FLOCK 4G 1, 62666
Orbit data source: Space-Track
FLOCK 4G 1, 62666 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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62666 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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4G 1
1 62666U 25009BK 26127.69144666 .00008025 00000-0 28897-3 0 9994
2 62666 97.4018 209.8861 0005785 106.5625 253.6251 15.28830296 72727Epoch: 2026-05-07T16:35Z
TLE epoch observation values (Epoch: 2026-05-07T16:35:40.991Z)
Latitude
0.00001°
Longitude
95.43135°
Altitude
483.531 km
Speed
7.623 km/s
True Right ascension
13h 59m 32s
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
06:16:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.227 km
Perigee altitude
472.296 km
Semi-major axis
6,854.399 km
Eccentricity
0.00058
Inclination
97.4018°
RAAN
209.8861°
Arg. of periapsis
106.5625°
True anomaly
253.56151°
Mean anomaly
253.6251°
Eccentric anomaly
253.5933°
Mean motion
3.82463 °/min
Orbital period
94.13 mins
BSTAR
0.00028897
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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 1 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 | 2026-05-08 05:17:34.410Z | 152.724° SSE | 2026-05-08 05:20:34.410Z | 55.981° ENE | 40.082° | 2026-05-08 05:23:34.410Z | 356.759° N |
| 5 mins | 2026-05-08 18:18:34.410Z | 16.201° NNE | 2026-05-08 18:20:34.410Z | 172.418° S | 43.185° | 2026-05-08 18:23:34.410Z | 190.409° SSW |
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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