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: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4G 22
1 62645U 25009AN 26002.80601822 .00014987 00000-0 59224-3 0 9990
2 62645 97.4168 85.9719 0003205 144.6240 215.5211 15.25588922 53675Epoch: 2026-01-02T19:20Z
TLE epoch observation values (Epoch: 2026-01-02T19:20:39.974Z)
Latitude
-0.00003°
Longitude
53.36439°
Altitude
493.907 km
Speed
7.617 km/s
True Right ascension
05h 43m 53s
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
10:04:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.176 km
Perigee altitude
483.776 km
Semi-major axis
6,864.113 km
Eccentricity
0.00032
Inclination
97.4168°
RAAN
85.9719°
Arg. of periapsis
144.624°
True anomaly
215.49977°
Mean anomaly
215.5211°
Eccentric anomaly
215.51043°
Mean motion
3.81651 °/min
Orbital period
94.33 mins
BSTAR
0.00059224
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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 | 2026-01-03 17:56:30.015Z | 25.302° NE | 2026-01-03 17:59:30.015Z | 84.621° E | 35.435° | 2026-01-03 18:02:30.015Z | 170.337° S |
| 4 mins | 2026-01-04 04:33:30.015Z | 105.351° ESE | 2026-01-04 04:35:30.015Z | 67.347° ENE | 16.912° | 2026-01-04 04:37:30.015Z | 30.313° NE |
| 4 mins | 2026-01-04 06:07:30.015Z | 230.155° WSW | 2026-01-04 06:08:30.015Z | 255.639° W | 23.38° | 2026-01-04 06:11:30.015Z | 318.97° 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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