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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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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4G 22
1 62645U 25009AN 26140.20202024 .00007076 00000-0 25658-3 0 9993
2 62645 97.4007 222.3654 0003295 65.6351 294.5232 15.28656131 74647Epoch: 2026-05-20T04:50Z
TLE epoch observation values (Epoch: 2026-05-20T04:50:54.548Z)
Latitude
-0.00009°
Longitude
-88.22684°
Altitude
481.993 km
Speed
7.625 km/s
True Right ascension
14h 49m 27s
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
07:13:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.041 km
Perigee altitude
474.524 km
Semi-major axis
6,854.92 km
Eccentricity
0.00033
Inclination
97.4007°
RAAN
222.3654°
Arg. of periapsis
65.6351°
True anomaly
294.48884°
Mean anomaly
294.5232°
Eccentric anomaly
294.50602°
Mean motion
3.82419 °/min
Orbital period
94.14 mins
BSTAR
0.00025658
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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 | 2026-05-21 06:07:31.624Z | 217.684° SW | 2026-05-21 06:09:31.624Z | 270.624° WNW | 24.929° | 2026-05-21 06:11:31.624Z | 315.343° NNW |
| 4 mins | 2026-05-21 19:07:31.624Z | 324.458° NNW | 2026-05-21 19:09:31.624Z | 277.461° WNW | 19.801° | 2026-05-21 19:11:31.624Z | 241.349° WSW |
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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