[amsat-bb] Ten-Koh, PROITERES-2, DIWATA-2B, Stars-AO, AUTcube2 Launch info

Masahiro Arai m-arai at a.email.ne.jp
Sat Oct 27 17:11:02 UTC 2018


Five satellites which operate amateur band launch at 0408z 29th Oct by
H-IIA F40.
The satellites are Ten-Koh, PROITERES-2, DIWATA-2B, Stars-AO and
AUTcube2. They will separate around Antarctica and toward South
America.

Ten-Koh's web site shows its initial TLE as following. This will help
for chasing the satellites.
http://kit-okuyama-lab.com/%e3%81%a6%e3%82%93%e3%81%93%e3%81%86/ten-koh-orbital-infomation/

TENKOH STK sim
1 99999U          18302.19537037  .00000103  00000-0  98916-5 0 00009
2 99999 097.7878  44.6815 0022959 006.5055 234.0628 14.92980398000011



Ten-Koh
http://kit-okuyama-lab.com/%e3%81%a6%e3%82%93%e3%81%93%e3%81%86/ten-koh-orbital-infomation/
(in Japanese)

http://www.amsatuk.me.uk/iaru/finished_detail.php?serialnum=579
downlink 437.390MHz AFSK 1200bps, BPSK 9600bps, CW
          437.510MHz WSJT
uplink 435.280MHz


PROITERES-2
http://www.amsatuk.me.uk/iaru/finished_detail.php?serialnum=566
downlink 145.850MHz AFSK, CW
uplink 435.650MHz


DIWATA-2B
http://phl-microsat.upd.edu.ph/diwata2

http://www.amsatuk.me.uk/iaru/finished_detail.php?serialnum=593
downlink 145.900MHz FM Repeater, CW tlm, APRS, AFSK
uplink 437.500MHz FM Repeater


Stars-AO
http://stars.eng.shizuoka.ac.jp/starsao.html
https://stars-ao.info/
(in Japanese)

http://www.amsatuk.me.uk/iaru/finished_detail.php?serialnum=558
downlink 437.350MHz CW, 437.400MHz AFSK, 437.200MHz HighSpeed degital


AUTcube 2
http://www1.aut.ac.jp/~nishio-lab/AUTcube2/index_AUTcube2_E.html

http://www.amsatuk.me.uk/iaru/finished_detail.php?serialnum=575
downlink 437.385MHz AFSK 1200bps FSK 9600bps, 437.505MHz WSJT



Launch live broadcast by JAXA and MHI on YouTube from 0330z 29th Oct
https://www.youtube.com/watch?v=OAyL0VCf_L4
https://www.youtube.com/watch?v=42lrAkmBNvg



JAXA Special Website: Earth Observation Satellites
http://fanfun.jaxa.jp/eos/en/index.html



MHI Launch Services Twitter
https://twitter.com/MHI_LS



H-IIA F40 Launch Procedure

                 event                     T      altitude
                                        HH:MM:SS     km
--------------------------------------------------------
  1  liftoff                            00:00:00        0
  2  solid rocket booster burnout       00:01:48       42
  3  solid rocket booster separation    00:02:06       54
  4  upper fairing separtion            00:04:20      131
  5  1st stage main engine cuttoff      00:06:38      271
  6  1st/2nd stage separation           00:06:46      283
  7  2nd stage engine ignition          00:06:55      297
  8  2nd stage engine cuttoff           00:15:26      613
  9  Ibuki-2(GOSAT-2) separation        00:16:16      613
10  lower fairing (adapter) jettison   00:19:51      613
11  lower fairing (cylinder) jettison  00:19:56      613
12  KhalifaSat separation              00:24:21      616
13  Ten-Koh separation                 00:33:20      623
14  PROITERES-2 separation             00:38:20      624
15  DIWATA-2B separation               00:43:20      621
16  Stars-AO separation                00:48:20      614
17  AUTcube2 separation                00:51:00      610

    Source: Rocket Launch Plan  by JAXA and MHI  Aug 2018



Masa  JN1GKZ     Tokyo Japan



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