▸Orbital parameters

Orbit class	LEO
Inclination	45.4057°
Eccentricity	0.0005863
Period	95.4 min
Apogee	543 km
Perigee	535 km
Mean motion	15.09123634 rev/day
RAAN	28.8035°
Arg of perigee	148.7145°
Mean anomaly	211.4087°
B*	1.7712e-4
Rev at epoch	3,851

▸Two-line element set (TLE)

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

1 66302U 25248K 26187.98735860 .00002603 00000-0 17712-3 0 9990

2 66302 45.4057 28.8035 0005863 148.7145 211.4087 15.09123634 38516

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ICEYE-X67",
  "OBJECT_ID": "2025-248K",
  "EPOCH": "2026-07-06T23:41:47.783+00:00",
  "MEAN_MOTION": 15.09123634,
  "ECCENTRICITY": 0.0005863,
  "INCLINATION": 45.4057,
  "RA_OF_ASC_NODE": 28.8035,
  "ARG_OF_PERICENTER": 148.7145,
  "MEAN_ANOMALY": 211.4087,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66302,
  "REV_AT_EPOCH": 3851,
  "BSTAR": 0.00017712,
  "MEAN_MOTION_DOT": 0.00002603,
  "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-X67
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/66302

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