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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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 23
1 62647U 25009AQ 26215.77859203 .00045859 00000-0 12889-2 0 9999
2 62647 97.3905 297.5304 0002980 136.5499 223.5980 15.36370365 86222Epoch: 2026-08-03T18:41Z
TLE epoch observation values (Epoch: 2026-08-03T18:41:10.351Z)
Latitude
-0.00005°
Longitude
64.88046°
Altitude
461.442 km
Speed
7.635 km/s
True Right ascension
19h 50m 07s
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
18:59:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.832 km
Perigee altitude
451.761 km
Semi-major axis
6,831.934 km
Eccentricity
0.0003
Inclination
97.3905°
RAAN
297.5304°
Arg. of periapsis
136.5499°
True anomaly
223.57446°
Mean anomaly
223.598°
Eccentric anomaly
223.58623°
Mean motion
3.84351 °/min
Orbital period
93.66 mins
BSTAR
0.0012889
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-05 05:12:16.272Z | 144.339° SSE | 2026-08-05 05:15:16.272Z | 67.881° E | 34.079° | 2026-08-05 05:18:16.272Z | 2.722° NNE |
| 5 mins | 2026-08-05 18:09:16.272Z | 31.095° NE | 2026-08-05 18:11:16.272Z | 109.602° ESE | 38.361° | 2026-08-05 18:14:16.272Z | 177.444° 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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