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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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4G 35
1 62683U 25009CC 25286.48052291 .00033555 00000-0 13842-2 0 9996
2 62683 97.4222 5.1233 0006170 113.1339 247.0549 15.23961763 98902Epoch: 2025-10-13T11:31Z
TLE epoch observation values (Epoch: 2025-10-13T11:31:57.179Z)
Latitude
-0.00002°
Longitude
169.85236°
Altitude
498.656 km
Speed
7.614 km/s
True Right ascension
00h 20m 29s
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
13:49:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.104 km
Perigee altitude
486.628 km
Semi-major axis
6,869.003 km
Eccentricity
0.00062
Inclination
97.4222°
RAAN
5.1233°
Arg. of periapsis
113.1339°
True anomaly
246.98981°
Mean anomaly
247.0549°
Eccentric anomaly
247.02235°
Mean motion
3.81244 °/min
Orbital period
94.43 mins
BSTAR
0.0013842
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-14 04:59:54.608Z | 141.822° SSE | 2025-10-14 05:02:54.608Z | 71.107° E | 33.304° | 2025-10-14 05:05:54.608Z | 4.864° NNE |
| 5 mins | 2025-10-14 18:02:54.608Z | 24.845° NE | 2025-10-14 18:04:54.608Z | 80.803° E | 40.823° | 2025-10-14 18:07:54.608Z | 179.51° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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