▸Orbital parameters

Orbit class	LEO
Inclination	54.9845°
Eccentricity	0.0014807
Period	104.3 min
Apogee	973 km
Perigee	951 km
Mean motion	13.80618201 rev/day
RAAN	222.6797°
Arg of perigee	112.0085°
Mean anomaly	248.2446°
B*	1.7441e-4
Rev at epoch	7,749

▸Two-line element set (TLE)

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

1 62584U 25007K 26188.17538875 .00000043 00000-0 17441-3 0 9995

2 62584 54.9845 222.6797 0014807 112.0085 248.2446 13.80618201 77491

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CENTISPACE-1 S15",
  "OBJECT_ID": "2025-007K",
  "EPOCH": "2026-07-07T04:12:33.588+00:00",
  "MEAN_MOTION": 13.80618201,
  "ECCENTRICITY": 0.0014807,
  "INCLINATION": 54.9845,
  "RA_OF_ASC_NODE": 222.6797,
  "ARG_OF_PERICENTER": 112.0085,
  "MEAN_ANOMALY": 248.2446,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62584,
  "REV_AT_EPOCH": 7749,
  "BSTAR": 0.00017441,
  "MEAN_MOTION_DOT": 4.3e-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 S15
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/62584

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