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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4G 20
1 62636U 25009AD 25290.17179222 .00014157 00000-0 60654-3 0 9990
2 62636 97.4159 8.6293 0003781 97.5187 262.6479 15.22875013 41830Epoch: 2025-10-17T04:07Z
TLE epoch observation values (Epoch: 2025-10-17T04:07:22.847Z)
Latitude
-0.00007°
Longitude
-79.13687°
Altitude
500.601 km
Speed
7.614 km/s
True Right ascension
00h 34m 31s
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
16:09:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.735 km
Perigee altitude
491.538 km
Semi-major axis
6,872.273 km
Eccentricity
0.00038
Inclination
97.4159°
RAAN
8.6293°
Arg. of periapsis
97.5187°
True anomaly
262.60493°
Mean anomaly
262.6479°
Eccentric anomaly
262.62642°
Mean motion
3.80972 °/min
Orbital period
94.5 mins
BSTAR
0.00060654
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-18 05:28:47.481Z | 172.962° S | 2025-10-18 05:31:47.481Z | 263.164° W | 44.14° | 2025-10-18 05:34:47.481Z | 343.905° N |
| 5 mins | 2025-10-18 18:32:47.481Z | 349.216° N | 2025-10-18 18:34:47.481Z | 275.168° WNW | 37.006° | 2025-10-18 18:37:47.481Z | 211.516° SW |
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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