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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4BE 31
1 60488U 24149W 26276.93205047 .00034879 00000-0 63912-3 0 9994
2 60488 97.3735 4.1417 0002484 203.9025 156.2112 15.49233453119185Epoch: 2026-10-03T22:22Z
TLE epoch observation values (Epoch: 2026-10-03T22:22:09.160Z)
Latitude
0.00006°
Longitude
15.97097°
Altitude
423.643 km
Speed
7.656 km/s
True Right ascension
00h 16m 34s
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
02:50:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
417.58 km
Perigee altitude
414.205 km
Semi-major axis
6,794.03 km
Eccentricity
0.00025
Inclination
97.3735°
RAAN
4.1417°
Arg. of periapsis
203.9025°
True anomaly
156.22268°
Mean anomaly
156.2112°
Eccentric anomaly
156.21694°
Mean motion
3.87572 °/min
Orbital period
92.89 mins
BSTAR
0.00063912
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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 | 2026-10-04 19:04:19.189Z | 359.614° N | 2026-10-04 19:07:19.189Z | 273.457° WNW | 48.904° | 2026-10-04 19:09:19.189Z | 214.575° SW |
| 4 mins | 2026-10-05 05:31:19.189Z | 123.85° SE | 2026-10-05 05:33:19.189Z | 61.298° ENE | 30.924° | 2026-10-05 05:35:19.189Z | 14.354° 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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