FLOCK 4Q 7, 58318
Orbit data source: Space-Track
FLOCK 4Q 7, 58318 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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58318 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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4Q 7
1 58318U 23174BQ 25289.13497240 .00029850 00000-0 75032-3 0 9992
2 58318 97.4115 10.0402 0007472 295.5042 64.5431 15.39890743108009Epoch: 2025-10-16T03:14Z
TLE epoch observation values (Epoch: 2025-10-16T03:14:21.615Z)
Latitude
0.00001°
Longitude
-63.44891°
Altitude
447.36 km
Speed
7.645 km/s
True Right ascension
00h 40m 09s
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
05:40:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
448.469 km
Perigee altitude
438.275 km
Semi-major axis
6,821.509 km
Eccentricity
0.00075
Inclination
97.4115°
RAAN
10.0402°
Arg. of periapsis
295.5042°
True anomaly
64.62044°
Mean anomaly
64.5431°
Eccentric anomaly
64.58177°
Mean motion
3.85232 °/min
Orbital period
93.45 mins
BSTAR
0.00075032
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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 7 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 17:51:03.806Z | 45.257° ENE | 2025-10-16 17:53:03.806Z | 95.894° ESE | 25.751° | 2025-10-16 17:55:03.806Z | 148.182° SSE |
| 4 mins | 2025-10-17 05:54:03.806Z | 206.396° SW | 2025-10-17 05:55:03.806Z | 243.605° WSW | 34.697° | 2025-10-17 05:58:03.806Z | 332.153° NNW |
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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