FLOCK 4V 6, 46289 (Decayed)

Orbit data source: Space-Track

FLOCK 4V 6, 46289 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 6 details

Identifier	46289, 2020-061T
Orbit	Decayed
Last TLE update	4 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, Small (<0.1 m²)

Expand to show TLE details & history

TLE from 4 months ago

0 FLOCK 4V 6
1 46289U 20061T   24245.47483942  .15360631  25244-5  53278-3 0  9991
2 46289  97.3305 321.8066 0013098 267.7691  92.2111 16.43243854221835

Epoch: 2024-09-01T11:23Z

Definitive object data (Epoch: 2024-09-01T11:23:46.125Z)

Latitude	-0.00001°
Longitude	169.7458°
Altitude	160.787 km
Speed	7.809 km/s
True Right ascension	21h 27m 13s
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	162.544 km
Perigee altitude	145.432 km
Semi-major axis	6,532.125 km
Eccentricity	0.0013098
Inclination	97.3305°
RAAN	321.8066°
Arg. of periapsis	267.7691°
True anomaly	92.36107°
Mean anomaly	92.2111°
Eccentric anomaly	92.28609°
Mean motion	4.11113 °/min
BSTAR	0.00053278
Orbital period	87.57 mins