CNCE4, 52767 (Decayed)
Orbit data source: Space-Track
CNCE4, 52767 was a payload satellite owned by MDA (US) in LEO that was launched on Wed, 25 May 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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52767 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
1 year ago
Origin
Manufacturer
AFRL?
Mission
Decayed Defense Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 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 & history
TLE from 1 year ago
0 CNCE4
1 52767U 22057AM 24109.88813878 .10686156 26072-5 11827-2 0 9996
2 52767 97.5206 246.2159 0012945 266.9407 93.0409 16.36988063106239Epoch: 2024-04-18T21:18Z
TLE epoch observation values (Epoch: 2024-04-18T21:18:55.19Z)
Latitude
-0.00005°
Longitude
79.00801°
Altitude
177.532 km
Speed
7.799 km/s
True Right ascension
16h 24m 51s
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
13:21:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
179.121 km
Perigee altitude
162.167 km
Semi-major axis
6,548.781 km
Eccentricity
0.00129
Inclination
97.5206°
RAAN
246.2159°
Arg. of periapsis
266.9407°
True anomaly
93.18902°
Mean anomaly
93.0409°
Eccentric anomaly
93.11496°
Mean motion
4.09546 °/min
Orbital period
87.9 mins
BSTAR
0.0011827
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Other satellites on launch #57 in the year 2022 (2022-05-25 UTC)
CNCE4 Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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