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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4G 18
1 62680U 25009BZ 26202.13274432 .00030280 00000-0 96493-3 0 9993
2 62680 97.3995 283.8040 0006672 191.1048 169.0048 15.32470382141735Epoch: 2026-07-21T03:11Z
TLE epoch observation values (Epoch: 2026-07-21T03:11:09.109Z)
Latitude
0.00002°
Longitude
-62.89078°
Altitude
476.037 km
Speed
7.625 km/s
True Right ascension
18h 55m 12s
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
00:00:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.959 km
Perigee altitude
460.827 km
Semi-major axis
6,843.53 km
Eccentricity
0.00067
Inclination
97.3995°
RAAN
283.804°
Arg. of periapsis
191.1048°
True anomaly
169.01937°
Mean anomaly
169.0048°
Eccentric anomaly
169.01209°
Mean motion
3.83374 °/min
Orbital period
93.9 mins
BSTAR
0.00096493
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-21 17:51:35.533Z | 38.001° NE | 2026-07-21 17:54:35.533Z | 114.906° SE | 26.701° | 2026-07-21 17:56:35.533Z | 156.588° SSE |
| 5 mins | 2026-07-22 05:57:35.533Z | 199.111° SSW | 2026-07-22 05:59:35.533Z | 249.101° W | 31.69° | 2026-07-22 06:02:35.533Z | 328.156° NNW |
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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