Showing default

FLOCK 4BE 20, 60489

Orbit data source: Space-Track

FLOCK 4BE 20, 60489 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
60489, 2024-149X
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: 17 hours ago

TLE from 17 hours ago
0 FLOCK 4BE 20
1 60489U 24149X   26199.53112499  .00007342  00000-0  19307-3 0  9997
2 60489  97.3686 281.7106 0005283 144.5593 215.6004 15.38867209107030
Epoch: 2026-07-18T12:44Z
TLE epoch observation values (Epoch: 2026-07-18T12:44:49.199Z)
Latitude
-0.00004°
Longitude
154.16307°
Altitude
455.509 km
Speed
7.638 km/s
True Right ascension
18h 46m 50s
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
18:52:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.002 km
Perigee altitude
442.792 km
Semi-major axis
6,824.534 km
Eccentricity
0.00053
Inclination
97.3686°
RAAN
281.7106°
Arg. of periapsis
144.5593°
True anomaly
215.56518°
Mean anomaly
215.6004°
Eccentric anomaly
215.58279°
Mean motion
3.84976 °/min
Orbital period
93.51 mins
BSTAR
0.00019307
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
|