▸Orbital parameters

Orbit class	SSO
Inclination	97.3937°
Eccentricity	0.0005409
Period	92.0 min
Apogee	375 km
Perigee	367 km
Mean motion	15.65814731 rev/day
RAAN	277.9727°
Arg of perigee	224.3974°
Mean anomaly	135.6853°
B*	1.3052e-3
Rev at epoch	8,242

▸Two-line element set (TLE)

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

1 62618U 25009K 26187.24303740 .00134054 00000-0 13052-2 0 9996

2 62618 97.3937 277.9727 0005409 224.3974 135.6853 15.65814731 82421

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AE1D",
  "OBJECT_ID": "2025-009K",
  "EPOCH": "2026-07-06T05:49:58.431+00:00",
  "MEAN_MOTION": 15.65814731,
  "ECCENTRICITY": 0.00054093,
  "INCLINATION": 97.3937,
  "RA_OF_ASC_NODE": 277.9727,
  "ARG_OF_PERICENTER": 224.3974,
  "MEAN_ANOMALY": 135.6853,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62618,
  "REV_AT_EPOCH": 8242,
  "BSTAR": 0.0013051956,
  "MEAN_MOTION_DOT": 0.00134054,
  "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	AE1D
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/62618

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