[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 2nd 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) : 16490 3108 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
033/03:47:30
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
1
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
1
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
046/21:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 222
4
Coasting Arc #1 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2021/032/13:47:11
137
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4512850
53 A = 6799730
79 meter
Y = 3836711
19 meter E =
0003660
Z = -3343922
96 I = 51
28550
XDOT = -1566
610689 Wp = 59
81585
YDOT = -5883
327833 meter/sec RA = 292
72484 deg
ZDOT = -4638
117531 TA = 159
23740
MA = 159
22253
Ha = 228
802 n
mi
Hp = 223
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14805940
06 X = -4539175
97
Y = 12587635
15 feet Y = 3786098
00 meter
Z = -10970875
86 Z = -3365908
03
XDOT = -5139
798850 XDOT = -1478
176372
YDOT = -19302
256670 feet/sec YDOT = -5900
352410 meter/sec
ZDOT = -15216
921034 ZDOT = -4645
512429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18386106
38 X = -5604085
23
Y = 6112661
66 feet Y = 1863139
28 meter
Z = -11072984
97 Z = -3375045
82
XDOT = 3051
317793 XDOT = 930
041663
YDOT = -18437
167473 feet/sec YDOT = -5619
648646 meter/sec
ZDOT = -15251
060269 ZDOT = -4648
523170
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
59968327
00016717 00000-0 10270-3 0 9004
2 25544 51
6443 293
3630 0002566 321
3854 38
7112 15
48915271 27572
Satellite: ISS
Catalog Number: 25544
Epoch time: 21032
59968327 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 293
3630 deg
Eccentricity:
0002566
Arg of perigee: 321
3854 deg
Mean anomaly: 38
7112 deg
Mean motion: 15
48915271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2757
Checksum: 310
Coasting Arc #2 (Orbit 2765)
---------------------------------------
Vector Time (GMT): 2021/033/03:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4604140
14 A = 6796364
00 meter
Y = 2468899
20 meter E =
0008652
Z = -4356254
45 I = 51
26654
XDOT = -441
495700 Wp = 54
76991
YDOT = -6836
580054 meter/sec RA = 289
82125 deg
ZDOT = -3407
926358 TA = 180
41266
MA = 180
41337
Ha = 228
885 n
mi
Hp = 223
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15105446
66 X = -4610246
25
Y = 8100063
00 feet Y = 2417378
16 meter
Z = -14292173
40 Z = -4378633
91
XDOT = -1448
476707 XDOT = -348
460802
YDOT = -22429
724587 feet/sec YDOT = -6840
997051 meter/sec
ZDOT = -11180
860754 ZDOT = -3409
844830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13639568
14 X = 4157340
37
Y = -10235584
70 feet Y = -3119806
22 meter
Z = -14396067
06 Z = -4387921
24
XDOT = 3936
724228 XDOT = 1199
913545
YDOT = 20984
106316 feet/sec YDOT = 6395
955605 meter/sec
ZDOT = -11189
575906 ZDOT = -3410
582736
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
18034602
00016717 00000-0 10270-3 0 9011
2 25544 51
6436 290
4895 0002225 327
4178 32
6834 15
48937842 27665
Satellite: ISS
Catalog Number: 25544
Epoch time: 21033
18034602 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 290
4895 deg
Eccentricity:
0002225
Arg of perigee: 327
4178 deg
Mean anomaly: 32
6834 deg
Mean motion: 15
48937842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2766
Checksum: 310
Coasting Arc #3 (Orbit 2781)
---------------------------------------
Vector Time (GMT): 2021/034/03:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4364447
82 A = 6796450
09 meter
Y = -2872553
05 meter E =
0008112
Z = 4340015
97 I = 51
25534
XDOT = 1046
925234 Wp = 96
63467
YDOT = 6774
597138 meter/sec RA = 284
84859 deg
ZDOT = 3424
666878 TA = 318
