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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4G 22
1 62645U 25009AN 26275.45607607 .00006391 00000-0 21508-3 0 9994
2 62645 97.3939 357.0464 0000700 255.8291 104.2872 15.31136263 95327Epoch: 2026-10-02T10:56Z
TLE epoch observation values (Epoch: 2026-10-02T10:56:44.972Z)
Latitude
-0.00007°
Longitude
-178.31874°
Altitude
475.645 km
Speed
7.628 km/s
True Right ascension
23h 48m 11s
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
12:45:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.851 km
Perigee altitude
468.892 km
Semi-major axis
6,847.508 km
Eccentricity
0.00007
Inclination
97.3939°
RAAN
357.0464°
Arg. of periapsis
255.8291°
True anomaly
104.29497°
Mean anomaly
104.2872°
Eccentric anomaly
104.29109°
Mean motion
3.8304 °/min
Orbital period
93.98 mins
BSTAR
0.00021508
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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 | 2026-10-02 19:20:48.540Z | 331.574° NNW | 2026-10-02 19:22:48.540Z | 295.746° NW | 17.146° | 2026-10-02 19:24:48.540Z | 256.634° W |
| 5 mins | 2026-10-03 05:54:48.540Z | 198.474° SSW | 2026-10-03 05:56:48.540Z | 287.895° WNW | 46.52° | 2026-10-03 05:59:48.540Z | 337.257° NNW |
| 5 mins | 2026-10-03 18:52:48.540Z | 347.245° N | 2026-10-03 18:54:48.540Z | 298.941° NW | 36.772° | 2026-10-03 18:57:48.540Z | 221.924° SW |
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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