▸Orbital parameters

Orbit class	SSO
Inclination	96.5820°
Eccentricity	0.0007813
Period	90.2 min
Apogee	290 km
Perigee	279 km
Mean motion	15.96343614 rev/day
RAAN	118.7622°
Arg of perigee	89.4404°
Mean anomaly	270.7770°
B*	1.4206e-4
Rev at epoch	5,086

▸Two-line element set (TLE)

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

1 65269U 25182C 26188.07258338 .00058406 31438-5 14206-3 0 9990

2 65269 96.5820 118.7622 0007813 89.4404 270.7770 15.96343614 50866

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2593",
  "OBJECT_ID": "2025-182C",
  "EPOCH": "2026-07-07T01:44:31.204+00:00",
  "MEAN_MOTION": 15.96343614,
  "ECCENTRICITY": 0.0007813,
  "INCLINATION": 96.582,
  "RA_OF_ASC_NODE": 118.7622,
  "ARG_OF_PERICENTER": 89.4404,
  "MEAN_ANOMALY": 270.777,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65269,
  "REV_AT_EPOCH": 5086,
  "BSTAR": 0.00014206,
  "MEAN_MOTION_DOT": 0.00058406,
  "MEAN_MOTION_DDOT": 0.0000031438
}

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 2593
Operator	Russian Ministry of DefenseHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Aug 21, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	520HIGHvia 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/65269

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