▸Orbital parameters

Orbit class	SSO
Inclination	97.3953°
Eccentricity	0.0010444
Period	95.7 min
Apogee	561 km
Perigee	546 km
Mean motion	15.04301633 rev/day
RAAN	224.6062°
Arg of perigee	265.2628°
Mean anomaly	94.7406°
B*	7.9122e-5
Rev at epoch	41,479

▸Two-line element set (TLE)

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

1 43792U 18099AL 26188.06950325 .00001045 00000-0 79122-4 0 9992

2 43792 97.3953 224.6062 0010444 265.2628 94.7406 15.04301633414790

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ESEO",
  "OBJECT_ID": "2018-099AL",
  "EPOCH": "2026-07-07T01:40:05.081+00:00",
  "MEAN_MOTION": 15.04301633,
  "ECCENTRICITY": 0.0010444,
  "INCLINATION": 97.3953,
  "RA_OF_ASC_NODE": 224.6062,
  "ARG_OF_PERICENTER": 265.2628,
  "MEAN_ANOMALY": 94.7406,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43792,
  "REV_AT_EPOCH": 41479,
  "BSTAR": 0.000079122,
  "MEAN_MOTION_DOT": 0.00001045,
  "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	ESEO
Operator	European Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree University of BolognaMEDIUMvia Wikidata
Country	ESA
Launch date	Dec 3, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	120HIGHvia GCAT — Jonathan McDowell's General Catalog⚠

▸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/43792

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