FLOCK 4G 23, 62647
Orbit data source: Space-Track
FLOCK 4G 23, 62647 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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62647 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: 21 hours ago
TLE from 21 hours ago
0 FLOCK 4G 23
1 62647U 25009AQ 25346.77381735 .00017173 00000-0 69033-3 0 9995
2 62647 97.4121 64.7929 0000900 258.2546 101.8591 15.24989527 50461Epoch: 2025-12-12T18:34Z
TLE epoch observation values (Epoch: 2025-12-12T18:34:17.819Z)
Latitude
0.00002°
Longitude
64.50803°
Altitude
494.041 km
Speed
7.618 km/s
True Right ascension
04h 19m 10s
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
13:38:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.394 km
Perigee altitude
487.158 km
Semi-major axis
6,865.913 km
Eccentricity
0.00009
Inclination
97.4121°
RAAN
64.7929°
Arg. of periapsis
258.2546°
True anomaly
101.86919°
Mean anomaly
101.8591°
Eccentric anomaly
101.86415°
Mean motion
3.81501 °/min
Orbital period
94.36 mins
BSTAR
0.00069033
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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 23 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 | 2025-12-13 18:46:27.638Z | 330.516° NNW | 2025-12-13 18:47:27.638Z | 301.743° NW | 28.704° | 2025-12-13 18:50:27.638Z | 226.563° WSW |
| 5 mins | 2025-12-14 05:21:27.638Z | 160.859° S | 2025-12-14 05:23:27.638Z | 107.743° ESE | 44.251° | 2025-12-14 05:26:27.638Z | 351.477° N |
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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