[amsat-bb] preliminary TLE data for NEXUS sat (jan-17)

[Akira Kaneko]

Dear Jarda san,
Thanks your support.
Preliminary TLE update.
NEXUS
1 99999U 99999A   19017.08240741 0.00000000  00000-0  00000-0 0  9994
2 99999  97.2200  79.6000 0014000 196.1000 199.2528 15.22513194    00
http://sat.aero.cst.nihon-u.ac.jp/nexus/E2_ini.html

JA1OGZ Akira

Sent from iPad 金子明
ja1ogz at jcom.home.ne.jp
ja1ogz at jarl.com

2019/01/10 20:14、ok2gz <ok2gz at seznam.cz>のメール:

> Nexus cubesat will be launched on January 17, 2019.
> In document <a href="http://sat.aero.cst.nihon-u.ac.jp/nexus/download/About_initial_operation_immediately_after_separation_e.pdf">About_initial_operation_immediately_after_separation_e.pdf</a> from ANS-006 AMSAT NEWS SERVICE
>    are given the preliminary TLE data.
> 
> NEXUS
> 1 99999U 99999A 19017.08394676 0.00000000 00000-0 00000-0 0 9991
> 2 99999 97.2400 80.2200 0010290 211.2310 184.0310 15.23623214 09
> 
> 
> The TLE data depends on the exact positions of each item. Positions are compromised when copying documents.
> Such damaged TLE data are not in sat programs as GPredict) processed.
> 
> The repair is simple. Just compare the positions of dots and dashes in TLE data  and move items to the correct positions.
> 
> Already for FOX-1D I wrote a TLEdoctor program that can display flawed positions and can easily be corrected by comparing with the template.  After repair,  GPredict data can be uploaded and we can take all advantages of our sat program during the first pass.
> 
> TLE doctor:  http://oscar.ok2gz.eu/fox1d.php
> 
> Yet planned orbit params for NEXUS
> 
> period: 94.515 min
> apogeum : 502.1 km
> perigeum: 489.0 km
> max qso length:  4904 km
> inclination: 97.24 degrees
> 
> 73  jarda ok2gz
> 
> 
> 
> 
> ---
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