PROXIMA I, 43694 (Decayed)

Orbit data source: Space-Track

PROXIMA I, 43694 was a payload satellite owned by Fleet Space (AU) in LEO that was launched on Sun, 11 Nov 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

PROXIMA I details

Identifier	43694, 2018-088E
Orbit	Decayed
Last TLE update	7 months ago
Origin	Fleet Space (AU / AUS)
Manufacturer	Fleet Space
Mission	Decayed Commercial Communications
Bus & Motor	CUBESAT 1.5U, Unknown motor
Mass	2 kg wet, 2 kg dry
Launch date (UTC)	2018-11-11 (6 years ago)
Launch vehicle	ELECTRON
Launch site	Rocket Lab Launch Complex (RLLC)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 0.15 m
Radar Cross Section	0.026 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 7 months ago

0 PROXIMA I
1 43694U 18088E   24139.06678571  .11242035 -15002-5  41498-3 0  9991
2 43694  84.9859 193.3122 0011906 260.3583  99.6379 16.43111434308020

Epoch: 2024-05-18T01:36Z

Definitive object data (Epoch: 2024-05-18T01:36:10.285Z)

Latitude	-0.00002°
Longitude	-66.96845°
Altitude	162.167 km
Speed	7.808 km/s
True Right ascension	12h 53m 14s
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	162.029 km
Perigee altitude	146.474 km
Semi-major axis	6,532.389 km
Eccentricity	0.0011906
Inclination	84.9859°
RAAN	193.3122°
Arg. of periapsis	260.3583°
True anomaly	99.77237°
Mean anomaly	99.6379°
Eccentric anomaly	99.70514°
Mean motion	4.11088 °/min
BSTAR	0.00041498
Orbital period	87.57 mins