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: 21 hours ago
TLE from 21 hours ago
0 FLOCK 4G 25
1 62646U 25009AP 26261.49934135 .00007878 00000-0 26471-3 0 9998
2 62646 97.3955 343.2426 0001479 23.8599 336.2710 15.31105779 93198Epoch: 2026-09-18T11:59Z
TLE epoch observation values (Epoch: 2026-09-18T11:59:03.092Z)
Latitude
-0.00008°
Longitude
166.05838°
Altitude
474.69 km
Speed
7.629 km/s
True Right ascension
22h 52m 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
01:34:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.475 km
Perigee altitude
468.45 km
Semi-major axis
6,847.599 km
Eccentricity
0.00015
Inclination
97.3955°
RAAN
343.2426°
Arg. of periapsis
23.8599°
True anomaly
336.26418°
Mean anomaly
336.271°
Eccentric anomaly
336.26759°
Mean motion
3.83033 °/min
Orbital period
93.99 mins
BSTAR
0.00026471
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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 | 2026-09-19 18:21:04.635Z | 16.467° NNE | 2026-09-19 18:24:04.635Z | 159.781° S | 66.041° | 2026-09-19 18:27:04.635Z | 188.152° SSW |
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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