FLOCK 4G 22, 62645
Orbit data source: Space-Track
FLOCK 4G 22, 62645 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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62645 intel report (Beta)
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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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4G 22
1 62645U 25009AN 26095.15540208 .00015271 00000-0 56279-3 0 9994
2 62645 97.4020 177.6035 0002881 163.8174 196.3158 15.27902332 67768Epoch: 2026-04-05T03:43Z
TLE epoch observation values (Epoch: 2026-04-05T03:43:46.739Z)
Latitude
-0.00003°
Longitude
-71.80612°
Altitude
487.083 km
Speed
7.621 km/s
True Right ascension
11h 50m 24s
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
20:37:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.015 km
Perigee altitude
477.064 km
Semi-major axis
6,857.176 km
Eccentricity
0.00029
Inclination
97.402°
RAAN
177.6035°
Arg. of periapsis
163.8174°
True anomaly
196.30653°
Mean anomaly
196.3158°
Eccentric anomaly
196.31116°
Mean motion
3.8223 °/min
Orbital period
94.18 mins
BSTAR
0.00056279
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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 22 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 | 2026-04-05 18:26:07.701Z | 6.356° NNE | 2026-04-05 18:29:07.701Z | 266.398° W | 43.348° | 2026-04-05 18:32:07.701Z | 200.326° SSW |
| 4 mins | 2026-04-06 05:02:07.701Z | 119.23° SE | 2026-04-06 05:03:07.701Z | 91.091° ESE | 29.039° | 2026-04-06 05:06:07.701Z | 11.696° NNE |
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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