▸Orbital parameters

Orbit class	LEO
Inclination	54.9787°
Eccentricity	0.0012446
Period	104.3 min
Apogee	971 km
Perigee	953 km
Mean motion	13.80617222 rev/day
RAAN	221.7179°
Arg of perigee	120.2819°
Mean anomaly	239.9370°
B*	4.2102e-5
Rev at epoch	7,748

▸Two-line element set (TLE)

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

1 62582U 25007H 26188.13955193 -.00000096 00000-0 42102-4 0 9997

2 62582 54.9787 221.7179 0012446 120.2819 239.9370 13.80617222 77485

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CENTISPACE-1 S13",
  "OBJECT_ID": "2025-007H",
  "EPOCH": "2026-07-07T03:20:57.287+00:00",
  "MEAN_MOTION": 13.80617222,
  "ECCENTRICITY": 0.0012446,
  "INCLINATION": 54.9787,
  "RA_OF_ASC_NODE": 221.7179,
  "ARG_OF_PERICENTER": 120.2819,
  "MEAN_ANOMALY": 239.937,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62582,
  "REV_AT_EPOCH": 7748,
  "BSTAR": 0.000042102,
  "MEAN_MOTION_DOT": -9.6e-7,
  "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	CENTISPACE-1 S13
Operator	Beijing Future Navigation Technology Co. Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jan 13, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	140HIGHvia 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/62582

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