▸Orbital parameters

Orbit class	LEO
Inclination	54.9985°
Eccentricity	0.0016458
Period	98.5 min
Apogee	697 km
Perigee	674 km
Mean motion	14.62308068 rev/day
RAAN	134.9371°
Arg of perigee	110.2373°
Mean anomaly	250.0392°
B*	1.3072e-4
Rev at epoch	19,992

▸Two-line element set (TLE)

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

1 54021U 22126B 26188.17358186 .00000476 00000-0 13072-3 0 9992

2 54021 54.9985 134.9371 0016458 110.2373 250.0392 14.62308068199922

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CENTISPACE-1 S6",
  "OBJECT_ID": "2022-126B",
  "EPOCH": "2026-07-07T04:09:57.473+00:00",
  "MEAN_MOTION": 14.62308068,
  "ECCENTRICITY": 0.0016458,
  "INCLINATION": 54.9985,
  "RA_OF_ASC_NODE": 134.9371,
  "ARG_OF_PERICENTER": 110.2373,
  "MEAN_ANOMALY": 250.0392,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54021,
  "REV_AT_EPOCH": 19992,
  "BSTAR": 0.00013072,
  "MEAN_MOTION_DOT": 0.00000476,
  "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 S6
Operator	Beijing Future Navigation Technology Co. Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Oct 7, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	97HIGHvia 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/54021

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