[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 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) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 4 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
006/03:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
8
000/00:00:00
000 0
0 0
0 222
4
006/15:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 222
3
011/14:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 222
4
Coasting Arc #1 (Orbit 2274)
---------------------------------------
Vector Time (GMT): 2021/001/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2759863
62 A = 6799622
94 meter
Y = 5396272
92 meter E =
0004116
Z = -3085156
91 I = 52
04449
XDOT = -3560
308400 Wp = 86
46941
YDOT = 4640
667164 meter/sec RA = 86
30676 deg
ZDOT = 4938
030329 TA = 238
40911
MA = 238
44929
Ha = 228
688 n
mi
Hp = 222
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9054670
67 X = 2714301
38
Y = 17704307
48 feet Y = 5426881
37 meter
Z = -10121905
88 Z = -3071860
75
XDOT = -11680
801836 XDOT = -3635
922800
YDOT = 15225
285972 feet/sec YDOT = 4600
429768 meter/sec
ZDOT = 16200
886905 ZDOT = 4920
553068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15754924
58 X = -4802101
01
Y = 12184190
33 feet Y = 3713741
21 meter
Z = -10060337
98 Z = -3066391
02
XDOT = -16224
061876 XDOT = -4945
094060
YDOT = -7685
132806 feet/sec YDOT = -2342
428479 meter/sec
ZDOT = 16119
565040 ZDOT = 4913
243424
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 21001
50629723
00016717 00000-0 10270-3 0 9005
2 25544 51
6448 87
1913 0001121 190
1107 170
0021 15
49236999 22757
Satellite: ISS
Catalog Number: 25544
Epoch time: 21001
50629723 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 87
1913 deg
Eccentricity:
0001121
Arg of perigee: 190
1107 deg
Mean anomaly: 170
0021 deg
Mean motion: 15
49236999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2275
Checksum: 276
Coasting Arc #2 (Orbit 2290)
---------------------------------------
Vector Time (GMT): 2021/002/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3155837
47 A = 6799778
84 meter
Y = -5215395
05 meter E =
0013183
Z = 2998381
36 I = 52
04216
XDOT = 3216
046689 Wp = 101
49858
YDOT = -4832
018156 meter/sec RA = 81
38548 deg
ZDOT = -5003
879036 TA = 44
46063
MA = 44
35490
Ha = 228
719 n
mi
Hp = 222
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10353797
46 X = -3111846
90
Y = -17110876
16 feet Y = -5250440
28 meter
Z = 9837209
19 Z = 2983158
09
XDOT = 10551
334283 XDOT = 3294
146232
YDOT = -15853
077941 feet/sec YDOT = -4795
616746 meter/sec
ZDOT = -16416
925970 ZDOT = -4988
067944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14704158
98 X = 4481827
66
Y = -13607107
28 feet Y = -4147446
30 meter
Z = 9766689
78 Z = 2976887
05
XDOT = 16661
387859 XDOT = 5078
391019
YDOT = 6236
047564 feet/sec YDOT = 1900
747297 meter/sec
ZDOT = -16343
325216 ZDOT = -4981
445526
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 21002
53837431
00016717 00000-0 10270-3 0 9017
2 25544 51
6452 82
0844 0000965 187
5846 172
5289 15
49261705 22918
Satellite: ISS
Catalog Number: 25544
Epoch time: 21002
53837431 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 82
0844 deg
Eccentricity:
0000965
Arg of perigee: 187
5846 deg
Mean anomaly: 172
5289 deg
Mean motion: 15
49261705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2291
Checksum: 309
Coasting Arc #3 (Orbit 2305)
---------------------------------------
Vector Time (GMT): 2021/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3560746
