▸Orbital parameters

Orbit class	SSO
Inclination	97.4341°
Eccentricity	0.0009008
Period	94.9 min
Apogee	518 km
Perigee	506 km
Mean motion	15.17975610 rev/day
RAAN	241.6732°
Arg of perigee	224.9396°
Mean anomaly	135.1109°
B*	1.6820e-4
Rev at epoch	41,585

▸Two-line element set (TLE)

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

1 43800U 18099AU 26188.18286419 .00003353 00000-0 16820-3 0 9990

2 43800 97.4341 241.6732 0009008 224.9396 135.1109 15.17975610415857

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ICEYE-X2",
  "OBJECT_ID": "2018-099AU",
  "EPOCH": "2026-07-07T04:23:19.466+00:00",
  "MEAN_MOTION": 15.1797561,
  "ECCENTRICITY": 0.0009008,
  "INCLINATION": 97.4341,
  "RA_OF_ASC_NODE": 241.6732,
  "ARG_OF_PERICENTER": 224.9396,
  "MEAN_ANOMALY": 135.1109,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43800,
  "REV_AT_EPOCH": 41585,
  "BSTAR": 0.0001682,
  "MEAN_MOTION_DOT": 0.00003353,
  "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-X2
Operator	ICEYEHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Finland
Launch date	Dec 3, 2018HIGHvia 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/43800

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