FLOCK 4V 3, 46322 (Decayed)

Orbit data source: Space-Track

FLOCK 4V 3, 46322 was a payload satellite owned by Planet (US) in LEO that was launched on Thu, 03 Sep 2020 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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

FLOCK 4V 3 details

Identifier	46322, 2020-061BC
Orbit	Decayed
Last TLE update	8 months ago
Origin	Planet (US)
Manufacturer	Planet
Mission	Decayed Commercial Imaging
Bus & Motor	CUBESAT 3U, Unknown motor
Mass	5.7 kg wet, 5.7 kg dry
Launch date (UTC)	2020-09-03 (4 years ago)
Launch vehicle	VEGA
Launch site	French Guiana (FRGUI)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, 0.3 m
Radar Cross Section	0.108 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 8 months ago

0 FLOCK 4V 3
1 46322U 20061BC  24099.04543804  .15951235  26134-5  54385-3 0  9998
2 46322  97.3614 179.9181 0010348 234.0005 126.0338 16.43694821199618

Epoch: 2024-04-08T01:05Z

Definitive object data (Epoch: 2024-04-08T01:05:25.846Z)

Latitude	-0.00002°
Longitude	-33.23045°
Altitude	163.233 km
Speed	7.806 km/s
True Right ascension	11h 59m 40s
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	159.551 km
Perigee altitude	146.035 km
Semi-major axis	6,530.93 km
Eccentricity	0.0010348
Inclination	97.3614°
RAAN	179.9181°
Arg. of periapsis	234.0005°
True anomaly	126.12962°
Mean anomaly	126.0338°
Eccentric anomaly	126.08172°
Mean motion	4.11226 °/min
BSTAR	0.00054385
Orbital period	87.54 mins