37391
MA = 318
43563
Ha = 228
887 n
mi
Hp = 223
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14319054
54 X = 4375164
31
Y = -9424386
65 feet Y = -2823686
67 meter
Z = 14238897
52 Z = 4361242
40
XDOT = 3434
794075 XDOT = 954
457061
YDOT = 22226
368562 feet/sec YDOT = 6785
787634 meter/sec
ZDOT = 11235
783721 ZDOT = 3429
527657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12467372
78 X = -3800055
22
Y = 11644866
53 feet Y = 3549355
32 meter
Z = 14337443
59 Z = 4370052
81
XDOT = -6136
283958 XDOT = -1870
339350
YDOT = -20456
945062 feet/sec YDOT = -6235
276855 meter/sec
ZDOT = 11258
167449 ZDOT = 3431
489438
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
21263364
00016717 00000-0 10270-3 0 9026
2 25544 51
6426 285
3829 0002324 335
6125 24
4915 15
48922530 27822
Satellite: ISS
Catalog Number: 25544
Epoch time: 21034
21263364 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 285
3829 deg
Eccentricity:
0002324
Arg of perigee: 335
6125 deg
Mean anomaly: 24
4915 deg
Mean motion: 15
48922530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2782
Checksum: 292
Coasting Arc #4 (Orbit 2796)
---------------------------------------
Vector Time (GMT): 2021/035/03:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4104746
91 A = 6796427
09 meter
Y = 3249308
79 meter E =
0009027
Z = -4343719
22 I = 51
24716
XDOT = -1634
125415 Wp = 54
31664
YDOT = -6643
693954 meter/sec RA = 279
87677 deg
ZDOT = -3425
453947 TA = 180
64791
MA = 180
64908
Ha = 229
054 n
mi
Hp = 223
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13467017
41 X = -4119677
64
Y = 10660461
91 feet Y = 3203323
08 meter
Z = -14251047
29 Z = -4363694
39
XDOT = -5361
303854 XDOT = -1543
073528
YDOT = -21796
896175 feet/sec YDOT = -6661
458807 meter/sec
ZDOT = -11238
365969 ZDOT = -3433
170638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11202120
71 X = 3414406
39
Y = -12917682
58 feet Y = -3937309
65 meter
Z = -14343790
42 Z = -4371987
32
XDOT = 8225
874698 XDOT = 2507
246608
YDOT = 19652
526550 feet/sec YDOT = 5990
090092 meter/sec
ZDOT = -11274
016807 ZDOT = -3436
320323
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
18040081
00016717 00000-0 10270-3 0 9033
2 25544 51
6419 280
5971 0002356 338
6743 21
4308 15
48936609 27974
Satellite: ISS
Catalog Number: 25544
Epoch time: 21035
18040081 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 280
5971 deg
Eccentricity:
0002356
Arg of perigee: 338
6743 deg
Mean anomaly: 21
4308 deg
Mean motion: 15
48936609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2797
Checksum: 311
Coasting Arc #5 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2021/036/03:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3796748
78 A = 6796486
92 meter
Y = -3603485
70 meter E =
0008266
Z = 4328211
41 I = 51
24153
XDOT = 2217
373182 Wp = 94
91544
YDOT = 6477
732682 meter/sec RA = 274
90387 deg
ZDOT = 3441
584906 TA = 319
88847
MA = 319
94947
Ha = 228
956 n
mi
Hp = 223
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12456524
87 X = 3815738
24
Y = -11822459
65 feet Y = -3560921
66 meter
Z = 14200168
66 Z = 4346700
26
XDOT = 7274
846399 XDOT = 2128
055417
YDOT = 21252
403812 feet/sec YDOT = 6502
029448 meter/sec
ZDOT = 11291
289061 ZDOT = 3452
139104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9756979
97 X = -2973927
49
Y = 14046044
30 feet Y = 4281234
30 meter
Z = 14286018
88 Z = 4354378
56
XDOT = -10260
729711 XDOT = -3127
470416
YDOT = -18682
633877 feet/sec YDOT = -5694
466806 meter/sec
ZDOT = 11340
121966 ZDOT = 3456
469175
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
21268579
00016717 00000-0 10270-3 0 9043
2 25544 51
6407 275
4913 0002477 339
7158 20
3893 15
48929522 28138