35 A = 6799951
19 meter
Y = 4993630
07 meter E =
0004078
Z = -2938715
95 I = 52
03558
XDOT = -2849
026334 Wp = 75
29275
YDOT = 4999
000738 meter/sec RA = 76
46390 deg
ZDOT = 5049
359318 TA = 251
47109
MA = 251
51540
Ha = 228
644 n
mi
Hp = 222
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11682238
69 X = 3518915
73
Y = 16383300
75 feet Y = 5033215
28 meter
Z = -9641456
52 Z = -2921520
72
XDOT = -9347
199257 XDOT = -2929
241331
YDOT = 16400
921058 feet/sec YDOT = 4966
691895 meter/sec
ZDOT = 16566
139495 ZDOT = 5035
325789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13471906
63 X = -4106237
14
Y = 14997503
03 feet Y = 4571238
92 meter
Z = -9561776
14 Z = -2914429
37
XDOT = -16959
302943 XDOT = -5169
195537
YDOT = -4728
392741 feet/sec YDOT = -1441
214107 meter/sec
ZDOT = 16500
780085 ZDOT = 5029
437770
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 21003
50594340
00016717 00000-0 10270-3 0 9025
2 25544 51
6444 77
2969 0000933 193
3222 166
7904 15
49255339 23063
Satellite: ISS
Catalog Number: 25544
Epoch time: 21003
50594340 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 77
2969 deg
Eccentricity:
0000933
Arg of perigee: 193
3222 deg
Mean anomaly: 166
7904 deg
Mean motion: 15
49255339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2306
Checksum: 302
Coasting Arc #4 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2021/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3929897
76 A = 6800092
53 meter
Y = -4754125
26 meter E =
0013299
Z = 2847461
57 I = 52
02696
XDOT = 2493
850049 Wp = 103
15094
YDOT = -5134
374056 meter/sec RA = 71
54196 deg
ZDOT = -5113
397058 TA = 44
72904
MA = 44
62187
Ha = 228
642 n
mi
Hp = 222
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12893365
34 X = -3890274
70
Y = -15597523
81 feet Y = -4797850
87 meter
Z = 9342065
51 Z = 2828467
88
XDOT = 8181
922732 XDOT = 2575
916348
YDOT = -16845
059240 feet/sec YDOT = -5106
026791 meter/sec
ZDOT = -16776
237067 ZDOT = -5101
084185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12167225
10 X = 3708570
21
Y = -16220892
48 feet Y = -4944128
03 meter
Z = 9254030
88 Z = 2820628
61
XDOT = 17127
812654 XDOT = 5220
557297
YDOT = 3277
079213 feet/sec YDOT = 998
853744 meter/sec
ZDOT = -16718
856503 ZDOT = -5095
907462
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 21004
53801474
00016717 00000-0 10270-3 0 9039
2 25544 51
6441 72
1901 0000807 195
4940 164
6185 15
49285212 23229
Satellite: ISS
Catalog Number: 25544
Epoch time: 21004
53801474 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 72
1901 deg
Eccentricity:
0000807
Arg of perigee: 195
4940 deg
Mean anomaly: 164
6185 deg
Mean motion: 15
49285212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2322
Checksum: 282
Coasting Arc #5 (Orbit 2336)
---------------------------------------
Vector Time (GMT): 2021/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4301602
20 A = 6800290
16 meter
Y = 4471527
56 meter E =
0004164
Z = -2783955
15 I = 52
01517
XDOT = -2119
763061 Wp = 65
89184
YDOT = 5245
486382 meter/sec RA = 66
61892 deg
ZDOT = 5157
580175 TA = 262
81708
MA = 262
86443
Ha = 228
606 n
mi
Hp = 222
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14112868
10 X = 4264803
19
Y = 14670366
01 feet Y = 4519425
59 meter
Z = -9133711
13 Z = -2763149
03
XDOT = -6954
603218 XDOT = -2203
314367
YDOT = 17209
600992 feet/sec YDOT = 5221
314174 meter/sec
ZDOT = 16921
194800 ZDOT = 5147
