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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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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 (4 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: 20 hours ago

TLE from 20 hours ago

0 ACCENTURE-1
1 66767U 25276DF  26092.14797083  .00004955  00000-0  23731-3 0  9994
2 66767  97.4204 167.0585 0002225  95.6921 264.4568 15.19395804 18880

Epoch: 2026-04-02T03:33Z

TLE epoch observation values (Epoch: 2026-04-02T03:33:04.679Z)

Latitude

0.00001°

Longitude

-76.71161°

Altitude

510.903 km

Speed

7.608 km/s

True Right ascension

11h 08m 14s

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

04:49:18

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

506.164 km

Perigee altitude

503.101 km

Semi-major axis

6,882.77 km

Eccentricity

0.00022

Inclination

97.4204°

RAAN

167.0585°

Arg. of periapsis

95.6921°

True anomaly

264.43142°

Mean anomaly

264.4568°

Eccentric anomaly

264.44411°

Mean motion

3.801 °/min

Orbital period

94.71 mins

BSTAR

0.00023731

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

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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.
7 mins	2026-04-03 04:57:34.431Z	166.308° S	2026-04-03 05:00:34.431Z	162.959° S	42.705°	2026-04-03 05:04:34.431Z	348.544° N
5 mins	2026-04-03 18:03:34.431Z	356.478° N	2026-04-03 18:05:34.431Z	294.386° NW	40.038°	2026-04-03 18:08:34.431Z	208.468° SW

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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: 20 hours ago

TLE from 20 hours ago

TLE epoch observation values (Epoch: 2026-04-02T03:33:04.679Z)

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: 20 hours ago