FLOCK 4G 30, 62679
Orbit data source: Space-Track
FLOCK 4G 30, 62679 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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62679 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 14 hours ago
TLE from 14 hours ago
0 FLOCK 4G 30
1 62679U 25009BY 26307.22297503 .00035922 00000-0 80744-3 0 9991
2 62679 97.3814 29.2203 0003177 179.0729 181.0525 15.43251470157901Epoch: 2026-11-03T05:21Z
TLE epoch observation values (Epoch: 2026-11-03T05:21:05.042Z)
Latitude
-0.00005°
Longitude
-93.53943°
Altitude
441.808 km
Speed
7.646 km/s
True Right ascension
01h 56m 52s
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
14:44:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
435.619 km
Perigee altitude
431.29 km
Semi-major axis
6,811.591 km
Eccentricity
0.00032
Inclination
97.3814°
RAAN
29.2203°
Arg. of periapsis
179.0729°
True anomaly
181.05183°
Mean anomaly
181.0525°
Eccentric anomaly
181.05217°
Mean motion
3.86074 °/min
Orbital period
93.25 mins
BSTAR
0.00080744
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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 30 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 | 2026-11-04 04:50:58.314Z | 105.702° ESE | 2026-11-04 04:52:58.314Z | 63.47° ENE | 17.604° | 2026-11-04 04:54:58.314Z | 26.128° NE |
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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