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: 13 hours ago
TLE from 13 hours ago
0 FLOCK 4G 14
1 62667U 25009BL 26035.26855033 .00010407 00000-0 40208-3 0 9990
2 62667 97.4129 117.9432 0005568 77.1414 283.0446 15.26422908 58601Epoch: 2026-02-04T06:26Z
TLE epoch observation values (Epoch: 2026-02-04T06:26:42.748Z)
Latitude
-0.00006°
Longitude
-113.17247°
Altitude
488.754 km
Speed
7.621 km/s
True Right ascension
07h 51m 46s
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
21:39:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.294 km
Perigee altitude
479.653 km
Semi-major axis
6,861.611 km
Eccentricity
0.00056
Inclination
97.4129°
RAAN
117.9432°
Arg. of periapsis
77.1414°
True anomaly
282.98243°
Mean anomaly
283.0446°
Eccentric anomaly
283.01352°
Mean motion
3.8186 °/min
Orbital period
94.28 mins
BSTAR
0.00040208
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-05 04:37:16.883Z | 112.542° SE | 2026-02-05 04:39:16.883Z | 75.422° E | 18.333° | 2026-02-05 04:41:16.883Z | 33.428° NE |
| 4 mins | 2026-02-05 06:11:16.883Z | 227.404° WSW | 2026-02-05 06:13:16.883Z | 275.138° WNW | 20.756° | 2026-02-05 06:15:16.883Z | 313.23° NW |
| 4 mins | 2026-02-05 17:39:16.883Z | 67.256° ENE | 2026-02-05 17:40:16.883Z | 94.264° ESE | 23.401° | 2026-02-05 17:43:16.883Z | 153.604° SSE |
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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