NOKHCHO, 61767
Orbit data source: Space-Track
NOKHCHO, 61767 is a payload satellite owned by Chechen State U (CIS) in SSO 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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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Yugo-Zapad. GU
Mission
Operational 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: 10 hours ago
TLE from 10 hours ago
0 NOKHCHO
1 61767U 24199AJ 25312.84818223 .00206860 00000-0 19022-2 0 9999
2 61767 97.3152 186.2500 0004914 12.8892 347.2493 15.67020408100664Epoch: 2025-11-08T20:21Z
TLE epoch observation values (Epoch: 2025-11-08T20:21:22.944Z)
Latitude
-0.00008°
Longitude
-167.3675°
Altitude
367.357 km
Speed
7.691 km/s
True Right ascension
12h 25m 00s
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
02:08:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
367.647 km
Perigee altitude
361.021 km
Semi-major axis
6,742.471 km
Eccentricity
0.00049
Inclination
97.3152°
RAAN
186.25°
Arg. of periapsis
12.8892°
True anomaly
347.23686°
Mean anomaly
347.2493°
Eccentric anomaly
347.24308°
Mean motion
3.92026 °/min
Orbital period
91.83 mins
BSTAR
0.0019022
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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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| NOKHCHO is likely not visible in the next few days. |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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