▸Orbital parameters

Orbit class	SSO
Inclination	97.7725°
Eccentricity	0.0003510
Period	96.4 min
Apogee	587 km
Perigee	582 km
Mean motion	14.94408614 rev/day
RAAN	302.5084°
Arg of perigee	260.9051°
Mean anomaly	99.1772°
B*	1.4926e-4
Rev at epoch	5,689

▸Two-line element set (TLE)

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

1 64589U 25135BP 26188.18341985 .00001550 00000-0 14926-3 0 9998

2 64589 97.7725 302.5084 0003510 260.9051 99.1772 14.94408614 56899

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SATORO-T3",
  "OBJECT_ID": "2025-135BP",
  "EPOCH": "2026-07-07T04:24:07.475+00:00",
  "MEAN_MOTION": 14.94408614,
  "ECCENTRICITY": 0.000351,
  "INCLINATION": 97.7725,
  "RA_OF_ASC_NODE": 302.5084,
  "ARG_OF_PERICENTER": 260.9051,
  "MEAN_ANOMALY": 99.1772,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64589,
  "REV_AT_EPOCH": 5689,
  "BSTAR": 0.00014926,
  "MEAN_MOTION_DOT": 0.0000155,
  "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	SATORO-T3
Operator	Satoro SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Taiwan
Launch date	Jun 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4HIGHvia 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/64589

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