LUNA-1, 66777
Orbit data source: Space-Track
LUNA-1, 66777 is a payload satellite owned by Aselsan (TR) 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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66777 intel report (Beta)
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Identifier
Orbit
Country
TR / TURKRelated business
Manufacturer
Aselsan
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U?, Unknown motor
Mass
~12 kg wet, ~12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m²
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LUNA-1
1 66777U 25276DR 26063.17608826 .00015180 00000-0 69351-3 0 9992
2 66777 97.4346 138.8371 0001628 193.4130 166.7063 15.20666184 14493Epoch: 2026-03-04T04:13Z
TLE epoch observation values (Epoch: 2026-03-04T04:13:34.025Z)
Latitude
0.00002°
Longitude
-86.49923°
Altitude
508.011 km
Speed
7.609 km/s
True Right ascension
09h 15m 20s
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
09:04:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.916 km
Perigee altitude
499.676 km
Semi-major axis
6,878.933 km
Eccentricity
0.00016
Inclination
97.4346°
RAAN
138.8371°
Arg. of periapsis
193.413°
True anomaly
166.71059°
Mean anomaly
166.7063°
Eccentric anomaly
166.70844°
Mean motion
3.80418 °/min
Orbital period
94.63 mins
BSTAR
0.00069351
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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.LUNA-1 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 | 2026-03-05 05:37:36.438Z | 211.193° SW | 2026-03-05 05:39:36.438Z | 253.663° W | 25.09° | 2026-03-05 05:42:36.438Z | 319.678° NNW |
| 4 mins | 2026-03-05 17:08:36.438Z | 62.434° ENE | 2026-03-05 17:09:36.438Z | 85.273° E | 21.611° | 2026-03-05 17:12:36.438Z | 146.982° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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