▸Orbital parameters

Orbit class	LEO
Inclination	67.1493°
Eccentricity	0.0006677
Period	103.1 min
Apogee	910 km
Perigee	901 km
Mean motion	13.96679284 rev/day
RAAN	58.6100°
Arg of perigee	272.2985°
Mean anomaly	87.7335°
B*	2.1254e-5
Rev at epoch	18,356

▸Two-line element set (TLE)

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

1 54381U 22163A 26188.20251182 -.00000046 00000-0 21254-4 0 9990

2 54381 67.1493 58.6100 0006677 272.2985 87.7335 13.96679284183565

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2565",
  "OBJECT_ID": "2022-163A",
  "EPOCH": "2026-07-07T04:51:37.021+00:00",
  "MEAN_MOTION": 13.96679284,
  "ECCENTRICITY": 0.0006677,
  "INCLINATION": 67.1493,
  "RA_OF_ASC_NODE": 58.61,
  "ARG_OF_PERICENTER": 272.2985,
  "MEAN_ANOMALY": 87.7335,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54381,
  "REV_AT_EPOCH": 18356,
  "BSTAR": 0.000021254,
  "MEAN_MOTION_DOT": -4.6e-7,
  "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 2565
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)	6575HIGHvia 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/54381

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