▸Orbital parameters

Orbit class	SSO
Inclination	97.9826°
Eccentricity	0.0001869
Period	97.4 min
Apogee	635 km
Perigee	632 km
Mean motion	14.78661364 rev/day
RAAN	254.7650°
Arg of perigee	88.4280°
Mean anomaly	271.7145°
B*	1.5470e-4
Rev at epoch	41,037

▸Two-line element set (TLE)

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

1 43719U 18096A 26188.17436678 .00001082 00000-0 15470-3 0 9996

2 43719 97.9826 254.7650 0001869 88.4280 271.7145 14.78661364410378

▸ source OMM (JSON)

{
  "OBJECT_NAME": "HYSIS",
  "OBJECT_ID": "2018-096A",
  "EPOCH": "2026-07-07T04:11:05.29+00:00",
  "MEAN_MOTION": 14.78661364,
  "ECCENTRICITY": 0.0001869,
  "INCLINATION": 97.9826,
  "RA_OF_ASC_NODE": 254.765,
  "ARG_OF_PERICENTER": 88.428,
  "MEAN_ANOMALY": 271.7145,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43719,
  "REV_AT_EPOCH": 41037,
  "BSTAR": 0.0001547,
  "MEAN_MOTION_DOT": 0.00001082,
  "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	HYSIS
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Nov 29, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	380HIGH

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/43719

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