▸Orbital parameters

Orbit class	GEO
Inclination	0.0291°
Eccentricity	0.0002537
Period	1436.1 min
Apogee	35,798 km
Perigee	35,776 km
Mean motion	1.00269907 rev/day
RAAN	31.4631°
Arg of perigee	59.2472°
Mean anomaly	344.6106°
B*	0.0000e+0
Rev at epoch	4,310

▸Two-line element set (TLE)

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

1 40147U 14054B 26188.16308795 -.00000226 00000-0 00000-0 0 9995

2 40147 0.0291 31.4631 0002537 59.2472 344.6106 1.00269907 43100

▸ source OMM (JSON)

{
  "OBJECT_NAME": "MEASAT-3B",
  "OBJECT_ID": "2014-054B",
  "EPOCH": "2026-07-07T03:54:50.799+00:00",
  "MEAN_MOTION": 1.00269907,
  "ECCENTRICITY": 0.0002537,
  "INCLINATION": 0.0291,
  "RA_OF_ASC_NODE": 31.4631,
  "ARG_OF_PERICENTER": 59.2472,
  "MEAN_ANOMALY": 344.6106,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40147,
  "REV_AT_EPOCH": 4310,
  "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-3B
Operator	MeasatHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree MEASAT Satellite SystemsMEDIUMvia Wikidata
Country	MalaysiaMEDIUMvia Wikidata
Launch date	Sep 11, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5897HIGH

▸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/40147

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