080743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10685566
15 X = -3256960
56
Y = 17377111
75 feet Y = 5296543
66 meter
Z = -9037257
73 Z = -2754556
16
XDOT = -17160
678555 XDOT = -5230
574824
YDOT = -1791
119632 feet/sec YDOT = -545
933264 meter/sec
ZDOT = 16872
224107 ZDOT = 5142
653908
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 21005
50557964
00016717 00000-0 10270-3 0 9040
2 25544 51
6437 67
4024 0000890 197
0970 163
0150 15
49269727 23374
Satellite: ISS
Catalog Number: 25544
Epoch time: 21005
50557964 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 67
4024 deg
Eccentricity:
0000890
Arg of perigee: 197
0970 deg
Mean anomaly: 163
0150 deg
Mean motion: 15
49269727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2337
Checksum: 308
Coasting Arc #6 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2021/006/03:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3377012
36 A = 6791797
74 meter
Y = 2538961
88 meter E =
0003184
Z = 5315710
00 I = 51
97481
XDOT = -3882
398615 Wp = 127
40418
YDOT = -6572
135690 meter/sec RA = 63
36671 deg
ZDOT = 670
471537 TA = 316
20585
MA = 316
23109
Ha = 228
809 n
mi
Hp = 222
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11079436
89 X = -3430973
22
Y = 8329927
44 feet Y = 2500895
65 meter
Z = 17439993
44 Z = 5299175
08
XDOT = -12737
528265 XDOT = -3811
875180
YDOT = -21562
124968 feet/sec YDOT = -6615
157185 meter/sec
ZDOT = 2199
709768 ZDOT = 651
783440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13002484
44 X = 3963157
26
Y = -5074764
56 feet Y = -1546788
24 meter
Z = 17363097
29 Z = 5292272
05
XDOT = 6230
234811 XDOT = 1898
975570
YDOT = 23217
504695 feet/sec YDOT = 7076
695431 meter/sec
ZDOT = 2113
186730 ZDOT = 644
099315
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 21006
21512613
00016717 00000-0 10270-3 0 9052
2 25544 51
6415 63
8886 0000692 193
8265 166
2867 15
49225452 23486
Satellite: ISS
Catalog Number: 25544
Epoch time: 21006
21512613 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 63
8886 deg
Eccentricity:
0000692
Arg of perigee: 193
8265 deg
Mean anomaly: 166
2867 deg
Mean motion: 15
49225452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 312
Coasting Arc #7 (Orbit 2354)
---------------------------------------
Vector Time (GMT): 2021/006/15:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 983277
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4063807
44 A = 6802820
48 meter
Y = -5296566
20 meter E =
0014004
Z = 1271207
98 I = 52
00658
XDOT = 3125
096243 Wp = 122
89583
YDOT = -3814
743953 meter/sec RA = 61
05625 deg
ZDOT = -5864
678701 TA = 43
37366
MA = 43
26354
Ha = 228
682 n
mi
Hp = 222
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13332701
59 X = -4010452
34
Y = -17377185
71 feet Y = -5341712
38 meter
Z = 4170629
86 Z = 1251597
01
XDOT = 10252
940431 XDOT = 3196
008601
YDOT = -12515
564150 feet/sec YDOT = -3779
399992 meter/sec
ZDOT = -19241
071854 ZDOT = -5849
326367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4019491
71 X = -1225141
07
Y = -21548104
06 feet Y = -6567862
12 meter
Z = 4079775
26 Z = 1243515
50
XDOT = 13362
900588 XDOT = 4073
012099
YDOT = -6147
096627 feet/sec YDOT = -1873
635052 meter/sec
ZDOT = -19169
612615 ZDOT = -5842
897925
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 21006
66665208
00016717 00000-0 10270-3 0 9061
2 25544 51
6434 61
6575 0000532 178
1051 182
0101 15
49276713 23551
Satellite: ISS
Catalog Number: 25544
Epoch time: 21006
