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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 31
1 62652U 25009AV 26215.77981615 .00010132 00000-0 35196-3 0 9991
2 62652 97.3950 297.1050 0003021 124.4650 235.6876 15.29945153 86182Epoch: 2026-08-03T18:42Z
TLE epoch observation values (Epoch: 2026-08-03T18:42:56.115Z)
Latitude
-0.00005°
Longitude
64.01317°
Altitude
480.248 km
Speed
7.625 km/s
True Right ascension
19h 48m 25s
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
18:59:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.998 km
Perigee altitude
470.859 km
Semi-major axis
6,851.065 km
Eccentricity
0.0003
Inclination
97.395°
RAAN
297.105°
Arg. of periapsis
124.465°
True anomaly
235.65901°
Mean anomaly
235.6876°
Eccentric anomaly
235.67331°
Mean motion
3.82742 °/min
Orbital period
94.06 mins
BSTAR
0.00035196
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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 | 2026-08-05 05:22:26.818Z | 157.549° S | 2026-08-05 05:25:26.818Z | 87.221° E | 42.438° | 2026-08-05 05:28:26.818Z | 355.169° N |
| 5 mins | 2026-08-05 18:22:26.818Z | 11.617° NNE | 2026-08-05 18:24:26.818Z | 9.402° NNE | 42.985° | 2026-08-05 18:27:26.818Z | 193.381° SSW |
| 4 mins | 2026-08-06 04:57:26.818Z | 105.129° ESE | 2026-08-06 04:58:26.818Z | 76.696° E | 25.067° | 2026-08-06 05:01:26.818Z | 13.288° 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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