Showing default

FLOCK 4BE 8, 60515

Orbit data source: Space-Track

FLOCK 4BE 8, 60515 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
60515, 2024-149AZ
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Planet
Mission
Non-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 8
1 60515U 24149AZ  26087.19685540  .01038093  53839-3  20523-2 0  9997
2 60515  97.3550 175.4858 0008997 270.9811  89.0436 16.00037161 90191
Epoch: 2026-03-28T04:43Z
TLE epoch observation values (Epoch: 2026-03-28T04:43:28.306Z)
Latitude
-0.00008°
Longitude
-81.00269°
Altitude
277.421 km
Speed
7.741 km/s
True Right ascension
11h 41m 56s
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
17:46:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
277.156 km
Perigee altitude
265.191 km
Semi-major axis
6,649.31 km
Eccentricity
0.0009
Inclination
97.355°
RAAN
175.4858°
Arg. of periapsis
270.9811°
True anomaly
89.14669°
Mean anomaly
89.0436°
Eccentric anomaly
89.09514°
Mean motion
4.00293 °/min
Orbital period
89.93 mins
BSTAR
0.0020523
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
|