66665208 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 61
6575 deg
Eccentricity:
0000532
Arg of perigee: 178
1051 deg
Mean anomaly: 182
0101 deg
Mean motion: 15
49276713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2355
Checksum: 286
Coasting Arc #8 (Orbit 2369)
---------------------------------------
Vector Time (GMT): 2021/007/15:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 983277
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4469451
54 A = 6802791
60 meter
Y = 4982395
27 meter E =
0008759
Z = -1195670
12 I = 51
98882
XDOT = -2868
244973 Wp = 40
75244
YDOT = 3977
356795 meter/sec RA = 56
13235 deg
ZDOT = 5882
892314 TA = 306
35081
MA = 306
43162
Ha = 228
640 n
mi
Hp = 222
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14663554
91 X = 4419212
54
Y = 16346441
16 feet Y = 5032095
08 meter
Z = -3922802
23 Z = -1174081
02
XDOT = -9410
252537 XDOT = -2941
083359
YDOT = 13049
070851 feet/sec YDOT = 3944
874269 meter/sec
ZDOT = 19300
827801 ZDOT = 5868
783005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6036029
33 X = 1839781
74
Y = 21132136
56 feet Y = 6441075
22 meter
Z = -3822762
44 Z = -1165177
99
XDOT = -12757
173978 XDOT = -3888
386628
YDOT = 7104
761061 feet/sec YDOT = 2165
531171 meter/sec
ZDOT = 19235
127002 ZDOT = 5862
866710
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 21007
63421011
00016717 00000-0 10270-3 0 9072
2 25544 51
6428 56
8706 0000675 177
3621 182
7533 15
49311401 23705
Satellite: ISS
Catalog Number: 25544
Epoch time: 21007
63421011 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 56
8706 deg
Eccentricity:
0000675
Arg of perigee: 177
3621 deg
Mean anomaly: 182
7533 deg
Mean motion: 15
49311401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2370
Checksum: 281
Coasting Arc #9 (Orbit 2385)
---------------------------------------
Vector Time (GMT): 2021/008/15:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 983277
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4830423
58 A = 6802980
09 meter
Y = -4656360
27 meter E =
0013640
Z = 1083576
09 I = 51
96841
XDOT = 2626
300447 Wp = 124
89027
YDOT = -4110
067686 meter/sec RA = 51
20607 deg
ZDOT = -5909
165973 TA = 43
43142
MA = 43
32405
Ha = 228
596 n
mi
Hp = 222
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15847846
40 X = -4783259
10
Y = -15276772
55 feet Y = -4710113
94 meter
Z = 3555039
66 Z = 1060225
97
XDOT = 8616
471283 XDOT = 2700
768470
YDOT = -13484
474034 feet/sec YDOT = -4080
281509 meter/sec
ZDOT = -19387
027472 ZDOT = -5896
228065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7921865
26 X = -2414584
53
Y = -20555675
52 feet Y = -6265369
90 meter
Z = 3446821
24 Z = 1050591
11
XDOT = 12132
713777 XDOT = 3698
051159
YDOT = -7942
072255 feet/sec YDOT = -2420
743623 meter/sec
ZDOT = -19326
751832 ZDOT = -5890
793959
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 21008
66627072
00016717 00000-0 10270-3 0 9082
2 25544 51
6420 51
7630 0000396 202
0635 158
0498 15
49285787 23868
Satellite: ISS
Catalog Number: 25544
Epoch time: 21008
66627072 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 51
7630 deg
Eccentricity:
0000396
Arg of perigee: 202
0635 deg
Mean anomaly: 158
0498 deg
Mean motion: 15
49285787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2386
Checksum: 314
Coasting Arc #10 (Orbit 2400)
---------------------------------------
Vector Time (GMT): 2021/009/15:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 983277
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5184039
