▸Orbital parameters

Orbit class	SSO
Inclination	98.5556°
Eccentricity	0.0001122
Period	101.4 min
Apogee	826 km
Perigee	824 km
Mean motion	14.20136153 rev/day
RAAN	244.8231°
Arg of perigee	86.7090°
Mean anomaly	273.4215°
B*	-1.7608e-5
Rev at epoch	92,080

▸Two-line element set (TLE)

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

1 33396U 08049A 26188.18965764 -.00000080 00000-0 -17608-4 0 9992

2 33396 98.5556 244.8231 0001122 86.7090 273.4215 14.20136153920803

▸ source OMM (JSON)

{
  "OBJECT_NAME": "THEOS",
  "OBJECT_ID": "2008-049A",
  "EPOCH": "2026-07-07T04:33:06.42+00:00",
  "MEAN_MOTION": 14.20136153,
  "ECCENTRICITY": 0.0001122,
  "INCLINATION": 98.5556,
  "RA_OF_ASC_NODE": 244.8231,
  "ARG_OF_PERICENTER": 86.709,
  "MEAN_ANOMALY": 273.4215,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 33396,
  "REV_AT_EPOCH": 92080,
  "BSTAR": -0.000017608,
  "MEAN_MOTION_DOT": -8e-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	THEOS
Operator	Geo-Informatics and Space Technology Development AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog Geo-Informatics and Space Technology Development AgencyMEDIUMvia Wikidata
Country	ThailandMEDIUMvia Wikidata
Launch date	Oct 1, 2008HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	750HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/33396

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