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: 2 days ago
TLE from 2 days ago
0 FLOCK 4G 3
1 62639U 25009AG 25254.78143681 .00008105 00000-0 35604-3 0 9993
2 62639 97.4273 334.0616 0003283 178.5315 181.5931 15.22175915 36442Epoch: 2025-09-11T18:45Z
TLE epoch observation values (Epoch: 2025-09-11T18:45:16.14Z)
Latitude
-0.00006°
Longitude
61.70578°
Altitude
504.629 km
Speed
7.611 km/s
True Right ascension
22h 16m 14s
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
03:38:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.499 km
Perigee altitude
493.986 km
Semi-major axis
6,874.38 km
Eccentricity
0.00033
Inclination
97.4273°
RAAN
334.0616°
Arg. of periapsis
178.5315°
True anomaly
181.59205°
Mean anomaly
181.5931°
Eccentric anomaly
181.59258°
Mean motion
3.80796 °/min
Orbital period
94.54 mins
BSTAR
0.00035604
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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 | 2025-09-13 18:39:35.004Z | 344.827° N | 2025-09-13 18:41:35.004Z | 282.17° WNW | 33.484° | 2025-09-13 18:44:35.004Z | 217.245° SW |
| 5 mins | 2025-09-14 05:16:35.004Z | 151.839° SSE | 2025-09-14 05:18:35.004Z | 53.991° ENE | 42.343° | 2025-09-14 05:21:35.004Z | 354.53° 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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