▸Orbital parameters

Orbit class	SSO
Inclination	97.4015°
Eccentricity	0.0010723
Period	94.8 min
Apogee	515 km
Perigee	501 km
Mean motion	15.19312324 rev/day
RAAN	238.8395°
Arg of perigee	284.8338°
Mean anomaly	75.1709°
B*	2.2248e-4
Rev at epoch	41,587

▸Two-line element set (TLE)

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

1 43786U 18099AE 26187.71598029 .00004636 00000-0 22248-3 0 9990

2 43786 97.4015 238.8395 0010723 284.8338 75.1709 15.19312324415878

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ITASAT",
  "OBJECT_ID": "2018-099AE",
  "EPOCH": "2026-07-06T17:11:00.697+00:00",
  "MEAN_MOTION": 15.19312324,
  "ECCENTRICITY": 0.0010723,
  "INCLINATION": 97.4015,
  "RA_OF_ASC_NODE": 238.8395,
  "ARG_OF_PERICENTER": 284.8338,
  "MEAN_ANOMALY": 75.1709,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43786,
  "REV_AT_EPOCH": 41587,
  "BSTAR": 0.00022248,
  "MEAN_MOTION_DOT": 0.00004636,
  "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	ITASAT
Operator	Instituto Tecnologico de AeronauticaHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	BrazilMEDIUMvia Wikidata
Launch date	Dec 3, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	8HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/43786

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