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FLOCK 4BE 24, 60505

Orbit data source: Space-Track

FLOCK 4BE 24, 60505 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.

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Identifier
60505, 2024-149AP
Orbit
SSO
Last TLE update
1 day ago
Origin
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 (11 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 1 day ago
0 FLOCK 4BE 24
1 60505U 24149AP  25198.66674242  .00008577  00000-0  30101-3 0  9993
2 60505  97.4035 276.9361 0005686  51.3674 308.8075 15.29649296 51012
Epoch: 2025-07-17T16:00Z
TLE epoch observation values (Epoch: 2025-07-17T16:00:06.545Z)
Latitude
0.00004°
Longitude
101.17955°
Altitude
477.521 km
Speed
7.628 km/s
True Right ascension
18h 27m 44s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
51.30101°
Longitude
-68.53768°
Altitude
484.477 km
Speed
7.628 km/s
Apparent Right ascension
12h 49m 08s
Apparent Declination
24° 40' 02"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
04:52:59
Azimuth
52.797° ENE
Elevation
-4.043°
Doppler factor
1
Orbital elements
Apogee altitude
477.709 km
Perigee altitude
469.917 km
Semi-major axis
6,851.95 km
Eccentricity
0.00057
Inclination
97.4035°
RAAN
276.9361°
Arg. of periapsis
51.3674°
True anomaly
308.7567°
Mean anomaly
308.8075°
Eccentric anomaly
308.7821°
Mean motion
3.82668 °/min
Orbital period
94.08 mins
BSTAR
0.00030101
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