FLOCK 4BE 31, 60488
Orbit data source: Space-Track
FLOCK 4BE 31, 60488 is a payload satellite owned by Planet (US) in SSO that was launched on Fri, 16 Aug 2024 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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60488 intel report (Beta)
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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 4BE 31
1 60488U 24149W 26175.21154371 .00018203 00000-0 39649-3 0 9999
2 60488 97.3796 260.6028 0002072 209.0117 151.1017 15.44327660103462Epoch: 2026-06-24T05:04Z
TLE epoch observation values (Epoch: 2026-06-24T05:04:37.376Z)
Latitude
0.00002°
Longitude
-87.92495°
Altitude
437.714 km
Speed
7.649 km/s
True Right ascension
17h 22m 24s
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
19:18:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.697 km
Perigee altitude
428.876 km
Semi-major axis
6,808.424 km
Eccentricity
0.00021
Inclination
97.3796°
RAAN
260.6028°
Arg. of periapsis
209.0117°
True anomaly
151.11317°
Mean anomaly
151.1017°
Eccentric anomaly
151.10744°
Mean motion
3.86343 °/min
Orbital period
93.18 mins
BSTAR
0.00039649
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Other satellites on launch #149 in the year 2024 (2024-08-16 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 4BE 31 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 | 2026-06-25 18:57:28.872Z | 351.917° N | 2026-06-25 18:59:28.872Z | 304.451° NW | 32.399° | 2026-06-25 19:02:28.872Z | 217.283° SW |
| 4 mins | 2026-06-26 05:26:28.872Z | 124.209° SE | 2026-06-26 05:27:28.872Z | 86.235° E | 33.225° | 2026-06-26 05:30:28.872Z | 4.536° NNE |
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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