▸Orbital parameters

Orbit class	GEO
Inclination	0.0171°
Eccentricity	0.0006550
Period	1436.1 min
Apogee	35,814 km
Perigee	35,759 km
Mean motion	1.00271711 rev/day
RAAN	83.3734°
Arg of perigee	0.8876°
Mean anomaly	304.4066°
B*	0.0000e+0
Rev at epoch	3,334

▸Two-line element set (TLE)

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

1 42747U 17031A 26188.15461182 .00000140 00000-0 00000-0 0 9994

2 42747 0.0171 83.3734 0006550 0.8876 304.4066 1.00271711 33344

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GSAT-19",
  "OBJECT_ID": "2017-031A",
  "EPOCH": "2026-07-07T03:42:38.461+00:00",
  "MEAN_MOTION": 1.00271711,
  "ECCENTRICITY": 0.000655,
  "INCLINATION": 0.0171,
  "RA_OF_ASC_NODE": 83.3734,
  "ARG_OF_PERICENTER": 0.8876,
  "MEAN_ANOMALY": 304.4066,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 42747,
  "REV_AT_EPOCH": 3334,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.0000014,
  "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-19
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Jun 5, 2017HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3136HIGH

▸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/42747

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