CHOMPTT, 43855 (Decayed)

Orbit data source: Space-Track

CHOMPTT, 43855 was a payload satellite owned by UFla (US) in LEO that was launched on Sun, 16 Dec 2018 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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

CHOMPTT details

Identifier	43855, 2018-104G
Orbit	Decayed
Last TLE update	7 months ago
Origin	UFla (US)
Manufacturer	UFla
Mission	Decayed Amateur Technology
Bus & Motor	CUBESAT 3U, Unknown motor
Mass	3.59 kg wet, 3.59 kg dry
Launch date (UTC)	2018-12-16 (6 years ago)
Launch vehicle	ELECTRON
Launch site	Rocket Lab Launch Complex (RLLC)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 0.3 m
Radar Cross Section	0.035 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 7 months ago

0 CHOMPTT
1 43855U 18104G   24134.35325181  .12320967 -15037-5  27872-3 0  9992
2 43855  84.9866 294.2530 0011178 259.2513 100.7537 16.45723631302149

Epoch: 2024-05-13T08:28Z

Definitive object data (Epoch: 2024-05-13T08:28:40.956Z)

Latitude	-0.00003°
Longitude	-64.50956°
Altitude	155.31 km
Speed	7.812 km/s
True Right ascension	19h 37m 00s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow 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	154.625 km
Perigee altitude	140.036 km
Semi-major axis	6,525.468 km
Eccentricity	0.0011178
Inclination	84.9866°
RAAN	294.253°
Arg. of periapsis	259.2513°
True anomaly	100.87951°
Mean anomaly	100.7537°
Eccentric anomaly	100.81661°
Mean motion	4.11743 °/min
BSTAR	0.00027872
Orbital period	87.43 mins