▸Orbital parameters

Orbit class	LEO
Inclination	58.6816°
Eccentricity	0.0428069
Period	99.9 min
Apogee	1,060 km
Perigee	449 km
Mean motion	14.41130862 rev/day
RAAN	153.0803°
Arg of perigee	131.3946°
Mean anomaly	232.4719°
B*	1.3645e-4
Rev at epoch	12,817

▸Two-line element set (TLE)

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

1 58851U 24018C 26188.18767882 .00001089 00000-0 13645-3 0 9994

2 58851 58.6816 153.0803 0428069 131.3946 232.4719 14.41130862128176

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2024-018C",
  "OBJECT_ID": "2024-018C",
  "EPOCH": "2026-07-07T04:30:15.45+00:00",
  "MEAN_MOTION": 14.41130862,
  "ECCENTRICITY": 0.0428069,
  "INCLINATION": 58.6816,
  "RA_OF_ASC_NODE": 153.0803,
  "ARG_OF_PERICENTER": 131.3946,
  "MEAN_ANOMALY": 232.4719,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58851,
  "REV_AT_EPOCH": 12817,
  "BSTAR": 0.00013645,
  "MEAN_MOTION_DOT": 0.00001089,
  "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	2024-018C
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)	1500HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	ROCKET_BODYHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/58851

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