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: 2 days ago
TLE from 2 days ago
0 FLOCK 4G 30
1 62679U 25009BY 26215.47660689 .00049348 00000-0 14275-2 0 9997
2 62679 97.3891 296.7874 0004699 148.2096 211.9432 15.35441796143791Epoch: 2026-08-03T11:26Z
TLE epoch observation values (Epoch: 2026-08-03T11:26:18.835Z)
Latitude
-0.00001°
Longitude
173.14976°
Altitude
465.448 km
Speed
7.632 km/s
True Right ascension
19h 47m 08s
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
20:49:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.765 km
Perigee altitude
453.341 km
Semi-major axis
6,834.69 km
Eccentricity
0.00047
Inclination
97.3891°
RAAN
296.7874°
Arg. of periapsis
148.2096°
True anomaly
211.91473°
Mean anomaly
211.9432°
Eccentric anomaly
211.92896°
Mean motion
3.84118 °/min
Orbital period
93.72 mins
BSTAR
0.0014275
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-05 18:44:13.910Z | 352.48° N | 2026-08-05 18:47:13.910Z | 261.495° W | 31.78° | 2026-08-05 18:49:13.910Z | 219.606° SW |
| 5 mins | 2026-08-06 05:16:13.910Z | 141.776° SSE | 2026-08-06 05:18:13.910Z | 67.889° E | 37.51° | 2026-08-06 05:21:13.910Z | 359.8° N |
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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