CAPELLA-17 (ACADIA), 64583
Orbit data source: Space-Track
CAPELLA-17 (ACADIA), 64583 is a payload satellite owned by Capella Space (US) in SSO that was launched on Mon, 23 Jun 2025 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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64583 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, 5.0 m
Radar Cross Section
0.463 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 CAPELLA-17 (ACADIA)
1 64583U 25135BH 26249.09869721 .00003080 00000-0 30824-3 0 9998
2 64583 97.7735 1.5685 0006443 88.7381 271.4576 14.92129072 65913Epoch: 2026-09-06T02:22Z
TLE epoch observation values (Epoch: 2026-09-06T02:22:07.438Z)
Latitude
-0.00006°
Longitude
-19.16117°
Altitude
594.229 km
Speed
7.563 km/s
True Right ascension
00h 06m 16s
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
13:47:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.806 km
Perigee altitude
583.829 km
Semi-major axis
6,966.454 km
Eccentricity
0.00064
Inclination
97.7735°
RAAN
1.5685°
Arg. of periapsis
88.7381°
True anomaly
271.38379°
Mean anomaly
271.4576°
Eccentric anomaly
271.4207°
Mean motion
3.73272 °/min
Orbital period
96.44 mins
BSTAR
0.00030824
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-17 (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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-07 07:27:19.132Z | 158.759° S | 2026-09-07 07:31:19.132Z | 57.731° ENE | 70.453° | 2026-09-07 07:35:19.132Z | 352.19° N |
| 6 mins | 2026-09-07 20:47:19.132Z | 357.217° N | 2026-09-07 20:50:19.132Z | 266.989° W | 53.181° | 2026-09-07 20:53:19.132Z | 211.284° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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