Showing default

FLOCK 4BE 28, 60519

Orbit data source: Space-Track

FLOCK 4BE 28, 60519 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
60519, 2024-149BD
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 28
1 60519U 24149BD  26255.69005194  .00018132  00000-0  32683-3 0  9995
2 60519  97.3709 343.1046 0002878 359.6262   0.4987 15.49832729115978
Epoch: 2026-09-12T16:33Z
TLE epoch observation values (Epoch: 2026-09-12T16:33:40.487Z)
Latitude
-0°
Longitude
102.99047°
Altitude
418.391 km
Speed
7.661 km/s
True Right ascension
22h 52m 25s
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
22:02:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
416.094 km
Perigee altitude
412.185 km
Semi-major axis
6,792.277 km
Eccentricity
0.00029
Inclination
97.3709°
RAAN
343.1046°
Arg. of periapsis
359.6262°
True anomaly
0.49899°
Mean anomaly
0.4987°
Eccentric anomaly
0.49884°
Mean motion
3.87722 °/min
Orbital period
92.85 mins
BSTAR
0.00032683
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
|