▸Orbital parameters

Orbit class	SSO
Inclination	97.7763°
Eccentricity	0.0000604
Period	96.4 min
Apogee	587 km
Perigee	586 km
Mean motion	14.93632277 rev/day
RAAN	302.2652°
Arg of perigee	235.9177°
Mean anomaly	124.1985°
B*	1.2753e-4
Rev at epoch	5,687

▸Two-line element set (TLE)

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

1 64572U 25135AW 26188.23505462 .00001290 00000-0 12753-3 0 9995

2 64572 97.7763 302.2652 0000604 235.9177 124.1985 14.93632277 56879

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ICEYE-X52",
  "OBJECT_ID": "2025-135AW",
  "EPOCH": "2026-07-07T05:38:28.719+00:00",
  "MEAN_MOTION": 14.93632277,
  "ECCENTRICITY": 0.0000604,
  "INCLINATION": 97.7763,
  "RA_OF_ASC_NODE": 302.2652,
  "ARG_OF_PERICENTER": 235.9177,
  "MEAN_ANOMALY": 124.1985,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64572,
  "REV_AT_EPOCH": 5687,
  "BSTAR": 0.00012753,
  "MEAN_MOTION_DOT": 0.0000129,
  "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-X52
Operator	ICEYEHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Finland
Launch date	Jun 23, 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/64572

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