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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4G 25
1 62646U 25009AP 26136.19060793 .00006995 00000-0 25276-3 0 9997
2 62646 97.4021 218.4319 0003325 83.3929 276.7690 15.28774659 74039Epoch: 2026-05-16T04:34Z
TLE epoch observation values (Epoch: 2026-05-16T04:34:28.525Z)
Latitude
0.00007°
Longitude
-84.09809°
Altitude
482.308 km
Speed
7.624 km/s
True Right ascension
14h 33m 43s
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
20:23:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.707 km
Perigee altitude
474.149 km
Semi-major axis
6,854.565 km
Eccentricity
0.00033
Inclination
97.4021°
RAAN
218.4319°
Arg. of periapsis
83.3929°
True anomaly
276.73116°
Mean anomaly
276.769°
Eccentric anomaly
276.75008°
Mean motion
3.82449 °/min
Orbital period
94.13 mins
BSTAR
0.00025276
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-16 17:42:30.998Z | 39.474° NE | 2026-05-16 17:45:30.998Z | 101.853° ESE | 23.621° | 2026-05-16 17:47:30.998Z | 146.067° SSE |
| 5 mins | 2026-05-17 05:50:30.998Z | 191.97° SSW | 2026-05-17 05:52:30.998Z | 240.262° WSW | 35.228° | 2026-05-17 05:55:30.998Z | 331.555° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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