▸Orbital parameters

Orbit class	SSO
Inclination	97.7551°
Eccentricity	0.0002487
Period	96.5 min
Apogee	591 km
Perigee	587 km
Mean motion	14.92842217 rev/day
RAAN	146.1148°
Arg of perigee	132.6730°
Mean anomaly	227.4699°
B*	2.3494e-4
Rev at epoch	1,470

▸Two-line element set (TLE)

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

1 68487U 26067BZ 26188.12358057 .00002376 00000-0 23494-3 0 9993

2 68487 97.7551 146.1148 0002487 132.6730 227.4699 14.92842217 14708

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AE1A",
  "OBJECT_ID": "2026-067BZ",
  "EPOCH": "2026-07-07T02:57:57.361+00:00",
  "MEAN_MOTION": 14.92842217,
  "ECCENTRICITY": 0.0002487,
  "INCLINATION": 97.7551,
  "RA_OF_ASC_NODE": 146.1148,
  "ARG_OF_PERICENTER": 132.673,
  "MEAN_ANOMALY": 227.4699,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68487,
  "REV_AT_EPOCH": 1470,
  "BSTAR": 0.00023494,
  "MEAN_MOTION_DOT": 0.00002376,
  "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	AE1A
Operator	ArkEdge SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Japan
Launch date	Mar 30, 2026HIGHvia 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/68487

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