▸Orbital parameters

Orbit class	GEO
Inclination	0.0290°
Eccentricity	0.0000259
Period	1436.1 min
Apogee	35,788 km
Perigee	35,785 km
Mean motion	1.00272154 rev/day
RAAN	270.1698°
Arg of perigee	160.4646°
Mean anomaly	107.6421°
B*	0.0000e+0
Rev at epoch	4,654

▸Two-line element set (TLE)

EPOCH Jul 5, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 39487U 13077A 26186.31924735 -.00000267 00000-0 00000-0 0 9992

2 39487 0.0290 270.1698 0000259 160.4646 107.6421 1.00272154 46542

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EXPRESS-AM5",
  "OBJECT_ID": "2013-077A",
  "EPOCH": "2026-07-05T07:39:42.971+00:00",
  "MEAN_MOTION": 1.00272154,
  "ECCENTRICITY": 0.0000259,
  "INCLINATION": 0.029,
  "RA_OF_ASC_NODE": 270.1698,
  "ARG_OF_PERICENTER": 160.4646,
  "MEAN_ANOMALY": 107.6421,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39487,
  "REV_AT_EPOCH": 4654,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000267,
  "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-AM5
Operator	Russian Satellite Communications Co.HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Russian Satellite Communications CompanyMEDIUMvia Wikidata
Country	RussiaMEDIUMvia Wikidata
Launch date	Dec 26, 2013HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3200HIGH

▸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/39487

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