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: 3 days ago
TLE from 3 days ago
0 FLOCK 4G 22
1 62645U 25009AN 25312.22455428 .00014921 00000-0 61680-3 0 9995
2 62645 97.4217 30.9078 0002572 30.5323 329.6064 15.24078153 45201Epoch: 2025-11-08T05:23Z
TLE epoch observation values (Epoch: 2025-11-08T05:23:21.489Z)
Latitude
-0°
Longitude
-97.58897°
Altitude
495.126 km
Speed
7.618 km/s
True Right ascension
02h 03m 37s
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
00:07:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.283 km
Perigee altitude
488.749 km
Semi-major axis
6,868.653 km
Eccentricity
0.00026
Inclination
97.4217°
RAAN
30.9078°
Arg. of periapsis
30.5323°
True anomaly
329.59148°
Mean anomaly
329.6064°
Eccentric anomaly
329.59894°
Mean motion
3.81273 °/min
Orbital period
94.42 mins
BSTAR
0.0006168
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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 | 2025-11-11 06:00:52.346Z | 218.336° SW | 2025-11-11 06:02:52.346Z | 275.136° WNW | 26.182° | 2025-11-11 06:04:52.346Z | 317.985° NNW |
| 4 mins | 2025-11-11 19:02:52.346Z | 326.863° NNW | 2025-11-11 19:04:52.346Z | 281.543° WNW | 20.426° | 2025-11-11 19:06:52.346Z | 243.631° WSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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