Showing default

AC1-002, 66745

Orbit data source: Space-Track

AC1-002, 66745 is a UK payload satellite 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
66745, 2025-276CH
Orbit
SSO
Country
Flag of UKUK
Related business
Manufacturer
INSBAE
Mission
Operational spacecraft
Bus & Motor
P10, Unknown motor
Mass
140 kg wet, 140 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
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 AC1-002
1 66745U 25276CH  26034.15925498  .00003232  00000-0  16355-3 0  9991
2 66745  97.4343 109.9930 0003753  95.4152 264.7510 15.17717648 10075
Epoch: 2026-02-03T03:49Z
TLE epoch observation values (Epoch: 2026-02-03T03:49:19.630Z)
Latitude
-0.00001°
Longitude
-80.68298°
Altitude
516.064 km
Speed
7.605 km/s
True Right ascension
07h 19m 58s
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
04:16:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.295 km
Perigee altitude
507.125 km
Semi-major axis
6,887.847 km
Eccentricity
0.00038
Inclination
97.4343°
RAAN
109.993°
Arg. of periapsis
95.4152°
True anomaly
264.70818°
Mean anomaly
264.751°
Eccentric anomaly
264.72959°
Mean motion
3.7968 °/min
Orbital period
94.82 mins
BSTAR
0.00016355
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
|