Showing default

HIBARI, 49400

Orbit data source: Space-Track

HIBARI, 49400 is a Japanese payload satellite in SSO that was launched on Tue, 09 Nov 2021 UTC via an EPSILON launch vehicle from the Kagoshima Space Center University Of Tokyo (KSCUT). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
49400, 2021-102F
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
TITech
Mission
Operational Amateur Technology
Bus & Motor
HIBARI, Unknown motor
Mass
55 kg wet, 55 kg dry
Launch date (UTC)
2021-11-09 (5 years ago)
Launch vehicle
EPSILON
Launch site
Kagoshima Space Center University Of Tokyo (KSCUT)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.499 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 HIBARI
1 49400U 21102F   26155.13525938  .00012043  00000-0  39817-3 0  9999
2 49400  97.3242 201.1894 0010087 242.0486 117.9735 15.31456330252196
Epoch: 2026-06-04T03:14Z
TLE epoch observation values (Epoch: 2026-06-04T03:14:46.410Z)
Latitude
-0.00002°
Longitude
-100.08784°
Altitude
477.822 km
Speed
7.625 km/s
True Right ascension
13h 24m 45s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
12:30:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.32 km
Perigee altitude
461.507 km
Semi-major axis
6,846.551 km
Eccentricity
0.00101
Inclination
97.3242°
RAAN
201.1894°
Arg. of periapsis
242.0486°
True anomaly
118.07552°
Mean anomaly
117.9735°
Eccentric anomaly
118.02452°
Mean motion
3.83121 °/min
Orbital period
93.97 mins
BSTAR
0.00039817
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|