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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Edit Public Description
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 36
1 62675U 25009BU 25286.47488146 .00018664 00000-0 79789-3 0 9995
2 62675 97.4239 5.1769 0006636 111.4183 248.7762 15.22874287 41265Epoch: 2025-10-13T11:23Z
TLE epoch observation values (Epoch: 2025-10-13T11:23:49.758Z)
Latitude
-0.00001°
Longitude
171.94244°
Altitude
501.924 km
Speed
7.612 km/s
True Right ascension
00h 20m 42s
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
21:21:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.699 km
Perigee altitude
489.578 km
Semi-major axis
6,872.276 km
Eccentricity
0.00066
Inclination
97.4239°
RAAN
5.1769°
Arg. of periapsis
111.4183°
True anomaly
248.70534°
Mean anomaly
248.7762°
Eccentric anomaly
248.74077°
Mean motion
3.80971 °/min
Orbital period
94.5 mins
BSTAR
0.00079789
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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 | 2025-10-14 04:52:52.386Z | 133.024° SE | 2025-10-14 04:55:52.386Z | 62.384° ENE | 28.281° | 2025-10-14 04:57:52.386Z | 16.523° NNE |
| 5 mins | 2025-10-14 17:56:52.386Z | 40.678° NE | 2025-10-14 17:58:52.386Z | 127.526° SE | 35.166° | 2025-10-14 18:01:52.386Z | 175.493° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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