▸Orbital parameters

Orbit class	SSO
Inclination	97.3419°
Eccentricity	0.0001655
Period	94.4 min
Apogee	489 km
Perigee	487 km
Mean motion	15.25985392 rev/day
RAAN	92.0317°
Arg of perigee	71.6841°
Mean anomaly	288.4577°
B*	1.9287e-4
Rev at epoch	21,763

▸Two-line element set (TLE)

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

1 53370U 22096A 26188.16351457 .00004885 00000-0 19287-3 0 9999

2 53370 97.3419 92.0317 0001655 71.6841 288.4577 15.25985392217638

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KHAYYAM",
  "OBJECT_ID": "2022-096A",
  "EPOCH": "2026-07-07T03:55:27.659+00:00",
  "MEAN_MOTION": 15.25985392,
  "ECCENTRICITY": 0.0001655,
  "INCLINATION": 97.3419,
  "RA_OF_ASC_NODE": 92.0317,
  "ARG_OF_PERICENTER": 71.6841,
  "MEAN_ANOMALY": 288.4577,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 53370,
  "REV_AT_EPOCH": 21763,
  "BSTAR": 0.00019287,
  "MEAN_MOTION_DOT": 0.00004885,
  "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	KHAYYAM
Operator	Iranian Space Agency / Bonyan Danesh SharghHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Iranian Space AgencyMEDIUMvia Wikidata
Country	IranMEDIUMvia Wikidata
Launch date	Aug 9, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	650HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/53370

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