▸Orbital parameters

Orbit class	SSO
Inclination	97.5574°
Eccentricity	0.0001301
Period	94.4 min
Apogee	492 km
Perigee	490 km
Mean motion	15.25028882 rev/day
RAAN	112.3880°
Arg of perigee	44.1291°
Mean anomaly	316.0050°
B*	1.2334e-4
Rev at epoch	9,352

▸Two-line element set (TLE)

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

1 61730U 24197A 26188.21772064 .00003006 00000-0 12334-3 0 9999

2 61730 97.5574 112.3880 0001301 44.1291 316.0050 15.25028882 93520

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2579",
  "OBJECT_ID": "2024-197A",
  "EPOCH": "2026-07-07T05:13:31.063+00:00",
  "MEAN_MOTION": 15.25028882,
  "ECCENTRICITY": 0.0001301,
  "INCLINATION": 97.5574,
  "RA_OF_ASC_NODE": 112.388,
  "ARG_OF_PERICENTER": 44.1291,
  "MEAN_ANOMALY": 316.005,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61730,
  "REV_AT_EPOCH": 9352,
  "BSTAR": 0.00012334,
  "MEAN_MOTION_DOT": 0.00003006,
  "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 2579
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Oct 31, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3700HIGHvia 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/61730

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