▸Orbital parameters

Orbit class	GEO
Inclination	0.0637°
Eccentricity	0.0001851
Period	1436.1 min
Apogee	35,795 km
Perigee	35,779 km
Mean motion	1.00269542 rev/day
RAAN	93.4063°
Arg of perigee	9.3826°
Mean anomaly	301.8041°
B*	0.0000e+0
Rev at epoch	2,764

▸Two-line element set (TLE)

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

1 43864U 18105A 26188.15745462 .00000042 00000-0 00000-0 0 9995

2 43864 0.0637 93.4063 0001851 9.3826 301.8041 1.00269542 27646

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GSAT-7A",
  "OBJECT_ID": "2018-105A",
  "EPOCH": "2026-07-07T03:46:44.079+00:00",
  "MEAN_MOTION": 1.00269542,
  "ECCENTRICITY": 0.0001851,
  "INCLINATION": 0.0637,
  "RA_OF_ASC_NODE": 93.4063,
  "ARG_OF_PERICENTER": 9.3826,
  "MEAN_ANOMALY": 301.8041,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43864,
  "REV_AT_EPOCH": 2764,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 4.2e-7,
  "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-7A
Operator	Indian Air Force / Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Dec 19, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2250

▸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/43864

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