▸Orbital parameters

Orbit class	LEO
Inclination	82.5035°
Eccentricity	0.0022869
Period	115.9 min
Apogee	1,512 km
Perigee	1,476 km
Mean motion	12.42894213 rev/day
RAAN	289.5757°
Arg of perigee	130.9756°
Mean anomaly	229.3307°
B*	1.4429e-3
Rev at epoch	25,351

▸Two-line element set (TLE)

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

1 47229U 20091C 26188.23820067 .00000210 00000-0 14429-2 0 9994

2 47229 82.5035 289.5757 0022869 130.9756 229.3307 12.42894213253518

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GONETS-M 22",
  "OBJECT_ID": "2020-091C",
  "EPOCH": "2026-07-07T05:43:00.538+00:00",
  "MEAN_MOTION": 12.42894213,
  "ECCENTRICITY": 0.0022869,
  "INCLINATION": 82.5035,
  "RA_OF_ASC_NODE": 289.5757,
  "ARG_OF_PERICENTER": 130.9756,
  "MEAN_ANOMALY": 229.3307,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 47229,
  "REV_AT_EPOCH": 25351,
  "BSTAR": 0.0014429,
  "MEAN_MOTION_DOT": 0.0000021,
  "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 22
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/47229

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