▸Orbital parameters

Orbit class	GEO
Inclination	1.3128°
Eccentricity	0.0003763
Period	1436.1 min
Apogee	35,802 km
Perigee	35,771 km
Mean motion	1.00272020 rev/day
RAAN	83.9190°
Arg of perigee	20.2821°
Mean anomaly	291.9438°
B*	0.0000e+0
Rev at epoch	4,959

▸Two-line element set (TLE)

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

1 39022U 12070A 26188.15589458 .00000100 00000-0 00000-0 0 9997

2 39022 1.3128 83.9190 0003763 20.2821 291.9438 1.00272020 49594

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAMAL 402",
  "OBJECT_ID": "2012-070A",
  "EPOCH": "2026-07-07T03:44:29.292+00:00",
  "MEAN_MOTION": 1.0027202,
  "ECCENTRICITY": 0.0003763,
  "INCLINATION": 1.3128,
  "RA_OF_ASC_NODE": 83.919,
  "ARG_OF_PERICENTER": 20.2821,
  "MEAN_ANOMALY": 291.9438,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39022,
  "REV_AT_EPOCH": 4959,
  "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	YAMAL 402
Operator	Gazprom Space SystemsHIGHvia GCAT — Jonathan McDowell's General Catalog Gazprom Space SystemsMEDIUMvia Wikidata
Country	Russia
Launch date	Dec 8, 2012HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4463HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree

▸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/39022

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