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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 27
1 62641U 25009AJ 25320.48942225 .00017877 00000-0 73563-3 0 9990
2 62641 97.4151 38.6775 0002142 13.3406 346.7888 15.24192050 46441Epoch: 2025-11-16T11:44Z
TLE epoch observation values (Epoch: 2025-11-16T11:44:46.082Z)
Latitude
0.00002°
Longitude
166.68201°
Altitude
494.875 km
Speed
7.618 km/s
True Right ascension
02h 34m 42s
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
10:38:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.644 km
Perigee altitude
488.702 km
Semi-major axis
6,868.31 km
Eccentricity
0.00021
Inclination
97.4151°
RAAN
38.6775°
Arg. of periapsis
13.3406°
True anomaly
346.78319°
Mean anomaly
346.7888°
Eccentric anomaly
346.78599°
Mean motion
3.81301 °/min
Orbital period
94.41 mins
BSTAR
0.00073563
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-17 18:14:23.402Z | 11.486° NNE | 2025-11-17 18:17:23.402Z | 2.849° NNE | 44.565° | 2025-11-17 18:20:23.402Z | 193.659° SSW |
| 4 mins | 2025-11-18 04:52:23.402Z | 110.333° ESE | 2025-11-18 04:53:23.402Z | 81.847° E | 27.033° | 2025-11-18 04:56:23.402Z | 13.012° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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