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: 18 hours ago
TLE from 18 hours ago
0 FLOCK 4G 29
1 62642U 25009AK 25308.66775684 .00011963 00000-0 49974-3 0 9999
2 62642 97.4238 27.2953 0003142 33.5044 326.6391 15.23774512 44647Epoch: 2025-11-04T16:01Z
TLE epoch observation values (Epoch: 2025-11-04T16:01:34.190Z)
Latitude
-0.00009°
Longitude
102.75137°
Altitude
495.759 km
Speed
7.618 km/s
True Right ascension
01h 49m 10s
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
06:01:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.588 km
Perigee altitude
489.271 km
Semi-major axis
6,869.566 km
Eccentricity
0.00031
Inclination
97.4238°
RAAN
27.2953°
Arg. of periapsis
33.5044°
True anomaly
326.61929°
Mean anomaly
326.6391°
Eccentric anomaly
326.6292°
Mean motion
3.81197 °/min
Orbital period
94.44 mins
BSTAR
0.00049974
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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 | 2025-11-05 17:48:57.102Z | 35.555° NE | 2025-11-05 17:50:57.102Z | 77.653° E | 30.285° | 2025-11-05 17:53:57.102Z | 161.143° S |
| 4 mins | 2025-11-06 05:59:57.102Z | 222.915° SW | 2025-11-06 06:00:57.102Z | 250.361° W | 26.648° | 2025-11-06 06:03:57.102Z | 321.446° NNW |
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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