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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4G 22
1 62645U 25009AN 25260.19987621 .00007977 00000-0 34671-3 0 9991
2 62645 97.4259 339.4606 0003512 160.2206 199.9167 15.22541493 37288Epoch: 2025-09-17T04:47Z
TLE epoch observation values (Epoch: 2025-09-17T04:47:49.304Z)
Latitude
-0.00005°
Longitude
-88.87407°
Altitude
503.542 km
Speed
7.611 km/s
True Right ascension
22h 37m 50s
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
16:50:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.555 km
Perigee altitude
492.727 km
Semi-major axis
6,873.278 km
Eccentricity
0.00035
Inclination
97.4259°
RAAN
339.4606°
Arg. of periapsis
160.2206°
True anomaly
199.903°
Mean anomaly
199.9167°
Eccentric anomaly
199.90985°
Mean motion
3.80888 °/min
Orbital period
94.52 mins
BSTAR
0.00034671
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 04:36:04.765Z | 117.159° SE | 2025-09-18 04:39:04.765Z | 59.952° ENE | 19.113° | 2025-09-18 04:41:04.765Z | 24.168° NE |
| 4 mins | 2025-09-18 06:11:04.765Z | 236.11° WSW | 2025-09-18 06:12:04.765Z | 259.725° W | 21.067° | 2025-09-18 06:15:04.765Z | 317.119° NNW |
| 4 mins | 2025-09-18 17:40:04.765Z | 58.243° ENE | 2025-09-18 17:41:04.765Z | 83.567° E | 24.852° | 2025-09-18 17:44:04.765Z | 152.49° SSE |
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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