Showing default

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.

Loading next visibility...
Identifier
60499, 2024-149AH
Orbit
SSO
Country
Flag of USUS
Related 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)
2024-08-16 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 FLOCK 4BE 30
1 60499U 24149AH  26087.20368514  .00088887  00000-0  21297-2 0  9992
2 60499  97.3818 171.0277 0003342 212.6714 147.4326 15.41082484 89243
Epoch: 2026-03-28T04:53Z
TLE epoch observation values (Epoch: 2026-03-28T04:53:18.396Z)
Latitude
-0.00003°
Longitude
-87.92624°
Altitude
447.955 km
Speed
7.642 km/s
True Right ascension
11h 24m 06s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
17:46:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
442.129 km
Perigee altitude
437.571 km
Semi-major axis
6,817.987 km
Eccentricity
0.00033
Inclination
97.3818°
RAAN
171.0277°
Arg. of periapsis
212.6714°
True anomaly
147.45321°
Mean anomaly
147.4326°
Eccentric anomaly
147.4429°
Mean motion
3.85531 °/min
Orbital period
93.38 mins
BSTAR
0.0021297
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|