▸Orbital parameters

Orbit class	GEO
Inclination	0.0143°
Eccentricity	0.0000764
Period	1436.1 min
Apogee	35,790 km
Perigee	35,784 km
Mean motion	1.00271332 rev/day
RAAN	300.8364°
Arg of perigee	197.7595°
Mean anomaly	337.4030°
B*	0.0000e+0
Rev at epoch	4,328

▸Two-line element set (TLE)

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

1 40141U 14052A 26188.19697714 -.00000347 00000-0 00000-0 0 9996

2 40141 0.0143 300.8364 0000764 197.7595 337.4030 1.00271332 43280

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASIASAT 6",
  "OBJECT_ID": "2014-052A",
  "EPOCH": "2026-07-07T04:43:38.825+00:00",
  "MEAN_MOTION": 1.00271332,
  "ECCENTRICITY": 0.0000764,
  "INCLINATION": 0.0143,
  "RA_OF_ASC_NODE": 300.8364,
  "ARG_OF_PERICENTER": 197.7595,
  "MEAN_ANOMALY": 337.403,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40141,
  "REV_AT_EPOCH": 4328,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000347,
  "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	ASIASAT 6
Operator	Asia Satellite Telecom, Hong KongHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree AsiaSatMEDIUMvia Wikidata
Country	HK
Launch date	Sep 7, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3700HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/40141

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