64 A = 6802982
61 meter
Y = 4282798
99 meter E =
0009320
Z = -1004850
81 I = 51
94667
XDOT = -2362
011470 Wp = 40
27733
YDOT = 4240
310392 meter/sec RA = 46
27943 deg
ZDOT = 5924
643979 TA = 308
90467
MA = 308
98775
Ha = 228
603 n
mi
Hp = 222
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17008004
07 X = 5140643
75
Y = 14051177
79 feet Y = 4340528
14 meter
Z = -3296754
62 Z = -979773
80
XDOT = -7749
381463 XDOT = -2438
030678
YDOT = 13911
779502 feet/sec YDOT = 4213
470871 meter/sec
ZDOT = 19437
808331 ZDOT = 5912
986243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9831356
26 X = 2996597
39
Y = 19768792
99 feet Y = 6025528
10 meter
Z = -3180510
75 Z = -969419
68
XDOT = -11423
979631 XDOT = -3482
028992
YDOT = 8779
302524 feet/sec YDOT = 2675
931409 meter/sec
ZDOT = 19383
461994 ZDOT = 5908
079216
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 21009
63382518
00016717 00000-0 10270-3 0 9094
2 25544 51
6423 46
9760 0000566 188
6309 171
4831 15
49306431 24015
Satellite: ISS
Catalog Number: 25544
Epoch time: 21009
63382518 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 46
9760 deg
Eccentricity:
0000566
Arg of perigee: 188
6309 deg
Mean anomaly: 171
4831 deg
Mean motion: 15
49306431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2401
Checksum: 303
Coasting Arc #11 (Orbit 2416)
---------------------------------------
Vector Time (GMT): 2021/010/15:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 983277
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5491130
74 A = 6803102
99 meter
Y = -3905296
94 meter E =
0013305
Z = 888484
89 I = 51
92311
XDOT = 2117
523256 Wp = 126
65375
YDOT = -4342
553583 meter/sec RA = 41
34990 deg
ZDOT = -5946
603201 TA = 43
78700
MA = 43
68158
Ha = 228
543 n
mi
Hp = 222
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18015520
80 X = -5451368
11
Y = -12812654
00 feet Y = -3966480
52 meter
Z = 2914976
67 Z = 861907
43
XDOT = 6947
254776 XDOT = 2194
810491
YDOT = -14247
223040 feet/sec YDOT = -4318
440906 meter/sec
ZDOT = -19509
853021 ZDOT = -5936
130140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11579484
80 X = -3529426
97
Y = -18850512
44 feet Y = -5745636
19 meter
Z = 2791754
57 Z = 850926
79
XDOT = 10719
399260 XDOT = 3267
272895
YDOT = -9494
224670 feet/sec YDOT = -2893
839679 meter/sec
ZDOT = -19460
994167 ZDOT = -5931
711022
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 21010
66587934
00016717 00000-0 10270-3 0 9100
2 25544 51
6428 41
8680 0000285 227
2660 132
8466 15
49298324 24176
Satellite: ISS
Catalog Number: 25544
Epoch time: 21010
66587934 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 41
8680 deg
Eccentricity:
0000285
Arg of perigee: 227
2660 deg
Mean anomaly: 132
8466 deg
Mean motion: 15
49298324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2417
Checksum: 310
Coasting Arc #12 (Orbit 2431)
---------------------------------------
Vector Time (GMT): 2021/011/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 956684
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5577301
42 A = 6803397
53 meter
Y = -3876178
34 meter E =
0012462
Z = 268977
38 I = 51
89783
XDOT = 2498
806705 Wp = 132
97443
YDOT = -4024
893755 meter/sec RA = 36
57856 deg
ZDOT = -6020
767073 TA = 44
14314
MA = 44
04375
Ha = 228
541 n
mi
Hp = 222
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18298233
01 X = -5534848
82
Y = -12717120
54 feet Y = -3938310
41 meter
Z = 882471
73 Z = 241988
01
XDOT = 8198
184728 XDOT = 2572
873512
