FLOCK 4G 29, 62642
Orbit data source: Space-Track
FLOCK 4G 29, 62642 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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62642 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
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 29
1 62642U 25009AK 25356.18759956 .00011501 00000-0 46061-3 0 9995
2 62642 97.4186 74.3608 0003066 174.4079 185.7194 15.25205807 51884Epoch: 2025-12-22T04:30Z
TLE epoch observation values (Epoch: 2025-12-22T04:30:08.601Z)
Latitude
-0.00002°
Longitude
-84.16433°
Altitude
495.36 km
Speed
7.616 km/s
True Right ascension
04h 57m 26s
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
23:00:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.232 km
Perigee altitude
485.022 km
Semi-major axis
6,865.264 km
Eccentricity
0.00031
Inclination
97.4186°
RAAN
74.3608°
Arg. of periapsis
174.4079°
True anomaly
185.7159°
Mean anomaly
185.7194°
Eccentric anomaly
185.71765°
Mean motion
3.81555 °/min
Orbital period
94.35 mins
BSTAR
0.00046061
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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 29 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 | 2025-12-23 05:50:18.970Z | 203.99° SW | 2025-12-23 05:52:18.970Z | 274.002° WNW | 33.387° | 2025-12-23 05:55:18.970Z | 332.676° NNW |
| 4 mins | 2025-12-23 18:52:18.970Z | 326.654° NNW | 2025-12-23 18:53:18.970Z | 299.64° NW | 25.996° | 2025-12-23 18:56:18.970Z | 230.511° WSW |
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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