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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Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 CAPELLA-15 (ACADIA)
1 60544U 24149CE 26219.74800699 .00002472 00000-0 24677-3 0 9996
2 60544 97.6743 291.3550 0003299 231.5283 128.5641 14.92402640107545TLE epoch observation values (Epoch: 2026-08-07T17:57:07.803Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-08 03:46:43.885Z | 91.888° ESE | 2026-08-08 03:48:43.885Z | 58.483° ENE | 15.426° | 2026-08-08 03:50:43.885Z | 29.167° NE |
| 6 mins | 2026-08-08 05:20:43.885Z | 198.545° SSW | 2026-08-08 05:23:43.885Z | 271.051° WNW | 32.758° | 2026-08-08 05:26:43.885Z | 328.422° NNW |
| 5 mins | 2026-08-08 17:04:43.885Z | 53.596° ENE | 2026-08-08 17:06:43.885Z | 100.474° ESE | 26.384° | 2026-08-08 17:09:43.885Z | 154.556° SSE |
| 4 mins | 2026-08-08 18:40:43.885Z | 316.004° NNW | 2026-08-08 18:41:43.885Z | 296.386° NW | 19.737° | 2026-08-08 18:44:43.885Z | 246.042° 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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