▸Orbital parameters

Orbit class	SSO
Inclination	97.6763°
Eccentricity	0.0006944
Period	96.0 min
Apogee	572 km
Perigee	562 km
Mean motion	15.00030277 rev/day
RAAN	264.4489°
Arg of perigee	69.0679°
Mean anomaly	291.1287°
B*	3.0278e-4
Rev at epoch	10,304

▸Two-line element set (TLE)

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

1 60546U 24149CG 26187.68979990 .00003711 00000-0 30278-3 0 9997

2 60546 97.6763 264.4489 0006944 69.0679 291.1287 15.00030277103041

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ICEYE-X39",
  "OBJECT_ID": "2024-149CG",
  "EPOCH": "2026-07-06T16:33:18.711+00:00",
  "MEAN_MOTION": 15.00030277,
  "ECCENTRICITY": 0.0006944,
  "INCLINATION": 97.6763,
  "RA_OF_ASC_NODE": 264.4489,
  "ARG_OF_PERICENTER": 69.0679,
  "MEAN_ANOMALY": 291.1287,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60546,
  "REV_AT_EPOCH": 10304,
  "BSTAR": 0.00030278,
  "MEAN_MOTION_DOT": 0.00003711,
  "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-X39
Operator	Brazilian Air Force / ICEYEHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Brazil
Launch date	Aug 16, 2024HIGHvia 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/60546

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