FLOCK 4Q 34, 58316
Orbit data source: Space-Track
FLOCK 4Q 34, 58316 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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58316 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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4Q 34
1 58316U 23174BN 25335.23601019 .00037959 00000-0 76844-3 0 9995
2 58316 97.4026 57.4978 0008142 131.8066 228.3880 15.46301558115188Epoch: 2025-12-01T05:39Z
TLE epoch observation values (Epoch: 2025-12-01T05:39:51.280Z)
Latitude
-0.00003°
Longitude
-97.80428°
Altitude
434.366 km
Speed
7.649 km/s
True Right ascension
03h 49m 59s
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
09:16:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
430.026 km
Perigee altitude
418.948 km
Semi-major axis
6,802.624 km
Eccentricity
0.00081
Inclination
97.4026°
RAAN
57.4978°
Arg. of periapsis
131.8066°
True anomaly
228.31829°
Mean anomaly
228.388°
Eccentric anomaly
228.35314°
Mean motion
3.86837 °/min
Orbital period
93.06 mins
BSTAR
0.00076844
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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 34 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 | 2025-12-01 18:39:01.117Z | 4.723° NNE | 2025-12-01 18:41:01.117Z | 327.394° NNW | 41.359° | 2025-12-01 18:44:01.117Z | 201.422° SSW |
| 4 mins | 2025-12-02 05:07:01.117Z | 112.489° ESE | 2025-12-02 05:08:01.117Z | 87.334° E | 22.591° | 2025-12-02 05:11:01.117Z | 16.068° NNE |
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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