▸Orbital parameters

Orbit class	GEO
Inclination	0.0615°
Eccentricity	0.0003279
Period	1436.1 min
Apogee	35,800 km
Perigee	35,772 km
Mean motion	1.00273523 rev/day
RAAN	257.2424°
Arg of perigee	183.9116°
Mean anomaly	315.1710°
B*	0.0000e+0
Rev at epoch	2,798

▸Two-line element set (TLE)

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

1 43698U 18089A 26188.15598125 .00000100 00000-0 00000-0 0 9998

2 43698 0.0615 257.2424 0003279 183.9116 315.1710 1.00273523 27987

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GSAT-29",
  "OBJECT_ID": "2018-089A",
  "EPOCH": "2026-07-07T03:44:36.78+00:00",
  "MEAN_MOTION": 1.00273523,
  "ECCENTRICITY": 0.0003279,
  "INCLINATION": 0.0615,
  "RA_OF_ASC_NODE": 257.2424,
  "ARG_OF_PERICENTER": 183.9116,
  "MEAN_ANOMALY": 315.171,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43698,
  "REV_AT_EPOCH": 2798,
  "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-29
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Nov 14, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3423HIGH

▸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/43698

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