FLOCK 4G 12, 62625
Orbit data source: Space-Track
FLOCK 4G 12, 62625 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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62625 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: 21 hours ago
TLE from 21 hours ago
0 FLOCK 4G 12
1 62625U 25009S 26067.73677411 .00014451 00000-0 54695-3 0 9991
2 62625 97.4062 150.2139 0002866 316.3695 43.7317 15.27035121 63569Epoch: 2026-03-08T17:40Z
TLE epoch observation values (Epoch: 2026-03-08T17:40:57.283Z)
Latitude
0°
Longitude
78.53544°
Altitude
486.36 km
Speed
7.623 km/s
True Right ascension
10h 00m 51s
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
18:55:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.604 km
Perigee altitude
479.672 km
Semi-major axis
6,859.775 km
Eccentricity
0.00029
Inclination
97.4062°
RAAN
150.2139°
Arg. of periapsis
316.3695°
True anomaly
43.75441°
Mean anomaly
43.7317°
Eccentric anomaly
43.74305°
Mean motion
3.82013 °/min
Orbital period
94.24 mins
BSTAR
0.00054695
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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 12 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 | 2026-03-09 17:50:12.804Z | 31.843° NE | 2026-03-09 17:53:12.804Z | 99.161° ESE | 30.707° | 2026-03-09 17:56:12.804Z | 164.808° S |
| 4 mins | 2026-03-10 06:00:12.804Z | 222.185° SW | 2026-03-10 06:01:12.804Z | 252.067° W | 28.043° | 2026-03-10 06:04:12.804Z | 323.837° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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