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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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 27
1 62641U 25009AJ 26254.47096532 .00008036 00000-0 27241-3 0 9996
2 62641 97.3894 335.4293 0002416 41.8186 318.3239 15.30811271 92099Epoch: 2026-09-11T11:18Z
TLE epoch observation values (Epoch: 2026-09-11T11:18:11.403Z)
Latitude
-0.00006°
Longitude
175.38795°
Altitude
475.26 km
Speed
7.629 km/s
True Right ascension
22h 21m 43s
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
12:01:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.996 km
Perigee altitude
468.687 km
Semi-major axis
6,848.478 km
Eccentricity
0.00024
Inclination
97.3894°
RAAN
335.4293°
Arg. of periapsis
41.8186°
True anomaly
318.30549°
Mean anomaly
318.3239°
Eccentric anomaly
318.31469°
Mean motion
3.82959 °/min
Orbital period
94 mins
BSTAR
0.00027241
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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 | 2026-09-12 04:42:43.722Z | 109.807° ESE | 2026-09-12 04:44:43.722Z | 71.096° E | 18.872° | 2026-09-12 04:46:43.722Z | 30.973° NE |
| 4 mins | 2026-09-12 06:16:43.722Z | 235.481° WSW | 2026-09-12 06:17:43.722Z | 260.355° W | 22.885° | 2026-09-12 06:20:43.722Z | 318.715° NNW |
| 4 mins | 2026-09-12 17:41:43.722Z | 55.559° ENE | 2026-09-12 17:43:43.722Z | 103.505° ESE | 23.335° | 2026-09-12 17:45:43.722Z | 144.28° SSE |
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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