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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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Iframe URL

https://www.satcat.com/sats-embedded/66767?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

66767, 2025-276DF

Orbit

SSO

Country

Related business

Accenture (IE)

Manufacturer

Open Cosmos

Mission

Operational Commercial Communications

Bus & Motor

CUBESAT 6U, Unknown motor

Mass

12 kg wet, 12 kg dry

Launch date (UTC)

2025-11-28 (6 months ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 0.2 m

Radar Cross Section

0.100 m²

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 ACCENTURE-1
1 66767U 25276DF  26147.19727727  .00004413  00000-0  20928-3 0  9992
2 66767  97.4167 221.1604 0001113 109.6916 250.4439 15.19798297 27242

Epoch: 2026-05-27T04:44Z

TLE epoch observation values (Epoch: 2026-05-27T04:44:04.756Z)

Latitude

-0.00001°

Longitude

-94.61924°

Altitude

509.796 km

Speed

7.609 km/s

True Right ascension

14h 44m 38s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

03:48:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

504.182 km

Perigee altitude

502.65 km

Semi-major axis

6,881.553 km

Eccentricity

0.00011

Inclination

97.4167°

RAAN

221.1604°

Arg. of periapsis

109.6916°

True anomaly

250.43188°

Mean anomaly

250.4439°

Eccentric anomaly

250.43789°

Mean motion

3.80201 °/min

Orbital period

94.69 mins

BSTAR

0.00020928

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Other satellites on launch #276 in the year 2025 (2025-11-28 UTC)

IMPULSE-3 MIRA, 66687

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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	2026-05-28 04:34:38.486Z	138.103° SSE	2026-05-28 04:36:38.486Z	95.494° ESE	32.499°	2026-05-28 04:39:38.486Z	8.733° NNE
5 mins	2026-05-28 17:39:38.486Z	24.453° NE	2026-05-28 17:41:38.486Z	112.752° SE	42.495°	2026-05-28 17:44:38.486Z	182.989° SSW

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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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Check out ACCENTURE-1, 66767 on other resources

View ACCENTURE-1, 66767 on NASA - NSSDCA Website

View ACCENTURE-1, 66767 on Heavens-Above

View ACCENTURE-1, 66767 on Keep Track

View ACCENTURE-1, 66767 on Celestrak

View ACCENTURE-1, 66767 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

ACCENTURE-1, 66767

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-05-27T04:44:04.756Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #276 in the year 2025 (2025-11-28 UTC)

ACCENTURE-1 Visibility forecast

Co-orbital & Co-planar RSOs

Check out ACCENTURE-1, 66767 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago