FLOCK 4G 31, 62652
Orbit data source: Space-Track
FLOCK 4G 31, 62652 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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62652 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: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4G 31
1 62652U 25009AV 25300.69408996 .00010877 00000-0 45982-3 0 9992
2 62652 97.4178 19.2800 0002814 84.5805 275.5753 15.23395818 43448Epoch: 2025-10-27T16:39Z
TLE epoch observation values (Epoch: 2025-10-27T16:39:29.372Z)
Latitude
-0.00002°
Longitude
93.11536°
Altitude
498.514 km
Speed
7.615 km/s
True Right ascension
01h 17m 07s
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
03:51:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.502 km
Perigee altitude
490.635 km
Semi-major axis
6,870.706 km
Eccentricity
0.00028
Inclination
97.4178°
RAAN
19.28°
Arg. of periapsis
84.5805°
True anomaly
275.54321°
Mean anomaly
275.5753°
Eccentric anomaly
275.55925°
Mean motion
3.81102 °/min
Orbital period
94.46 mins
BSTAR
0.00045982
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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 31 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-28 18:26:11.605Z | 3.54° NNE | 2025-10-28 18:29:11.605Z | 300.969° NW | 40.891° | 2025-10-28 18:32:11.605Z | 206.433° SW |
| 5 mins | 2025-10-29 05:04:11.605Z | 130.119° SE | 2025-10-29 05:06:11.605Z | 52.599° ENE | 33.829° | 2025-10-29 05:09:11.605Z | 1.549° NNE |
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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