▸Orbital parameters

Orbit class	SSO
Inclination	97.3099°
Eccentricity	0.0011953
Period	94.3 min
Apogee	491 km
Perigee	475 km
Mean motion	15.27688765 rev/day
RAAN	326.0317°
Arg of perigee	117.8731°
Mean anomaly	242.3721°
B*	1.9524e-4
Rev at epoch	59,373

▸Two-line element set (TLE)

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

1 41026U 15064A 26188.17130587 .00005220 00000-0 19524-3 0 9999

2 41026 97.3099 326.0317 0011953 117.8731 242.3721 15.27688765593734

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-28",
  "OBJECT_ID": "2015-064A",
  "EPOCH": "2026-07-07T04:06:40.827+00:00",
  "MEAN_MOTION": 15.27688765,
  "ECCENTRICITY": 0.0011953,
  "INCLINATION": 97.3099,
  "RA_OF_ASC_NODE": 326.0317,
  "ARG_OF_PERICENTER": 117.8731,
  "MEAN_ANOMALY": 242.3721,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41026,
  "REV_AT_EPOCH": 59373,
  "BSTAR": 0.00019524,
  "MEAN_MOTION_DOT": 0.0000522,
  "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-28
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Nov 8, 2015HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3000HIGHvia 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/41026

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