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: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4G 29
1 62642U 25009AK 25312.21373090 .00016201 00000-0 67303-3 0 9996
2 62642 97.4227 30.8042 0002865 21.9599 338.1761 15.23892329 45187Epoch: 2025-11-08T05:07Z
TLE epoch observation values (Epoch: 2025-11-08T05:07:46.349Z)
Latitude
0.00001°
Longitude
-93.78549°
Altitude
495.381 km
Speed
7.618 km/s
True Right ascension
02h 03m 13s
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
16:43:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.043 km
Perigee altitude
489.107 km
Semi-major axis
6,869.212 km
Eccentricity
0.00029
Inclination
97.4227°
RAAN
30.8042°
Arg. of periapsis
21.9599°
True anomaly
338.16389°
Mean anomaly
338.1761°
Eccentric anomaly
338.17°
Mean motion
3.81226 °/min
Orbital period
94.43 mins
BSTAR
0.00067303
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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 | 2025-11-09 04:54:40.954Z | 129.808° SE | 2025-11-09 04:56:40.954Z | 85.992° E | 28.174° | 2025-11-09 04:59:40.954Z | 12.45° NNE |
| 5 mins | 2025-11-09 17:57:40.954Z | 38.495° NE | 2025-11-09 17:59:40.954Z | 119.998° SE | 35.973° | 2025-11-09 18:02:40.954Z | 174.765° 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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