▸Orbital parameters

Orbit class	SSO
Inclination	97.7047°
Eccentricity	0.0003093
Period	96.1 min
Apogee	576 km
Perigee	571 km
Mean motion	14.97900702 rev/day
RAAN	267.5834°
Arg of perigee	87.4629°
Mean anomaly	272.6947°
B*	1.8673e-4
Rev at epoch	8,040

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 62714U 25009DK 26187.72984647 .00002141 00000-0 18673-3 0 9993

2 62714 97.7047 267.5834 0003093 87.4629 272.6947 14.97900702 80400

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CENTAURI-8",
  "OBJECT_ID": "2025-009DK",
  "EPOCH": "2026-07-06T17:30:58.735+00:00",
  "MEAN_MOTION": 14.97900702,
  "ECCENTRICITY": 0.0003093,
  "INCLINATION": 97.7047,
  "RA_OF_ASC_NODE": 267.5834,
  "ARG_OF_PERICENTER": 87.4629,
  "MEAN_ANOMALY": 272.6947,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62714,
  "REV_AT_EPOCH": 8040,
  "BSTAR": 0.00018673,
  "MEAN_MOTION_DOT": 0.00002141,
  "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	CENTAURI-8
Operator	Fleet Space Technologies Pty LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Australia
Launch date	Jan 14, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	25HIGHvia 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/62714

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