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: 8 hours ago
TLE from 8 hours ago
0 CAPELLA-17 (ACADIA)
1 64583U 25135BH 26283.89890574 .00008516 00000-0 83525-3 0 9999
2 64583 97.7780 35.9202 0004402 339.8531 20.2514 14.92458474 71100Epoch: 2026-10-10T21:34Z
TLE epoch observation values (Epoch: 2026-10-10T21:34:25.455Z)
Latitude
-0.00002°
Longitude
52.81472°
Altitude
590.436 km
Speed
7.566 km/s
True Right ascension
02h 23m 40s
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
23:55:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.358 km
Perigee altitude
584.225 km
Semi-major axis
6,965.428 km
Eccentricity
0.00044
Inclination
97.778°
RAAN
35.9202°
Arg. of periapsis
339.8531°
True anomaly
20.26887°
Mean anomaly
20.2514°
Eccentric anomaly
20.26013°
Mean motion
3.73355 °/min
Orbital period
96.42 mins
BSTAR
0.00083525
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-11 07:21:21.142Z | 151.11° SSE | 2026-10-11 07:24:21.142Z | 95.479° ESE | 57.079° | 2026-10-11 07:28:21.142Z | 356.673° N |
| 7 mins | 2026-10-11 20:40:21.142Z | 3.905° NNE | 2026-10-11 20:43:21.142Z | 284.061° WNW | 66.82° | 2026-10-11 20:47:21.142Z | 203.061° SW |
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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