▸Orbital parameters

Orbit class	SSO
Inclination	97.4016°
Eccentricity	0.0002118
Period	94.7 min
Apogee	507 km
Perigee	504 km
Mean motion	15.20102141 rev/day
RAAN	85.5260°
Arg of perigee	273.1025°
Mean anomaly	86.9968°
B*	2.3762e-4
Rev at epoch	983

▸Two-line element set (TLE)

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

1 69020U 26100AS 26188.12372051 .00005065 00000-0 23762-3 0 9991

2 69020 97.4016 85.5260 0002118 273.1025 86.9968 15.20102141 9837

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SELENE",
  "OBJECT_ID": "2026-100AS",
  "EPOCH": "2026-07-07T02:58:09.452+00:00",
  "MEAN_MOTION": 15.20102141,
  "ECCENTRICITY": 0.0002118,
  "INCLINATION": 97.4016,
  "RA_OF_ASC_NODE": 85.526,
  "ARG_OF_PERICENTER": 273.1025,
  "MEAN_ANOMALY": 86.9968,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69020,
  "REV_AT_EPOCH": 983,
  "BSTAR": 0.00023762,
  "MEAN_MOTION_DOT": 0.00005065,
  "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	SELENE
Operator	Emtech Space S.A.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Greece
Launch date	May 3, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	8HIGHvia 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/69020

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