▸Orbital parameters

Orbit class	SSO
Inclination	97.4150°
Eccentricity	0.0002217
Period	94.7 min
Apogee	504 km
Perigee	501 km
Mean motion	15.21038323 rev/day
RAAN	261.3009°
Arg of perigee	108.0046°
Mean anomaly	252.1432°
B*	2.1779e-4
Rev at epoch	3,343

▸Two-line element set (TLE)

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

1 66766U 25276DE 26187.87951948 .00004766 00000-0 21779-3 0 9990

2 66766 97.4150 261.3009 0002217 108.0046 252.1432 15.21038323 33431

▸ source OMM (JSON)

{
  "OBJECT_NAME": "T.MICROSAT-1",
  "OBJECT_ID": "2025-276DE",
  "EPOCH": "2026-07-06T21:06:30.483+00:00",
  "MEAN_MOTION": 15.21038323,
  "ECCENTRICITY": 0.0002217,
  "INCLINATION": 97.415,
  "RA_OF_ASC_NODE": 261.3009,
  "ARG_OF_PERICENTER": 108.0046,
  "MEAN_ANOMALY": 252.1432,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66766,
  "REV_AT_EPOCH": 3343,
  "BSTAR": 0.00021779,
  "MEAN_MOTION_DOT": 0.00004766,
  "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	T.MICROSAT-1
Operator	Taiwan Space Agency / Tron Future TechHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Taiwan
Launch date	Nov 28, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	15HIGHvia 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/66766

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