▸Orbital parameters

Orbit class	LEO
Inclination	54.9830°
Eccentricity	0.0014758
Period	104.3 min
Apogee	973 km
Perigee	951 km
Mean motion	13.80617744 rev/day
RAAN	221.8307°
Arg of perigee	154.9432°
Mean anomaly	205.2244°
B*	4.1574e-5
Rev at epoch	7,748

▸Two-line element set (TLE)

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

1 62577U 25007C 26188.13235308 -.00000097 00000-0 41574-4 0 9993

2 62577 54.9830 221.8307 0014758 154.9432 205.2244 13.80617744 77480

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CENTISPACE-1 S8",
  "OBJECT_ID": "2025-007C",
  "EPOCH": "2026-07-07T03:10:35.306+00:00",
  "MEAN_MOTION": 13.80617744,
  "ECCENTRICITY": 0.0014758,
  "INCLINATION": 54.983,
  "RA_OF_ASC_NODE": 221.8307,
  "ARG_OF_PERICENTER": 154.9432,
  "MEAN_ANOMALY": 205.2244,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62577,
  "REV_AT_EPOCH": 7748,
  "BSTAR": 0.000041574,
  "MEAN_MOTION_DOT": -9.7e-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 S8
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/62577

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