▸Orbital parameters

Orbit class	LEO
Inclination	50.0092°
Eccentricity	0.0011706
Period	100.8 min
Apogee	807 km
Perigee	790 km
Mean motion	14.27971184 rev/day
RAAN	238.2309°
Arg of perigee	129.6914°
Mean anomaly	230.5034°
B*	2.6681e-5
Rev at epoch	10,978

▸Two-line element set (TLE)

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

1 59284U 24052E 26188.14187132 -.00000095 00000-0 26681-4 0 9995

2 59284 50.0092 238.2309 0011706 129.6914 230.5034 14.27971184109786

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YUNHAI-2 02E",
  "OBJECT_ID": "2024-052E",
  "EPOCH": "2026-07-07T03:24:17.682+00:00",
  "MEAN_MOTION": 14.27971184,
  "ECCENTRICITY": 0.0011706,
  "INCLINATION": 50.0092,
  "RA_OF_ASC_NODE": 238.2309,
  "ARG_OF_PERICENTER": 129.6914,
  "MEAN_ANOMALY": 230.5034,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59284,
  "REV_AT_EPOCH": 10978,
  "BSTAR": 0.000026681,
  "MEAN_MOTION_DOT": -9.5e-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 02E
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/59284

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