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: 12 hours ago
TLE from 12 hours ago
0 MENUT
1 55010U 23001B 25335.83111025 .00039069 00000-0 99665-3 0 9991
2 55010 97.3541 35.5936 0007374 104.7379 255.4684 15.39383377161848Epoch: 2025-12-01T19:56Z
TLE epoch observation values (Epoch: 2025-12-01T19:56:47.925Z)
Latitude
-0.00007°
Longitude
25.46895°
Altitude
452.316 km
Speed
7.64 km/s
True Right ascension
02h 22m 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
06:07:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.901 km
Perigee altitude
439.838 km
Semi-major axis
6,823.006 km
Eccentricity
0.00074
Inclination
97.3541°
RAAN
35.5936°
Arg. of periapsis
104.7379°
True anomaly
255.38662°
Mean anomaly
255.4684°
Eccentric anomaly
255.42751°
Mean motion
3.85105 °/min
Orbital period
93.48 mins
BSTAR
0.00099665
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-02 16:47:03.519Z | 22.452° NNE | 2025-12-02 16:50:03.519Z | 103.176° ESE | 39.06° | 2025-12-02 16:53:03.519Z | 178.164° S |
| 4 mins | 2025-12-03 04:51:03.519Z | 224.366° SW | 2025-12-03 04:53:03.519Z | 278.358° WNW | 21.768° | 2025-12-03 04:55:03.519Z | 317.342° 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 descending 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 descending order |
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