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
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: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4G 20
1 62636U 25009AD 26171.18618575 .00105405 00000-0 16043-2 0 9998
2 62636 97.3863 255.7089 0003743 237.3183 122.7710 15.54144788 79587Epoch: 2026-06-20T04:28Z
TLE epoch observation values (Epoch: 2026-06-20T04:28:06.448Z)
Latitude
-0.00004°
Longitude
-79.72239°
Altitude
409.152 km
Speed
7.665 km/s
True Right ascension
17h 02m 50s
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
10:19:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
404.097 km
Perigee altitude
399.022 km
Semi-major axis
6,779.696 km
Eccentricity
0.00037
Inclination
97.3863°
RAAN
255.7089°
Arg. of periapsis
237.3183°
True anomaly
122.80706°
Mean anomaly
122.771°
Eccentric anomaly
122.78903°
Mean motion
3.88801 °/min
Orbital period
92.59 mins
BSTAR
0.0016043
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 05:19:46.047Z | 138.609° SSE | 2026-06-21 05:21:46.047Z | 90.942° ESE | 30.397° | 2026-06-21 05:24:46.047Z | 6.534° NNE |
| 4 mins | 2026-06-21 18:07:46.047Z | 47.91° ENE | 2026-06-21 18:08:46.047Z | 76.837° E | 27.512° | 2026-06-21 18:11:46.047Z | 162.645° S |
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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