▸Orbital parameters

Orbit class	SSO
Inclination	97.5035°
Eccentricity	0.0002329
Period	95.1 min
Apogee	525 km
Perigee	522 km
Mean motion	15.14291676 rev/day
RAAN	14.1809°
Arg of perigee	71.6435°
Mean anomaly	288.5050°
B*	2.1107e-4
Rev at epoch	18,069

▸Two-line element set (TLE)

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

1 56153U 23047A 26187.31784646 .00003797 00000-0 21107-3 0 9999

2 56153 97.5035 14.1809 0002329 71.6435 288.5050 15.14291676180690

▸ source OMM (JSON)

{
  "OBJECT_NAME": "PIESAT A",
  "OBJECT_ID": "2023-047A",
  "EPOCH": "2026-07-06T07:37:41.934+00:00",
  "MEAN_MOTION": 15.14291676,
  "ECCENTRICITY": 0.0002329,
  "INCLINATION": 97.5035,
  "RA_OF_ASC_NODE": 14.1809,
  "ARG_OF_PERICENTER": 71.6435,
  "MEAN_ANOMALY": 288.505,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 56153,
  "REV_AT_EPOCH": 18069,
  "BSTAR": 0.00021107,
  "MEAN_MOTION_DOT": 0.00003797,
  "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	PIESAT A
Operator	PIESAT Information Technology Co. Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Mar 30, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	320HIGHvia 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/56153

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