CAPELLA-15 (ACADIA), 60544
Orbit data source: Space-Track
CAPELLA-15 (ACADIA), 60544 is a payload satellite owned by Capella Space (US) in SSO that was launched on Fri, 16 Aug 2024 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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60544 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-15 (ACADIA)
1 60544U 24149CE 26258.63559539 .00000408 00000-0 45279-4 0 9990
2 60544 97.6698 329.2417 0005531 119.2643 240.9130 14.92337763113340Epoch: 2026-09-15T15:15Z
TLE epoch observation values (Epoch: 2026-09-15T15:15:15.441Z)
Latitude
-0.00002°
Longitude
105.82866°
Altitude
595.569 km
Speed
7.561 km/s
True Right ascension
21h 56m 58s
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
06:20:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.515 km
Perigee altitude
583.81 km
Semi-major axis
6,965.8 km
Eccentricity
0.00055
Inclination
97.6698°
RAAN
329.2417°
Arg. of periapsis
119.2643°
True anomaly
240.85763°
Mean anomaly
240.913°
Eccentric anomaly
240.88531°
Mean motion
3.73325 °/min
Orbital period
96.43 mins
BSTAR
0.000045279
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-15 (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 17:42:28.580Z | 11.522° NNE | 2026-09-17 17:45:28.580Z | 3.121° NNE | 75.747° | 2026-09-17 17:49:28.580Z | 194.447° SSW |
| 6 mins | 2026-09-18 04:32:28.580Z | 146.173° SSE | 2026-09-18 04:35:28.580Z | 60.217° ENE | 53.968° | 2026-09-18 04:38:28.580Z | 0.098° NNE |
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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