FLOCK 4BE 30, 60499
Orbit data source: Space-Track
FLOCK 4BE 30, 60499 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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60499 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: 13 hours ago
TLE from 13 hours ago
0 FLOCK 4BE 30
1 60499U 24149AH 25296.95034967 .00021639 00000-0 69281-3 0 9995
2 60499 97.4030 15.1380 0004353 54.2744 305.8902 15.32401415 65411Epoch: 2025-10-23T22:48Z
TLE epoch observation values (Epoch: 2025-10-23T22:48:30.211Z)
Latitude
-0.00005°
Longitude
0.40988°
Altitude
470.01 km
Speed
7.632 km/s
True Right ascension
01h 00m 33s
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
07:22:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.578 km
Perigee altitude
462.62 km
Semi-major axis
6,843.736 km
Eccentricity
0.00044
Inclination
97.403°
RAAN
15.138°
Arg. of periapsis
54.2744°
True anomaly
305.84978°
Mean anomaly
305.8902°
Eccentric anomaly
305.86999°
Mean motion
3.83357 °/min
Orbital period
93.91 mins
BSTAR
0.00069281
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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 30 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-24 18:10:17.574Z | 13.652° NNE | 2025-10-24 18:13:17.574Z | 91.777° ESE | 44.827° | 2025-10-24 18:16:17.574Z | 190.46° SSW |
| 4 mins | 2025-10-25 04:44:17.574Z | 114.251° SE | 2025-10-25 04:46:17.574Z | 64.928° ENE | 22.653° | 2025-10-25 04:48:17.574Z | 22.051° NNE |
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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