▸Orbital parameters

Orbit class	SSO
Inclination	97.8045°
Eccentricity	0.0003062
Period	96.9 min
Apogee	612 km
Perigee	607 km
Mean motion	14.86298427 rev/day
RAAN	186.2630°
Arg of perigee	96.0303°
Mean anomaly	264.1261°
B*	7.3789e-5
Rev at epoch	2,622

▸Two-line element set (TLE)

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

1 67381U 26004U 26187.96706117 .00000596 00000-0 73789-4 0 9996

2 67381 97.8045 186.2630 0003062 96.0303 264.1261 14.86298427 26223

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AETHER-10",
  "OBJECT_ID": "2026-004U",
  "EPOCH": "2026-07-06T23:12:34.085+00:00",
  "MEAN_MOTION": 14.86298427,
  "ECCENTRICITY": 0.0003062,
  "INCLINATION": 97.8045,
  "RA_OF_ASC_NODE": 186.263,
  "ARG_OF_PERICENTER": 96.0303,
  "MEAN_ANOMALY": 264.1261,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67381,
  "REV_AT_EPOCH": 2622,
  "BSTAR": 0.000073789,
  "MEAN_MOTION_DOT": 0.00000596,
  "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	AETHER-10
Operator	Kepler Communications Inc.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Canada
Launch date	Jan 11, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	300HIGHvia 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/67381

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