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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4G 23
1 62647U 25009AQ 26038.17698536 .00012757 00000-0 49093-3 0 9995
2 62647 97.4034 120.6676 0002972 83.8235 276.3342 15.26512388 59069Epoch: 2026-02-07T04:14Z
TLE epoch observation values (Epoch: 2026-02-07T04:14:51.535Z)
Latitude
-0.00002°
Longitude
-80.35138°
Altitude
489.122 km
Speed
7.621 km/s
True Right ascension
08h 02m 40s
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
14:23:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.244 km
Perigee altitude
481.166 km
Semi-major axis
6,861.342 km
Eccentricity
0.0003
Inclination
97.4034°
RAAN
120.6676°
Arg. of periapsis
83.8235°
True anomaly
276.30035°
Mean anomaly
276.3342°
Eccentric anomaly
276.31728°
Mean motion
3.81882 °/min
Orbital period
94.27 mins
BSTAR
0.00049093
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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 | 2026-02-07 17:24:58.694Z | 56.261° ENE | 2026-02-07 17:26:58.694Z | 94.707° ESE | 17.178° | 2026-02-07 17:28:58.694Z | 132.865° SE |
| 4 mins | 2026-02-07 18:58:58.694Z | 324.487° NNW | 2026-02-07 18:59:58.694Z | 301.07° NW | 22.07° | 2026-02-07 19:02:58.694Z | 237.123° WSW |
| 5 mins | 2026-02-08 05:33:58.694Z | 179.485° S | 2026-02-08 05:35:58.694Z | 307.626° NW | 42.135° | 2026-02-08 05:38:58.694Z | 343.766° 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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