▸Orbital parameters

Orbit class	SSO
Inclination	97.8042°
Eccentricity	0.0002536
Period	96.9 min
Apogee	611 km
Perigee	608 km
Mean motion	14.86276407 rev/day
RAAN	186.2449°
Arg of perigee	120.8969°
Mean anomaly	239.2496°
B*	7.8046e-5
Rev at epoch	2,623

▸Two-line element set (TLE)

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

1 67375U 26004N 26187.97362861 .00000633 00000-0 78046-4 0 9997

2 67375 97.8042 186.2449 0002536 120.8969 239.2496 14.86276407 26238

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AETHER-4",
  "OBJECT_ID": "2026-004N",
  "EPOCH": "2026-07-06T23:22:01.512+00:00",
  "MEAN_MOTION": 14.86276407,
  "ECCENTRICITY": 0.0002536,
  "INCLINATION": 97.8042,
  "RA_OF_ASC_NODE": 186.2449,
  "ARG_OF_PERICENTER": 120.8969,
  "MEAN_ANOMALY": 239.2496,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67375,
  "REV_AT_EPOCH": 2623,
  "BSTAR": 0.000078046,
  "MEAN_MOTION_DOT": 0.00000633,
  "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-4
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/67375

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