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: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4G 35
1 62683U 25009CC 26171.18790472 .00028540 00000-0 72158-3 0 9991
2 62683 97.3965 254.8404 0002663 294.2662 65.8306 15.39746262137139Epoch: 2026-06-20T04:30Z
TLE epoch observation values (Epoch: 2026-06-20T04:30:34.967Z)
Latitude
0.00001°
Longitude
-81.21142°
Altitude
449.232 km
Speed
7.643 km/s
True Right ascension
16h 59m 21s
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
10:19:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.615 km
Perigee altitude
441.981 km
Semi-major axis
6,821.935 km
Eccentricity
0.00027
Inclination
97.3965°
RAAN
254.8404°
Arg. of periapsis
294.2662°
True anomaly
65.85844°
Mean anomaly
65.8306°
Eccentric anomaly
65.84452°
Mean motion
3.85196 °/min
Orbital period
93.46 mins
BSTAR
0.00072158
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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 | 2026-06-21 05:35:49.432Z | 163.341° S | 2026-06-21 05:38:49.432Z | 4.999° NNE | 41.722° | 2026-06-21 05:40:49.432Z | 350.93° N |
| 5 mins | 2026-06-21 18:30:49.432Z | 10.187° NNE | 2026-06-21 18:32:49.432Z | 249.106° W | 44.879° | 2026-06-21 18:35:49.432Z | 194.518° 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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