▸Orbital parameters

Orbit class	LEO
Inclination	50.0103°
Eccentricity	0.0005237
Period	100.8 min
Apogee	802 km
Perigee	795 km
Mean motion	14.27996843 rev/day
RAAN	118.2855°
Arg of perigee	253.0302°
Mean anomaly	107.0039°
B*	3.8795e-5
Rev at epoch	12,201

▸Two-line element set (TLE)

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

1 59285U 24052F 26188.16636833 -.00000064 00000-0 38795-4 0 9990

2 59285 50.0103 118.2855 0005237 253.0302 107.0039 14.27996843122011

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YUNHAI-2 02F",
  "OBJECT_ID": "2024-052F",
  "EPOCH": "2026-07-07T03:59:34.224+00:00",
  "MEAN_MOTION": 14.27996843,
  "ECCENTRICITY": 0.0005237,
  "INCLINATION": 50.0103,
  "RA_OF_ASC_NODE": 118.2855,
  "ARG_OF_PERICENTER": 253.0302,
  "MEAN_ANOMALY": 107.0039,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59285,
  "REV_AT_EPOCH": 12201,
  "BSTAR": 0.000038795,
  "MEAN_MOTION_DOT": -6.4e-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 02F
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/59285

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