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: 14 hours ago
TLE from 14 hours ago
0 CAPELLA-17 (ACADIA)
1 64583U 25135BH 26178.26752192 .00008060 00000-0 81155-3 0 9997
2 64583 97.7697 291.7405 0004003 331.4926 28.6073 14.91427574 55354Epoch: 2026-06-27T06:25Z
TLE epoch observation values (Epoch: 2026-06-27T06:25:13.893Z)
Latitude
-0.00005°
Longitude
-79.95151°
Altitude
594.074 km
Speed
7.564 km/s
True Right ascension
19h 26m 57s
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
07:44:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.293 km
Perigee altitude
587.714 km
Semi-major axis
6,968.64 km
Eccentricity
0.0004
Inclination
97.7697°
RAAN
291.7405°
Arg. of periapsis
331.4926°
True anomaly
28.62927°
Mean anomaly
28.6073°
Eccentric anomaly
28.61829°
Mean motion
3.73096 °/min
Orbital period
96.49 mins
BSTAR
0.00081155
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-27 21:28:46.726Z | 333.167° NNW | 2026-06-27 21:30:46.726Z | 301.819° NW | 18.172° | 2026-06-27 21:33:46.726Z | 251.423° W |
| 4 mins | 2026-06-28 06:44:46.726Z | 93.331° ESE | 2026-06-28 06:45:46.726Z | 73.302° E | 20.461° | 2026-06-28 06:48:46.726Z | 21.783° NNE |
| 5 mins | 2026-06-28 08:19:46.726Z | 225.118° WSW | 2026-06-28 08:21:46.726Z | 272.864° WNW | 25.343° | 2026-06-28 08:24:46.726Z | 322.199° NNW |
| 6 mins | 2026-06-28 20:02:46.726Z | 40.071° NE | 2026-06-28 20:04:46.726Z | 90.155° ESE | 33.759° | 2026-06-28 20:08:46.726Z | 169.826° S |
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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