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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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4BE 30
1 60499U 24149AH 26171.47062337 .00125967 00000-0 17065-2 0 9998
2 60499 97.3766 257.1010 0004804 230.1488 129.9345 15.57242964102287Epoch: 2026-06-20T11:17Z
TLE epoch observation values (Epoch: 2026-06-20T11:17:41.859Z)
Latitude
-0.00002°
Longitude
178.99181°
Altitude
400.872 km
Speed
7.669 km/s
True Right ascension
17h 08m 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
07:24:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
395.808 km
Perigee altitude
389.303 km
Semi-major axis
6,770.693 km
Eccentricity
0.00048
Inclination
97.3766°
RAAN
257.101°
Arg. of periapsis
230.1488°
True anomaly
129.97669°
Mean anomaly
129.9345°
Eccentric anomaly
129.9556°
Mean motion
3.89577 °/min
Orbital period
92.41 mins
BSTAR
0.0017065
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 05:55:40.777Z | 177.85° S | 2026-06-21 05:58:40.777Z | 303.284° NW | 39.355° | 2026-06-21 06:00:40.777Z | 339.507° N |
| 4 mins | 2026-06-21 18:42:40.777Z | 2.99° NNE | 2026-06-21 18:43:40.777Z | 336.425° NNW | 42.31° | 2026-06-21 18:46:40.777Z | 198.379° SSW |
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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