FLOCK 4G 18, 62680
Orbit data source: Space-Track
FLOCK 4G 18, 62680 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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62680 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: 18 hours ago
TLE from 18 hours ago
0 FLOCK 4G 18
1 62680U 25009BZ 26307.19374757 .00034467 00000-0 84887-3 0 9991
2 62680 97.3905 29.3729 0004700 182.5528 177.5695 15.40500561157865Epoch: 2026-11-03T04:38Z
TLE epoch observation values (Epoch: 2026-11-03T04:38:59.790Z)
Latitude
-0.00001°
Longitude
-82.83615°
Altitude
450.954 km
Speed
7.64 km/s
True Right ascension
01h 57m 29s
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
18:09:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
444.774 km
Perigee altitude
438.364 km
Semi-major axis
6,819.706 km
Eccentricity
0.00047
Inclination
97.3905°
RAAN
29.3729°
Arg. of periapsis
182.5528°
True anomaly
177.57178°
Mean anomaly
177.5695°
Eccentric anomaly
177.57064°
Mean motion
3.85385 °/min
Orbital period
93.41 mins
BSTAR
0.00084887
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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 18 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 | 2026-11-04 05:43:19.787Z | 170.217° S | 2026-11-04 05:46:19.787Z | 329.885° NNW | 68.003° | 2026-11-04 05:49:19.787Z | 346.513° N |
| 5 mins | 2026-11-04 18:38:19.787Z | 1.974° NNE | 2026-11-04 18:40:19.787Z | 240.875° WSW | 64.348° | 2026-11-04 18:43:19.787Z | 199.747° SSW |
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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