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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 12
1 62625U 25009S 26237.19038898 .00010769 00000-0 36759-3 0 9999
2 62625 97.3994 318.7510 0005539 76.3853 283.8005 15.30487501 89459Epoch: 2026-08-25T04:34Z
TLE epoch observation values (Epoch: 2026-08-25T04:34:09.607Z)
Latitude
0.00001°
Longitude
-83.25033°
Altitude
476.558 km
Speed
7.628 km/s
True Right ascension
21h 15m 00s
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
03:00:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.102 km
Perigee altitude
467.514 km
Semi-major axis
6,849.445 km
Eccentricity
0.00055
Inclination
97.3994°
RAAN
318.751°
Arg. of periapsis
76.3853°
True anomaly
283.73885°
Mean anomaly
283.8005°
Eccentric anomaly
283.76968°
Mean motion
3.82878 °/min
Orbital period
94.02 mins
BSTAR
0.00036759
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-26 18:47:44.915Z | 348.006° N | 2026-08-26 18:49:44.915Z | 292.434° WNW | 33.143° | 2026-08-26 18:52:44.915Z | 217.817° SW |
| 5 mins | 2026-08-27 05:21:44.915Z | 143.335° SSE | 2026-08-27 05:23:44.915Z | 46.041° ENE | 38.641° | 2026-08-27 05:26:44.915Z | 356.8° N |
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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