FLOCK 4G 32, 62643
Orbit data source: Space-Track
FLOCK 4G 32, 62643 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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62643 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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 32
1 62643U 25009AL 25322.17203569 .00057497 00000-0 18895-2 0 9999
2 62643 97.4130 40.6957 0000898 337.4943 22.6258 15.31346341 46721Epoch: 2025-11-18T04:07Z
TLE epoch observation values (Epoch: 2025-11-18T04:07:43.883Z)
Latitude
-0.0001°
Longitude
-78.69907°
Altitude
474.332 km
Speed
7.629 km/s
True Right ascension
02h 42m 46s
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
02:16:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.36 km
Perigee altitude
468.131 km
Semi-major axis
6,846.882 km
Eccentricity
0.00009
Inclination
97.413°
RAAN
40.6957°
Arg. of periapsis
337.4943°
True anomaly
22.62976°
Mean anomaly
22.6258°
Eccentric anomaly
22.62778°
Mean motion
3.83093 °/min
Orbital period
93.97 mins
BSTAR
0.0018895
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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 32 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 | 2025-11-19 05:23:01.096Z | 149.19° SSE | 2025-11-19 05:24:01.096Z | 28.858° NE | 43.415° | 2025-11-19 05:27:01.096Z | 351.357° N |
| 5 mins | 2025-11-19 18:20:01.096Z | 8.027° NNE | 2025-11-19 18:22:01.096Z | 341.076° N | 43.323° | 2025-11-19 18:25:01.096Z | 197.496° SSW |
| 4 mins | 2025-11-20 04:54:01.096Z | 113.105° SE | 2025-11-20 04:55:01.096Z | 85.936° E | 26.098° | 2025-11-20 04:58:01.096Z | 13.888° NNE |
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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