FLOCK 4V 10, 46296 (Decayed)

Orbit data source: Space-Track

FLOCK 4V 10, 46296 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 10 details

Identifier	46296, 2020-061AA
Orbit	Decayed
Last TLE update	3 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 3 months ago

0 FLOCK 4V 10
1 46296U 20061AA  24253.44695939  .20275665  25456-5  25261-3 0  9990
2 46296  97.3164 330.9523 0014468 271.9790  87.9858 16.48873205223110

Epoch: 2024-09-09T10:43Z

Definitive object data (Epoch: 2024-09-09T10:43:37.291Z)

Latitude	0.00005°
Longitude	-178.9294°
Altitude	145.252 km
Speed	7.819 km/s
True Right ascension	22h 03m 48s
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	148.526 km
Perigee altitude	129.668 km
Semi-major axis	6,517.234 km
Eccentricity	0.0014468
Inclination	97.3164°
RAAN	330.9523°
Arg. of periapsis	271.979°
True anomaly	88.1515°
Mean anomaly	87.9858°
Eccentric anomaly	88.06865°
Mean motion	4.12523 °/min
BSTAR	0.00025261
Orbital period	87.27 mins