▸Orbital parameters

Orbit class	LEO
Inclination	54.9869°
Eccentricity	0.0012490
Period	104.3 min
Apogee	971 km
Perigee	953 km
Mean motion	13.80614888 rev/day
RAAN	221.5602°
Arg of perigee	128.5540°
Mean anomaly	231.6537°
B*	4.8881e-5
Rev at epoch	7,749

▸Two-line element set (TLE)

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

1 62579U 25007E 26188.18295064 -.00000089 00000-0 48881-4 0 9994

2 62579 54.9869 221.5602 0012490 128.5540 231.6537 13.80614888 77492

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CENTISPACE-1 S10",
  "OBJECT_ID": "2025-007E",
  "EPOCH": "2026-07-07T04:23:26.935+00:00",
  "MEAN_MOTION": 13.80614888,
  "ECCENTRICITY": 0.001249,
  "INCLINATION": 54.9869,
  "RA_OF_ASC_NODE": 221.5602,
  "ARG_OF_PERICENTER": 128.554,
  "MEAN_ANOMALY": 231.6537,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62579,
  "REV_AT_EPOCH": 7749,
  "BSTAR": 0.000048881,
  "MEAN_MOTION_DOT": -8.9e-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 S10
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/62579

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