▸Orbital parameters

Orbit class	MEO
Inclination	19.9386°
Eccentricity	0.0008007
Period	271.1 min
Apogee	7,508 km
Perigee	7,486 km
Mean motion	5.31206174 rev/day
RAAN	205.9528°
Arg of perigee	261.3386°
Mean anomaly	98.5963°
B*	0.0000e+0
Rev at epoch	1,310

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 65563U 25202A 26187.25429625 .00000008 00000-0 00000-0 0 9993

2 65563 19.9386 205.9528 0008007 261.3386 98.5963 5.31206174 13102

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-45",
  "OBJECT_ID": "2025-202A",
  "EPOCH": "2026-07-06T06:06:11.196+00:00",
  "MEAN_MOTION": 5.31206174,
  "ECCENTRICITY": 0.00080069,
  "INCLINATION": 19.9386,
  "RA_OF_ASC_NODE": 205.9528,
  "ARG_OF_PERICENTER": 261.3386,
  "MEAN_ANOMALY": 98.5963,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65563,
  "REV_AT_EPOCH": 1310,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 8e-8,
  "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-45
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 9, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5000HIGHvia 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/65563

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