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: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4G 14
1 62667U 25009BL 25301.18512446 .00013440 00000-0 56850-3 0 9994
2 62667 97.4234 19.7637 0005896 69.4372 290.7497 15.23312176 43501Epoch: 2025-10-28T04:26Z
TLE epoch observation values (Epoch: 2025-10-28T04:26:34.753Z)
Latitude
-0.00002°
Longitude
-83.65735°
Altitude
497.519 km
Speed
7.617 km/s
True Right ascension
01h 19m 03s
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
19:12:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.872 km
Perigee altitude
488.769 km
Semi-major axis
6,870.957 km
Eccentricity
0.00059
Inclination
97.4234°
RAAN
19.7637°
Arg. of periapsis
69.4372°
True anomaly
290.6865°
Mean anomaly
290.7497°
Eccentric anomaly
290.7181°
Mean motion
3.81081 °/min
Orbital period
94.47 mins
BSTAR
0.0005685
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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 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-29 05:48:45.315Z | 205.891° SW | 2025-10-29 05:50:45.315Z | 280.087° WNW | 33.005° | 2025-10-29 05:53:45.315Z | 333.47° NNW |
| 5 mins | 2025-10-29 18:50:45.315Z | 339.42° N | 2025-10-29 18:52:45.315Z | 293.105° NW | 26.118° | 2025-10-29 18:55:45.315Z | 229.402° WSW |
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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