▸Orbital parameters

Orbit class	SSO
Inclination	96.5858°
Eccentricity	0.0006655
Period	90.2 min
Apogee	289 km
Perigee	280 km
Mean motion	15.96422965 rev/day
RAAN	118.8216°
Arg of perigee	92.3454°
Mean anomaly	267.8586°
B*	1.7061e-4
Rev at epoch	5,087

▸Two-line element set (TLE)

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

1 65268U 25182B 26188.11957970 .00070502 37420-5 17061-3 0 9992

2 65268 96.5858 118.8216 0006655 92.3454 267.8586 15.96422965 50877

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2592",
  "OBJECT_ID": "2025-182B",
  "EPOCH": "2026-07-07T02:52:11.686+00:00",
  "MEAN_MOTION": 15.96422965,
  "ECCENTRICITY": 0.0006655,
  "INCLINATION": 96.5858,
  "RA_OF_ASC_NODE": 118.8216,
  "ARG_OF_PERICENTER": 92.3454,
  "MEAN_ANOMALY": 267.8586,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65268,
  "REV_AT_EPOCH": 5087,
  "BSTAR": 0.00017061,
  "MEAN_MOTION_DOT": 0.00070502,
  "MEAN_MOTION_DDOT": 0.000003742
}

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 2592
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/65268

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