▸Orbital parameters

Orbit class	SSO
Inclination	97.8006°
Eccentricity	0.0005468
Period	96.8 min
Apogee	608 km
Perigee	600 km
Mean motion	14.88043691 rev/day
RAAN	186.2235°
Arg of perigee	73.1606°
Mean anomaly	287.0210°
B*	7.8356e-5
Rev at epoch	2,623

▸Two-line element set (TLE)

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

1 67374U 26004M 26187.92994536 .00000666 00000-0 78356-4 0 9991

2 67374 97.8006 186.2235 0005468 73.1606 287.0210 14.88043691 26239

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AETHER-3",
  "OBJECT_ID": "2026-004M",
  "EPOCH": "2026-07-06T22:19:07.279+00:00",
  "MEAN_MOTION": 14.88043691,
  "ECCENTRICITY": 0.0005468,
  "INCLINATION": 97.8006,
  "RA_OF_ASC_NODE": 186.2235,
  "ARG_OF_PERICENTER": 73.1606,
  "MEAN_ANOMALY": 287.021,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67374,
  "REV_AT_EPOCH": 2623,
  "BSTAR": 0.000078356,
  "MEAN_MOTION_DOT": 0.00000666,
  "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-3
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/67374

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