▸Orbital parameters

Orbit class	SSO
Inclination	98.0019°
Eccentricity	0.0001374
Period	97.1 min
Apogee	621 km
Perigee	619 km
Mean motion	14.83101057 rev/day
RAAN	216.8793°
Arg of perigee	21.9128°
Mean anomaly	338.2144°
B*	1.0560e-5
Rev at epoch	57,359

▸Two-line element set (TLE)

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

1 41038U 15069A 26188.21572397 .00000032 00000-0 10560-4 0 9999

2 41038 98.0019 216.8793 0001374 21.9128 338.2144 14.83101057573593

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-29",
  "OBJECT_ID": "2015-069A",
  "EPOCH": "2026-07-07T05:10:38.551+00:00",
  "MEAN_MOTION": 14.83101057,
  "ECCENTRICITY": 0.0001374,
  "INCLINATION": 98.0019,
  "RA_OF_ASC_NODE": 216.8793,
  "ARG_OF_PERICENTER": 21.9128,
  "MEAN_ANOMALY": 338.2144,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41038,
  "REV_AT_EPOCH": 57359,
  "BSTAR": 0.00001056,
  "MEAN_MOTION_DOT": 3.2e-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	YAOGAN-29
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Nov 26, 2015HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1040HIGHvia 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/41038

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