FLOCK 4Q 1, 58270
Orbit data source: Space-Track
FLOCK 4Q 1, 58270 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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58270 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: 1 day ago
TLE from 1 day ago
0 FLOCK 4Q 1
1 58270U 23174Q 25288.20481564 .00054805 00000-0 13812-2 0 9993
2 58270 97.4087 8.4020 0007150 325.9611 34.1176 15.39676099107828Epoch: 2025-10-15T04:54Z
TLE epoch observation values (Epoch: 2025-10-15T04:54:56.071Z)
Latitude
0.00006°
Longitude
-89.31388°
Altitude
446.143 km
Speed
7.647 km/s
True Right ascension
00h 33m 36s
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
01:34:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
448.884 km
Perigee altitude
439.128 km
Semi-major axis
6,822.143 km
Eccentricity
0.00072
Inclination
97.4087°
RAAN
8.402°
Arg. of periapsis
325.9611°
True anomaly
34.16359°
Mean anomaly
34.1176°
Eccentric anomaly
34.14059°
Mean motion
3.85178 °/min
Orbital period
93.46 mins
BSTAR
0.0013812
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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 1 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 18:54:56.022Z | 336.138° NNW | 2025-10-16 18:56:56.022Z | 281.303° WNW | 25.619° | 2025-10-16 18:58:56.022Z | 234.356° WSW |
| 4 mins | 2025-10-17 05:24:56.022Z | 153.519° SSE | 2025-10-17 05:26:56.022Z | 21.121° NNE | 40.258° | 2025-10-17 05:28:56.022Z | 354.551° 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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