FLOCK 4G 36, 62675
Orbit data source: Space-Track
FLOCK 4G 36, 62675 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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62675 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 36
1 62675U 25009BU 26215.78090030 .00011331 00000-0 38996-3 0 9992
2 62675 97.3993 297.3161 0005876 139.5724 220.5954 15.30207038 86172Epoch: 2026-08-03T18:44Z
TLE epoch observation values (Epoch: 2026-08-03T18:44:29.785Z)
Latitude
-0.00008°
Longitude
63.83292°
Altitude
481.358 km
Speed
7.623 km/s
True Right ascension
19h 49m 15s
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
17:44:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.171 km
Perigee altitude
468.121 km
Semi-major axis
6,850.283 km
Eccentricity
0.00059
Inclination
97.3993°
RAAN
297.3161°
Arg. of periapsis
139.5724°
True anomaly
220.55161°
Mean anomaly
220.5954°
Eccentric anomaly
220.5735°
Mean motion
3.82807 °/min
Orbital period
94.04 mins
BSTAR
0.00038996
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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 36 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 | 2026-08-05 05:24:12.873Z | 156.252° SSE | 2026-08-05 05:27:12.873Z | 28.031° NE | 40.241° | 2026-08-05 05:29:12.873Z | 356.254° N |
| 5 mins | 2026-08-05 18:24:12.873Z | 11.236° NNE | 2026-08-05 18:26:12.873Z | 198.359° SSW | 43.733° | 2026-08-05 18:29:12.873Z | 193.576° 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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