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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4G 36
1 62675U 25009BU 26307.47869125 .00007245 00000-0 23800-3 0 9996
2 62675 97.3932 28.7298 0004769 167.0253 193.1112 15.31856406100207Epoch: 2026-11-03T11:29Z
TLE epoch observation values (Epoch: 2026-11-03T11:29:18.923Z)
Latitude
-0.00001°
Longitude
173.66018°
Altitude
476.562 km
Speed
7.626 km/s
True Right ascension
01h 54m 55s
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
15:56:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.488 km
Perigee altitude
463.959 km
Semi-major axis
6,845.36 km
Eccentricity
0.00048
Inclination
97.3932°
RAAN
28.7298°
Arg. of periapsis
167.0253°
True anomaly
193.09881°
Mean anomaly
193.1112°
Eccentric anomaly
193.105°
Mean motion
3.8322 °/min
Orbital period
93.94 mins
BSTAR
0.000238
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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 | 2026-11-04 04:52:51.141Z | 116.967° SE | 2026-11-04 04:54:51.141Z | 77.558° E | 22.011° | 2026-11-04 04:57:51.141Z | 18.553° NNE |
| 4 mins | 2026-11-04 17:51:51.141Z | 56.941° ENE | 2026-11-04 17:52:51.141Z | 81.988° E | 26.446° | 2026-11-04 17:55:51.141Z | 152.365° SSE |
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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