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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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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4G 14
1 62667U 25009BL 26305.19463588 .00011070 00000-0 36422-3 0 9992
2 62667 97.3937 26.5285 0004478 168.5583 191.5761 15.31676987 99858Epoch: 2026-11-01T04:40Z
TLE epoch observation values (Epoch: 2026-11-01T04:40:16.540Z)
Latitude
-0°
Longitude
-84.02992°
Altitude
476.92 km
Speed
7.626 km/s
True Right ascension
01h 46m 06s
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
06:02:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.824 km
Perigee altitude
464.693 km
Semi-major axis
6,845.895 km
Eccentricity
0.00045
Inclination
97.3937°
RAAN
26.5285°
Arg. of periapsis
168.5583°
True anomaly
191.56581°
Mean anomaly
191.5761°
Eccentric anomaly
191.57095°
Mean motion
3.83176 °/min
Orbital period
93.95 mins
BSTAR
0.00036422
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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 | 2026-11-01 17:47:04.900Z | 42.455° NE | 2026-11-01 17:50:04.900Z | 107.368° ESE | 24.028° | 2026-11-01 17:52:04.900Z | 147.307° SSE |
| 5 mins | 2026-11-02 05:54:04.900Z | 194.216° SSW | 2026-11-02 05:56:04.900Z | 279.669° WNW | 50.597° | 2026-11-02 05:59:04.900Z | 337.371° NNW |
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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