▸Orbital parameters

Orbit class	SSO
Inclination	96.6139°
Eccentricity	0.0002723
Period	91.4 min
Apogee	345 km
Perigee	342 km
Mean motion	15.75382406 rev/day
RAAN	71.2297°
Arg of perigee	106.2341°
Mean anomaly	253.9225°
B*	1.2741e-3
Rev at epoch	13,877

▸Two-line element set (TLE)

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

1 58929U 24026A 26188.13626773 .00195939 00000-0 12741-2 0 9990

2 58929 96.6139 71.2297 0002723 106.2341 253.9225 15.75382406138773

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2575",
  "OBJECT_ID": "2024-026A",
  "EPOCH": "2026-07-07T03:16:13.532+00:00",
  "MEAN_MOTION": 15.75382406,
  "ECCENTRICITY": 0.0002723,
  "INCLINATION": 96.6139,
  "RA_OF_ASC_NODE": 71.2297,
  "ARG_OF_PERICENTER": 106.2341,
  "MEAN_ANOMALY": 253.9225,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58929,
  "REV_AT_EPOCH": 13877,
  "BSTAR": 0.0012741,
  "MEAN_MOTION_DOT": 0.00195939,
  "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 2575
Operator	Russian Ministry of DefenseHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Feb 9, 2024HIGHvia 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/58929

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