MAX VALIER SAT, 42778 (Decayed)

Orbit data source: Space-Track

MAX VALIER SAT, 42778 was an Italian payload satellite in LEO that was launched on Fri, 23 Jun 2017 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). 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

MAX VALIER SAT details

Identifier	42778, 2017-036P
Orbit	Decayed
Last TLE update	6 months ago
Origin	GOBBZ/GOBME (IT)
Manufacturer	Amat. Max Valier
Mission	Decayed Amateur Astronomy
Bus & Motor	MAXVALIER, Unknown motor
Mass	10 kg wet, 10 kg dry
Launch date (UTC)	2017-06-23 (8 years ago)
Launch vehicle	PSLV-XL
Launch site	Sirharikota (SRI)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 0.4 m
Radar Cross Section	0.120 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 6 months ago

0 MAX VALIER SAT
1 42778U 17036P   24181.51780098  .07500886  23432-5  86307-3 0  9999
2 42778  97.0566 220.7984 0007714 249.3707 110.6764 16.36858806391577

Epoch: 2024-06-29T12:25Z

Definitive object data (Epoch: 2024-06-29T12:25:38.004Z)

Latitude	-0.00011°
Longitude	116.31054°
Altitude	179.218 km
Speed	7.798 km/s
True Right ascension	14h 43m 11s
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	176.02 km
Perigee altitude	165.916 km
Semi-major axis	6,549.105 km
Eccentricity	0.0007714
Inclination	97.0566°
RAAN	220.7984°
Arg. of periapsis	249.3707°
True anomaly	110.75907°
Mean anomaly	110.6764°
Eccentric anomaly	110.71774°
Mean motion	4.09515 °/min
BSTAR	0.00086307
Orbital period	87.91 mins