▸Orbital parameters

Orbit class	SSO
Inclination	97.6832°
Eccentricity	0.0014178
Period	95.7 min
Apogee	560 km
Perigee	540 km
Mean motion	15.05479092 rev/day
RAAN	189.5678°
Arg of perigee	127.0666°
Mean anomaly	233.1859°
B*	1.3249e-4
Rev at epoch	20,075

▸Two-line element set (TLE)

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

1 54227U 22147A 26188.05603105 .00001845 00000-0 13249-3 0 9991

2 54227 97.6832 189.5678 0014178 127.0666 233.1859 15.05479092200757

▸ source OMM (JSON)

{
  "OBJECT_NAME": "MATS",
  "OBJECT_ID": "2022-147A",
  "EPOCH": "2026-07-07T01:20:41.083+00:00",
  "MEAN_MOTION": 15.05479092,
  "ECCENTRICITY": 0.0014178,
  "INCLINATION": 97.6832,
  "RA_OF_ASC_NODE": 189.5678,
  "ARG_OF_PERICENTER": 127.0666,
  "MEAN_ANOMALY": 233.1859,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54227,
  "REV_AT_EPOCH": 20075,
  "BSTAR": 0.00013249,
  "MEAN_MOTION_DOT": 0.00001845,
  "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	MATS
Operator	Swedish National Space BoardHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree OHB SwedenMEDIUMvia Wikidata
Country	Sweden
Launch date	Nov 4, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	54HIGHvia GCAT — Jonathan McDowell's General Catalog⚠

▸Data quality

Score95 / 100

Claims10

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/54227

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