FLOCK 4G 35, 62683
Orbit data source: Space-Track
FLOCK 4G 35, 62683 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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62683 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Non-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 35
1 62683U 25009CC 26261.48829366 .00031145 00000-0 65282-3 0 9994
2 62683 97.3905 346.4326 0002577 347.5908 12.5277 15.45353810151056Epoch: 2026-09-18T11:43Z
TLE epoch observation values (Epoch: 2026-09-18T11:43:08.572Z)
Latitude
-0°
Longitude
173.23642°
Altitude
431.751 km
Speed
7.654 km/s
True Right ascension
23h 05m 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
01:54:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.024 km
Perigee altitude
425.516 km
Semi-major axis
6,805.407 km
Eccentricity
0.00026
Inclination
97.3905°
RAAN
346.4326°
Arg. of periapsis
347.5908°
True anomaly
12.53411°
Mean anomaly
12.5277°
Eccentric anomaly
12.5309°
Mean motion
3.866 °/min
Orbital period
93.12 mins
BSTAR
0.00065282
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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 35 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-19 19:21:59.996Z | 327.006° NNW | 2026-09-19 19:23:59.996Z | 276.911° WNW | 21.205° | 2026-09-19 19:25:59.996Z | 238.724° WSW |
| 5 mins | 2026-09-20 05:48:59.996Z | 165.763° S | 2026-09-20 05:50:59.996Z | 100.047° ESE | 86.821° | 2026-09-20 05:53:59.996Z | 348.852° N |
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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