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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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 4
1 62659U 25009BC 25300.69072691 .00011575 00000-0 49132-3 0 9995
2 62659 97.4166 19.0873 0003804 76.6017 283.5644 15.23239820101046Epoch: 2025-10-27T16:34Z
TLE epoch observation values (Epoch: 2025-10-27T16:34:38.805Z)
Latitude
0.00004°
Longitude
94.13666°
Altitude
498.558 km
Speed
7.616 km/s
True Right ascension
01h 16m 20s
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
01:27:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.652 km
Perigee altitude
490.424 km
Semi-major axis
6,871.175 km
Eccentricity
0.00038
Inclination
97.4166°
RAAN
19.0873°
Arg. of periapsis
76.6017°
True anomaly
283.52202°
Mean anomaly
283.5644°
Eccentric anomaly
283.54321°
Mean motion
3.81063 °/min
Orbital period
94.47 mins
BSTAR
0.00049132
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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 | 2025-10-28 18:21:35.024Z | 6.137° NNE | 2025-10-28 18:24:35.024Z | 303.322° NW | 42.926° | 2025-10-28 18:27:35.024Z | 202.037° SSW |
| 4 mins | 2025-10-29 04:59:35.024Z | 125.867° SE | 2025-10-29 05:01:35.024Z | 56.62° ENE | 31.604° | 2025-10-29 05:03:35.024Z | 11.202° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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