▸Orbital parameters

Orbit class	GEO
Inclination	5.3971°
Eccentricity	0.0017394
Period	1436.0 min
Apogee	35,858 km
Perigee	35,712 km
Mean motion	1.00277260 rev/day
RAAN	96.3335°
Arg of perigee	183.7124°
Mean anomaly	14.9319°
B*	0.0000e+0
Rev at epoch	3,786

▸Two-line element set (TLE)

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

1 41384U 16015A 26187.93764226 .00000170 00000-0 00000-0 0 9994

2 41384 5.3971 96.3335 0017394 183.7124 14.9319 1.00277260 37862

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRNSS-1F",
  "OBJECT_ID": "2016-015A",
  "EPOCH": "2026-07-06T22:30:12.291+00:00",
  "MEAN_MOTION": 1.0027726,
  "ECCENTRICITY": 0.0017394,
  "INCLINATION": 5.3971,
  "RA_OF_ASC_NODE": 96.3335,
  "ARG_OF_PERICENTER": 183.7124,
  "MEAN_ANOMALY": 14.9319,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41384,
  "REV_AT_EPOCH": 3786,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.0000017,
  "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-1F
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Mar 10, 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/41384

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