▸Orbital parameters

Orbit class	SSO
Inclination	97.8018°
Eccentricity	0.0003455
Period	96.9 min
Apogee	612 km
Perigee	607 km
Mean motion	14.86309168 rev/day
RAAN	186.0919°
Arg of perigee	101.7190°
Mean anomaly	258.4413°
B*	7.1871e-5
Rev at epoch	2,621

▸Two-line element set (TLE)

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

1 67379U 26004S 26187.93334434 .00000579 00000-0 71871-4 0 9990

2 67379 97.8018 186.0919 0003455 101.7190 258.4413 14.86309168 26211

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AETHER-8",
  "OBJECT_ID": "2026-004S",
  "EPOCH": "2026-07-06T22:24:00.951+00:00",
  "MEAN_MOTION": 14.86309168,
  "ECCENTRICITY": 0.0003455,
  "INCLINATION": 97.8018,
  "RA_OF_ASC_NODE": 186.0919,
  "ARG_OF_PERICENTER": 101.719,
  "MEAN_ANOMALY": 258.4413,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67379,
  "REV_AT_EPOCH": 2621,
  "BSTAR": 0.000071871,
  "MEAN_MOTION_DOT": 0.00000579,
  "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-8
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/67379

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