▸Orbital parameters

Orbit class	GEO
Inclination	0.0222°
Eccentricity	0.0000808
Period	1436.4 min
Apogee	35,796 km
Perigee	35,789 km
Mean motion	1.00250760 rev/day
RAAN	289.1502°
Arg of perigee	259.8985°
Mean anomaly	30.3466°
B*	0.0000e+0
Rev at epoch	3,954

▸Two-line element set (TLE)

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

1 40895U 15048A 26187.85714279 -.00000100 00000-0 00000-0 0 9993

2 40895 0.0222 289.1502 0000808 259.8985 30.3466 1.00250760 39547

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EXPRESS-AM8",
  "OBJECT_ID": "2015-048A",
  "EPOCH": "2026-07-06T20:34:17.137+00:00",
  "MEAN_MOTION": 1.0025076,
  "ECCENTRICITY": 0.0000808,
  "INCLINATION": 0.0222,
  "RA_OF_ASC_NODE": 289.1502,
  "ARG_OF_PERICENTER": 259.8985,
  "MEAN_ANOMALY": 30.3466,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40895,
  "REV_AT_EPOCH": 3954,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.000001,
  "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-AM8
Operator	Russian Satellite Communications Co.HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Russian Satellite Communications CompanyMEDIUMvia Wikidata
Country	RussiaMEDIUMvia Wikidata
Launch date	Sep 14, 2015HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2163

▸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/40895

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