Satellite: ISS
Catalog Number: 25544
Epoch time: 21036
21268579 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 275
4913 deg
Eccentricity:
0002477
Arg of perigee: 339
7158 deg
Mean anomaly: 20
3893 deg
Mean motion: 15
48929522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2813
Checksum: 325
Coasting Arc #6 (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 = 4185744
95 A = 6793404
52 meter
Y = -1602376
14 meter E =
0003126
Z = 5102494
64 I = 51
23290
XDOT = 900
328573 Wp = 96
08053
YDOT = 7439
693248 meter/sec RA = 272
95138 deg
ZDOT = 1596
603080 TA = 338
41213
MA = 338
42531
Ha = 228
950 n
mi
Hp = 223
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13732759
03 X = 4178567
53
Y = -5257139
57 feet Y = -1555608
44 meter
Z = 16740467
98 Z = 5122809
53
XDOT = 2953
833901 XDOT = 809
313483
YDOT = 24408
442416 feet/sec YDOT = 7449
252417 meter/sec
ZDOT = 5238
199080 ZDOT = 1600
755660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14505720
12 X = 4421343
49
Y = 1626269
60 feet Y = 495686
97 meter
Z = 16834749
37 Z = 5131231
61
XDOT = -8565
575574 XDOT = -2610
787435
YDOT = 21939
656446 feet/sec YDOT = 6687
207285 meter/sec
ZDOT = 5257
319155 ZDOT = 1602
430879
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
59979236
00016717 00000-0 10270-3 0 9054
2 25544 51
6435 273
5777 0002668 339
6273 20
4771 15
48919771 28192
Satellite: ISS
Catalog Number: 25544
Epoch time: 21036
59979236 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 273
5777 deg
Eccentricity:
0002668
Arg of perigee: 339
6273 deg
Mean anomaly: 20
4771 deg
Mean motion: 15
48919771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2819
Checksum: 350
Coasting Arc #7 (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 = -4035469
44 A = 6793328
36 meter
Y = 1972585
64 meter E =
0013397
Z = -5108386
75 I = 51
23179
XDOT = -1546
287441 Wp = 66
02456
YDOT = -7318
532725 meter/sec RA = 267
97713 deg
ZDOT = -1602
514687 TA = 188
37868
MA = 188
40107
Ha = 229
074 n
mi
Hp = 222
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13239729
15 X = -4032414
44
Y = 6471737
65 feet Y = 1927475
47 meter
Z = -16759799
06 Z = -5127981
57
XDOT = -5073
121525 XDOT = -1456
550505
YDOT = -24010
934136 feet/sec YDOT = -7335
322586 meter/sec
ZDOT = -5257
594116 ZDOT = -1609
808246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14632571
09 X = -4460007
67
Y = -69513
65 feet Y = -21187
76 meter
Z = -16850748
11 Z = -5136108
02
XDOT = 6208
589238 XDOT = 1892
378000
YDOT = -22666
840893 feet/sec YDOT = -6908
853104 meter/sec
ZDOT = -5291
306787 ZDOT = -1612
790309
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
56755488
00016717 00000-0 10270-3 0 9064
2 25544 51
6428 268
7901 0002762 340
3151 19
7892 15
48954194 28348
Satellite: ISS
Catalog Number: 25544
Epoch time: 21037
56755488 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 268
7901 deg
Eccentricity:
0002762
Arg of perigee: 340
3151 deg
Mean anomaly: 19
7892 deg
Mean motion: 15
48954194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2834
Checksum: 336
Coasting Arc #8 (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 = 3840874
99 A = 6793431
65 meter
Y = -2317419
09 meter E =
0003484
Z = 5098776
46 I = 51
23402
XDOT = 2183
044756 Wp = 93
12794
YDOT = 7165
962012 meter/sec RA = 263
00404 deg
ZDOT = 1611
347446 TA = 341
21894
MA = 341
23179
Ha = 229
098 n
mi
Hp = 223
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12601295
91 X = 3841737
28
Y = -7603080
99 feet Y = -2274463
16 meter
Z = 16728269
23 Z = 5117435
43
XDOT = 7162
220329 XDOT = 2094
923721
YDOT = 23510
374054 feet/sec YDOT = 7189
881572 meter/sec
ZDOT = 5286
572984 ZDOT = 1621
737996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14543359
