▸Orbital parameters

Orbit class	SSO
Inclination	97.4835°
Eccentricity	0.0010721
Period	93.1 min
Apogee	435 km
Perigee	421 km
Mean motion	15.46164687 rev/day
RAAN	169.7421°
Arg of perigee	52.7743°
Mean anomaly	307.4482°
B*	1.6925e-4
Rev at epoch	13,173

▸Two-line element set (TLE)

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

1 59065U 24039Q 26188.18604073 .00008225 00000-0 16925-3 0 9990

2 59065 97.4835 169.7421 0010721 52.7743 307.4482 15.46164687131733

▸ source OMM (JSON)

{
  "OBJECT_NAME": "PARS 1",
  "OBJECT_ID": "2024-039Q",
  "EPOCH": "2026-07-07T04:27:53.919+00:00",
  "MEAN_MOTION": 15.46164687,
  "ECCENTRICITY": 0.0010721,
  "INCLINATION": 97.4835,
  "RA_OF_ASC_NODE": 169.7421,
  "ARG_OF_PERICENTER": 52.7743,
  "MEAN_ANOMALY": 307.4482,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59065,
  "REV_AT_EPOCH": 13173,
  "BSTAR": 0.00016925,
  "MEAN_MOTION_DOT": 0.00008225,
  "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	PARS 1
Operator	Iranian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Iran
Launch date	Feb 29, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	134HIGHvia GCAT — Jonathan McDowell's General Catalog 134MEDIUMvia 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/59065

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