▸Orbital parameters

Orbit class	LEO
Inclination	50.0098°
Eccentricity	0.0011615
Period	100.8 min
Apogee	807 km
Perigee	790 km
Mean motion	14.27967267 rev/day
RAAN	358.2401°
Arg of perigee	214.9480°
Mean anomaly	145.0673°
B*	3.6681e-5
Rev at epoch	10,107

▸Two-line element set (TLE)

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

1 59280U 24052A 26188.11910671 -.00000070 00000-0 36681-4 0 9994

2 59280 50.0098 358.2401 0011615 214.9480 145.0673 14.27967267101079

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YUNHAI-2 02A",
  "OBJECT_ID": "2024-052A",
  "EPOCH": "2026-07-07T02:51:30.82+00:00",
  "MEAN_MOTION": 14.27967267,
  "ECCENTRICITY": 0.0011615,
  "INCLINATION": 50.0098,
  "RA_OF_ASC_NODE": 358.2401,
  "ARG_OF_PERICENTER": 214.948,
  "MEAN_ANOMALY": 145.0673,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59280,
  "REV_AT_EPOCH": 10107,
  "BSTAR": 0.000036681,
  "MEAN_MOTION_DOT": -7e-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 02A
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/59280

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