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 26129.79353768 .00006980 00000-0 25417-3 0 9992
2 62645 97.4001 212.0187 0003722 87.3343 272.8323 15.28517960 73055Epoch: 2026-05-09T19:02Z
TLE epoch observation values (Epoch: 2026-05-09T19:02:41.655Z)
Latitude
-0.00001°
Longitude
58.73927°
Altitude
483.219 km
Speed
7.624 km/s
True Right ascension
14h 08m 04s
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
14:21:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.748 km
Perigee altitude
474.645 km
Semi-major axis
6,855.333 km
Eccentricity
0.00037
Inclination
97.4001°
RAAN
212.0187°
Arg. of periapsis
87.3343°
True anomaly
272.7897°
Mean anomaly
272.8323°
Eccentric anomaly
272.811°
Mean motion
3.82385 °/min
Orbital period
94.15 mins
BSTAR
0.00025417
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-10 06:10:47.855Z | 217.948° SW | 2026-05-10 06:12:47.855Z | 264.322° W | 22.942° | 2026-05-10 06:14:47.855Z | 310.131° NW |
| 4 mins | 2026-05-10 17:37:47.855Z | 59.935° ENE | 2026-05-10 17:39:47.855Z | 107.78° ESE | 20.271° | 2026-05-10 17:41:47.855Z | 144.917° SSE |
| 5 mins | 2026-05-11 05:44:47.855Z | 186.331° SSW | 2026-05-11 05:46:47.855Z | 243.227° WSW | 39.475° | 2026-05-11 05:49:47.855Z | 336.757° NNW |
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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