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: 2 days ago
TLE from 2 days ago
0 CAPELLA-20 (ACADIA)
1 68485U 26067BX 26258.60461481 .00004518 00000-0 46450-3 0 9995
2 68485 97.7772 215.4456 0001260 75.4041 284.7317 14.90828795 25203Epoch: 2026-09-15T14:30Z
TLE epoch observation values (Epoch: 2026-09-15T14:30:38.719Z)
Latitude
-0.00002°
Longitude
3.2161°
Altitude
598.166 km
Speed
7.561 km/s
True Right ascension
14h 21m 46s
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
06:19:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.249 km
Perigee altitude
591.493 km
Semi-major axis
6,970.508 km
Eccentricity
0.00013
Inclination
97.7772°
RAAN
215.4456°
Arg. of periapsis
75.4041°
True anomaly
284.71774°
Mean anomaly
284.7317°
Eccentric anomaly
284.72472°
Mean motion
3.72947 °/min
Orbital period
96.53 mins
BSTAR
0.0004645
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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 | 2026-09-17 21:24:20.384Z | 176.83° S | 2026-09-17 21:27:20.384Z | 251.096° W | 69.602° | 2026-09-17 21:31:20.384Z | 342.369° N |
| 4 mins | 2026-09-18 09:09:20.384Z | 61.689° ENE | 2026-09-18 09:11:20.384Z | 96.701° ESE | 18.858° | 2026-09-18 09:13:20.384Z | 129.986° SE |
| 6 mins | 2026-09-18 10:44:20.384Z | 343.091° N | 2026-09-18 10:47:20.384Z | 274.463° WNW | 32.349° | 2026-09-18 10:50:20.384Z | 226.681° WSW |
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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