▸Orbital parameters

Orbit class	SSO
Inclination	97.9654°
Eccentricity	0.0010884
Period	97.3 min
Apogee	638 km
Perigee	622 km
Mean motion	14.79787243 rev/day
RAAN	271.3638°
Arg of perigee	31.9850°
Mean anomaly	328.2020°
B*	8.2641e-4
Rev at epoch	4,679

▸Two-line element set (TLE)

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

1 65298U 25185B 26188.16169139 .00006177 00000-0 82641-3 0 9997

2 65298 97.9654 271.3638 0010884 31.9850 328.2020 14.79787243 46794

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FOURIER",
  "OBJECT_ID": "2025-185B",
  "EPOCH": "2026-07-07T03:52:50.136+00:00",
  "MEAN_MOTION": 14.79787243,
  "ECCENTRICITY": 0.0010884,
  "INCLINATION": 97.9654,
  "RA_OF_ASC_NODE": 271.3638,
  "ARG_OF_PERICENTER": 31.985,
  "MEAN_ANOMALY": 328.202,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65298,
  "REV_AT_EPOCH": 4679,
  "BSTAR": 0.00082641,
  "MEAN_MOTION_DOT": 0.00006177,
  "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	FOURIER
Operator	E-SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	RW
Launch date	Aug 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	30HIGHvia 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/65298

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