FLOCK 4G 25, 62646
Orbit data source: Space-Track
FLOCK 4G 25, 62646 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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62646 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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4G 25
1 62646U 25009AP 26079.94740538 .00010117 00000-0 37707-3 0 9991
2 62646 97.4044 162.5375 0001017 212.3235 147.7942 15.27635629 65449Epoch: 2026-03-20T22:44Z
TLE epoch observation values (Epoch: 2026-03-20T22:44:15.824Z)
Latitude
-0.00006°
Longitude
2.99641°
Altitude
486.574 km
Speed
7.622 km/s
True Right ascension
10h 50m 09s
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
14:09:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.536 km
Perigee altitude
479.141 km
Semi-major axis
6,857.975 km
Eccentricity
0.0001
Inclination
97.4044°
RAAN
162.5375°
Arg. of periapsis
212.3235°
True anomaly
147.80041°
Mean anomaly
147.7942°
Eccentric anomaly
147.79731°
Mean motion
3.82164 °/min
Orbital period
94.2 mins
BSTAR
0.00037707
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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 25 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 | 2026-03-21 18:10:14.243Z | 20.178° NNE | 2026-03-21 18:13:14.243Z | 145.877° SSE | 40.718° | 2026-03-21 18:16:14.243Z | 184.469° SSW |
| 4 mins | 2026-03-22 04:46:14.243Z | 101.958° ESE | 2026-03-22 04:47:14.243Z | 78.756° E | 20.873° | 2026-03-22 04:50:14.243Z | 18.89° NNE |
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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