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). Payload-class satellites include a variety of spacecraft 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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42775 intel report (Beta)
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AALTO 1 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
FI / FINRelated business
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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year 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 16.47090026401159Epoch: 2024-09-01T07:08Z
TLE epoch observation values (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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:55:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
151.187 km
Perigee altitude
136.4 km
Semi-major axis
6,521.93 km
Eccentricity
0.00113
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
Orbital period
87.36 mins
BSTAR
0.00023541
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Other satellites on launch #36 in the year 2017 (2017-06-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.AALTO 1 Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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