▸Orbital parameters

Orbit class	LEO
Inclination	49.9428°
Eccentricity	0.0006436
Period	95.1 min
Apogee	526 km
Perigee	517 km
Mean motion	15.14752663 rev/day
RAAN	64.8386°
Arg of perigee	68.3325°
Mean anomaly	291.8310°
B*	1.3317e-4
Rev at epoch	8,920

▸Two-line element set (TLE)

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

1 62112U 24221B 26188.16194619 .00002200 00000-0 13317-3 0 9997

2 62112 49.9428 64.8386 0006436 68.3325 291.8310 15.14752663 89204

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GUANGCHUAN 02",
  "OBJECT_ID": "2024-221B",
  "EPOCH": "2026-07-07T03:53:12.151+00:00",
  "MEAN_MOTION": 15.14752663,
  "ECCENTRICITY": 0.0006436,
  "INCLINATION": 49.9428,
  "RA_OF_ASC_NODE": 64.8386,
  "ARG_OF_PERICENTER": 68.3325,
  "MEAN_ANOMALY": 291.831,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62112,
  "REV_AT_EPOCH": 8920,
  "BSTAR": 0.00013317,
  "MEAN_MOTION_DOT": 0.000022,
  "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	GUANGCHUAN 02
Operator	HONGQ?HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Nov 27, 2024HIGHvia 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/62112

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