▸Orbital parameters

Orbit class	GEO
Inclination	28.8929°
Eccentricity	0.0022969
Period	1436.1 min
Apogee	35,883 km
Perigee	35,690 km
Mean motion	1.00272765 rev/day
RAAN	240.0829°
Arg of perigee	195.5386°
Mean anomaly	165.9835°
B*	0.0000e+0
Rev at epoch	4,498

▸Two-line element set (TLE)

EPOCH Jul 5, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 39635U 14017A 26186.73010079 .00000137 00000-0 00000-0 0 9990

2 39635 28.8929 240.0829 0022970 195.5386 165.9835 1.00272765 44980

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRNSS-1B",
  "OBJECT_ID": "2014-017A",
  "EPOCH": "2026-07-05T17:31:20.708+00:00",
  "MEAN_MOTION": 1.00272765,
  "ECCENTRICITY": 0.00229695,
  "INCLINATION": 28.8929,
  "RA_OF_ASC_NODE": 240.0829,
  "ARG_OF_PERICENTER": 195.5386,
  "MEAN_ANOMALY": 165.9835,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39635,
  "REV_AT_EPOCH": 4498,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000137,
  "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-1B
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Apr 4, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1432HIGH

▸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/39635

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