▸Orbital parameters

Orbit class	SSO
Inclination	98.1180°
Eccentricity	0.0054618
Period	97.3 min
Apogee	669 km
Perigee	592 km
Mean motion	14.79573399 rev/day
RAAN	252.1355°
Arg of perigee	182.2711°
Mean anomaly	177.8260°
B*	1.6084e-4
Rev at epoch	10,454

▸Two-line element set (TLE)

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

1 41790U 16059H 26188.16397183 .00001178 00000-0 16084-3 0 9994

2 41790 98.1180 252.1355 0054618 182.2711 177.8260 14.79573399104541

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SCATSAT 1",
  "OBJECT_ID": "2016-059H",
  "EPOCH": "2026-07-07T03:56:07.166+00:00",
  "MEAN_MOTION": 14.79573399,
  "ECCENTRICITY": 0.0054618,
  "INCLINATION": 98.118,
  "RA_OF_ASC_NODE": 252.1355,
  "ARG_OF_PERICENTER": 182.2711,
  "MEAN_ANOMALY": 177.826,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41790,
  "REV_AT_EPOCH": 10454,
  "BSTAR": 0.00016084,
  "MEAN_MOTION_DOT": 0.00001178,
  "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	SCATSAT 1
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Sep 26, 2016HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	370HIGH

▸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/41790

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