▸Orbital parameters

Orbit class	SSO
Inclination	98.4631°
Eccentricity	0.0018900
Period	99.7 min
Apogee	760 km
Perigee	733 km
Mean motion	14.43647204 rev/day
RAAN	246.8642°
Arg of perigee	154.3958°
Mean anomaly	205.8173°
B*	5.0108e-5
Rev at epoch	38,294

▸Two-line element set (TLE)

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

1 44078U 19018A 26188.17458700 .00000126 00000-0 50108-4 0 9996

2 44078 98.4631 246.8642 0018900 154.3958 205.8173 14.43647204382948

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EMISAT",
  "OBJECT_ID": "2019-018A",
  "EPOCH": "2026-07-07T04:11:24.317+00:00",
  "MEAN_MOTION": 14.43647204,
  "ECCENTRICITY": 0.00189,
  "INCLINATION": 98.4631,
  "RA_OF_ASC_NODE": 246.8642,
  "ARG_OF_PERICENTER": 154.3958,
  "MEAN_ANOMALY": 205.8173,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 44078,
  "REV_AT_EPOCH": 38294,
  "BSTAR": 0.000050108,
  "MEAN_MOTION_DOT": 0.00000126,
  "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	EMISAT
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Apr 1, 2019HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	436HIGH

▸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/44078

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