YDOT = -13205
032003 feet/sec YDOT = -3996
535243 meter/sec
ZDOT = -19753
172811 ZDOT = -6008
449781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8301064
18 X = -2530164
36
Y = -20684487
20 feet Y = -6304631
70 meter
Z = 757340
81 Z = 230837
48
XDOT = 12712
234866 XDOT = 3874
689187
YDOT = -5846
292029 feet/sec YDOT = -1781
949810 meter/sec
ZDOT = -19695
759622 ZDOT = -6003
267533
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 21011
63342823
00016717 00000-0 10270-3 0 9115
2 25544 51
6420 37
0804 0000249 229
6584 130
4545 15
49293794 24329
Satellite: ISS
Catalog Number: 25544
Epoch time: 21011
63342823 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 37
0804 deg
Eccentricity:
0000249
Arg of perigee: 229
6584 deg
Mean anomaly: 130
4545 deg
Mean motion: 15
49293794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2432
Checksum: 288
Coasting Arc #13 (Orbit 2446)
---------------------------------------
Vector Time (GMT): 2021/012/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 956684
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5859742
21 A = 6803322
02 meter
Y = 3441273
58 meter E =
0011346
Z = -184651
48 I = 51
86925
XDOT = -2260
479557 Wp = 44
65684
YDOT = 4159
773216 meter/sec RA = 31
64679 deg
ZDOT = 6022
215215 TA = 313
36426
MA = 313
45873
Ha = 228
519 n
mi
Hp = 222
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19224876
01 X = 5821722
24
Y = 11290267
66 feet Y = 3506588
88 meter
Z = -605811
93 Z = -156279
63
XDOT = -7416
271511 XDOT = -2336
079198
YDOT = 13647
549921 feet/sec YDOT = 4134
071307 meter/sec
ZDOT = 19757
923933 ZDOT = 6011
051949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10200413
39 X = 3109086
00
Y = 19828254
37 feet Y = 6043651
93 meter
Z = -474241
50 Z = -144548
81
XDOT = -12237
974168 XDOT = -3730
134526
YDOT = 6743
696871 feet/sec YDOT = 2055
478806 meter/sec
ZDOT = 19705
858883 ZDOT = 6006
345788
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 21012
60097583
00016717 00000-0 10270-3 0 9124
2 25544 51
6413 32
2932 0000463 206
8412 153
2714 15
49323458 24473
Satellite: ISS
Catalog Number: 25544
Epoch time: 21012
60097583 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 32
2932 deg
Eccentricity:
0000463
Arg of perigee: 206
8412 deg
Mean anomaly: 153
2714 deg
Mean motion: 15
49323458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2447
Checksum: 281
Coasting Arc #14 (Orbit 2462)
---------------------------------------
Vector Time (GMT): 2021/013/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 956684
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6093883
43 A = 6803391
98 meter
Y = -3011233
95 meter E =
0011959
Z = 62771
94 I = 51
84074
XDOT = 2041
354493 Wp = 135
02474
YDOT = -4271
114488 meter/sec RA = 26
71161 deg
ZDOT = -6023
240040 TA = 44
30235
MA = 44
20670
Ha = 228
478 n
mi
Hp = 222
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19993055
86 X = -6060062
89
Y = -9879376
47 feet Y = -3079191
04 meter
Z = 205944
67 Z = 33252
81
XDOT = 6697
357262 XDOT = 2118
220307
YDOT = -14012
842807 feet/sec YDOT = -4247
856013 meter/sec
ZDOT = -19761
286219 ZDOT = -6013
138094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11927975
63 X = -3635646
97
Y = -18843710
04 feet Y = -5743562
82 meter
Z = 69026
41 Z = 21039
25
XDOT = 11755
340820 XDOT = 3583
027882
YDOT = -7538
111928 feet/sec YDOT = -2297
616516 meter/sec
ZDOT = -19714
142907 ZDOT = -6008
870758
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 21013
63302336
