▸Orbital parameters

Orbit class	GEO
Inclination	0.0278°
Eccentricity	0.0000271
Period	1436.1 min
Apogee	35,789 km
Perigee	35,786 km
Mean motion	1.00269012 rev/day
RAAN	345.3772°
Arg of perigee	117.1655°
Mean anomaly	307.0978°
B*	0.0000e+0
Rev at epoch	1,484

▸Two-line element set (TLE)

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

1 52904U 22067B 26188.09190389 -.00000226 00000-0 00000-0 0 9992

2 52904 0.0278 345.3772 0000271 117.1655 307.0978 1.00269012 14848

▸ source OMM (JSON)

{
  "OBJECT_NAME": "MEASAT 3D",
  "OBJECT_ID": "2022-067B",
  "EPOCH": "2026-07-07T02:12:20.496+00:00",
  "MEAN_MOTION": 1.00269012,
  "ECCENTRICITY": 0.0000271,
  "INCLINATION": 0.0278,
  "RA_OF_ASC_NODE": 345.3772,
  "ARG_OF_PERICENTER": 117.1655,
  "MEAN_ANOMALY": 307.0978,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52904,
  "REV_AT_EPOCH": 1484,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000226,
  "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	MEASAT 3D
Operator	MeasatHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree MEASAT Satellite SystemsMEDIUMvia Wikidata
Country	MalaysiaMEDIUMvia Wikidata
Launch date	Jun 22, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5648HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/52904

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