RUZAEVKA-390, 61766 (Decayed)
Orbit data source: Space-Track
RUZAEVKA-390, 61766 was a payload satellite owned by Saransk PT (CIS) in LEO that was launched on Mon, 04 Nov 2024 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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61766 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Yugo-Zapad. GU
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 RUZAEVKA-390
1 61766U 24199AH 26069.38481491 .11440096 25250-5 56352-3 0 9990
2 61766 97.2628 311.9876 0007678 247.6224 112.4264 16.42346068119643Epoch: 2026-03-10T09:14Z
TLE epoch observation values (Epoch: 2026-03-10T09:14:08.008Z)
Latitude
0.00001°
Longitude
5.39006°
Altitude
164.746 km
Speed
7.806 km/s
True Right ascension
20h 47m 57s
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
19:46:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.385 km
Perigee altitude
151.35 km
Semi-major axis
6,534.504 km
Eccentricity
0.00077
Inclination
97.2628°
RAAN
311.9876°
Arg. of periapsis
247.6224°
True anomaly
112.5077°
Mean anomaly
112.4264°
Eccentric anomaly
112.46705°
Mean motion
4.10889 °/min
Orbital period
87.61 mins
BSTAR
0.00056352
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Other satellites on launch #199 in the year 2024 (2024-11-04 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.RUZAEVKA-390 Visibility
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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. |
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| This satellite is decayed. |
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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