▸Orbital parameters

Orbit class	LEO
Inclination	54.9860°
Eccentricity	0.0013329
Period	104.3 min
Apogee	972 km
Perigee	952 km
Mean motion	13.80617635 rev/day
RAAN	221.6783°
Arg of perigee	123.4155°
Mean anomaly	236.8078°
B*	1.7137e-4
Rev at epoch	7,746

▸Two-line element set (TLE)

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

1 62585U 25007L 26188.09585785 .00000040 00000-0 17137-3 0 9998

2 62585 54.9860 221.6783 0013329 123.4155 236.8078 13.80617635 77466

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CENTISPACE-1 S16",
  "OBJECT_ID": "2025-007L",
  "EPOCH": "2026-07-07T02:18:02.118+00:00",
  "MEAN_MOTION": 13.80617635,
  "ECCENTRICITY": 0.0013329,
  "INCLINATION": 54.986,
  "RA_OF_ASC_NODE": 221.6783,
  "ARG_OF_PERICENTER": 123.4155,
  "MEAN_ANOMALY": 236.8078,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62585,
  "REV_AT_EPOCH": 7746,
  "BSTAR": 0.00017137,
  "MEAN_MOTION_DOT": 4e-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 S16
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/62585

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