▸Orbital parameters

Orbit class	GEO
Inclination	0.0281°
Eccentricity	0.0003892
Period	1436.1 min
Apogee	35,803 km
Perigee	35,770 km
Mean motion	1.00272688 rev/day
RAAN	265.2061°
Arg of perigee	182.6488°
Mean anomaly	349.5857°
B*	0.0000e+0
Rev at epoch	3,899

▸Two-line element set (TLE)

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

1 41028U 15065A 26188.16334795 -.00000243 00000-0 00000-0 0 9995

2 41028 0.0281 265.2061 0003892 182.6488 349.5857 1.00272688 38993

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GSAT-15",
  "OBJECT_ID": "2015-065A",
  "EPOCH": "2026-07-07T03:55:13.263+00:00",
  "MEAN_MOTION": 1.00272688,
  "ECCENTRICITY": 0.0003892,
  "INCLINATION": 0.0281,
  "RA_OF_ASC_NODE": 265.2061,
  "ARG_OF_PERICENTER": 182.6488,
  "MEAN_ANOMALY": 349.5857,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41028,
  "REV_AT_EPOCH": 3899,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000243,
  "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-15
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Nov 10, 2015HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3165HIGH

▸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/41028

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