FLOCK 4G 6, 62660
Orbit data source: Space-Track
FLOCK 4G 6, 62660 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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62660 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: 12 hours ago
TLE from 12 hours ago
0 FLOCK 4G 6
1 62660U 25009BD 26034.17571221 .00013460 00000-0 51764-3 0 9997
2 62660 97.4047 116.5455 0004453 91.2230 268.9519 15.26515002116031Epoch: 2026-02-03T04:13Z
TLE epoch observation values (Epoch: 2026-02-03T04:13:01.534Z)
Latitude
-0.00004°
Longitude
-80.0713°
Altitude
489.396 km
Speed
7.62 km/s
True Right ascension
07h 46m 10s
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
18:04:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.252 km
Perigee altitude
480.142 km
Semi-major axis
6,861.334 km
Eccentricity
0.00045
Inclination
97.4047°
RAAN
116.5455°
Arg. of periapsis
91.223°
True anomaly
268.90088°
Mean anomaly
268.9519°
Eccentric anomaly
268.92639°
Mean motion
3.81883 °/min
Orbital period
94.27 mins
BSTAR
0.00051764
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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 6 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-03 17:23:24.624Z | 60.706° ENE | 2026-02-03 17:25:24.624Z | 100.421° ESE | 16.538° | 2026-02-03 17:27:24.624Z | 135.714° SSE |
| 4 mins | 2026-02-03 18:57:24.624Z | 319.815° NNW | 2026-02-03 18:58:24.624Z | 293.878° NW | 23.008° | 2026-02-03 19:01:24.624Z | 233.618° WSW |
| 5 mins | 2026-02-04 05:31:24.624Z | 174.43° S | 2026-02-04 05:33:24.624Z | 204.231° SW | 42.493° | 2026-02-04 05:36:24.624Z | 343.068° N |
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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