Showing default

ARASE (ERG), 41896

Orbit data source: Space-Track

ARASE (ERG), 41896 is a payload satellite owned by ISAS/JAXA (JP) in HEO that was launched on Tue, 20 Dec 2016 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
41896, 2016-080A
Orbit
HEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
ISAS/JAXA
Mission
Operational Civil Science
Bus & Motor
SPRINT-B, Unknown motor
Mass
350 kg wet, 350 kg dry
Launch date (UTC)
2016-12-20 (9 years ago)
Launch vehicle
EPSILON
Launch site
Kagoshima Space Center University Of Tokyo (KSCUT)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 4 Pan + 6 Ant, 3.0 m
Radar Cross Section
33.836 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 days ago

TLE from 5 days ago
0 ARASE (ERG)
1 41896U 16080A   25304.56911821  .00000267  00000-0  85404-3 0  9999
2 41896  31.4962  99.4016 6985551 267.7151  18.0074  2.57177406 82393
Epoch: 2025-10-31T13:39Z
TLE epoch observation values (Epoch: 2025-10-31T13:39:31.813Z)
Latitude
-0.00047°
Longitude
-145.64269°
Altitude
5,459.727 km
Speed
7.045 km/s
True Right ascension
06h 37m 24s
True Declination
0° 00' 02"
Sunlit
Object was in daylight 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
03:30:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
31,850.378 km
Perigee altitude
406.33 km
Semi-major axis
22,506.491 km
Eccentricity
0.69856
Inclination
31.4962°
RAAN
99.4016°
Arg. of periapsis
267.7151°
True anomaly
92.53453°
Mean anomaly
18.0074°
Eccentric anomaly
47.53101°
Mean motion
0.64281 °/min
Orbital period
560.04 mins
BSTAR
0.00085404
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...
Other satellites on launch #80 in the year 2016 (2016-12-20 UTC)

Documentation

Showing up to 5 results
|