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 26170.71993781 .00033216 00000-0 10481-2 0 9993
2 62647 97.3929 252.3863 0001511 209.4417 150.6740 15.32785456 79319Epoch: 2026-06-19T17:16Z
TLE epoch observation values (Epoch: 2026-06-19T17:16:42.626Z)
Latitude
-0.00006°
Longitude
85.26383°
Altitude
471.516 km
Speed
7.63 km/s
True Right ascension
16h 49m 32s
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
07:23:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.488 km
Perigee altitude
463.421 km
Semi-major axis
6,842.591 km
Eccentricity
0.00015
Inclination
97.3929°
RAAN
252.3863°
Arg. of periapsis
209.4417°
True anomaly
150.68248°
Mean anomaly
150.674°
Eccentric anomaly
150.67824°
Mean motion
3.83453 °/min
Orbital period
93.88 mins
BSTAR
0.0010481
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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 | 2026-06-21 05:26:13.926Z | 162.815° S | 2026-06-21 05:29:13.926Z | 108.151° ESE | 44.253° | 2026-06-21 05:32:13.926Z | 351.324° N |
| 5 mins | 2026-06-21 18:25:13.926Z | 7.157° NNE | 2026-06-21 18:27:13.926Z | 277.444° WNW | 44.47° | 2026-06-21 18:30:13.926Z | 197.183° SSW |
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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