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 Communications
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, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 ACCENTURE-1
1 66767U 25276DF 26155.09790002 .00004713 00000-0 22276-3 0 9997
2 66767 97.4162 228.9265 0001306 112.7840 247.3533 15.19876350 28440Epoch: 2026-06-04T02:20Z
TLE epoch observation values (Epoch: 2026-06-04T02:20:58.561Z)
Latitude
-0.00005°
Longitude
-58.86455°
Altitude
509.65 km
Speed
7.609 km/s
True Right ascension
15h 15m 42s
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
13:17:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.079 km
Perigee altitude
502.282 km
Semi-major axis
6,881.317 km
Eccentricity
0.00013
Inclination
97.4162°
RAAN
228.9265°
Arg. of periapsis
112.784°
True anomaly
247.33949°
Mean anomaly
247.3533°
Eccentric anomaly
247.34639°
Mean motion
3.80221 °/min
Orbital period
94.68 mins
BSTAR
0.00022276
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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 | 2026-06-10 05:25:45.613Z | 201.99° SSW | 2026-06-10 05:27:45.613Z | 250.832° W | 31.173° | 2026-06-10 05:30:45.613Z | 326.33° NNW |
| 4 mins | 2026-06-10 18:30:45.613Z | 325.981° NNW | 2026-06-10 18:32:45.613Z | 275.34° WNW | 22.712° | 2026-06-10 18:34:45.613Z | 238.04° WSW |
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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