▸Orbital parameters

Orbit class	SSO
Inclination	97.8041°
Eccentricity	0.0004750
Period	96.9 min
Apogee	613 km
Perigee	606 km
Mean motion	14.86300019 rev/day
RAAN	186.1293°
Arg of perigee	77.6733°
Mean anomaly	282.5014°
B*	7.2915e-5
Rev at epoch	2,622

▸Two-line element set (TLE)

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

1 67376U 26004P 26187.94020419 .00000588 00000-0 72915-4 0 9993

2 67376 97.8041 186.1293 0004750 77.6733 282.5014 14.86300019 26225

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AETHER-5",
  "OBJECT_ID": "2026-004P",
  "EPOCH": "2026-07-06T22:33:53.642+00:00",
  "MEAN_MOTION": 14.86300019,
  "ECCENTRICITY": 0.000475,
  "INCLINATION": 97.8041,
  "RA_OF_ASC_NODE": 186.1293,
  "ARG_OF_PERICENTER": 77.6733,
  "MEAN_ANOMALY": 282.5014,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67376,
  "REV_AT_EPOCH": 2622,
  "BSTAR": 0.000072915,
  "MEAN_MOTION_DOT": 0.00000588,
  "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-5
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/67376

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