MAUVE, 66756
Orbit data source: Space-Track
MAUVE, 66756 is a Hungarian payload satellite in SSO that was launched on Fri, 28 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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66756 intel report (Beta)
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Identifier
Orbit
Country
HU / HUNRelated business
Manufacturer
C3S
Mission
Operational Commercial Astronomy
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
24 kg wet, 24 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.124 m²
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 MAUVE
1 66756U 25276CU 26144.89491763 .00007505 00000-0 34853-3 0 9999
2 66756 97.4210 218.9950 0002853 68.4574 291.6965 15.20292460 26895Epoch: 2026-05-24T21:28Z
TLE epoch observation values (Epoch: 2026-05-24T21:28:40.883Z)
Latitude
-0.00002°
Longitude
14.33415°
Altitude
507.322 km
Speed
7.611 km/s
True Right ascension
14h 35m 58s
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
13:55:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.887 km
Perigee altitude
499.961 km
Semi-major axis
6,880.061 km
Eccentricity
0.00029
Inclination
97.421°
RAAN
218.995°
Arg. of periapsis
68.4574°
True anomaly
291.66612°
Mean anomaly
291.6965°
Eccentric anomaly
291.68131°
Mean motion
3.80325 °/min
Orbital period
94.66 mins
BSTAR
0.00034853
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Other satellites on launch #276 in the year 2025 (2025-11-28 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.MAUVE 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 | 2026-05-25 05:30:12.934Z | 202.111° SSW | 2026-05-25 05:33:12.934Z | 274.675° WNW | 28.202° | 2026-05-25 05:35:12.934Z | 319.305° NNW |
| 4 mins | 2026-05-25 18:35:12.934Z | 327.152° NNW | 2026-05-25 18:37:12.934Z | 281.502° WNW | 21.076° | 2026-05-25 18:39:12.934Z | 243.303° WSW |
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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