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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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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4BE 31
1 60488U 24149W 25290.66169186 .00028552 00000-0 89338-3 0 9993
2 60488 97.4032 9.0220 0004077 66.8773 293.2899 15.33081039 65085Epoch: 2025-10-17T15:52Z
TLE epoch observation values (Epoch: 2025-10-17T15:52:50.176Z)
Latitude
0.00001°
Longitude
104.40908°
Altitude
468.632 km
Speed
7.633 km/s
True Right ascension
00h 36m 05s
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
20:59:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.364 km
Perigee altitude
460.785 km
Semi-major axis
6,841.712 km
Eccentricity
0.00041
Inclination
97.4032°
RAAN
9.022°
Arg. of periapsis
66.8773°
True anomaly
293.24698°
Mean anomaly
293.2899°
Eccentric anomaly
293.26844°
Mean motion
3.83527 °/min
Orbital period
93.87 mins
BSTAR
0.00089338
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-18 04:33:47.676Z | 111.243° ESE | 2025-10-18 04:35:47.676Z | 72.934° E | 17.673° | 2025-10-18 04:37:47.676Z | 31.747° NE |
| 4 mins | 2025-10-18 17:31:47.676Z | 58.304° ENE | 2025-10-18 17:33:47.676Z | 106.872° ESE | 20.475° | 2025-10-18 17:35:47.676Z | 145.299° SSE |
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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