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: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4G 30
1 62679U 25009BY 26171.17766492 .00021640 00000-0 69665-3 0 9993
2 62679 97.3918 252.4655 0001963 296.3393 63.7647 15.32231419137007Epoch: 2026-06-20T04:15Z
TLE epoch observation values (Epoch: 2026-06-20T04:15:50.249Z)
Latitude
-0.00001°
Longitude
-79.8899°
Altitude
471.67 km
Speed
7.631 km/s
True Right ascension
16h 49m 51s
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
07:21:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
467.449 km
Perigee altitude
464.762 km
Semi-major axis
6,844.242 km
Eccentricity
0.0002
Inclination
97.3918°
RAAN
252.4655°
Arg. of periapsis
296.3393°
True anomaly
63.78488°
Mean anomaly
63.7647°
Eccentric anomaly
63.77479°
Mean motion
3.83314 °/min
Orbital period
93.92 mins
BSTAR
0.00069665
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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 | 2026-06-21 05:27:52.823Z | 166.089° S | 2026-06-21 05:30:52.823Z | 143.52° SSE | 44.817° | 2026-06-21 05:33:52.823Z | 348.807° N |
| 5 mins | 2026-06-21 18:26:52.823Z | 4.23° NNE | 2026-06-21 18:28:52.823Z | 320.846° NNW | 42.337° | 2026-06-21 18:31:52.823Z | 201.587° SSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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