▸Orbital parameters

Orbit class	LEO
Inclination	58.6848°
Eccentricity	0.0435495
Period	100.0 min
Apogee	1,071 km
Perigee	449 km
Mean motion	14.39580567 rev/day
RAAN	159.7543°
Arg of perigee	128.8870°
Mean anomaly	235.1852°
B*	1.3052e-4
Rev at epoch	12,805

▸Two-line element set (TLE)

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

1 58849U 24018A 26188.17790183 .00001023 00000-0 13052-3 0 9990

2 58849 58.6848 159.7543 0435495 128.8870 235.1852 14.39580567128053

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2024-018A",
  "OBJECT_ID": "2024-018A",
  "EPOCH": "2026-07-07T04:16:10.718+00:00",
  "MEAN_MOTION": 14.39580567,
  "ECCENTRICITY": 0.0435495,
  "INCLINATION": 58.6848,
  "RA_OF_ASC_NODE": 159.7543,
  "ARG_OF_PERICENTER": 128.887,
  "MEAN_ANOMALY": 235.1852,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58849,
  "REV_AT_EPOCH": 12805,
  "BSTAR": 0.00013052,
  "MEAN_MOTION_DOT": 0.00001023,
  "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	2024-018A
Operator	Iranian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Iran
Launch date	Jan 28, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	32HIGHvia GCAT — Jonathan McDowell's General Catalog 32MEDIUMvia Wikidata
Mission purpose	—

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/58849

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