07 X = 4432815
85
Y = -1478138
24 feet Y = -450536
54 meter
Z = 16814883
44 Z = 5125176
47
XDOT = -3811
668841 XDOT = -1161
796663
YDOT = 23225
391146 feet/sec YDOT = 7079
099221 meter/sec
ZDOT = 5334
678867 ZDOT = 1626
010119
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
59983488
00016717 00000-0 10270-3 0 9072
2 25544 51
6425 263
6843 0002743 347
2756 12
8325 15
48919104 28505
Satellite: ISS
Catalog Number: 25544
Epoch time: 21038
59983488 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 263
6843 deg
Eccentricity:
0002743
Arg of perigee: 347
2756 deg
Mean anomaly: 12
8325 deg
Mean motion: 15
48919104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2850
Checksum: 331
Coasting Arc #9 (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 = -3628353
84 A = 6793365
74 meter
Y = 2653516
65 meter E =
0013781
Z = -5105860
61 I = 51
23716
XDOT = -2795
853930 Wp = 66
45341
YDOT = -6934
642920 meter/sec RA = 258
03095 deg
ZDOT = -1615
215942 TA = 187
82410
MA = 187
84561
Ha = 229
231 n
mi
Hp = 222
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11904048
04 X = -3632955
99
Y = 8705763
29 feet Y = 2612916
36 meter
Z = -16751511
19 Z = -5123496
23
XDOT = -9172
749114 XDOT = -2710
255281
YDOT = -22751
453151 feet/sec YDOT = -6965
429462 meter/sec
ZDOT = -5299
264902 ZDOT = -1628
589233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14339511
72 X = -4370683
17
Y = 3020835
76 feet Y = 920750
74 meter
Z = -16833382
20 Z = -5130814
90
XDOT = 1361
887016 XDOT = 415
103162
YDOT = -23445
242632 feet/sec YDOT = -7146
109954 meter/sec
ZDOT = -5361
239757 ZDOT = -1634
105878
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
56759404
00016717 00000-0 10270-3 0 9080
2 25544 51
6403 258
8975 0002701 349
2936 10
8156 15
48949652 28656
Satellite: ISS
Catalog Number: 25544
Epoch time: 21039
56759404 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 258
8975 deg
Eccentricity:
0002701
Arg of perigee: 349
2936 deg
Mean anomaly: 10
8156 deg
Mean motion: 15
48949652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 340
Coasting Arc #10 (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 = 2575988
00 A = 6795597
39 meter
Y = -4355967
29 meter E =
0007691
Z = 4529177
95 I = 51
25104
XDOT = 4127
757724 Wp = 96
04813
YDOT = 5665
922265 meter/sec RA = 254
68692 deg
ZDOT = 3096
210700 TA = 322
72357
MA = 322
77692
Ha = 229
092 n
mi
Hp = 222
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8451404
20 X = 2602506
87
Y = -14291231
27 feet Y = -4327012
70 meter
Z = 14859507
70 Z = 4541754
86
XDOT = 13542
512219 XDOT = 4049
053742
YDOT = 18588
983809 feet/sec YDOT = 5711
641600 meter/sec
ZDOT = 10158
171587 ZDOT = 3116
070229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2502945
80 X = 762897
88
Y = 16360362
11 feet Y = 4986638
37 meter
Z = 14917919
00 Z = 4546981
71
XDOT = -20974
905209 XDOT = -6393
151108
YDOT = -6153
566768 feet/sec YDOT = -1875
607151 meter/sec
ZDOT = 10250
279448 ZDOT = 3124
285176
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
27728412
00016717 00000-0 10270-3 0 9096
2 25544 51
6411 255
3886 0002630 351
2109 8
8994 15
48985577 28769
Satellite: ISS
Catalog Number: 25544
Epoch time: 21040
27728412 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 255
3886 deg
Eccentricity:
0002630
Arg of perigee: 351
2109 deg
Mean anomaly: 8
8994 deg
Mean motion: 15
48985577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2876
Checksum: 329
Coasting Arc #11 (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 = 4067106
64 A = 6799814
02 meter
Y = 4365978
32 meter E =
0012266
Z = 3252906
45 I = 51
26769
XDOT = -2236
102857 Wp = 79
92204
YDOT = 5608
713740 meter/sec RA = 252
