▸Orbital parameters

Orbit class	LEO
Inclination	54.9749°
Eccentricity	0.0015733
Period	104.3 min
Apogee	973 km
Perigee	950 km
Mean motion	13.80613774 rev/day
RAAN	221.5499°
Arg of perigee	160.6377°
Mean anomaly	199.5179°
B*	3.5121e-5
Rev at epoch	7,749

▸Two-line element set (TLE)

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

1 62581U 25007G 26188.15390310 -.00000103 00000-0 35121-4 0 9994

2 62581 54.9749 221.5499 0015733 160.6377 199.5179 13.80613774 77491

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CENTISPACE-1 S12",
  "OBJECT_ID": "2025-007G",
  "EPOCH": "2026-07-07T03:41:37.228+00:00",
  "MEAN_MOTION": 13.80613774,
  "ECCENTRICITY": 0.0015733,
  "INCLINATION": 54.9749,
  "RA_OF_ASC_NODE": 221.5499,
  "ARG_OF_PERICENTER": 160.6377,
  "MEAN_ANOMALY": 199.5179,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62581,
  "REV_AT_EPOCH": 7749,
  "BSTAR": 0.000035121,
  "MEAN_MOTION_DOT": -0.00000103,
  "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 S12
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/62581

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