Showing default

FLOCK 4H 3, 66706

Orbit data source: Space-Track

FLOCK 4H 3, 66706 is a payload satellite owned by Planet (US) in SSO that was launched on Fri, 28 Nov 2025 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
66706, 2025-276AS
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Planet
Mission
Partially operational Commercial Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5.7 kg wet, 5.7 kg dry
Launch date (UTC)
2025-11-28 (6 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, 1.0 m
Radar Cross Section
0.072 m²

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 FLOCK 4H 3
1 66706U 25276AS  26141.13805683  .00004205  00000-0  20066-3 0  9993
2 66706  97.4244 215.2344 0005653  98.0450 262.1426 15.19593947 26311
Epoch: 2026-05-21T03:18Z
TLE epoch observation values (Epoch: 2026-05-21T03:18:48.110Z)
Latitude
-0.00004°
Longitude
-73.25362°
Altitude
510.691 km
Speed
7.608 km/s
True Right ascension
14h 20m 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
02:09:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.925 km
Perigee altitude
500.144 km
Semi-major axis
6,882.171 km
Eccentricity
0.00057
Inclination
97.4244°
RAAN
215.2344°
Arg. of periapsis
98.045°
True anomaly
262.07844°
Mean anomaly
262.1426°
Eccentric anomaly
262.11052°
Mean motion
3.8015 °/min
Orbital period
94.7 mins
BSTAR
0.00020066
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
|