▸Orbital parameters

Orbit class	LEO
Inclination	67.1490°
Eccentricity	0.0006034
Period	103.1 min
Apogee	910 km
Perigee	901 km
Mean motion	13.96674012 rev/day
RAAN	2.1688°
Arg of perigee	262.6403°
Mean anomaly	97.3996°
B*	1.1162e-5
Rev at epoch	8,093

▸Two-line element set (TLE)

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

1 62216U 24230A 26188.21450230 -.00000060 00000-0 11162-4 0 9992

2 62216 67.1490 2.1688 0006034 262.6403 97.3996 13.96674012 80939

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2580",
  "OBJECT_ID": "2024-230A",
  "EPOCH": "2026-07-07T05:08:52.999+00:00",
  "MEAN_MOTION": 13.96674012,
  "ECCENTRICITY": 0.0006034,
  "INCLINATION": 67.149,
  "RA_OF_ASC_NODE": 2.1688,
  "ARG_OF_PERICENTER": 262.6403,
  "MEAN_ANOMALY": 97.3996,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62216,
  "REV_AT_EPOCH": 8093,
  "BSTAR": 0.000011162,
  "MEAN_MOTION_DOT": -6e-7,
  "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 2580
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Dec 4, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	6575HIGHvia 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/62216

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