▸Orbital parameters

Orbit class	GEO
Inclination	0.0420°
Eccentricity	0.0007864
Period	1436.1 min
Apogee	35,820 km
Perigee	35,754 km
Mean motion	1.00269440 rev/day
RAAN	240.1474°
Arg of perigee	214.3085°
Mean anomaly	152.3326°
B*	0.0000e+0
Rev at epoch	5,029

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 38779U 12051B 26187.66432233 -.00000149 00000-0 00000-0 0 9991

2 38779 0.0420 240.1474 0007864 214.3085 152.3326 1.00269440 50296

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GSAT-10",
  "OBJECT_ID": "2012-051B",
  "EPOCH": "2026-07-06T15:56:37.449+00:00",
  "MEAN_MOTION": 1.0026944,
  "ECCENTRICITY": 0.0007864,
  "INCLINATION": 0.042,
  "RA_OF_ASC_NODE": 240.1474,
  "ARG_OF_PERICENTER": 214.3085,
  "MEAN_ANOMALY": 152.3326,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 38779,
  "REV_AT_EPOCH": 5029,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000149,
  "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-10
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	India
Launch date	Sep 28, 2012HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3400HIGHvia GCAT — Jonathan McDowell's General Catalog 3400MEDIUMvia Wikidata
Mission purpose	—

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/38779

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