TEN-KOH Orbital Information
Two Line Element (TLE) Data (Last updated 2019/2/28):
Launch Information:
- Launch Vehicle: H-IIA launch vehicle No.40 (H-IIA F40)
- Launch Date: 29th October 2018 (Monday)
- Launch time (Japan Standard Time (JST)): between 13:08 and 13:20
- Launch time (Universal Time Coordinated (UTC)): between 04:08 and 04:20
- 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 for Kyutech ground station: