[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: January 10th 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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