▸Orbital parameters

Orbit class	GEO
Inclination	4.7524°
Eccentricity	0.0002857
Period	1436.1 min
Apogee	35,799 km
Perigee	35,775 km
Mean motion	1.00271892 rev/day
RAAN	75.5035°
Arg of perigee	30.0906°
Mean anomaly	160.8815°
B*	0.0000e+0
Rev at epoch	4,549

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 27718U 03014A 26187.54003346 -.00000210 00000-0 00000-0 0 9996

2 27718 4.7524 75.5035 0002857 30.0906 160.8815 1.00271892 45495

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASIASAT 4",
  "OBJECT_ID": "2003-014A",
  "EPOCH": "2026-07-06T12:57:38.891+00:00",
  "MEAN_MOTION": 1.00271892,
  "ECCENTRICITY": 0.00028569,
  "INCLINATION": 4.7524,
  "RA_OF_ASC_NODE": 75.5035,
  "ARG_OF_PERICENTER": 30.0906,
  "MEAN_ANOMALY": 160.8815,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 27718,
  "REV_AT_EPOCH": 4549,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.0000021,
  "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 4
Operator	Asia Satellite Telecom, Hong KongHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	HK
Launch date	Apr 12, 2003HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4137HIGHvia 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/27718

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