FLOCK 4G 3, 62639
Orbit data source: Space-Track
FLOCK 4G 3, 62639 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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62639 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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4G 3
1 62639U 25009AG 25286.25999100 .00018014 00000-0 76321-3 0 9996
2 62639 97.4239 5.1686 0004458 97.8272 262.3471 15.23198734 41232Epoch: 2025-10-13T06:14Z
TLE epoch observation values (Epoch: 2025-10-13T06:14:23.222Z)
Latitude
-0.00002°
Longitude
-110.49348°
Altitude
499.703 km
Speed
7.614 km/s
True Right ascension
00h 20m 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
06:39:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.225 km
Perigee altitude
490.099 km
Semi-major axis
6,871.299 km
Eccentricity
0.00045
Inclination
97.4239°
RAAN
5.1686°
Arg. of periapsis
97.8272°
True anomaly
262.29647°
Mean anomaly
262.3471°
Eccentric anomaly
262.32179°
Mean motion
3.81053 °/min
Orbital period
94.48 mins
BSTAR
0.00076321
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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 3 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 | 2025-10-13 17:50:22.476Z | 29.366° NE | 2025-10-13 17:53:22.476Z | 95.199° ESE | 32.88° | 2025-10-13 17:56:22.476Z | 166.891° S |
| 4 mins | 2025-10-14 06:02:22.476Z | 228.106° WSW | 2025-10-14 06:03:22.476Z | 255.697° W | 25.541° | 2025-10-14 06:06:22.476Z | 321.252° NNW |
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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