95918 deg
ZDOT = -4714
732464 TA = 62
22768
MA = 62
10337
Ha = 229
127 n
mi
Hp = 222
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13343525
72 X = 4002182
44
Y = 14324075
85 feet Y = 4411096
47 meter
Z = 10672265
26 Z = 3272504
72
XDOT = -7336
295462 XDOT = -2275
754321
YDOT = 18401
291798 feet/sec YDOT = 5583
486545 meter/sec
ZDOT = -15468
282363 ZDOT = -4725
690245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7828788
29 X = 2386214
67
Y = 17888266
20 feet Y = 5452343
54 meter
Z = 10763181
66 Z = 3280617
77
XDOT = -11567
796238 XDOT = -3525
864293
YDOT = 14434
350355 feet/sec YDOT = 4399
589988 meter/sec
ZDOT = -15519
187469 ZDOT = -4730
248341
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
59986891
00016717 00000-0 10270-3 0 9100
2 25544 51
6405 253
7910 0002762 348
1981 11
9104 15
48976673 28812
Satellite: ISS
Catalog Number: 25544
Epoch time: 21040
59986891 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 253
7910 deg
Eccentricity:
0002762
Arg of perigee: 348
1981 deg
Mean anomaly: 11
9104 deg
Mean motion: 15
48976673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 326
Coasting Arc #12 (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 = -4438581
70 A = 6799808
18 meter
Y = -3979208
24 meter E =
0005393
Z = -3272003
38 I = 51
27768
XDOT = 1727
892652 Wp = 56
23111
YDOT = -5788
177238 meter/sec RA = 247
98629 deg
ZDOT = 4703
835607 TA = 265
69054
MA = 265
75216
Ha = 229
253 n
mi
Hp = 222
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14562275
92 X = -4377862
16
Y = -13055145
15 feet Y = -4028504
07 meter
Z = -10734919
21 Z = -3293416
11
XDOT = 5668
939147 XDOT = 1769
641699
YDOT = -18990
082803 feet/sec YDOT = -5768
621385 meter/sec
ZDOT = 15432
531519 ZDOT = 4712
329971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9688840
51 X = -2953158
59
Y = -16925716
06 feet Y = -5158958
25 meter
Z = -10834283
12 Z = -3302289
49
XDOT = 9977
987302 XDOT = 3041
290530
YDOT = -15597
667718 feet/sec YDOT = -4754
169120 meter/sec
ZDOT = 15471
989539 ZDOT = 4715
862411
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
56762665
00016717 00000-0 10270-3 0 9110
2 25544 51
6395 249
0033 0002570 356
2123 3
9007 15
48957144 28960
Satellite: ISS
Catalog Number: 25544
Epoch time: 21041
56762665 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 249
0033 deg
Eccentricity:
0002570
Arg of perigee: 356
2123 deg
Mean anomaly: 3
9007 deg
Mean motion: 15
48957144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 304
Coasting Arc #13 (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 = 4759783
94 A = 6799811
27 meter
Y = 3592945
72 meter E =
0012716
Z = 3258351
63 I = 51
29146
XDOT = -1226
321815 Wp = 80
34822
YDOT = 5914
354158 meter/sec RA = 243
01490 deg
ZDOT = -4712
397895 TA = 61
74040
MA = 61
61211
Ha = 229
279 n
mi
Hp = 222
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15616089
05 X = 4703426
16
Y = 11787879
66 feet Y = 3645857
94 meter
Z = 10690130
03 Z = 3281335
05
XDOT = -4023
365536 XDOT = -1269
477519
YDOT = 19404
049074 feet/sec YDOT = 5900
399243 meter/sec
ZDOT = -15460
623016 ZDOT = -4718
459476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11360297
08 X = 3462618
55
Y = 15857736
39 feet Y = 4833438
05 meter
Z = 10796808
36 Z = 3290867
19
XDOT = -8324
084533 XDOT = -2537
180966
YDOT = 16548
431652 feet/sec YDOT = 5043
961967 meter/sec
ZDOT = -15488
771997 ZDOT = -4720
977705
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
59989628
00016717 00000-0 10270-3 0 9125
2 25544 51
6393 243
8970 0002669 358
0552 2
0587 15
48967889 29124
Satellite: ISS
Catalog Number: 25544
Epoch time: 21042
59989628 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 243
8970 deg
