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: 14 hours ago
TLE from 14 hours ago
0 FLOCK 4G 32
1 62643U 25009AL 25300.64965029 .00050795 00000-0 18433-2 0 9995
2 62643 97.4134 19.2365 0001082 109.9067 250.2289 15.28149100 43433Epoch: 2025-10-27T15:35Z
TLE epoch observation values (Epoch: 2025-10-27T15:35:29.785Z)
Latitude
-0.00001°
Longitude
109.11394°
Altitude
484.698 km
Speed
7.623 km/s
True Right ascension
01h 16m 56s
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
01:21:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.043 km
Perigee altitude
477.559 km
Semi-major axis
6,856.438 km
Eccentricity
0.00011
Inclination
97.4134°
RAAN
19.2365°
Arg. of periapsis
109.9067°
True anomaly
250.21723°
Mean anomaly
250.2289°
Eccentric anomaly
250.22307°
Mean motion
3.82292 °/min
Orbital period
94.17 mins
BSTAR
0.0018433
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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 | 2025-10-28 18:52:46.779Z | 331.503° NNW | 2025-10-28 18:54:46.779Z | 278.235° WNW | 24.447° | 2025-10-28 18:56:46.779Z | 236.139° WSW |
| 5 mins | 2025-10-29 05:26:46.779Z | 169.191° S | 2025-10-29 05:28:46.779Z | 195.428° SSW | 44.731° | 2025-10-29 05:31:46.779Z | 346.907° 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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