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: 13 hours ago
TLE from 13 hours ago
0 FLOCK 4G 6
1 62660U 25009BD 25286.16895462 .00019086 00000-0 81457-3 0 9992
2 62660 97.4165 4.7092 0004930 121.4252 238.7467 15.22934709 98814Epoch: 2025-10-13T04:03Z
TLE epoch observation values (Epoch: 2025-10-13T04:03:17.679Z)
Latitude
-0.00003°
Longitude
-78.09006°
Altitude
501.848 km
Speed
7.612 km/s
True Right ascension
00h 18m 50s
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
11:24:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.344 km
Perigee altitude
490.569 km
Semi-major axis
6,872.093 km
Eccentricity
0.00049
Inclination
97.4165°
RAAN
4.7092°
Arg. of periapsis
121.4252°
True anomaly
238.69842°
Mean anomaly
238.7467°
Eccentric anomaly
238.72256°
Mean motion
3.80986 °/min
Orbital period
94.49 mins
BSTAR
0.00081457
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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 | 2025-10-13 17:15:19.034Z | 59.047° ENE | 2025-10-13 17:17:19.034Z | 93.988° ESE | 14.558° | 2025-10-13 17:19:19.034Z | 128.451° SE |
| 4 mins | 2025-10-13 18:49:19.034Z | 333.39° NNW | 2025-10-13 18:51:19.034Z | 278.138° WNW | 26.326° | 2025-10-13 18:53:19.034Z | 234.381° WSW |
| 5 mins | 2025-10-14 05:25:19.034Z | 168.764° S | 2025-10-14 05:27:19.034Z | 177.244° S | 43.527° | 2025-10-14 05:30:19.034Z | 346.879° 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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