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: 2 days ago
TLE from 2 days ago
0 FLOCK 4G 22
1 62645U 25009AN 25306.18389020 .00011717 00000-0 48761-3 0 9992
2 62645 97.4223 24.9294 0002985 47.9688 312.1803 15.23909390 44285Epoch: 2025-11-02T04:24Z
TLE epoch observation values (Epoch: 2025-11-02T04:24:48.113Z)
Latitude
0°
Longitude
-82.97434°
Altitude
495.78 km
Speed
7.618 km/s
True Right ascension
01h 39m 43s
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
13:05:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.074 km
Perigee altitude
488.973 km
Semi-major axis
6,869.161 km
Eccentricity
0.0003
Inclination
97.4223°
RAAN
24.9294°
Arg. of periapsis
47.9688°
True anomaly
312.15495°
Mean anomaly
312.1803°
Eccentric anomaly
312.16762°
Mean motion
3.81231 °/min
Orbital period
94.43 mins
BSTAR
0.00048761
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-03 18:48:51.746Z | 330.374° NNW | 2025-11-03 18:49:51.746Z | 303.351° NW | 27.528° | 2025-11-03 18:52:51.746Z | 228.924° WSW |
| 5 mins | 2025-11-04 05:24:51.746Z | 163.664° S | 2025-11-04 05:26:51.746Z | 2.486° NNE | 43.444° | 2025-11-04 05:29:51.746Z | 349.365° N |
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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