▸Orbital parameters

Orbit class	HEO
Inclination	0.5362°
Eccentricity	0.3649702
Period	1436.7 min
Apogee	51,193 km
Perigee	20,406 km
Mean motion	1.00227089 rev/day
RAAN	79.3910°
Arg of perigee	21.9424°
Mean anomaly	284.9008°
B*	0.0000e+0
Rev at epoch	380

▸Two-line element set (TLE)

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

1 64527U 25131D 26188.01310634 -.00000261 00000-0 00000-0 0 9999

2 64527 0.5362 79.3910 3649702 21.9424 284.9008 1.00227089 3805

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2590",
  "OBJECT_ID": "2025-131D",
  "EPOCH": "2026-07-07T00:18:52.388+00:00",
  "MEAN_MOTION": 1.00227089,
  "ECCENTRICITY": 0.3649702,
  "INCLINATION": 0.5362,
  "RA_OF_ASC_NODE": 79.391,
  "ARG_OF_PERICENTER": 21.9424,
  "MEAN_ANOMALY": 284.9008,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64527,
  "REV_AT_EPOCH": 380,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000261,
  "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 2590
Operator	OAO M. Reshetnev Information Satellite SystemsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Jun 19, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	200HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims6

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/64527

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