Showing default

FLOCK 4H 9, 66712

Orbit data source: Space-Track

FLOCK 4H 9, 66712 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
66712, 2025-276AY
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)
2025-11-28 (2 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: 21 hours ago

TLE from 21 hours ago
0 FLOCK 4H 9
1 66712U 25276AY  26034.19884672  .00006963  00000-0  33961-3 0  9993
2 66712  97.4358 110.1114 0004797  91.3024 268.8760 15.18610668 10083
Epoch: 2026-02-03T04:46Z
TLE epoch observation values (Epoch: 2026-02-03T04:46:20.356Z)
Latitude
-0.00002°
Longitude
-94.85663°
Altitude
513.193 km
Speed
7.607 km/s
True Right ascension
07h 20m 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
04:09:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.31 km
Perigee altitude
503.705 km
Semi-major axis
6,885.145 km
Eccentricity
0.00048
Inclination
97.4358°
RAAN
110.1114°
Arg. of periapsis
91.3024°
True anomaly
268.82104°
Mean anomaly
268.876°
Eccentric anomaly
268.84852°
Mean motion
3.79904 °/min
Orbital period
94.76 mins
BSTAR
0.00033961
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
|