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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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, 1.0 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 MENUT
1 55010U 23001B 26115.51905436 .00061699 00000-0 95121-3 0 9997
2 55010 97.3200 182.0801 0002877 301.2987 58.7985 15.53962695184206Epoch: 2026-04-25T12:27Z
TLE epoch observation values (Epoch: 2026-04-25T12:27:26.296Z)
Latitude
-0.00002°
Longitude
141.68427°
Altitude
407.298 km
Speed
7.667 km/s
True Right ascension
12h 08m 19s
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
03:04:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
404.037 km
Perigee altitude
400.136 km
Semi-major axis
6,780.224 km
Eccentricity
0.00029
Inclination
97.32°
RAAN
182.0801°
Arg. of periapsis
301.2987°
True anomaly
58.8267°
Mean anomaly
58.7985°
Eccentric anomaly
58.8126°
Mean motion
3.88756 °/min
Orbital period
92.6 mins
BSTAR
0.00095121
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-26 04:03:14.263Z | 134.171° SE | 2026-04-26 04:05:14.263Z | 78.663° E | 29.687° | 2026-04-26 04:07:14.263Z | 15.85° NNE |
| 4 mins | 2026-04-26 16:51:14.263Z | 50.57° ENE | 2026-04-26 16:52:14.263Z | 80.603° E | 27.187° | 2026-04-26 16:55:14.263Z | 162.005° S |
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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