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, 5.0 m
Radar Cross Section
0.463 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 CAPELLA-15 (ACADIA)
1 60544U 24149CE 26171.47377027 .00003255 00000-0 32315-3 0 9995
2 60544 97.6768 244.2947 0004546 70.1549 290.0160 14.92412183100342Epoch: 2026-06-20T11:22Z
TLE epoch observation values (Epoch: 2026-06-20T11:22:13.751Z)
Latitude
-0.00002°
Longitude
165.04952°
Altitude
592.378 km
Speed
7.564 km/s
True Right ascension
16h 17m 10s
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
07:21:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.598 km
Perigee altitude
584.265 km
Semi-major axis
6,965.568 km
Eccentricity
0.00045
Inclination
97.6768°
RAAN
244.2947°
Arg. of periapsis
70.1549°
True anomaly
289.96704°
Mean anomaly
290.016°
Eccentric anomaly
289.99152°
Mean motion
3.73343 °/min
Orbital period
96.43 mins
BSTAR
0.00032315
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 05:12:00.621Z | 186.849° SSW | 2026-06-21 05:15:00.621Z | 269.849° W | 39.001° | 2026-06-21 05:18:00.621Z | 334.773° NNW |
| 5 mins | 2026-06-21 16:56:00.621Z | 58.438° ENE | 2026-06-21 16:58:00.621Z | 97.692° ESE | 21.085° | 2026-06-21 17:01:00.621Z | 146.258° SSE |
| 5 mins | 2026-06-21 18:31:00.621Z | 337.165° NNW | 2026-06-21 18:33:00.621Z | 299.521° NW | 24.2° | 2026-06-21 18:36:00.621Z | 239.992° WSW |
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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