▸Orbital parameters

Orbit class	LEO
Inclination	5.9982°
Eccentricity	0.0008506
Period	97.1 min
Apogee	627 km
Perigee	615 km
Mean motion	14.82542388 rev/day
RAAN	19.4758°
Arg of perigee	302.4435°
Mean anomaly	57.4871°
B*	1.3877e-4
Rev at epoch	58,263

▸Two-line element set (TLE)

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

1 40930U 15052A 26187.06238198 .00001814 00000-0 13877-3 0 9993

2 40930 5.9982 19.4758 0008506 302.4435 57.4871 14.82542388582636

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASTROSAT",
  "OBJECT_ID": "2015-052A",
  "EPOCH": "2026-07-06T01:29:49.803+00:00",
  "MEAN_MOTION": 14.82542388,
  "ECCENTRICITY": 0.0008506,
  "INCLINATION": 5.9982,
  "RA_OF_ASC_NODE": 19.4758,
  "ARG_OF_PERICENTER": 302.4435,
  "MEAN_ANOMALY": 57.4871,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40930,
  "REV_AT_EPOCH": 58263,
  "BSTAR": 0.00013877,
  "MEAN_MOTION_DOT": 0.00001814,
  "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	ASTROSAT
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Sep 28, 2015HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1513HIGH

▸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/40930

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