▸Orbital parameters

Orbit class	GEO
Inclination	0.0234°
Eccentricity	0.0001472
Period	1436.1 min
Apogee	35,793 km
Perigee	35,780 km
Mean motion	1.00271769 rev/day
RAAN	288.4854°
Arg of perigee	177.2372°
Mean anomaly	344.1411°
B*	0.0000e+0
Rev at epoch	10,235

▸Two-line element set (TLE)

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

1 40107U 14046A 26188.16502919 -.00000318 00000-0 00000-0 0 9998

2 40107 0.0234 288.4854 0001472 177.2372 344.1411 1.00271769102357

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASIASAT 8 (AMOS-7)",
  "OBJECT_ID": "2014-046A",
  "EPOCH": "2026-07-07T03:57:38.522+00:00",
  "MEAN_MOTION": 1.00271769,
  "ECCENTRICITY": 0.0001472,
  "INCLINATION": 0.0234,
  "RA_OF_ASC_NODE": 288.4854,
  "ARG_OF_PERICENTER": 177.2372,
  "MEAN_ANOMALY": 344.1411,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40107,
  "REV_AT_EPOCH": 10235,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000318,
  "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 8 (AMOS-7)
Operator	Asia Satellite Telecom, Hong KongHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree AsiaSatMEDIUMvia Wikidata
Country	People's Republic of ChinaMEDIUMvia Wikidata
Launch date	Aug 5, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4535HIGH

▸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/40107

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