▸Orbital parameters

Orbit class	LEO
Inclination	67.1420°
Eccentricity	0.0003567
Period	103.0 min
Apogee	904 km
Perigee	899 km
Mean motion	13.97714389 rev/day
RAAN	53.3789°
Arg of perigee	17.9896°
Mean anomaly	342.1314°
B*	4.8116e-5
Rev at epoch	18,336

▸Two-line element set (TLE)

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

1 54383U 22163C 26188.19367934 -.00000007 00000-0 48116-4 0 9996

2 54383 67.1420 53.3789 0003567 17.9896 342.1314 13.97714389183362

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2566",
  "OBJECT_ID": "2022-163C",
  "EPOCH": "2026-07-07T04:38:53.895+00:00",
  "MEAN_MOTION": 13.97714389,
  "ECCENTRICITY": 0.0003567,
  "INCLINATION": 67.142,
  "RA_OF_ASC_NODE": 53.3789,
  "ARG_OF_PERICENTER": 17.9896,
  "MEAN_ANOMALY": 342.1314,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54383,
  "REV_AT_EPOCH": 18336,
  "BSTAR": 0.000048116,
  "MEAN_MOTION_DOT": -7e-8,
  "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	COSMOS 2566
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Nov 30, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia 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/54383

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