▸Orbital parameters

Orbit class	SSO
Inclination	97.4203°
Eccentricity	0.0002846
Period	94.5 min
Apogee	498 km
Perigee	494 km
Mean motion	15.23318074 rev/day
RAAN	261.8380°
Arg of perigee	305.6308°
Mean anomaly	54.4664°
B*	3.5021e-4
Rev at epoch	3,347

▸Two-line element set (TLE)

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

1 66685U 25276V 26188.05393066 .00008245 00000-0 35021-3 0 9993

2 66685 97.4203 261.8380 0002846 305.6308 54.4664 15.23318074 33471

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AE5RA",
  "OBJECT_ID": "2025-276V",
  "EPOCH": "2026-07-07T01:17:39.609+00:00",
  "MEAN_MOTION": 15.23318074,
  "ECCENTRICITY": 0.0002846,
  "INCLINATION": 97.4203,
  "RA_OF_ASC_NODE": 261.838,
  "ARG_OF_PERICENTER": 305.6308,
  "MEAN_ANOMALY": 54.4664,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66685,
  "REV_AT_EPOCH": 3347,
  "BSTAR": 0.00035021,
  "MEAN_MOTION_DOT": 0.00008245,
  "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	AE5RA
Operator	ArkEdge SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Japan
Launch date	Nov 28, 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/66685

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