Showing default

FLOCK 4BE 14, 60517

Orbit data source: Space-Track

FLOCK 4BE 14, 60517 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.

Not visible in the next 10 days
Identifier
60517, 2024-149BB
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 (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: 13 hours ago

TLE from 13 hours ago
0 FLOCK 4BE 14
1 60517U 24149BB  26255.68978962  .00028177  00000-0  62111-3 0  9993
2 60517  97.3651 340.3590 0003340 349.6234  10.4945 15.43881914115810
Epoch: 2026-09-12T16:33Z
TLE epoch observation values (Epoch: 2026-09-12T16:33:17.823Z)
Latitude
0.00003°
Longitude
100.33955°
Altitude
435.551 km
Speed
7.652 km/s
True Right ascension
22h 41m 26s
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
22:03:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
433.872 km
Perigee altitude
429.323 km
Semi-major axis
6,809.735 km
Eccentricity
0.00033
Inclination
97.3651°
RAAN
340.359°
Arg. of periapsis
349.6234°
True anomaly
10.50147°
Mean anomaly
10.4945°
Eccentric anomaly
10.49799°
Mean motion
3.86232 °/min
Orbital period
93.21 mins
BSTAR
0.00062111
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
|