▸Orbital parameters

Orbit class	GEO
Inclination	0.0378°
Eccentricity	0.0007495
Period	1436.1 min
Apogee	35,818 km
Perigee	35,755 km
Mean motion	1.00271084 rev/day
RAAN	262.8675°
Arg of perigee	187.9033°
Mean anomaly	305.5833°
B*	0.0000e+0
Rev at epoch	4,230

▸Two-line element set (TLE)

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

1 40332U 14078A 26188.15598125 .00000100 00000-0 00000-0 0 9994

2 40332 0.0378 262.8675 0007495 187.9033 305.5833 1.00271084 42303

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GSAT-16",
  "OBJECT_ID": "2014-078A",
  "EPOCH": "2026-07-07T03:44:36.78+00:00",
  "MEAN_MOTION": 1.00271084,
  "ECCENTRICITY": 0.0007495,
  "INCLINATION": 0.0378,
  "RA_OF_ASC_NODE": 262.8675,
  "ARG_OF_PERICENTER": 187.9033,
  "MEAN_ANOMALY": 305.5833,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40332,
  "REV_AT_EPOCH": 4230,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.000001,
  "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	GSAT-16
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	India
Launch date	Dec 6, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3180HIGHvia GCAT — Jonathan McDowell's General Catalog⚠

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/40332

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