Showing default

FLOCK 4BE 9, 60514

Orbit data source: Space-Track

FLOCK 4BE 9, 60514 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
60514, 2024-149AY
Orbit
SSO
Country
Flag of USUS
Related 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)
2024-08-16 (1 year 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: 7 hours ago

TLE from 7 hours ago
0 FLOCK 4BE 9
1 60514U 24149AY  26036.20422315  .00023083  00000-0  65139-3 0  9995
2 60514  97.3884 119.5797 0003729  69.8483 290.3162 15.36388536 82028
Epoch: 2026-02-05T04:54Z
TLE epoch observation values (Epoch: 2026-02-05T04:54:04.880Z)
Latitude
Longitude
-89.30044°
Altitude
459.028 km
Speed
7.638 km/s
True Right ascension
07h 58m 19s
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
14:08:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.29 km
Perigee altitude
451.195 km
Semi-major axis
6,831.88 km
Eccentricity
0.00037
Inclination
97.3884°
RAAN
119.5797°
Arg. of periapsis
69.8483°
True anomaly
290.27612°
Mean anomaly
290.3162°
Eccentric anomaly
290.29616°
Mean motion
3.84355 °/min
Orbital period
93.66 mins
BSTAR
0.00065139
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
|