NOKHCHO, 61767 (Decayed)
Orbit data source: Space-Track
NOKHCHO, 61767 was a payload satellite owned by Chechen State U (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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61767 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Yugo-Zapad. GU
Mission
Decayed Amateur Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
2.5 kg wet, 2.5 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 NOKHCHO
1 61767U 24199AJ 25363.38690139 .10165052 24539-5 11813-2 0 9994
2 61767 97.2732 240.1382 0004854 95.9620 264.2231 16.36835873108662Epoch: 2025-12-29T09:17Z
TLE epoch observation values (Epoch: 2025-12-29T09:17:08.280Z)
Latitude
-0.00004°
Longitude
2.76844°
Altitude
177.806 km
Speed
7.799 km/s
True Right ascension
16h 00m 33s
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
07:12:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
174.218 km
Perigee altitude
167.86 km
Semi-major axis
6,549.176 km
Eccentricity
0.00049
Inclination
97.2732°
RAAN
240.1382°
Arg. of periapsis
95.962°
True anomaly
264.16776°
Mean anomaly
264.2231°
Eccentric anomaly
264.19543°
Mean motion
4.09509 °/min
Orbital period
87.91 mins
BSTAR
0.0011813
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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.NOKHCHO 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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