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: 3 days ago
TLE from 3 days ago
0 CAPELLA-20 (ACADIA)
1 68485U 26067BX 26260.81967816 .00004090 00000-0 42249-3 0 9991
2 68485 97.7635 217.6314 0002920 70.7006 289.4528 14.90689369 25535Epoch: 2026-09-17T19:40Z
TLE epoch observation values (Epoch: 2026-09-17T19:40:20.193Z)
Latitude
0.00003°
Longitude
-74.20418°
Altitude
598.147 km
Speed
7.561 km/s
True Right ascension
14h 30m 31s
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
03:12:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.841 km
Perigee altitude
590.77 km
Semi-major axis
6,970.942 km
Eccentricity
0.00029
Inclination
97.7635°
RAAN
217.6314°
Arg. of periapsis
70.7006°
True anomaly
289.42125°
Mean anomaly
289.4528°
Eccentric anomaly
289.43702°
Mean motion
3.72912 °/min
Orbital period
96.54 mins
BSTAR
0.00042249
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-20 11:04:18.494Z | 331.882° NNW | 2026-09-20 11:06:18.494Z | 298.327° NW | 20.7° | 2026-09-20 11:09:18.494Z | 247.904° W |
| 4 mins | 2026-09-20 20:20:18.494Z | 93.167° ESE | 2026-09-20 20:21:18.494Z | 74.169° E | 20.76° | 2026-09-20 20:24:18.494Z | 23.468° NE |
| 5 mins | 2026-09-20 21:55:18.494Z | 221.534° SW | 2026-09-20 21:57:18.494Z | 270.619° WNW | 30.545° | 2026-09-20 22:00:18.494Z | 322.695° NNW |
| 6 mins | 2026-09-21 09:38:18.494Z | 36.699° NE | 2026-09-21 09:41:18.494Z | 111.396° ESE | 39.403° | 2026-09-21 09:44:18.494Z | 165.46° S |
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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