▸Orbital parameters

Orbit class	LEO
Inclination	43.0025°
Eccentricity	0.0237890
Period	97.0 min
Apogee	782 km
Perigee	449 km
Mean motion	14.84424511 rev/day
RAAN	301.1771°
Arg of perigee	0.9505°
Mean anomaly	359.1741°
B*	1.6138e-4
Rev at epoch	6,835

▸Two-line element set (TLE)

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

1 63432U 25068A 26188.19407816 .00002045 00000-0 16138-3 0 9993

2 63432 43.0025 301.1771 0237890 0.9505 359.1741 14.84424511 68358

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANPING-3A 02",
  "OBJECT_ID": "2025-068A",
  "EPOCH": "2026-07-07T04:39:28.353+00:00",
  "MEAN_MOTION": 14.84424511,
  "ECCENTRICITY": 0.023789,
  "INCLINATION": 43.0025,
  "RA_OF_ASC_NODE": 301.1771,
  "ARG_OF_PERICENTER": 0.9505,
  "MEAN_ANOMALY": 359.1741,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63432,
  "REV_AT_EPOCH": 6835,
  "BSTAR": 0.00016138,
  "MEAN_MOTION_DOT": 0.00002045,
  "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	TIANPING-3A 02
Operator	ZJUNI-SATHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Apr 3, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	200HIGHvia 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/63432

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