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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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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 18
1 62680U 25009BZ 25301.46836417 .00014580 00000-0 61636-3 0 9991
2 62680 97.4221 19.9508 0006876 75.2075 284.9924 15.23305987101186Epoch: 2025-10-28T11:14Z
TLE epoch observation values (Epoch: 2025-10-28T11:14:26.664Z)
Latitude
0.00006°
Longitude
174.28427°
Altitude
497.751 km
Speed
7.616 km/s
True Right ascension
01h 19m 48s
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
07:59:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.564 km
Perigee altitude
488.115 km
Semi-major axis
6,870.976 km
Eccentricity
0.00069
Inclination
97.4221°
RAAN
19.9508°
Arg. of periapsis
75.2075°
True anomaly
284.91627°
Mean anomaly
284.9924°
Eccentric anomaly
284.95434°
Mean motion
3.81079 °/min
Orbital period
94.47 mins
BSTAR
0.00061636
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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 | 2025-10-29 17:45:31.309Z | 32.212° NE | 2025-10-29 17:48:31.309Z | 96.774° ESE | 30.182° | 2025-10-29 17:51:31.309Z | 163.304° S |
| 5 mins | 2025-10-30 05:56:31.309Z | 208.215° SW | 2025-10-30 05:58:31.309Z | 257.589° W | 28.061° | 2025-10-30 06:01:31.309Z | 324.608° NNW |
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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