▸Orbital parameters

Orbit class	LEO
Inclination	34.9963°
Eccentricity	0.0004523
Period	95.8 min
Apogee	562 km
Perigee	555 km
Mean motion	15.02774713 rev/day
RAAN	31.4630°
Arg of perigee	252.8686°
Mean anomaly	107.1527°
B*	2.0226e-4
Rev at epoch	27,616

▸Two-line element set (TLE)

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

1 48860U 21055A 26188.00171462 .00002732 00000-0 20226-3 0 9994

2 48860 34.9963 31.4630 0004523 252.8686 107.1527 15.02774713276162

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-30 10A",
  "OBJECT_ID": "2021-055A",
  "EPOCH": "2026-07-07T00:02:28.143+00:00",
  "MEAN_MOTION": 15.02774713,
  "ECCENTRICITY": 0.0004523,
  "INCLINATION": 34.9963,
  "RA_OF_ASC_NODE": 31.463,
  "ARG_OF_PERICENTER": 252.8686,
  "MEAN_ANOMALY": 107.1527,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 48860,
  "REV_AT_EPOCH": 27616,
  "BSTAR": 0.00020226,
  "MEAN_MOTION_DOT": 0.00002732,
  "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 10A
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jun 18, 2021HIGHvia 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/48860

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