▸Orbital parameters

Orbit class	SSO
Inclination	97.7338°
Eccentricity	0.0005945
Period	96.6 min
Apogee	598 km
Perigee	589 km
Mean motion	14.91400997 rev/day
RAAN	85.1846°
Arg of perigee	83.1099°
Mean anomaly	277.0796°
B*	1.8277e-4
Rev at epoch	967

▸Two-line element set (TLE)

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

1 68996U 26100S 26188.15083043 .00001770 00000-0 18277-3 0 9999

2 68996 97.7338 85.1846 0005945 83.1099 277.0796 14.91400997 9676

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ICEYE-X82",
  "OBJECT_ID": "2026-100S",
  "EPOCH": "2026-07-07T03:37:11.749+00:00",
  "MEAN_MOTION": 14.91400997,
  "ECCENTRICITY": 0.0005945,
  "INCLINATION": 97.7338,
  "RA_OF_ASC_NODE": 85.1846,
  "ARG_OF_PERICENTER": 83.1099,
  "MEAN_ANOMALY": 277.0796,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68996,
  "REV_AT_EPOCH": 967,
  "BSTAR": 0.00018277,
  "MEAN_MOTION_DOT": 0.0000177,
  "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-X82
Operator	ICEYEHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Finland
Launch date	May 3, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	120HIGHvia 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/68996

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