▸Orbital parameters

Orbit class	SSO
Inclination	97.8010°
Eccentricity	0.0002835
Period	96.9 min
Apogee	611 km
Perigee	608 km
Mean motion	14.86313276 rev/day
RAAN	186.0832°
Arg of perigee	117.5684°
Mean anomaly	242.5820°
B*	7.9039e-5
Rev at epoch	2,621

▸Two-line element set (TLE)

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

1 67380U 26004T 26187.92652965 .00000643 00000-0 79039-4 0 9999

2 67380 97.8010 186.0832 0002835 117.5684 242.5820 14.86313276 26214

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AETHER-9",
  "OBJECT_ID": "2026-004T",
  "EPOCH": "2026-07-06T22:14:12.162+00:00",
  "MEAN_MOTION": 14.86313276,
  "ECCENTRICITY": 0.0002835,
  "INCLINATION": 97.801,
  "RA_OF_ASC_NODE": 186.0832,
  "ARG_OF_PERICENTER": 117.5684,
  "MEAN_ANOMALY": 242.582,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67380,
  "REV_AT_EPOCH": 2621,
  "BSTAR": 0.000079039,
  "MEAN_MOTION_DOT": 0.00000643,
  "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-9
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/67380

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