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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 35
1 62683U 25009CC 26079.19873468 .00019231 00000-0 58195-3 0 9998
2 62683 97.4004 162.2527 0003348 257.7681 102.3187 15.34228857123003Epoch: 2026-03-20T04:46Z
TLE epoch observation values (Epoch: 2026-03-20T04:46:10.676Z)
Latitude
-0.00002°
Longitude
-87.02902°
Altitude
466.811 km
Speed
7.633 km/s
True Right ascension
10h 49m 00s
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
15:54:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.448 km
Perigee altitude
457.869 km
Semi-major axis
6,838.296 km
Eccentricity
0.00033
Inclination
97.4004°
RAAN
162.2527°
Arg. of periapsis
257.7681°
True anomaly
102.35618°
Mean anomaly
102.3187°
Eccentric anomaly
102.33744°
Mean motion
3.83814 °/min
Orbital period
93.8 mins
BSTAR
0.00058195
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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 | 2026-03-21 18:54:28.129Z | 335.15° NNW | 2026-03-21 18:56:28.129Z | 277.717° WNW | 26.439° | 2026-03-21 18:58:28.129Z | 232.471° WSW |
| 5 mins | 2026-03-22 05:26:28.129Z | 157.115° SSE | 2026-03-22 05:28:28.129Z | 27.129° NE | 42.644° | 2026-03-22 05:31:28.129Z | 351.874° 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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