AALTO 1, 42775 (Decayed)

Orbit data source: Space-Track

AALTO 1, 42775 was a payload satellite owned by Aalto univ. (FI) 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.

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Identifier	42775, 2017-036L
Orbit	Decayed
Last TLE update	7 months ago
Origin	Aalto univ. (FIN)
Manufacturer	Aalto univ.
Mission	Decayed Amateur Sci/Tech
Bus & Motor	CUBESAT 3U, Unknown motor
Mass	3.9 kg wet, 3.9 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, 0.3 m
Radar Cross Section	0.035 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 7 months ago

0 AALTO 1
1 42775U 17036L   24245.29764800  .13343114  24078-5  23541-3 0  9999
2 42775  97.0675 277.5924 0011337 248.5174 111.4922 16.47090026401159

Epoch: 2024-09-01T07:08Z

Definitive object data (Epoch: 2024-09-01T07:08:36.787Z)

Latitude	0.00003°
Longitude	-170.50485°
Altitude	152.998 km
Speed	7.813 km/s
True Right ascension	18h 30m 22s
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	151.187 km
Perigee altitude	136.4 km
Semi-major axis	6,521.93 km
Eccentricity	0.0011337
Inclination	97.0675°
RAAN	277.5924°
Arg. of periapsis	248.5174°
True anomaly	111.61302°
Mean anomaly	111.4922°
Eccentric anomaly	111.55261°
Mean motion	4.12078 °/min
BSTAR	0.00023541
Orbital period	87.36 mins