Ten-Koh Orbital infomation

TEN-KOH Orbital Information

Satellite Name: Ten-Koh

Callsign: JG6YKY

Launch Information:

  1. Launch Vehicle: H-IIA launch vehicle No.40 (H-IIA F40)
  2. Launch Date: 29th October 2018 (Monday)
  3. Launch time (Japan Standard Time (JST)): between 13:08 and 13:20
  4. Launch time (Universal Time Coordinated (UTC)): between 04:08 and 04:20
  5. Tenkoh separation coordinate: latitude -60°N, longitude 110°E

Table 1: Tenkoh Launch and Separation Time Range

 

JST

UTC

Launch Time

13:08:00

13:20:00

04:08:00

04:20:00

Tenkoh Separation Time

13:41:20

13:53:20

04:41:20

04:53:20

Orbital Parameters:

Table 2: Orbital Elements for Tenkoh

Orbital Element

Value

Inclination [deg]

97.835

Right Ascension of the Ascending Node (RAAN) [deg]

44.6815

Argument of perigee [deg]

27.546

Semi-major axis [km]

6,969.772

True anomaly [deg]

212.990

Eccentricity [-]

0.002586

Initial Pass Prediction:

  1. Tenkoh first week pass prediction - click here for details (PDF)
  2. Tenkoh ground station antenna azimuth, elevation and tracking range prediction (JST) - click here for details (PDF)
  3. Tenkoh ground station antenna azimuth, elevation and tracking range prediction (UTC) - click here for details (PDF)

Two Line Element (TLE) Data (Last updated 2018/9/20):

Tenkoh Initial TLE

Ten-Koh Real-Time Location

 

Note : The actual TLE will be updated upon confirmation from NORAD

Downlink Frequency: CW- 437.39 MHz

Copyright © 奥山 圭一 研究室 All Rights Reserved.