▸Orbital parameters

Orbit class	SSO
Inclination	97.4165°
Eccentricity	0.0003337
Period	94.5 min
Apogee	498 km
Perigee	494 km
Mean motion	15.23297231 rev/day
RAAN	261.4078°
Arg of perigee	311.4157°
Mean anomaly	48.6792°
B*	4.6522e-4
Rev at epoch	3,342

▸Two-line element set (TLE)

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

1 66677U 25276M 26187.72651978 .00010974 00000-0 46522-3 0 9996

2 66677 97.4165 261.4078 0003337 311.4157 48.6792 15.23297231 33425

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AE5RC",
  "OBJECT_ID": "2025-276M",
  "EPOCH": "2026-07-06T17:26:11.309+00:00",
  "MEAN_MOTION": 15.23297231,
  "ECCENTRICITY": 0.0003337,
  "INCLINATION": 97.4165,
  "RA_OF_ASC_NODE": 261.4078,
  "ARG_OF_PERICENTER": 311.4157,
  "MEAN_ANOMALY": 48.6792,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66677,
  "REV_AT_EPOCH": 3342,
  "BSTAR": 0.00046522,
  "MEAN_MOTION_DOT": 0.00010974,
  "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	AE5RC
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/66677

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