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: 13 hours ago
TLE from 13 hours ago
0 FLOCK 4G 14
1 62667U 25009BL 26175.22016847 .00009262 00000-0 32817-3 0 9997
2 62667 97.4025 257.0025 0002766 292.4428 67.6519 15.29324393 79976Epoch: 2026-06-24T05:17Z
TLE epoch observation values (Epoch: 2026-06-24T05:17:02.555Z)
Latitude
-0.00005°
Longitude
-94.63865°
Altitude
480.213 km
Speed
7.626 km/s
True Right ascension
17h 08m 00s
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
05:15:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.679 km
Perigee altitude
472.888 km
Semi-major axis
6,852.921 km
Eccentricity
0.00028
Inclination
97.4025°
RAAN
257.0025°
Arg. of periapsis
292.4428°
True anomaly
67.68122°
Mean anomaly
67.6519°
Eccentric anomaly
67.66656°
Mean motion
3.82586 °/min
Orbital period
94.1 mins
BSTAR
0.00032817
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-24 18:24:28.578Z | 9.175° NNE | 2026-06-24 18:27:28.578Z | 236.275° WSW | 44.227° | 2026-06-24 18:30:28.578Z | 196.454° SSW |
| 4 mins | 2026-06-25 04:59:28.578Z | 120.825° SE | 2026-06-25 05:01:28.578Z | 65.285° ENE | 27.044° | 2026-06-25 05:03:28.578Z | 18.259° NNE |
| 4 mins | 2026-06-25 17:59:28.578Z | 48.615° ENE | 2026-06-25 18:00:28.578Z | 81.444° E | 32.632° | 2026-06-25 18:03:28.578Z | 166.112° S |
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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