Showing default

CAPELLA-19 (ACADIA), 67384

Orbit data source: Space-Track

CAPELLA-19 (ACADIA), 67384 is a payload satellite owned by Capella Space (US) in SSO that was launched on Sun, 11 Jan 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
67384, 2026-004X
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Capella Space
Mission
Operational Commercial Radar Imaging
Bus & Motor
ACADIA, Unknown motor
Mass
180 kg wet, ~150 kg dry
Launch date (UTC)
2026-01-11 (8 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 Dish + 1 Rod, 1.8 m
Radar Cross Section
0.463 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CAPELLA-19 (ACADIA)
1 67384U 26004X   26263.57294020  .00002040  00000-0  23582-3 0  9997
2 67384  97.8028 260.2431 0001604  93.2556 266.8843 14.86652252 37449
Epoch: 2026-09-20T13:45Z
TLE epoch observation values (Epoch: 2026-09-20T13:45:02.033Z)
Latitude
-0.00005°
Longitude
54.51945°
Altitude
611.499 km
Speed
7.553 km/s
True Right ascension
17h 20m 58s
True Declination
0° 00' 00"
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
11:32:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
606.552 km
Perigee altitude
604.312 km
Semi-major axis
6,983.569 km
Eccentricity
0.00016
Inclination
97.8028°
RAAN
260.2431°
Arg. of periapsis
93.2556°
True anomaly
266.86595°
Mean anomaly
266.8843°
Eccentric anomaly
266.87512°
Mean motion
3.71901 °/min
Orbital period
96.8 mins
BSTAR
0.00023582
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
|