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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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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4G 30
1 62679U 25009BY 25308.94408112 .00009725 00000-0 40844-3 0 9999
2 62679 97.4156 27.0796 0005844 62.4623 297.7208 15.23636068102322Epoch: 2025-11-04T22:39Z
TLE epoch observation values (Epoch: 2025-11-04T22:39:28.608Z)
Latitude
0.00003°
Longitude
2.78655°
Altitude
496.112 km
Speed
7.618 km/s
True Right ascension
01h 48m 19s
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
05:51:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.86 km
Perigee altitude
487.831 km
Semi-major axis
6,869.983 km
Eccentricity
0.00058
Inclination
97.4156°
RAAN
27.0796°
Arg. of periapsis
62.4623°
True anomaly
297.6615°
Mean anomaly
297.7208°
Eccentric anomaly
297.69115°
Mean motion
3.81162 °/min
Orbital period
94.45 mins
BSTAR
0.00040844
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-05 18:07:59.142Z | 15.818° NNE | 2025-11-05 18:10:59.142Z | 96.504° ESE | 44.244° | 2025-11-05 18:13:59.142Z | 187.431° SSW |
| 4 mins | 2025-11-06 04:45:59.142Z | 108.051° ESE | 2025-11-06 04:46:59.142Z | 83.452° E | 23.736° | 2025-11-06 04:49:59.142Z | 17.205° NNE |
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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