▸Orbital parameters

Orbit class	SSO
Inclination	97.3894°
Eccentricity	0.0008502
Period	93.8 min
Apogee	467 km
Perigee	456 km
Mean motion	15.34801404 rev/day
RAAN	271.3218°
Arg of perigee	83.2102°
Mean anomaly	277.0108°
B*	1.3968e-4
Rev at epoch	14,827

▸Two-line element set (TLE)

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

1 58299U 23174AV 26188.02027970 .00004636 00000-0 13968-3 0 9991

2 58299 97.3894 271.3218 0008502 83.2102 277.0108 15.34801404148277

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AETHER-2",
  "OBJECT_ID": "2023-174AV",
  "EPOCH": "2026-07-07T00:29:12.166+00:00",
  "MEAN_MOTION": 15.34801404,
  "ECCENTRICITY": 0.0008502,
  "INCLINATION": 97.3894,
  "RA_OF_ASC_NODE": 271.3218,
  "ARG_OF_PERICENTER": 83.2102,
  "MEAN_ANOMALY": 277.0108,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58299,
  "REV_AT_EPOCH": 14827,
  "BSTAR": 0.00013968,
  "MEAN_MOTION_DOT": 0.00004636,
  "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-2
Operator	Kepler Communications Inc.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Canada
Launch date	Nov 11, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	125HIGHvia 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/58299

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