▸Orbital parameters

Orbit class	SSO
Inclination	97.4016°
Eccentricity	0.0001943
Period	93.1 min
Apogee	427 km
Perigee	424 km
Mean motion	15.47122014 rev/day
RAAN	276.1894°
Arg of perigee	193.1339°
Mean anomaly	166.9861°
B*	5.4352e-4
Rev at epoch	8,237

▸Two-line element set (TLE)

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

1 62649U 25009AS 26188.18310529 .00027522 00000-0 54352-3 0 9997

2 62649 97.4016 276.1894 0001943 193.1339 166.9861 15.47122014 82373

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AE1C",
  "OBJECT_ID": "2025-009AS",
  "EPOCH": "2026-07-07T04:23:40.297+00:00",
  "MEAN_MOTION": 15.47122014,
  "ECCENTRICITY": 0.0001943,
  "INCLINATION": 97.4016,
  "RA_OF_ASC_NODE": 276.1894,
  "ARG_OF_PERICENTER": 193.1339,
  "MEAN_ANOMALY": 166.9861,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62649,
  "REV_AT_EPOCH": 8237,
  "BSTAR": 0.00054352,
  "MEAN_MOTION_DOT": 0.00027522,
  "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	AE1C
Operator	ArkEdge SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Japan
Launch date	Jan 14, 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/62649

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