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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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 2 days ago
TLE from 2 days ago
0 FLOCK 4Q 29
1 58304U 23174BA 26171.23997463 .00080981 00000-0 11328-2 0 9990
2 58304 97.3934 263.0897 0005567 133.6062 226.5656 15.56534096146238Epoch: 2026-06-20T05:45Z
TLE epoch observation values (Epoch: 2026-06-20T05:45:33.808Z)
Latitude
0.00004°
Longitude
-91.75861°
Altitude
403.432 km
Speed
7.667 km/s
True Right ascension
17h 32m 21s
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
21:41:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
398.384 km
Perigee altitude
390.843 km
Semi-major axis
6,772.751 km
Eccentricity
0.00056
Inclination
97.3934°
RAAN
263.0897°
Arg. of periapsis
133.6062°
True anomaly
226.5193°
Mean anomaly
226.5656°
Eccentric anomaly
226.54245°
Mean motion
3.894 °/min
Orbital period
92.45 mins
BSTAR
0.0011328
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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 | 2026-06-22 18:29:30.569Z | 43.589° NE | 2026-06-22 18:31:30.569Z | 92.907° ESE | 23.373° | 2026-06-22 18:33:30.569Z | 147.464° SSE |
| 4 mins | 2026-06-23 06:24:30.569Z | 188.134° SSW | 2026-06-23 06:26:30.569Z | 296.267° NW | 37.761° | 2026-06-23 06:28:30.569Z | 337.072° 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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