Eccentricity:
0002669
Arg of perigee: 358
0552 deg
Mean anomaly: 2
0587 deg
Mean motion: 15
48967889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2912
Checksum: 353
Coasting Arc #14 (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 = -5058258
16 A = 6799767
75 meter
Y = -3149301
84 meter E =
0005785
Z = -3277284
57 I = 51
30727
XDOT = 695
546704 Wp = 60
31865
YDOT = -6001
151989 meter/sec RA = 238
04441 deg
ZDOT = 4702
361814 TA = 261
55086
MA = 261
61644
Ha = 229
405 n
mi
Hp = 222
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16595335
18 X = -5006747
18
Y = -10332355
11 feet Y = -3205579
00 meter
Z = -10752245
98 Z = -3301729
53
XDOT = 2281
977376 XDOT = 739
761175
YDOT = -19688
818860 feet/sec YDOT = -5993
126543 meter/sec
ZDOT = 15427
696239 ZDOT = 4705
847923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12977743
99 X = -3955616
37
Y = -14535735
02 feet Y = -4430492
04 meter
Z = -10865729
32 Z = -3311874
30
XDOT = 6527
872817 XDOT = 1989
695635
YDOT = -17350
708006 feet/sec YDOT = -5288
495800 meter/sec
ZDOT = 15443
871555 ZDOT = 4707
292050
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
56765029
00016717 00000-0 10270-3 0 9131
2 25544 51
6387 239
1098 0002501 8
1271 351
9919 15
48961907 29278
Satellite: ISS
Catalog Number: 25544
Epoch time: 21043
56765029 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 239
1098 deg
Eccentricity:
0002501
Arg of perigee: 8
1271 deg
Mean anomaly: 351
9919 deg
Mean motion: 15
48961907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 323
Coasting Arc #15 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2021/044/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5306820
56 A = 6799822
79 meter
Y = 2715207
21 meter E =
0013106
Z = 3262415
98 I = 51
32623
XDOT = -180
932210 Wp = 81
41919
YDOT = 6037
749533 meter/sec RA = 233
07561 deg
ZDOT = -4712
501058 TA = 60
63372
MA = 60
50290
Ha = 229
402 n
mi
Hp = 222
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17410828
62 X = 5260217
46
Y = 8908160
14 feet Y = 2774291
48 meter
Z = 10703464
51 Z = 3288080
26
XDOT = -593
609614 XDOT = -225
544856
YDOT = 19808
889544 feet/sec YDOT = 6035
476555 meter/sec
ZDOT = -15460
961476 ZDOT = -4713
488557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14387184
40 X = 4385213
81
Y = 13150518
36 feet Y = 4008278
00 meter
Z = 10822625
13 Z = 3298736
14
XDOT = -4715
335556 XDOT = -1437
234277
YDOT = 17935
231675 feet/sec YDOT = 5466
658614 meter/sec
ZDOT = -15465
519379 ZDOT = -4713
890307
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 21044
59991760
00016717 00000-0 10270-3 0 9149
2 25544 51
6386 234
0038 0002501 7
9141 352
2048 15
48956423 29430
Satellite: ISS
Catalog Number: 25544
Epoch time: 21044
59991760 = yrday
fracday
Element set: 914
Inclination: 51
6386 deg
RA of node: 234
0038 deg
Eccentricity:
0002501
Arg of perigee: 7
9141 deg
Mean anomaly: 352
2048 deg
Mean motion: 15
48956423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 303
Coasting Arc #16 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2021/045/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5524012
13 A = 6799719
53 meter
Y = -2228946
64 meter E =
0006061
Z = -3280801
63 I = 51
34976
XDOT = -355
128357 Wp = 62
56299
YDOT = -6029
524346 meter/sec RA = 228
10772 deg
ZDOT = 4703
797659 TA = 259
28589
MA = 259
35413
Ha = 229
496 n
mi
Hp = 222
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18123399
37 X = -5482741
03
Y = -7312817
05 feet Y = -2290489
55 meter
Z = -10763784
88 Z = -3307533
96
XDOT = -1165
119281 XDOT = -310
525664
YDOT = -19781
904023 feet/sec YDOT = -6033
245985 meter/sec
ZDOT = 15432
407017 ZDOT = 4702
181313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15694101
