▸Orbital parameters

Orbit class	LEO
Inclination	28.9966°
Eccentricity	0.0004035
Period	97.0 min
Apogee	617 km
Perigee	611 km
Mean motion	14.84966423 rev/day
RAAN	346.6750°
Arg of perigee	266.5721°
Mean anomaly	93.4411°
B*	1.8000e-4
Rev at epoch	11,058

▸Two-line element set (TLE)

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

1 60088U 24116A 26187.82235594 .00001696 00000-0 18000-3 0 9992

2 60088 28.9966 346.6750 0004035 266.5721 93.4411 14.84966423110580

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CATCH-1",
  "OBJECT_ID": "2024-116A",
  "EPOCH": "2026-07-06T19:44:11.553+00:00",
  "MEAN_MOTION": 14.84966423,
  "ECCENTRICITY": 0.0004035,
  "INCLINATION": 28.9966,
  "RA_OF_ASC_NODE": 346.675,
  "ARG_OF_PERICENTER": 266.5721,
  "MEAN_ANOMALY": 93.4411,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60088,
  "REV_AT_EPOCH": 11058,
  "BSTAR": 0.00018,
  "MEAN_MOTION_DOT": 0.00001696,
  "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	CATCH-1
Operator	China Aerospace Corp / National Space Research CenterHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree National Space Science CenterMEDIUMvia Wikidata
Country	FranceMEDIUMvia Wikidata
Launch date	Jun 22, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	930

▸Data quality

Score90 / 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/60088

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