▸Orbital parameters

Orbit class	GEO
Inclination	0.0184°
Eccentricity	0.0001758
Period	1436.1 min
Apogee	35,794 km
Perigee	35,780 km
Mean motion	1.00270451 rev/day
RAAN	4.6140°
Arg of perigee	200.4293°
Mean anomaly	154.9481°
B*	0.0000e+0
Rev at epoch	2,182

▸Two-line element set (TLE)

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

1 45986U 20053B 26187.98628424 .00000000 00000-0 00000-0 0 9999

2 45986 0.0184 4.6140 0001758 200.4293 154.9481 1.00270451 21828

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EXPRESS 80",
  "OBJECT_ID": "2020-053B",
  "EPOCH": "2026-07-06T23:40:14.958+00:00",
  "MEAN_MOTION": 1.00270451,
  "ECCENTRICITY": 0.0001758,
  "INCLINATION": 0.0184,
  "RA_OF_ASC_NODE": 4.614,
  "ARG_OF_PERICENTER": 200.4293,
  "MEAN_ANOMALY": 154.9481,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 45986,
  "REV_AT_EPOCH": 2182,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0,
  "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	EXPRESS 80
Operator	Russian Satellite Communications Co.HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Russian Satellite Communications CompanyMEDIUMvia Wikidata
Country	RussiaMEDIUMvia Wikidata
Launch date	Jul 30, 2020HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2110

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/45986

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