▸Orbital parameters

Orbit class	LEO
Inclination	50.0081°
Eccentricity	0.0005216
Period	100.8 min
Apogee	799 km
Perigee	791 km
Mean motion	14.29018638 rev/day
RAAN	81.6937°
Arg of perigee	73.6084°
Mean anomaly	286.5405°
B*	6.9886e-5
Rev at epoch	39,202

▸Two-line element set (TLE)

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

1 43913U 18112E 26188.22170560 .00000016 00000-0 69886-4 0 9999

2 43913 50.0081 81.6937 0005216 73.6084 286.5405 14.29018638392020

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YUNHAI-2 01E",
  "OBJECT_ID": "2018-112E",
  "EPOCH": "2026-07-07T05:19:15.364+00:00",
  "MEAN_MOTION": 14.29018638,
  "ECCENTRICITY": 0.0005216,
  "INCLINATION": 50.0081,
  "RA_OF_ASC_NODE": 81.6937,
  "ARG_OF_PERICENTER": 73.6084,
  "MEAN_ANOMALY": 286.5405,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43913,
  "REV_AT_EPOCH": 39202,
  "BSTAR": 0.000069886,
  "MEAN_MOTION_DOT": 1.6e-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 01E
Operator	China Aerospace CorpHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Dec 29, 2018HIGHvia 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/43913

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