Satellite description

EPSILON R/B, 41897 is space debris in HEO originally from a launch on Tue, 20 Dec 2016 UTC launched from the Kagoshima Space Center University Of Tokyo (KSCUT). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

Satellite metadata
Identifier
41897, 2016-080B
Orbit
HEO
Last TLE update
16 hours ago
Origin
Flag of JPISASJ (JP / JPN)
Manufacturer
IHI Ogikubo
Mission
Spacecraft
Bus & Motor
KM-V, Unknown motor
Mass
~400 kg wet, ~400 kg dry
Launch date (UTC)
2016-12-20 (8 years ago)
Launch vehicle
Unknown
Launch site
Kagoshima Space Center University Of Tokyo (KSCUT)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 2.2 m
Radar Cross Section
3.189 m², Large (>1 m²)
Visualization TLE readout
Latitude
-30.53719°
Longitude
101.64627°
Altitude
14,081.021 km
Speed
3.231 km/s
Apparent Right ascension
09h 24m 24s
Apparent Declination
-46° 02' 37"
Sunlit
Object is in daylight
Orbital elements
Apogee altitude
14,997.972 km
Perigee altitude
191.361 km
Semi-major axis
13,972.803 km
Eccentricity
0.5298368
Inclination
31.1931°
RAAN
230.0757°
Arg. of periapsis
116.6794°
True anomaly
243.36951°
Mean anomaly
306.3265°
Eccentric anomaly
276.14343°
Mean motion
1.31407 °/min
BSTAR
0.0010355
Orbital period
273.96 mins
41897, EPSILON R/B
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