▸Orbital parameters

Orbit class	SSO
Inclination	97.7706°
Eccentricity	0.0003508
Period	96.2 min
Apogee	578 km
Perigee	573 km
Mean motion	14.97314591 rev/day
RAAN	303.3064°
Arg of perigee	253.3584°
Mean anomaly	106.7252°
B*	3.6460e-4
Rev at epoch	5,695

▸Two-line element set (TLE)

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

1 64591U 25135BR 26188.20532771 .00004172 00000-0 36460-3 0 9999

2 64591 97.7706 303.3064 0003508 253.3584 106.7252 14.97314591 56950

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AE2A",
  "OBJECT_ID": "2025-135BR",
  "EPOCH": "2026-07-07T04:55:40.314+00:00",
  "MEAN_MOTION": 14.97314591,
  "ECCENTRICITY": 0.0003508,
  "INCLINATION": 97.7706,
  "RA_OF_ASC_NODE": 303.3064,
  "ARG_OF_PERICENTER": 253.3584,
  "MEAN_ANOMALY": 106.7252,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64591,
  "REV_AT_EPOCH": 5695,
  "BSTAR": 0.0003646,
  "MEAN_MOTION_DOT": 0.00004172,
  "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	AE2A
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/64591

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