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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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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4G 31
1 62652U 25009AV 26171.16220497 .00008714 00000-0 31097-3 0 9998
2 62652 97.3966 252.7184 0000511 43.6448 316.4833 15.29112778 79364Epoch: 2026-06-20T03:53Z
TLE epoch observation values (Epoch: 2026-06-20T03:53:34.509Z)
Latitude
0.00004°
Longitude
-74.05618°
Altitude
481.312 km
Speed
7.625 km/s
True Right ascension
16h 50m 52s
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
07:19:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.767 km
Perigee altitude
475.066 km
Semi-major axis
6,853.554 km
Eccentricity
0.00005
Inclination
97.3966°
RAAN
252.7184°
Arg. of periapsis
43.6448°
True anomaly
316.47927°
Mean anomaly
316.4833°
Eccentric anomaly
316.48128°
Mean motion
3.82533 °/min
Orbital period
94.11 mins
BSTAR
0.00031097
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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 | 2026-06-21 05:08:49.024Z | 146.613° SSE | 2026-06-21 05:11:49.024Z | 88.115° E | 34.598° | 2026-06-21 05:14:49.024Z | 4.753° NNE |
| 5 mins | 2026-06-21 18:09:49.024Z | 25.683° NE | 2026-06-21 18:11:49.024Z | 104.276° ESE | 41.516° | 2026-06-21 18:14:49.024Z | 181.214° SSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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