▸Orbital parameters

Orbit class	SSO
Inclination	97.3937°
Eccentricity	0.0007015
Period	94.6 min
Apogee	504 km
Perigee	494 km
Mean motion	15.22252514 rev/day
RAAN	80.3517°
Arg of perigee	78.0972°
Mean anomaly	282.1050°
B*	1.2859e-4
Rev at epoch	7,287

▸Two-line element set (TLE)

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

1 63226U 25052S 26188.14550374 .00002889 00000-0 12859-3 0 9992

2 63226 97.3937 80.3517 0007015 78.0972 282.1050 15.22252514 72870

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ETIHAD-SAT",
  "OBJECT_ID": "2025-052S",
  "EPOCH": "2026-07-07T03:29:31.523+00:00",
  "MEAN_MOTION": 15.22252514,
  "ECCENTRICITY": 0.0007015,
  "INCLINATION": 97.3937,
  "RA_OF_ASC_NODE": 80.3517,
  "ARG_OF_PERICENTER": 78.0972,
  "MEAN_ANOMALY": 282.105,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63226,
  "REV_AT_EPOCH": 7287,
  "BSTAR": 0.00012859,
  "MEAN_MOTION_DOT": 0.00002889,
  "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	ETIHAD-SAT
Operator	Mohammed bin Rashid Space Centre, EIASTHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Arab Emirates
Launch date	Mar 15, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	220HIGHvia 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/63226

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