397 249
0031 0002557 355
2879 4
8247 15
48975961 28965
Satellite: ISS
Catalog Number: 25544
Epoch time: 21041
56754630 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 249
0031 deg
Eccentricity:
0002557
Arg of perigee: 355
2879 deg
Mean anomaly: 4
8247 deg
Mean motion: 15
48975961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 335
Coasting Arc #16 (Orbit 2911)
---------------------------------------
Vector Time (GMT): 2021/042/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4749727
42 A = 6799854
37 meter
Y = 3640174
75 meter E =
0012711
Z = 3220425
91 I = 51
29200
XDOT = -1274
715041 Wp = 81
05622
YDOT = 5877
535297 meter/sec RA = 243
01435 deg
ZDOT = -4745
508962 TA = 61
55041
MA = 61
42241
Ha = 229
231 n
mi
Hp = 222
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15583095
22 X = 4693026
48
Y = 11942830
54 feet Y = 3692972
59 meter
Z = 10565701
79 Z = 3243359
64
XDOT = -4182
135960 XDOT = -1317
294599
YDOT = 19283
252287 feet/sec YDOT = 5863
042436 meter/sec
ZDOT = -15569
255125 ZDOT = -4751
804210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11283770
86 X = 3439293
36
Y = 15996245
01 feet Y = 4875655
48 meter
Z = 10672149
41 Z = 3252871
14
XDOT = -8429
205596 XDOT = -2569
221866
YDOT = 16391
878891 feet/sec YDOT = 4996
244686 meter/sec
ZDOT = -15598
488677 ZDOT = -4754
419349
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 21042
59980278
00016717 00000-0 10270-3 0 9150
2 25544 51
6394 243
8967 0002660 357
1115 3
0019 15
48988983 29126
Satellite: ISS
Catalog Number: 25544
Epoch time: 21042
59980278 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 243
8967 deg
Eccentricity:
0002660
Arg of perigee: 357
1115 deg
Mean anomaly: 3
0019 deg
Mean motion: 15
48988983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2912
Checksum: 330
Coasting Arc #17 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2021/043/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5051532
41 A = 6799824
62 meter
Y = -3204322
08 meter E =
0005763
Z = -3233792
37 I = 51
30786
XDOT = 754
455909 Wp = 58
37409
YDOT = -5964
142641 meter/sec RA = 238
04374 deg
ZDOT = 4740
478142 TA = 264
08946
MA = 264
15516
Ha = 229
353 n
mi
Hp = 222
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16573269
07 X = -4999617
93
Y = -10512867
71 feet Y = -3260521
77 meter
Z = -10609555
03 Z = -3258203
67
XDOT = 2475
249046 XDOT = 798
067012
YDOT = -19567
397115 feet/sec YDOT = -5955
461803 meter/sec
ZDOT = 15552
749810 ZDOT = 4744
248932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12907086
09 X = -3934079
84
Y = -14703170
36 feet Y = -4481526
32 meter
Z = -10722882
23 Z = -3268334
50
XDOT = 6666
500713 XDOT = 2031
949417
YDOT = -17185
528589 feet/sec YDOT = -5238
149114 meter/sec
ZDOT = 15570
246727 ZDOT = 4745
811202
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 21043
56754363
00016717 00000-0 10270-3 0 9163
2 25544 51
6389 239
1094 0002485 7
1303 352
9882 15
48983617 29274
Satellite: ISS
Catalog Number: 25544
Epoch time: 21043
56754363 = yrday
fracday
Element set: 916
Inclination: 51
6389 deg
RA of node: 239
1094 deg
Eccentricity:
0002485
Arg of perigee: 7
1303 deg
Mean anomaly: 352
9882 deg
Mean motion: 15
48983617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 331
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