OPS-SAT, 44878 (Decayed)

Orbit data source: Space-Track

OPS-SAT, 44878 was a payload satellite owned by ESA (ESA) in LEO that was launched on Wed, 18 Dec 2019 UTC via a SOYUZ-ST-A 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

OPS-SAT details

Identifier	44878, 2019-092F
Orbit	Decayed
Last TLE update	7 months ago
Origin	ESA (ESA)
Manufacturer	TUG/GOMSP
Mission	Decayed Civil Technology
Bus & Motor	CUBESAT 3U, Unknown motor
Mass	7 kg wet, 7 kg dry
Launch date (UTC)	2019-12-18 (5 years ago)
Launch vehicle	SOYUZ-ST-A
Launch site	French Guiana (FRGUI)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, 0.5 m
Radar Cross Section	0.048 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 7 months ago

0 OPS-SAT
1 44878U 19092F   24143.84045348  .17176592  26004-5  26698-3 0  9991
2 44878  97.4081 350.0941 0014332 258.8962 101.0730 16.47500343246598

Epoch: 2024-05-22T20:10Z

Definitive object data (Epoch: 2024-05-22T20:10:15.18Z)

Latitude	-0.00003°
Longitude	166.58791°
Altitude	150.996 km
Speed	7.814 km/s
True Right ascension	23h 20m 22s
True Declination	0° 00' 00"
Sunlit	Object was in daylight 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	152.07 km
Perigee altitude	133.379 km
Semi-major axis	6,520.861 km
Eccentricity	0.0014332
Inclination	97.4081°
RAAN	350.0941°
Arg. of periapsis	258.8962°
True anomaly	101.23412°
Mean anomaly	101.073°
Eccentric anomaly	101.15357°
Mean motion	4.12179 °/min
BSTAR	0.00026698
Orbital period	87.34 mins