▸Orbital parameters

Orbit class	GEO
Inclination	33.2756°
Eccentricity	0.0019195
Period	1436.1 min
Apogee	35,868 km
Perigee	35,706 km
Mean motion	1.00269537 rev/day
RAAN	59.4648°
Arg of perigee	178.8904°
Mean anomaly	102.4500°
B*	0.0000e+0
Rev at epoch	3,827

▸Two-line element set (TLE)

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

1 41241U 16003A 26187.84511535 -.00000302 00000-0 00000-0 0 9994

2 41241 33.2756 59.4648 0019195 178.8904 102.4500 1.00269537 38273

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRNSS-1E",
  "OBJECT_ID": "2016-003A",
  "EPOCH": "2026-07-06T20:16:57.966+00:00",
  "MEAN_MOTION": 1.00269537,
  "ECCENTRICITY": 0.0019195,
  "INCLINATION": 33.2756,
  "RA_OF_ASC_NODE": 59.4648,
  "ARG_OF_PERICENTER": 178.8904,
  "MEAN_ANOMALY": 102.45,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41241,
  "REV_AT_EPOCH": 3827,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000302,
  "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	IRNSS-1E
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Jan 20, 2016HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1425HIGH

▸Data quality

Score95 / 100

Claims11

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/41241

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