▸Orbital parameters

Orbit class	LEO
Inclination	45.4051°
Eccentricity	0.0004668
Period	95.5 min
Apogee	546 km
Perigee	539 km
Mean motion	15.07893453 rev/day
RAAN	30.2151°
Arg of perigee	152.2695°
Mean anomaly	207.8436°
B*	1.9511e-4
Rev at epoch	3,850

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 66300U 25248H 26187.95825506 .00002793 00000-0 19511-3 0 9991

2 66300 45.4051 30.2151 0004668 152.2695 207.8436 15.07893453 38503

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ICEYE-X65",
  "OBJECT_ID": "2025-248H",
  "EPOCH": "2026-07-06T22:59:53.237+00:00",
  "MEAN_MOTION": 15.07893453,
  "ECCENTRICITY": 0.0004668,
  "INCLINATION": 45.4051,
  "RA_OF_ASC_NODE": 30.2151,
  "ARG_OF_PERICENTER": 152.2695,
  "MEAN_ANOMALY": 207.8436,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66300,
  "REV_AT_EPOCH": 3850,
  "BSTAR": 0.00019511,
  "MEAN_MOTION_DOT": 0.00002793,
  "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	ICEYE-X65
Operator	Space42 PlcHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Arab Emirates
Launch date	Nov 2, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	80HIGHvia 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/66300

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