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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4Q 29
1 58304U 23174BA 25338.13312522 .00051330 00000-0 11503-2 0 9991
2 58304 97.4088 59.8935 0008257 126.6311 233.5697 15.43231126115559Epoch: 2025-12-04T03:11Z
TLE epoch observation values (Epoch: 2025-12-04T03:11:42.019Z)
Latitude
-0.00001°
Longitude
-61.22552°
Altitude
443.048 km
Speed
7.644 km/s
True Right ascension
03h 59m 34s
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
08:08:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
439.14 km
Perigee altitude
427.891 km
Semi-major axis
6,811.653 km
Eccentricity
0.00083
Inclination
97.4088°
RAAN
59.8935°
Arg. of periapsis
126.6311°
True anomaly
233.49362°
Mean anomaly
233.5697°
Eccentric anomaly
233.53165°
Mean motion
3.86069 °/min
Orbital period
93.25 mins
BSTAR
0.0011503
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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 | 2025-12-04 17:46:22.464Z | 49.756° ENE | 2025-12-04 17:48:22.464Z | 91.173° ESE | 18.838° | 2025-12-04 17:50:22.464Z | 136.578° SSE |
| 5 mins | 2025-12-05 05:47:22.464Z | 177.985° S | 2025-12-05 05:49:22.464Z | 268.218° W | 43.265° | 2025-12-05 05:52:22.464Z | 343.03° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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