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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Edit Public Description
Identifier
Orbit
Country
HU / HUNRelated business
Manufacturer
C3S
Mission
Operational spacecraft
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
24 kg wet, 24 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 MAUVE
1 66756U 25276CU 26034.46178645 .00008443 00000-0 41106-3 0 9992
2 66756 97.4349 110.3588 0003018 77.5320 282.6252 15.18614212 10122Epoch: 2026-02-03T11:04Z
TLE epoch observation values (Epoch: 2026-02-03T11:04:58.349Z)
Latitude
0.00001°
Longitude
170.4733°
Altitude
512.662 km
Speed
7.608 km/s
True Right ascension
07h 21m 26s
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
05:37:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.075 km
Perigee altitude
504.919 km
Semi-major axis
6,885.134 km
Eccentricity
0.0003
Inclination
97.4349°
RAAN
110.3588°
Arg. of periapsis
77.532°
True anomaly
282.59145°
Mean anomaly
282.6252°
Eccentric anomaly
282.60833°
Mean motion
3.79905 °/min
Orbital period
94.76 mins
BSTAR
0.00041106
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-04 04:36:41.360Z | 142.496° SSE | 2026-02-04 04:39:41.360Z | 67.532° E | 34.52° | 2026-02-04 04:42:41.360Z | 3.7° NNE |
| 6 mins | 2026-02-04 17:41:41.360Z | 18.227° NNE | 2026-02-04 17:44:41.360Z | 114.913° SE | 43.28° | 2026-02-04 17:47:41.360Z | 184.799° SSW |
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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