▸Orbital parameters

Orbit class	SSO
Inclination	97.7389°
Eccentricity	0.0001320
Period	96.5 min
Apogee	593 km
Perigee	591 km
Mean motion	14.91850456 rev/day
RAAN	265.6884°
Arg of perigee	91.2261°
Mean anomaly	268.9109°
B*	1.5356e-4
Rev at epoch	8,020

▸Two-line element set (TLE)

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

1 62698U 25009CT 26187.72504742 .00001495 00000-0 15356-3 0 9994

2 62698 97.7389 265.6884 0001320 91.2261 268.9109 14.91850456 80200

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ICEYE-X42",
  "OBJECT_ID": "2025-009CT",
  "EPOCH": "2026-07-06T17:24:04.097+00:00",
  "MEAN_MOTION": 14.91850456,
  "ECCENTRICITY": 0.000132,
  "INCLINATION": 97.7389,
  "RA_OF_ASC_NODE": 265.6884,
  "ARG_OF_PERICENTER": 91.2261,
  "MEAN_ANOMALY": 268.9109,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62698,
  "REV_AT_EPOCH": 8020,
  "BSTAR": 0.00015356,
  "MEAN_MOTION_DOT": 0.00001495,
  "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-X42
Operator	Space42 PlcHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Arab Emirates
Launch date	Jan 14, 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/62698

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