Showing default

CAPELLA-20 (ACADIA), 68485

Orbit data source: Space-Track

CAPELLA-20 (ACADIA), 68485 is a payload satellite owned by Capella Space (US) in SSO that was launched on Mon, 30 Mar 2026 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
68485, 2026-067BX
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Capella Space
Mission
Operational spacecraft
Bus & Motor
ACADIA, Unknown motor
Mass
180 kg wet, ~150 kg dry
Launch date (UTC)
2026-03-30 (3 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 CAPELLA-20 (ACADIA)
1 68485U 26067BX  26171.33336806 -.00225659  00000-0 -23062-1 0  9996
2 68485  97.7583 129.5752 0001085  34.8742  80.0845 14.91894341  5751
Epoch: 2026-06-20T08:00Z
TLE epoch observation values (Epoch: 2026-06-20T08:00:03.000Z)
Latitude
64.01851°
Longitude
-62.84326°
Altitude
602.935 km
Speed
7.564 km/s
True Right ascension
21h 42m 52s
True Declination
63° 52' 47"
Sunlit
Object was in daylight 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
07:28:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.804 km
Perigee altitude
588.292 km
Semi-major axis
6,967.185 km
Eccentricity
0.00011
Inclination
97.7583°
RAAN
129.5752°
Arg. of periapsis
34.8742°
True anomaly
80.09675°
Mean anomaly
80.0845°
Eccentric anomaly
80.09062°
Mean motion
3.73213 °/min
Orbital period
96.46 mins
BSTAR
-0.023062
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
|