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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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 22
1 62645U 25009AN 26039.52628578 .00010015 00000-0 38630-3 0 9992
2 62645 97.4096 122.3887 0002995 57.7730 302.3799 15.26496964 59273Epoch: 2026-02-08T12:37Z
TLE epoch observation values (Epoch: 2026-02-08T12:37:51.091Z)
Latitude
0.00002°
Longitude
154.29163°
Altitude
488.292 km
Speed
7.622 km/s
True Right ascension
08h 09m 33s
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
07:49:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.306 km
Perigee altitude
481.196 km
Semi-major axis
6,861.388 km
Eccentricity
0.0003
Inclination
97.4096°
RAAN
122.3887°
Arg. of periapsis
57.773°
True anomaly
302.35091°
Mean anomaly
302.3799°
Eccentric anomaly
302.36541°
Mean motion
3.81878 °/min
Orbital period
94.27 mins
BSTAR
0.0003863
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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 | 2026-02-09 06:03:24.441Z | 202.929° SW | 2026-02-09 06:06:24.441Z | 262.924° W | 25.259° | 2026-02-09 06:09:24.441Z | 323.299° NNW |
| 4 mins | 2026-02-09 17:32:24.441Z | 62.508° ENE | 2026-02-09 17:33:24.441Z | 83.733° E | 19.192° | 2026-02-09 17:36:24.441Z | 143.46° SSE |
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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