▸Orbital parameters

Orbit class	SSO
Inclination	96.5819°
Eccentricity	0.0008308
Period	90.2 min
Apogee	290 km
Perigee	279 km
Mean motion	15.96424555 rev/day
RAAN	118.5818°
Arg of perigee	91.3803°
Mean anomaly	268.8427°
B*	1.3391e-4
Rev at epoch	5,085

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 65270U 25182D 26187.90018897 .00055287 30103-5 13391-3 0 9993

2 65270 96.5819 118.5818 0008308 91.3803 268.8427 15.96424555 50856

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2594",
  "OBJECT_ID": "2025-182D",
  "EPOCH": "2026-07-06T21:36:16.327+00:00",
  "MEAN_MOTION": 15.96424555,
  "ECCENTRICITY": 0.0008308,
  "INCLINATION": 96.5819,
  "RA_OF_ASC_NODE": 118.5818,
  "ARG_OF_PERICENTER": 91.3803,
  "MEAN_ANOMALY": 268.8427,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65270,
  "REV_AT_EPOCH": 5085,
  "BSTAR": 0.00013391,
  "MEAN_MOTION_DOT": 0.00055287,
  "MEAN_MOTION_DDOT": 0.0000030103
}

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 2594
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/65270

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