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
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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4G 18
1 62680U 25009BZ 26104.15045567 .00004979 00000-0 18421-3 0 9992
2 62680 97.4024 186.2137 0005475 180.5496 179.5739 15.28134121126752Epoch: 2026-04-14T03:36Z
TLE epoch observation values (Epoch: 2026-04-14T03:36:39.369Z)
Latitude
0°
Longitude
-70.28117°
Altitude
488.248 km
Speed
7.619 km/s
True Right ascension
12h 24m 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
19:14:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.099 km
Perigee altitude
474.591 km
Semi-major axis
6,856.482 km
Eccentricity
0.00055
Inclination
97.4024°
RAAN
186.2137°
Arg. of periapsis
180.5496°
True anomaly
179.57437°
Mean anomaly
179.5739°
Eccentric anomaly
179.57413°
Mean motion
3.82288 °/min
Orbital period
94.17 mins
BSTAR
0.00018421
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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 | 2026-04-14 18:19:09.256Z | 11.203° NNE | 2026-04-14 18:22:09.256Z | 201.073° SSW | 43.767° | 2026-04-14 18:25:09.256Z | 193.875° SSW |
| 4 mins | 2026-04-15 04:55:09.256Z | 107.054° ESE | 2026-04-15 04:56:09.256Z | 78.293° E | 26.085° | 2026-04-15 04:59:09.256Z | 12.97° NNE |
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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