▸Orbital parameters

Orbit class	LEO
Inclination	34.9926°
Eccentricity	0.0001374
Period	94.5 min
Apogee	497 km
Perigee	495 km
Mean motion	15.23139100 rev/day
RAAN	74.2440°
Arg of perigee	253.7209°
Mean anomaly	106.3354°
B*	2.3746e-4
Rev at epoch	10,244

▸Two-line element set (TLE)

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

1 60950U 24156F 26187.84463534 .00005711 00000-0 23746-3 0 9998

2 60950 34.9926 74.2440 0001374 253.7209 106.3354 15.23139100102447

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-43 02F",
  "OBJECT_ID": "2024-156F",
  "EPOCH": "2026-07-06T20:16:16.493+00:00",
  "MEAN_MOTION": 15.231391,
  "ECCENTRICITY": 0.0001374,
  "INCLINATION": 34.9926,
  "RA_OF_ASC_NODE": 74.244,
  "ARG_OF_PERICENTER": 253.7209,
  "MEAN_ANOMALY": 106.3354,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60950,
  "REV_AT_EPOCH": 10244,
  "BSTAR": 0.00023746,
  "MEAN_MOTION_DOT": 0.00005711,
  "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-43 02F
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 3, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	300HIGHvia 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/60950

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