▸Orbital parameters

Orbit class	SSO
Inclination	97.8020°
Eccentricity	0.0007565
Period	96.8 min
Apogee	610 km
Perigee	599 km
Mean motion	14.87972912 rev/day
RAAN	186.2147°
Arg of perigee	75.7316°
Mean anomaly	284.4740°
B*	1.4066e-4
Rev at epoch	2,623

▸Two-line element set (TLE)

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

1 67373U 26004L 26187.96170103 .00001236 00000-0 14066-3 0 9991

2 67373 97.8020 186.2147 0007565 75.7316 284.4740 14.87972912 26237

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ICEYE-X64",
  "OBJECT_ID": "2026-004L",
  "EPOCH": "2026-07-06T23:04:50.969+00:00",
  "MEAN_MOTION": 14.87972912,
  "ECCENTRICITY": 0.0007565,
  "INCLINATION": 97.802,
  "RA_OF_ASC_NODE": 186.2147,
  "ARG_OF_PERICENTER": 75.7316,
  "MEAN_ANOMALY": 284.474,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67373,
  "REV_AT_EPOCH": 2623,
  "BSTAR": 0.00014066,
  "MEAN_MOTION_DOT": 0.00001236,
  "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-X64
Operator	Finnish Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree University of ArizonaMEDIUMvia Wikidata
Country	United StatesMEDIUMvia Wikidata
Launch date	Jan 11, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	120HIGH

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/67373

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