▸Orbital parameters

Orbit class	LEO
Inclination	34.9942°
Eccentricity	0.0001990
Period	95.8 min
Apogee	560 km
Perigee	557 km
Mean motion	15.02769263 rev/day
RAAN	88.8558°
Arg of perigee	7.8085°
Mean anomaly	352.2654°
B*	1.7065e-4
Rev at epoch	34,349

▸Two-line element set (TLE)

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

1 45461U 20021B 26188.14068087 .00002300 00000-0 17065-3 0 9991

2 45461 34.9942 88.8558 0001990 7.8085 352.2654 15.02769263343493

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-30 07B",
  "OBJECT_ID": "2020-021B",
  "EPOCH": "2026-07-07T03:22:34.827+00:00",
  "MEAN_MOTION": 15.02769263,
  "ECCENTRICITY": 0.000199,
  "INCLINATION": 34.9942,
  "RA_OF_ASC_NODE": 88.8558,
  "ARG_OF_PERICENTER": 7.8085,
  "MEAN_ANOMALY": 352.2654,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 45461,
  "REV_AT_EPOCH": 34349,
  "BSTAR": 0.00017065,
  "MEAN_MOTION_DOT": 0.000023,
  "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-30 07B
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Mar 24, 2020HIGHvia 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/45461

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