FLOCK 4G 20, 62636
Orbit data source: Space-Track
FLOCK 4G 20, 62636 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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62636 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Non-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: 2 days ago
TLE from 2 days ago
0 FLOCK 4G 20
1 62636U 25009AD 26260.77457096 .00163112 00000-0 10180-2 0 9996
2 62636 97.3760 349.5182 0002920 291.8260 68.2694 15.76412767 93597Epoch: 2026-09-17T18:35Z
TLE epoch observation values (Epoch: 2026-09-17T18:35:22.930Z)
Latitude
-0.00014°
Longitude
73.96569°
Altitude
343.055 km
Speed
7.703 km/s
True Right ascension
23h 18m 04s
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
06:38:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
339.465 km
Perigee altitude
335.543 km
Semi-major axis
6,715.641 km
Eccentricity
0.00029
Inclination
97.376°
RAAN
349.5182°
Arg. of periapsis
291.826°
True anomaly
68.30049°
Mean anomaly
68.2694°
Eccentric anomaly
68.28494°
Mean motion
3.94377 °/min
Orbital period
91.28 mins
BSTAR
0.001018
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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 20 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 | 2026-09-19 18:22:15.655Z | 46.076° ENE | 2026-09-19 18:24:15.655Z | 99.831° ESE | 22.566° | 2026-09-19 18:26:15.655Z | 150.342° SSE |
| 5 mins | 2026-09-20 06:07:15.655Z | 169.689° S | 2026-09-20 06:09:15.655Z | 184.451° SSW | 68.109° | 2026-09-20 06:12:15.655Z | 346.644° 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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