▸Orbital parameters

Orbit class	LEO
Inclination	63.3517°
Eccentricity	0.0437046
Period	107.0 min
Apogee	1,415 km
Perigee	763 km
Mean motion	13.45517380 rev/day
RAAN	238.3778°
Arg of perigee	27.2785°
Mean anomaly	335.0477°
B*	2.8493e-5
Rev at epoch	66,882

▸Two-line element set (TLE)

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

1 39011U 12066A 26188.09783909 -.00000061 00000-0 28493-4 0 9997

2 39011 63.3517 238.3778 0437046 27.2785 335.0477 13.45517380668820

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-16 01A",
  "OBJECT_ID": "2012-066A",
  "EPOCH": "2026-07-07T02:20:53.297+00:00",
  "MEAN_MOTION": 13.4551738,
  "ECCENTRICITY": 0.0437046,
  "INCLINATION": 63.3517,
  "RA_OF_ASC_NODE": 238.3778,
  "ARG_OF_PERICENTER": 27.2785,
  "MEAN_ANOMALY": 335.0477,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39011,
  "REV_AT_EPOCH": 66882,
  "BSTAR": 0.000028493,
  "MEAN_MOTION_DOT": -6.1e-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-16 01A
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Nov 25, 2012HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	500HIGHvia 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/39011

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