▸Orbital parameters

Orbit class	SSO
Inclination	97.4158°
Eccentricity	0.0002167
Period	94.5 min
Apogee	497 km
Perigee	494 km
Mean motion	15.23320994 rev/day
RAAN	261.3823°
Arg of perigee	302.0783°
Mean anomaly	58.0243°
B*	3.8611e-4
Rev at epoch	3,342

▸Two-line element set (TLE)

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

1 66693U 25276AD 26187.72601009 .00009099 00000-0 38611-3 0 9990

2 66693 97.4158 261.3823 0002167 302.0783 58.0243 15.23320994 33422

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AE5RB",
  "OBJECT_ID": "2025-276AD",
  "EPOCH": "2026-07-06T17:25:27.272+00:00",
  "MEAN_MOTION": 15.23320994,
  "ECCENTRICITY": 0.0002167,
  "INCLINATION": 97.4158,
  "RA_OF_ASC_NODE": 261.3823,
  "ARG_OF_PERICENTER": 302.0783,
  "MEAN_ANOMALY": 58.0243,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66693,
  "REV_AT_EPOCH": 3342,
  "BSTAR": 0.00038611,
  "MEAN_MOTION_DOT": 0.00009099,
  "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	AE5RB
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/66693

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