ACCENTURE-1, 66767
Orbit data source: Space-Track
ACCENTURE-1, 66767 is a UK payload satellite in SSO that was launched on Fri, 28 Nov 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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66767 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
Open Cosmos
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ACCENTURE-1
1 66767U 25276DF 26238.16883694 .00003203 00000-0 15014-3 0 9992
2 66767 97.4121 310.5941 0001176 79.2214 280.9153 15.20402908 41061Epoch: 2026-08-26T04:03Z
TLE epoch observation values (Epoch: 2026-08-26T04:03:07.511Z)
Latitude
-0.0001°
Longitude
-84.61288°
Altitude
507.562 km
Speed
7.61 km/s
True Right ascension
20h 42m 22s
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
06:49:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.399 km
Perigee altitude
500.781 km
Semi-major axis
6,879.727 km
Eccentricity
0.00012
Inclination
97.4121°
RAAN
310.5941°
Arg. of periapsis
79.2214°
True anomaly
280.90207°
Mean anomaly
280.9153°
Eccentric anomaly
280.90868°
Mean motion
3.80353 °/min
Orbital period
94.65 mins
BSTAR
0.00015014
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Other satellites on launch #276 in the year 2025 (2025-11-28 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.ACCENTURE-1 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 | 2026-08-26 17:15:51.533Z | 39.631° NE | 2026-08-26 17:17:51.533Z | 81.343° E | 27.642° | 2026-08-26 17:20:51.533Z | 156.292° SSE |
| 5 mins | 2026-08-27 05:27:51.533Z | 208.953° SW | 2026-08-27 05:29:51.533Z | 264.673° W | 29.771° | 2026-08-27 05:32:51.533Z | 327.327° NNW |
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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