▸Orbital parameters

Orbit class	GEO
Inclination	0.0342°
Eccentricity	0.0001673
Period	1436.1 min
Apogee	35,795 km
Perigee	35,781 km
Mean motion	1.00268538 rev/day
RAAN	270.9576°
Arg of perigee	176.8291°
Mean anomaly	326.4177°
B*	0.0000e+0
Rev at epoch	6,190

▸Two-line element set (TLE)

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

1 35696U 09042A 26188.07961659 -.00000292 00000-0 00000-0 0 9996

2 35696 0.0342 270.9576 0001673 176.8291 326.4177 1.00268538 61906

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASIASAT 5",
  "OBJECT_ID": "2009-042A",
  "EPOCH": "2026-07-07T01:54:38.873+00:00",
  "MEAN_MOTION": 1.00268538,
  "ECCENTRICITY": 0.0001673,
  "INCLINATION": 0.0342,
  "RA_OF_ASC_NODE": 270.9576,
  "ARG_OF_PERICENTER": 176.8291,
  "MEAN_ANOMALY": 326.4177,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 35696,
  "REV_AT_EPOCH": 6190,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000292,
  "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 5
Operator	Asia Satellite Telecom, Hong KongHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree AsiaSatMEDIUMvia Wikidata
Country	HK
Launch date	Aug 11, 2009HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3760HIGHvia 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/35696

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