▸Orbital parameters

Orbit class	LEO
Inclination	64.5144°
Eccentricity	0.0008835
Period	99.8 min
Apogee	756 km
Perigee	743 km
Mean motion	14.42720992 rev/day
RAAN	22.6900°
Arg of perigee	267.7399°
Mean anomaly	92.2675°
B*	4.2494e-5
Rev at epoch	12,966

▸Two-line element set (TLE)

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

1 58817U 24015A 26188.21810197 .00000035 00000-0 42494-4 0 9990

2 58817 64.5144 22.6900 0008835 267.7399 92.2675 14.42720992129666

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SORAYA",
  "OBJECT_ID": "2024-015A",
  "EPOCH": "2026-07-07T05:14:04.01+00:00",
  "MEAN_MOTION": 14.42720992,
  "ECCENTRICITY": 0.0008835,
  "INCLINATION": 64.5144,
  "RA_OF_ASC_NODE": 22.69,
  "ARG_OF_PERICENTER": 267.7399,
  "MEAN_ANOMALY": 92.2675,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58817,
  "REV_AT_EPOCH": 12966,
  "BSTAR": 0.000042494,
  "MEAN_MOTION_DOT": 3.5e-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	SORAYA
Operator	Iranian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Iran
Launch date	Jan 20, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	50HIGHvia 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/58817

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