▸Orbital parameters

Orbit class	LEO
Inclination	50.0093°
Eccentricity	0.0006255
Period	100.8 min
Apogee	803 km
Perigee	794 km
Mean motion	14.27970443 rev/day
RAAN	57.5767°
Arg of perigee	232.8510°
Mean anomaly	127.1834°
B*	2.7365e-5
Rev at epoch	11,766

▸Two-line element set (TLE)

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

1 59282U 24052C 26188.21055476 -.00000093 00000-0 27365-4 0 9994

2 59282 50.0093 57.5767 0006255 232.8510 127.1834 14.27970443117669

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YUNHAI-2 02C",
  "OBJECT_ID": "2024-052C",
  "EPOCH": "2026-07-07T05:03:11.931+00:00",
  "MEAN_MOTION": 14.27970443,
  "ECCENTRICITY": 0.0006255,
  "INCLINATION": 50.0093,
  "RA_OF_ASC_NODE": 57.5767,
  "ARG_OF_PERICENTER": 232.851,
  "MEAN_ANOMALY": 127.1834,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59282,
  "REV_AT_EPOCH": 11766,
  "BSTAR": 0.000027365,
  "MEAN_MOTION_DOT": -9.3e-7,
  "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	YUNHAI-2 02C
Operator	China Aerospace CorpHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Mar 21, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	100HIGHvia 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/59282

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