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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4BE 30
1 60499U 24149AH 25311.18279814 .00019291 00000-0 60654-3 0 9996
2 60499 97.4016 29.3730 0003318 7.5562 352.5729 15.33008985 67593Epoch: 2025-11-07T04:23Z
TLE epoch observation values (Epoch: 2025-11-07T04:23:13.759Z)
Latitude
-0.00007°
Longitude
-83.06475°
Altitude
467.696 km
Speed
7.634 km/s
True Right ascension
01h 57m 29s
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
08:20:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.059 km
Perigee altitude
461.519 km
Semi-major axis
6,841.926 km
Eccentricity
0.00033
Inclination
97.4016°
RAAN
29.373°
Arg. of periapsis
7.5562°
True anomaly
352.56798°
Mean anomaly
352.5729°
Eccentric anomaly
352.57044°
Mean motion
3.83509 °/min
Orbital period
93.87 mins
BSTAR
0.00060654
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-07 17:29:42.425Z | 49.303° ENE | 2025-11-07 17:31:42.425Z | 89.11° E | 19.882° | 2025-11-07 17:33:42.425Z | 134.519° SE |
| 5 mins | 2025-11-08 05:35:42.425Z | 185.616° SSW | 2025-11-08 05:37:42.425Z | 281.823° WNW | 40.875° | 2025-11-08 05:40:42.425Z | 340.544° N |
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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