00016717 00000-0 10270-3 0 9134
2 25544 51
6423 27
1849 0000312 254
7284 105
3832 15
49303111 24637
Satellite: ISS
Catalog Number: 25544
Epoch time: 21013
63302336 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 27
1849 deg
Eccentricity:
0000312
Arg of perigee: 254
7284 deg
Mean anomaly: 105
3832 deg
Mean motion: 15
49303111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2463
Checksum: 265
Coasting Arc #15 (Orbit 2478)
---------------------------------------
Vector Time (GMT): 2021/014/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 956684
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6305010
64 A = 6803327
39 meter
Y = 2540471
99 meter E =
0011866
Z = 25718
54 I = 51
80991
XDOT = -1797
274163 Wp = 45
46568
YDOT = 4382
327877 meter/sec RA = 21
77541 deg
ZDOT = 6020
982929 TA = 314
81013
MA = 314
90653
Ha = 228
480 n
mi
Hp = 222
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20685730
43 X = 6276008
79
Y = 8334881
84 feet Y = 2610816
99 meter
Z = 84378
40 Z = 56274
70
XDOT = -5896
568776 XDOT = -1875
390691
YDOT = 14377
716132 feet/sec YDOT = 4361
792041 meter/sec
ZDOT = 19753
881001 ZDOT = 6012
063491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13627373
91 X = 4153623
57
Y = 17652772
09 feet Y = 5380564
93 meter
Z = 226133
46 Z = 68925
48
XDOT = -11189
364022 XDOT = -3410
518154
YDOT = 8358
607194 feet/sec YDOT = 2547
703473 meter/sec
ZDOT = 19712
224772 ZDOT = 6008
286111
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 21014
66506626
00016717 00000-0 10270-3 0 9147
2 25544 51
6424 22
0780 0000345 237
6526 122
4591 15
49324928 24799
Satellite: ISS
Catalog Number: 25544
Epoch time: 21014
66506626 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 22
0780 deg
Eccentricity:
0000345
Arg of perigee: 237
6526 deg
Mean anomaly: 122
4591 deg
Mean motion: 15
49324928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2479
Checksum: 300
Coasting Arc #16 (Orbit 2493)
---------------------------------------
Vector Time (GMT): 2021/015/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 956684
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6469491
08 A = 6803371
03 meter
Y = -2081927
53 meter E =
0011382
Z = -150893
83 I = 51
77815
XDOT = 1573
533908 Wp = 136
47863
YDOT = -4473
821342 meter/sec RA = 16
83665 deg
ZDOT = -6015
965234 TA = 45
14044
MA = 45
04804
Ha = 228
455 n
mi
Hp = 222
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21225364
43 X = -6444996
58
Y = -6830470
90 feet Y = -2154137
06 meter
Z = -495058
49 Z = -182259
77
XDOT = 5162
512820 XDOT = 1652
665784
YDOT = -14677
891541 feet/sec YDOT = -4455
782019 meter/sec
ZDOT = -19737
418748 ZDOT = -6008
130030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15135194
64 X = -4613207
33
Y = -16368629
64 feet Y = -4989158
32 meter
Z = -640591
63 Z = -195252
33
XDOT = 10628
047702 XDOT = 3239
428940
YDOT = -9083
795066 feet/sec YDOT = -2768
740736 meter/sec
ZDOT = -19700
796005 ZDOT = -6004
802622
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 21015
63260649
00016717 00000-0 10270-3 0 9158
2 25544 51
6427 17
2896 0000350 285
1065 75
0046 15
49304607 24945
Satellite: ISS
Catalog Number: 25544
Epoch time: 21015
63260649 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 17
2896 deg
Eccentricity:
0000350
Arg of perigee: 285
1065 deg
Mean anomaly: 75
0046 deg
Mean motion: 15
49304607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2494
Checksum: 297
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