▸Orbital parameters

Orbit class	SSO
Inclination	97.6867°
Eccentricity	0.0003052
Period	96.3 min
Apogee	583 km
Perigee	579 km
Mean motion	14.95343739 rev/day
RAAN	79.6760°
Arg of perigee	118.5054°
Mean anomaly	241.6475°
B*	1.4463e-4
Rev at epoch	7,163

▸Two-line element set (TLE)

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

1 63255U 25052AX 26188.16609639 .00001539 00000-0 14463-3 0 9999

2 63255 97.6867 79.6760 0003052 118.5054 241.6475 14.95343739 71639

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ICEYE-X50",
  "OBJECT_ID": "2025-052AX",
  "EPOCH": "2026-07-07T03:59:10.728+00:00",
  "MEAN_MOTION": 14.95343739,
  "ECCENTRICITY": 0.0003052,
  "INCLINATION": 97.6867,
  "RA_OF_ASC_NODE": 79.676,
  "ARG_OF_PERICENTER": 118.5054,
  "MEAN_ANOMALY": 241.6475,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63255,
  "REV_AT_EPOCH": 7163,
  "BSTAR": 0.00014463,
  "MEAN_MOTION_DOT": 0.00001539,
  "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-X50
Operator	ICEYEHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Finland
Launch date	Mar 15, 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/63255

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