▸Orbital parameters

Orbit class	SSO
Inclination	97.3667°
Eccentricity	0.0007899
Period	93.8 min
Apogee	466 km
Perigee	456 km
Mean motion	15.35014547 rev/day
RAAN	265.4854°
Arg of perigee	112.3655°
Mean anomaly	247.8426°
B*	2.3307e-4
Rev at epoch	14,796

▸Two-line element set (TLE)

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

1 58276U 23174W 26187.67886127 .00007844 00000-0 23307-3 0 9995

2 58276 97.3667 265.4854 0007899 112.3655 247.8426 15.35014547147963

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GENMAT-1",
  "OBJECT_ID": "2023-174W",
  "EPOCH": "2026-07-06T16:17:33.614+00:00",
  "MEAN_MOTION": 15.35014547,
  "ECCENTRICITY": 0.0007899,
  "INCLINATION": 97.3667,
  "RA_OF_ASC_NODE": 265.4854,
  "ARG_OF_PERICENTER": 112.3655,
  "MEAN_ANOMALY": 247.8426,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58276,
  "REV_AT_EPOCH": 14796,
  "BSTAR": 0.00023307,
  "MEAN_MOTION_DOT": 0.00007844,
  "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	GENMAT-1
Operator	Quantum Generative Materials LLCHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Nov 11, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	8.8HIGHvia 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/58276

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