▸Orbital parameters

Orbit class	SSO
Inclination	97.7697°
Eccentricity	0.0002810
Period	96.2 min
Apogee	577 km
Perigee	573 km
Mean motion	14.97406847 rev/day
RAAN	302.6477°
Arg of perigee	167.1503°
Mean anomaly	192.9791°
B*	4.8248e-4
Rev at epoch	5,688

▸Two-line element set (TLE)

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

1 64563U 25135AM 26187.87293066 .00005554 00000-0 48248-3 0 9993

2 64563 97.7697 302.6477 0002810 167.1503 192.9791 14.97406847 56889

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AE3VA",
  "OBJECT_ID": "2025-135AM",
  "EPOCH": "2026-07-06T20:57:01.209+00:00",
  "MEAN_MOTION": 14.97406847,
  "ECCENTRICITY": 0.000281,
  "INCLINATION": 97.7697,
  "RA_OF_ASC_NODE": 302.6477,
  "ARG_OF_PERICENTER": 167.1503,
  "MEAN_ANOMALY": 192.9791,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64563,
  "REV_AT_EPOCH": 5688,
  "BSTAR": 0.00048248,
  "MEAN_MOTION_DOT": 0.00005554,
  "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	AE3VA
Operator	ArkEdge SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Japan
Launch date	Jun 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia 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/64563

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