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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4G 3
1 62639U 25009AG 25258.46266232 .00015507 00000-0 67623-3 0 9990
2 62639 97.4270 337.6972 0003618 167.2027 192.9301 15.22251062 37008Epoch: 2025-09-15T11:06Z
TLE epoch observation values (Epoch: 2025-09-15T11:06:14.024Z)
Latitude
-0.0001°
Longitude
176.47181°
Altitude
504.571 km
Speed
7.611 km/s
True Right ascension
22h 30m 47s
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
13:30:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.503 km
Perigee altitude
493.529 km
Semi-major axis
6,874.153 km
Eccentricity
0.00036
Inclination
97.427°
RAAN
337.6972°
Arg. of periapsis
167.2027°
True anomaly
192.92083°
Mean anomaly
192.9301°
Eccentric anomaly
192.92546°
Mean motion
3.80815 °/min
Orbital period
94.53 mins
BSTAR
0.00067623
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-16 04:36:08.168Z | 117.281° SE | 2025-09-16 04:39:08.168Z | 59.821° ENE | 19.261° | 2025-09-16 04:41:08.168Z | 24.006° NE |
| 4 mins | 2025-09-16 06:11:08.168Z | 236.006° WSW | 2025-09-16 06:12:08.168Z | 259.412° W | 20.957° | 2025-09-16 06:15:08.168Z | 316.821° NNW |
| 4 mins | 2025-09-16 17:40:08.168Z | 55.268° ENE | 2025-09-16 17:42:08.168Z | 110.672° ESE | 25.066° | 2025-09-16 17:44:08.168Z | 151.271° 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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