▸Orbital parameters

Orbit class	GEO
Inclination	15.0918°
Eccentricity	0.0001647
Period	1436.2 min
Apogee	35,795 km
Perigee	35,782 km
Mean motion	1.00265129 rev/day
RAAN	193.4829°
Arg of perigee	25.1906°
Mean anomaly	162.9772°
B*	0.0000e+0
Rev at epoch	1,074

▸Two-line element set (TLE)

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

1 57624U 23120A 26188.02012639 -.00000154 00000-0 00000-0 0 9991

2 57624 15.0918 193.4829 0001647 25.1906 162.9772 1.00265129 10749

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LUDI TANCE-4 01A",
  "OBJECT_ID": "2023-120A",
  "EPOCH": "2026-07-07T00:28:58.92+00:00",
  "MEAN_MOTION": 1.00265129,
  "ECCENTRICITY": 0.0001647,
  "INCLINATION": 15.0918,
  "RA_OF_ASC_NODE": 193.4829,
  "ARG_OF_PERICENTER": 25.1906,
  "MEAN_ANOMALY": 162.9772,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 57624,
  "REV_AT_EPOCH": 1074,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000154,
  "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	LUDI TANCE-4 01A
Operator	China National Space AdministrationHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	People's Republic of ChinaMEDIUMvia Wikidata
Launch date	Aug 12, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3060HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/57624

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