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
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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4G 4
1 62659U 25009BC 26080.81131432 .00014260 00000-0 53933-3 0 9992
2 62659 97.3981 162.7504 0001128 256.5348 103.5766 15.27063919123161Epoch: 2026-03-21T19:28Z
TLE epoch observation values (Epoch: 2026-03-21T19:28:17.557Z)
Latitude
0.00006°
Longitude
51.35057°
Altitude
487.877 km
Speed
7.621 km/s
True Right ascension
10h 51m 00s
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
17:21:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.325 km
Perigee altitude
480.777 km
Semi-major axis
6,859.688 km
Eccentricity
0.00011
Inclination
97.3981°
RAAN
162.7504°
Arg. of periapsis
256.5348°
True anomaly
103.58916°
Mean anomaly
103.5766°
Eccentric anomaly
103.58288°
Mean motion
3.8202 °/min
Orbital period
94.24 mins
BSTAR
0.00053933
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-22 18:03:01.010Z | 21.812° NNE | 2026-03-22 18:06:01.010Z | 99.553° ESE | 40.379° | 2026-03-22 18:09:01.010Z | 178.861° S |
| 4 mins | 2026-03-23 06:13:01.010Z | 233.486° WSW | 2026-03-23 06:14:01.010Z | 256.028° W | 20.087° | 2026-03-23 06:17:01.010Z | 315.343° 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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