FLOCK 4Q 29, 58304
Orbit data source: Space-Track
FLOCK 4Q 29, 58304 is a payload satellite owned by Planet (US) in SSO that was launched on Sat, 11 Nov 2023 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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58304 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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4Q 29
1 58304U 23174BA 25288.99749326 .00027746 00000-0 69417-3 0 9997
2 58304 97.4122 10.0205 0006730 301.2320 58.8266 15.40054259107987Epoch: 2025-10-15T23:56Z
TLE epoch observation values (Epoch: 2025-10-15T23:56:23.417Z)
Latitude
-0.00004°
Longitude
-13.84061°
Altitude
446.691 km
Speed
7.645 km/s
True Right ascension
00h 40m 04s
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
05:39:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.479 km
Perigee altitude
438.298 km
Semi-major axis
6,821.025 km
Eccentricity
0.00067
Inclination
97.4122°
RAAN
10.0205°
Arg. of periapsis
301.232°
True anomaly
58.89261°
Mean anomaly
58.8266°
Eccentric anomaly
58.8596°
Mean motion
3.85273 °/min
Orbital period
93.44 mins
BSTAR
0.00069417
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Other satellites on launch #174 in the year 2023 (2023-11-11 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 4Q 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-16 17:39:59.319Z | 49.268° ENE | 2025-10-16 17:41:59.319Z | 89.362° E | 19.258° | 2025-10-16 17:43:59.319Z | 134.903° SE |
| 4 mins | 2025-10-17 05:42:59.319Z | 183.148° SSW | 2025-10-17 05:43:59.319Z | 209.094° SW | 40.509° | 2025-10-17 05:46:59.319Z | 340.87° N |
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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