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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4BE 30
1 60499U 24149AH 26126.20747741 .00082256 00000-0 15743-2 0 9992
2 60499 97.3779 210.6316 0002732 163.5491 196.5849 15.47762977 95263Epoch: 2026-05-06T04:58Z
TLE epoch observation values (Epoch: 2026-05-06T04:58:46.048Z)
Latitude
0.00006°
Longitude
-88.13155°
Altitude
428.182 km
Speed
7.654 km/s
True Right ascension
14h 02m 31s
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
20:42:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.057 km
Perigee altitude
418.342 km
Semi-major axis
6,798.336 km
Eccentricity
0.00027
Inclination
97.3779°
RAAN
210.6316°
Arg. of periapsis
163.5491°
True anomaly
196.57597°
Mean anomaly
196.5849°
Eccentric anomaly
196.58043°
Mean motion
3.87203 °/min
Orbital period
92.97 mins
BSTAR
0.0015743
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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 | 2026-05-06 17:57:08.571Z | 36.045° NE | 2026-05-06 18:00:08.571Z | 106.507° ESE | 25.082° | 2026-05-06 18:02:08.571Z | 153.376° SSE |
| 4 mins | 2026-05-07 05:57:08.571Z | 200.466° SSW | 2026-05-07 05:58:08.571Z | 236.033° WSW | 35.473° | 2026-05-07 06:01:08.571Z | 333.91° NNW |
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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