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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 FLOCK 4G 32
1 62643U 25009AL 25260.77311753 .00032458 00000-0 13674-2 0 9991
2 62643 97.4191 339.6969 0002399 192.6262 167.4915 15.23271908 37359Epoch: 2025-09-17T18:33Z
TLE epoch observation values (Epoch: 2025-09-17T18:33:17.354Z)
Latitude
-0.00005°
Longitude
64.43034°
Altitude
500.684 km
Speed
7.613 km/s
True Right ascension
22h 38m 47s
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
08:54:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.59 km
Perigee altitude
491.293 km
Semi-major axis
6,871.078 km
Eccentricity
0.00024
Inclination
97.4191°
RAAN
339.6969°
Arg. of periapsis
192.6262°
True anomaly
167.49745°
Mean anomaly
167.4915°
Eccentric anomaly
167.49448°
Mean motion
3.81071 °/min
Orbital period
94.47 mins
BSTAR
0.0013674
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 18:46:11.306Z | 342.749° N | 2025-09-18 18:48:11.306Z | 296.297° NW | 28.054° | 2025-09-18 18:51:11.306Z | 227.085° WSW |
| 5 mins | 2025-09-19 05:23:11.306Z | 164.205° S | 2025-09-19 05:25:11.306Z | 2.048° NNE | 43.777° | 2025-09-19 05:28:11.306Z | 349.201° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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