MENUT, 55010
Orbit data source: Space-Track
MENUT, 55010 is a Spanish payload satellite in LEO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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55010 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
Open Cosmos
Mission
Decayed Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 MENUT
1 55010U 23001B 26310.24323021 .04422235 23781-5 14667-2 0 9990
2 55010 97.2703 25.5733 0008305 286.0439 73.9939 16.25806641214763Epoch: 2026-11-06T05:50Z
TLE epoch observation values (Epoch: 2026-11-06T05:50:15.090Z)
Latitude
0.00006°
Longitude
-107.45522°
Altitude
205.566 km
Speed
7.784 km/s
True Right ascension
01h 42m 17s
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
23:36:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
206.117 km
Perigee altitude
195.19 km
Semi-major axis
6,578.791 km
Eccentricity
0.00083
Inclination
97.2703°
RAAN
25.5733°
Arg. of periapsis
286.0439°
True anomaly
74.0854°
Mean anomaly
73.9939°
Eccentric anomaly
74.03965°
Mean motion
4.06747 °/min
Orbital period
88.51 mins
BSTAR
0.0014667
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Other satellites on launch #1 in the year 2023 (2023-01-03 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.MENUT 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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| MENUT is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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