FLOCK 4X 16, 51020 (Decayed)
Orbit data source: Space-Track
FLOCK 4X 16, 51020 was a payload satellite owned by Planet (US) in LEO that was launched on Thu, 13 Jan 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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51020 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Decayed Commercial Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5.7 kg wet, 5.7 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.108 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 FLOCK 4X 16
1 51020U 22002AN 24291.22688389 .10603973 24536-5 26072-2 0 9991
2 51020 97.3564 12.0992 0010729 275.5924 84.4146 16.29125030154062Epoch: 2024-10-17T05:26Z
TLE epoch observation values (Epoch: 2024-10-17T05:26:42.768Z)
Latitude
-0.00001°
Longitude
-95.79299°
Altitude
197.451 km
Speed
7.788 km/s
True Right ascension
00h 48m 23s
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
10:53:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
198.761 km
Perigee altitude
184.663 km
Semi-major axis
6,569.849 km
Eccentricity
0.00107
Inclination
97.3564°
RAAN
12.0992°
Arg. of periapsis
275.5924°
True anomaly
84.53698°
Mean anomaly
84.4146°
Eccentric anomaly
84.47579°
Mean motion
4.07577 °/min
Orbital period
88.33 mins
BSTAR
0.0026072
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Other satellites on launch #2 in the year 2022 (2022-01-13 UTC)
FLOCK 4X 16 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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