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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4G 35
1 62683U 25009CC 26307.54118743 .00037439 00000-0 69250-3 0 9993
2 62683 97.3882 33.4299 0003916 159.8515 200.2891 15.48944786158177Epoch: 2026-11-03T12:59Z
TLE epoch observation values (Epoch: 2026-11-03T12:59:18.593Z)
Latitude
-0.00006°
Longitude
155.80006°
Altitude
425.439 km
Speed
7.655 km/s
True Right ascension
02h 13m 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
19:20:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419.399 km
Perigee altitude
414.077 km
Semi-major axis
6,794.875 km
Eccentricity
0.00039
Inclination
97.3882°
RAAN
33.4299°
Arg. of periapsis
159.8515°
True anomaly
200.27355°
Mean anomaly
200.2891°
Eccentric anomaly
200.28132°
Mean motion
3.87499 °/min
Orbital period
92.9 mins
BSTAR
0.0006925
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-04 06:10:12.299Z | 184.449° SSW | 2026-11-04 06:13:12.299Z | 288.337° WNW | 48.24° | 2026-11-04 06:15:12.299Z | 333.883° NNW |
| 4 mins | 2026-11-04 19:01:12.299Z | 349.04° N | 2026-11-04 19:02:12.299Z | 319.083° NNW | 45.802° | 2026-11-04 19:05:12.299Z | 210.773° SW |
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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