▸Orbital parameters

Orbit class	SSO
Inclination	97.4152°
Eccentricity	0.0002295
Period	94.7 min
Apogee	507 km
Perigee	504 km
Mean motion	15.20120714 rev/day
RAAN	261.4158°
Arg of perigee	103.6724°
Mean anomaly	256.4767°
B*	1.3884e-4
Rev at epoch	3,346

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 66767U 25276DF 26188.14534897 .00002932 00000-0 13884-3 0 9993

2 66767 97.4152 261.4158 0002295 103.6724 256.4767 15.20120714 33466

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ACCENTURE-1",
  "OBJECT_ID": "2025-276DF",
  "EPOCH": "2026-07-07T03:29:18.151+00:00",
  "MEAN_MOTION": 15.20120714,
  "ECCENTRICITY": 0.0002295,
  "INCLINATION": 97.4152,
  "RA_OF_ASC_NODE": 261.4158,
  "ARG_OF_PERICENTER": 103.6724,
  "MEAN_ANOMALY": 256.4767,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66767,
  "REV_AT_EPOCH": 3346,
  "BSTAR": 0.00013884,
  "MEAN_MOTION_DOT": 0.00002932,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	ACCENTURE-1
Operator	Accenture plc / Open Cosmos Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	IE
Launch date	Nov 28, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	12HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/66767

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.