FLOCK 4Q 24, 58314 (Decayed)
Orbit data source: Space-Track
FLOCK 4Q 24, 58314 was a payload satellite owned by Planet (US) in LEO 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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58314 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Decayed 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: 2 years ago
TLE from 2 years ago
0 FLOCK 4Q 24
1 58314U 23174BL 25031.43405299 .12284974 25241-5 10054-2 0 9993
2 58314 97.3941 115.5814 0011895 285.6115 74.3872 16.39619024 68829Epoch: 2025-01-31T10:25Z
TLE epoch observation values (Epoch: 2025-01-31T10:25:02.178Z)
Latitude
0.00007°
Longitude
-171.5745°
Altitude
167.98 km
Speed
7.807 km/s
True Right ascension
07h 42m 19s
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
04:24:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
171.405 km
Perigee altitude
155.843 km
Semi-major axis
6,541.761 km
Eccentricity
0.00119
Inclination
97.3941°
RAAN
115.5814°
Arg. of periapsis
285.6115°
True anomaly
74.51853°
Mean anomaly
74.3872°
Eccentric anomaly
74.45286°
Mean motion
4.10205 °/min
Orbital period
87.76 mins
BSTAR
0.0010054
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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 24 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 | 2026-10-13 09:57:38.297Z | 163.916° S | 2026-10-13 09:59:38.297Z | 100.521° ESE | 85.567° | 2026-10-13 10:01:38.297Z | 350.657° N |
| 4 mins | 2026-10-13 11:40:38.297Z | 203.509° SW | 2026-10-13 11:41:38.297Z | 238.359° WSW | 69.087° | 2026-10-13 11:44:38.297Z | 356.304° N |
| 4 mins | 2026-10-13 11:57:38.297Z | 208.181° SW | 2026-10-13 11:59:38.297Z | 304.872° NW | 65.828° | 2026-10-13 12:01:38.297Z | 356.497° N |
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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