RAPIS-1, 43932 (Decayed)

Orbit data source: Space-Track

RAPIS-1, 43932 was a payload satellite owned by JAXA (JP) in LEO that was launched on Fri, 18 Jan 2019 UTC via an EPSILON launch vehicle from the Kagoshima Space Center University Of Tokyo (KSCUT). Payloads include a variety of satellites, spacecraft, and rockets 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.

Not visible in the next 10 days

RAPIS-1 details

Identifier	43932, 2019-003A
Orbit	Decayed
Last TLE update	3 months ago
Origin	JAXA (JP / JPN)
Manufacturer	JAXA
Mission	Decayed Civil Technology
Bus & Motor	RAPIS, Unknown motor
Mass	200 kg wet, 200 kg dry
Launch date (UTC)	2019-01-18 (6 years ago)
Launch vehicle	EPSILON
Launch site	Kagoshima Space Center University Of Tokyo (KSCUT)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 1 Pan, 2.5 m
Radar Cross Section	1.908 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 3 months ago

0 RAPIS-1
1 43932U 19003A   24269.25296083  .15421290  24407-5  12290-2 0  9994
2 43932  97.1655 259.2580 0008766 254.9296 123.1605 16.40055852315048

Epoch: 2024-09-25T06:04Z

Definitive object data (Epoch: 2024-09-25T06:04:15.815Z)

Latitude	18.01874°
Longitude	161.30645°
Altitude	171.467 km
Speed	7.803 km/s
True Right ascension	17h 07m 42s
True Declination	17° 54' 32"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	168.185 km
Perigee altitude	156.718 km
Semi-major axis	6,540.588 km
Eccentricity	0.0008766
Inclination	97.1655°
RAAN	259.258°
Arg. of periapsis	254.9296°
True anomaly	123.24454°
Mean anomaly	123.1605°
Eccentric anomaly	123.20253°
Mean motion	4.10316 °/min
BSTAR	0.001229
Orbital period	87.74 mins