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: 13 hours ago
TLE from 13 hours ago
0 FLOCK 4G 22
1 62645U 25009AN 25260.85709069 .00008314 00000-0 36111-3 0 9999
2 62645 97.4261 340.1099 0003552 158.8915 201.2469 15.22553494 37387Epoch: 2025-09-17T20:34Z
TLE epoch observation values (Epoch: 2025-09-17T20:34:12.635Z)
Latitude
0°
Longitude
34.53023°
Altitude
503.512 km
Speed
7.611 km/s
True Right ascension
22h 40m 26s
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
02:44:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.546 km
Perigee altitude
492.664 km
Semi-major axis
6,873.242 km
Eccentricity
0.00036
Inclination
97.4261°
RAAN
340.1099°
Arg. of periapsis
158.8915°
True anomaly
201.23216°
Mean anomaly
201.2469°
Eccentric anomaly
201.23953°
Mean motion
3.80891 °/min
Orbital period
94.52 mins
BSTAR
0.00036111
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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 17:39:16.090Z | 45.189° ENE | 2025-09-18 17:41:16.090Z | 89.467° E | 25.235° | 2025-09-18 17:44:16.090Z | 154.445° SSE |
| 5 mins | 2025-09-19 05:50:16.090Z | 206.295° SW | 2025-09-19 05:52:16.090Z | 276.078° WNW | 32.714° | 2025-09-19 05:55:16.090Z | 332.294° NNW |
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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