MENUT, 55010
Orbit data source: Space-Track
MENUT, 55010 is a Spanish payload satellite in SSO 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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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
Open Cosmos
Mission
Operational 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, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 MENUT
1 55010U 23001B 25286.94695616 .00036920 00000-0 10773-2 0 9996
2 55010 97.3616 346.6528 0004127 279.2845 80.7932 15.35239182154334Epoch: 2025-10-13T22:43Z
TLE epoch observation values (Epoch: 2025-10-13T22:43:37.012Z)
Latitude
0.00002°
Longitude
-16.99385°
Altitude
462.872 km
Speed
7.635 km/s
True Right ascension
23h 06m 36s
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
02:26:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.975 km
Perigee altitude
454.333 km
Semi-major axis
6,835.291 km
Eccentricity
0.00041
Inclination
97.3616°
RAAN
346.6528°
Arg. of periapsis
279.2845°
True anomaly
80.83989°
Mean anomaly
80.7932°
Eccentric anomaly
80.81654°
Mean motion
3.84068 °/min
Orbital period
93.73 mins
BSTAR
0.0010773
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-14 16:29:50.966Z | 33.358° NE | 2025-10-14 16:32:50.966Z | 104.739° ESE | 29.117° | 2025-10-14 16:34:50.966Z | 155.749° SSE |
| 4 mins | 2025-10-15 04:35:50.966Z | 216.703° SW | 2025-10-15 04:36:50.966Z | 250.396° W | 30.643° | 2025-10-15 04:39:50.966Z | 327.635° NNW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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