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: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4G 12
1 62625U 25009S 26175.18747426 .00009679 00000-0 34286-3 0 9994
2 62625 97.4024 256.9950 0002553 284.5606 75.5351 15.29322263 79974Epoch: 2026-06-24T04:29Z
TLE epoch observation values (Epoch: 2026-06-24T04:29:57.776Z)
Latitude
0.00001°
Longitude
-82.84402°
Altitude
480.503 km
Speed
7.626 km/s
True Right ascension
17h 07m 58s
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
06:51:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.54 km
Perigee altitude
473.041 km
Semi-major axis
6,852.927 km
Eccentricity
0.00026
Inclination
97.4024°
RAAN
256.995°
Arg. of periapsis
284.5606°
True anomaly
75.56343°
Mean anomaly
75.5351°
Eccentric anomaly
75.54926°
Mean motion
3.82586 °/min
Orbital period
94.1 mins
BSTAR
0.00034286
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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 | 2026-06-25 05:45:00.003Z | 182.354° SSW | 2026-06-25 05:48:00.003Z | 271.571° WNW | 39.706° | 2026-06-25 05:51:00.003Z | 338.3° N |
| 5 mins | 2026-06-25 18:45:00.003Z | 351.23° N | 2026-06-25 18:47:00.003Z | 308.446° NW | 32.025° | 2026-06-25 18:50:00.003Z | 220.607° SW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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