06 X = -4783562
00
Y = -11530065
66 feet Y = -3514364
01 meter
Z = -10887917
19 Z = -3318637
16
XDOT = 2795
053376 XDOT = 851
932269
YDOT = -18341
326839 feet/sec YDOT = -5590
436420 meter/sec
ZDOT = 15424
859678 ZDOT = 4701
497230
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 21045
56766669
00016717 00000-0 10270-3 0 9156
2 25544 51
6408 229
2165 0002534 15
8267 344
2962 15
48971971 29582
Satellite: ISS
Catalog Number: 25544
Epoch time: 21045
56766669 = yrday
fracday
Element set: 915
Inclination: 51
6408 deg
RA of node: 229
2165 deg
Eccentricity:
0002534
Arg of perigee: 15
8267 deg
Mean anomaly: 344
2962 deg
Mean motion: 15
48971971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 342
Coasting Arc #17 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2021/046/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5693769
56 A = 6799806
64 meter
Y = 1761819
49 meter E =
0013611
Z = 3263649
22 I = 51
37274
XDOT = 865
103518 Wp = 82
01266
YDOT = 5975
589898 meter/sec RA = 223
14159 deg
ZDOT = -4716
270914 TA = 60
05062
MA = 59
91555
Ha = 229
562 n
mi
Hp = 222
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18680346
34 X = 5657792
65
Y = 5780247
66 feet Y = 1825290
36 meter
Z = 10707510
56 Z = 3291219
14
XDOT = 2838
266135 XDOT = 821
126720
YDOT = 19604
953734 feet/sec YDOT = 5985
017934 meter/sec
ZDOT = -15473
329771 ZDOT = -4712
175856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16784118
72 X = 5115799
39
Y = 9894531
89 feet Y = 3015853
32 meter
Z = 10835542
54 Z = 3302673
37
XDOT = -909
239596 XDOT = -277
136229
YDOT = 18533
116502 feet/sec YDOT = 5648
893910 meter/sec
ZDOT = -15454
259527 ZDOT = -4710
458304
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 21046
59992922
00016717 00000-0 10270-3 0 9164
2 25544 51
6400 224
1102 0002566 19
7889 340
3360 15
48958151 29749
Satellite: ISS
Catalog Number: 25544
Epoch time: 21046
59992922 = yrday
fracday
Element set: 916
Inclination: 51
6400 deg
RA of node: 224
1102 deg
Eccentricity:
0002566
Arg of perigee: 19
7889 deg
Mean anomaly: 340
3360 deg
Mean motion: 15
48958151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 317
Coasting Arc #18 (Orbit 2978)
---------------------------------------
Vector Time (GMT): 2021/046/21:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4043975
14 A = 6793115
93 meter
Y = -1883483
16 meter E =
0007256
Z = 5120084
37 I = 51
36089
XDOT = 4705
069952 Wp = 41
64596
YDOT = 5843
259339 meter/sec RA = 221
58932 deg
ZDOT = -1560
076650 TA = 63
50021
MA = 63
42581
Ha = 229
497 n
mi
Hp = 222
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13267634
98 X = 4039866
42
Y = -6179406
70 feet Y = -1838283
18 meter
Z = 16798177
08 Z = 5139718
09
XDOT = 15436
581207 XDOT = 4646
956932
YDOT = 19170
798356 feet/sec YDOT = 5895
549802 meter/sec
ZDOT = -5118
361714 ZDOT = -1537
363300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8533777
45 X = -2601095
37
Y = -11760920
88 feet Y = -3584728
68 meter
Z = 16889326
24 Z = 5147866
64
XDOT = 15074
136391 XDOT = 4594
596772
YDOT = -18167
486064 feet/sec YDOT = -5537
449752 meter/sec
ZDOT = -5012
835986 ZDOT = -1527
912409
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 21046
92250919
00016717 00000-0 10270-3 0 9175
2 25544 51
6423 222
5189 0002859 18
0947 342
0304 15
48993364 29790
Satellite: ISS
Catalog Number: 25544
Epoch time: 21046
92250919 = yrday
fracday
Element set: 917
Inclination: 51
6423 deg
RA of node: 222
5189 deg
Eccentricity:
0002859
Arg of perigee: 18
0947 deg
Mean anomaly: 342
0304 deg
Mean motion: 15
48993364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2979
Checksum: 329
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