▸Orbital parameters

Orbit class	LEO
Inclination	82.5053°
Eccentricity	0.0021972
Period	115.9 min
Apogee	1,512 km
Perigee	1,477 km
Mean motion	12.42894789 rev/day
RAAN	289.9900°
Arg of perigee	135.5248°
Mean anomaly	224.7600°
B*	9.6894e-4
Rev at epoch	25,356

▸Two-line element set (TLE)

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

1 47227U 20091A 26188.21073029 .00000144 00000-0 96894-3 0 9991

2 47227 82.5053 289.9900 0021972 135.5248 224.7600 12.42894789253569

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GONETS-M 20",
  "OBJECT_ID": "2020-091A",
  "EPOCH": "2026-07-07T05:03:27.097+00:00",
  "MEAN_MOTION": 12.42894789,
  "ECCENTRICITY": 0.0021972,
  "INCLINATION": 82.5053,
  "RA_OF_ASC_NODE": 289.99,
  "ARG_OF_PERICENTER": 135.5248,
  "MEAN_ANOMALY": 224.76,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 47227,
  "REV_AT_EPOCH": 25356,
  "BSTAR": 0.00096894,
  "MEAN_MOTION_DOT": 0.00000144,
  "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	GONETS-M 20
Operator	Gonets Satellite SystemsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Dec 3, 2020HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	225HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/47227

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