▸Orbital parameters

Orbit class	GEO
Inclination	6.7405°
Eccentricity	0.0000603
Period	1436.1 min
Apogee	35,789 km
Perigee	35,784 km
Mean motion	1.00273429 rev/day
RAAN	70.2816°
Arg of perigee	245.8062°
Mean anomaly	288.4891°
B*	0.0000e+0
Rev at epoch	3,870

▸Two-line element set (TLE)

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

1 41105U 15074A 26187.92832764 -.00000106 00000-0 00000-0 0 9991

2 41105 6.7405 70.2816 0000603 245.8062 288.4891 1.00273429 38701

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ELEKTRO-L 2",
  "OBJECT_ID": "2015-074A",
  "EPOCH": "2026-07-06T22:16:47.508+00:00",
  "MEAN_MOTION": 1.00273429,
  "ECCENTRICITY": 0.0000603,
  "INCLINATION": 6.7405,
  "RA_OF_ASC_NODE": 70.2816,
  "ARG_OF_PERICENTER": 245.8062,
  "MEAN_ANOMALY": 288.4891,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41105,
  "REV_AT_EPOCH": 3870,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000106,
  "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	ELEKTRO-L 2
Operator	Rosgidromet NITs Planeta / NPO Lavochkin, fil. ORKKHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Roscosmos State CorporationMEDIUMvia Wikidata
Country	Russia
Launch date	Dec 11, 2015HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1855HIGHvia GCAT — Jonathan McDowell's General Catalog

▸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/41105

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