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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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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4G 20
1 62636U 25009AD 25339.48265846 .00067583 00000-0 26126-2 0 9992
2 62636 97.4117 57.3764 0002464 307.7295 52.3720 15.25964879 49340Epoch: 2025-12-05T11:35Z
TLE epoch observation values (Epoch: 2025-12-05T11:35:01.690Z)
Latitude
-0.00003°
Longitude
169.09525°
Altitude
489.955 km
Speed
7.621 km/s
True Right ascension
03h 49m 30s
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
07:46:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.539 km
Perigee altitude
483.157 km
Semi-major axis
6,862.985 km
Eccentricity
0.00025
Inclination
97.4117°
RAAN
57.3764°
Arg. of periapsis
307.7295°
True anomaly
52.39437°
Mean anomaly
52.372°
Eccentric anomaly
52.38318°
Mean motion
3.81745 °/min
Orbital period
94.3 mins
BSTAR
0.0026126
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-06 18:02:39.135Z | 20.02° NNE | 2025-12-06 18:05:39.135Z | 88.83° E | 41.459° | 2025-12-06 18:08:39.135Z | 180.569° SSW |
| 4 mins | 2025-12-07 04:39:39.135Z | 103.861° ESE | 2025-12-07 04:40:39.135Z | 82.328° E | 20.001° | 2025-12-07 04:43:39.135Z | 21.372° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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