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.
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68485 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Capella Space
Mission
Operational Commercial Radar Imaging
Bus & Motor
ACADIA, Unknown motor
Mass
180 kg wet, ~150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 CAPELLA-20 (ACADIA)
1 68485U 26067BX 26255.11458465 .00004289 00000-0 43991-3 0 9998
2 68485 97.7693 212.0181 0002292 96.9234 263.2245 14.90952435 24683Epoch: 2026-09-12T02:45Z
TLE epoch observation values (Epoch: 2026-09-12T02:45:00.113Z)
Latitude
-0.00005°
Longitude
179.6394°
Altitude
598.194 km
Speed
7.561 km/s
True Right ascension
14h 08m 04s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:18:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.582 km
Perigee altitude
590.387 km
Semi-major axis
6,970.122 km
Eccentricity
0.00023
Inclination
97.7693°
RAAN
212.0181°
Arg. of periapsis
96.9234°
True anomaly
263.19842°
Mean anomaly
263.2245°
Eccentric anomaly
263.21146°
Mean motion
3.72977 °/min
Orbital period
96.52 mins
BSTAR
0.00043991
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Other satellites on launch #67 in the year 2026 (2026-03-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CAPELLA-20 (ACADIA) Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-12 20:36:05.218Z | 130.753° SE | 2026-09-12 20:39:05.218Z | 79.844° E | 31.492° | 2026-09-12 20:43:05.218Z | 8.177° NNE |
| 5 mins | 2026-09-12 22:13:05.218Z | 231.522° WSW | 2026-09-12 22:15:05.218Z | 266.818° W | 19.717° | 2026-09-12 22:18:05.218Z | 313.171° NW |
| 6 mins | 2026-09-13 09:56:05.218Z | 22.6° NE | 2026-09-13 09:59:05.218Z | 129.236° SE | 63.484° | 2026-09-13 10:02:05.218Z | 182.053° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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