▸Orbital parameters

Orbit class	SSO
Inclination	97.8721°
Eccentricity	0.0009871
Period	98.6 min
Apogee	700 km
Perigee	686 km
Mean motion	14.60015090 rev/day
RAAN	210.8906°
Arg of perigee	63.2172°
Mean anomaly	297.0037°
B*	1.1134e-4
Rev at epoch	41,346

▸Two-line element set (TLE)

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

1 43636U 18075A 26188.12075697 .00000491 00000-0 11134-3 0 9992

2 43636 97.8721 210.8906 0009871 63.2172 297.0037 14.60015090413462

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CENTISPACE-1 S1",
  "OBJECT_ID": "2018-075A",
  "EPOCH": "2026-07-07T02:53:53.402+00:00",
  "MEAN_MOTION": 14.6001509,
  "ECCENTRICITY": 0.0009871,
  "INCLINATION": 97.8721,
  "RA_OF_ASC_NODE": 210.8906,
  "ARG_OF_PERICENTER": 63.2172,
  "MEAN_ANOMALY": 297.0037,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43636,
  "REV_AT_EPOCH": 41346,
  "BSTAR": 0.00011134,
  "MEAN_MOTION_DOT": 0.00000491,
  "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 S1
Operator	Beijing Future Navigation Technology Co. Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 29, 2018HIGHvia 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/43636

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