FLOCK 4G 22, 62645
Orbit data source: Space-Track
FLOCK 4G 22, 62645 is a payload satellite owned by Planet (US) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62645 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Operational 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, 1.0 m
Radar Cross Section
0.072 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4G 22
1 62645U 25009AN 25300.20825599 .00010014 00000-0 41919-3 0 9992
2 62645 97.4218 19.0171 0003420 64.1733 295.9857 15.23751181 43374Epoch: 2025-10-27T04:59Z
TLE epoch observation values (Epoch: 2025-10-27T04:59:53.317Z)
Latitude
0.00002°
Longitude
-91.76846°
Altitude
496.603 km
Speed
7.617 km/s
True Right ascension
01h 16m 04s
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
22:24:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.849 km
Perigee altitude
489.15 km
Semi-major axis
6,869.636 km
Eccentricity
0.00034
Inclination
97.4218°
RAAN
19.0171°
Arg. of periapsis
64.1733°
True anomaly
295.95047°
Mean anomaly
295.9857°
Eccentric anomaly
295.96808°
Mean motion
3.81191 °/min
Orbital period
94.44 mins
BSTAR
0.00041919
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.FLOCK 4G 22 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-28 04:46:53.867Z | 124.454° SE | 2025-10-28 04:49:53.867Z | 57.106° ENE | 23.544° | 2025-10-28 04:51:53.867Z | 18.565° NNE |
| 5 mins | 2025-10-28 17:49:53.867Z | 43.689° NE | 2025-10-28 17:51:53.867Z | 105.864° ESE | 31.316° | 2025-10-28 17:54:53.867Z | 166.562° S |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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