FLOCK 4G 4, 62659
Orbit data source: Space-Track
FLOCK 4G 4, 62659 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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62659 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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 4
1 62659U 25009BC 26305.16884206 .00011048 00000-0 30485-3 0 9992
2 62659 97.3848 26.6762 0003830 143.2375 216.9133 15.37254612157517Epoch: 2026-11-01T04:03Z
TLE epoch observation values (Epoch: 2026-11-01T04:03:07.953Z)
Latitude
-0.00004°
Longitude
-74.57101°
Altitude
459.439 km
Speed
7.636 km/s
True Right ascension
01h 46m 42s
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
10:36:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.789 km
Perigee altitude
448.558 km
Semi-major axis
6,829.311 km
Eccentricity
0.00038
Inclination
97.3848°
RAAN
26.6762°
Arg. of periapsis
143.2375°
True anomaly
216.88695°
Mean anomaly
216.9133°
Eccentric anomaly
216.90012°
Mean motion
3.84572 °/min
Orbital period
93.61 mins
BSTAR
0.00030485
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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 4 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-02 18:06:57.219Z | 32.426° NE | 2026-11-02 18:08:57.219Z | 81.519° E | 41.42° | 2026-11-02 18:11:57.219Z | 168.706° S |
| 4 mins | 2026-11-03 06:10:57.219Z | 213.433° SW | 2026-11-03 06:12:57.219Z | 269.817° W | 29.84° | 2026-11-03 06:14:57.219Z | 317.483° NNW |
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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