FLOCK 4G 14, 62667
Orbit data source: Space-Track
FLOCK 4G 14, 62667 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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62667 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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 14
1 62667U 25009BL 25353.17957539 .00009213 00000-0 37176-3 0 9999
2 62667 97.4204 71.2427 0003913 223.5747 136.5182 15.25012272 51429Epoch: 2025-12-19T04:18Z
TLE epoch observation values (Epoch: 2025-12-19T04:18:35.313Z)
Latitude
-0.00005°
Longitude
-81.42887°
Altitude
495.796 km
Speed
7.616 km/s
True Right ascension
04h 44m 58s
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
04:13:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.395 km
Perigee altitude
485.022 km
Semi-major axis
6,865.845 km
Eccentricity
0.00039
Inclination
97.4204°
RAAN
71.2427°
Arg. of periapsis
223.5747°
True anomaly
136.54904°
Mean anomaly
136.5182°
Eccentric anomaly
136.53362°
Mean motion
3.81507 °/min
Orbital period
94.36 mins
BSTAR
0.00037176
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
Did you know?
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 14 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-20 05:37:16.421Z | 178.635° S | 2025-12-20 05:41:16.421Z | 297.872° NW | 38.791° | 2025-12-20 05:44:16.421Z | 340.266° N |
| 5 mins | 2025-12-20 18:40:16.421Z | 349.06° N | 2025-12-20 18:42:16.421Z | 300.697° NW | 32.593° | 2025-12-20 18:45:16.421Z | 220.165° SW |
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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