FLOCK 4G 27, 62641
Orbit data source: Space-Track
FLOCK 4G 27, 62641 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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62641 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: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4G 27
1 62641U 25009AJ 25348.77708342 .00009963 00000-0 40102-3 0 9992
2 62641 97.4119 66.6669 0001646 215.7285 144.3843 15.25077529 50755Epoch: 2025-12-14T18:39Z
TLE epoch observation values (Epoch: 2025-12-14T18:39:00.007Z)
Latitude
-0.00002°
Longitude
63.23174°
Altitude
494.569 km
Speed
7.617 km/s
True Right ascension
04h 26m 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
09:31:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.642 km
Perigee altitude
486.382 km
Semi-major axis
6,865.649 km
Eccentricity
0.00016
Inclination
97.4119°
RAAN
66.6669°
Arg. of periapsis
215.7285°
True anomaly
144.39528°
Mean anomaly
144.3843°
Eccentric anomaly
144.38979°
Mean motion
3.81523 °/min
Orbital period
94.36 mins
BSTAR
0.00040102
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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 27 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 | 2025-12-15 18:50:34.941Z | 334.835° NNW | 2025-12-15 18:52:34.941Z | 281.693° WNW | 26.16° | 2025-12-15 18:54:34.941Z | 235.978° WSW |
| 6 mins | 2025-12-16 05:25:34.941Z | 167.926° S | 2025-12-16 05:28:34.941Z | 343.694° N | 42.62° | 2025-12-16 05:31:34.941Z | 347.697° 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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