▸Orbital parameters

Orbit class	SSO
Inclination	99.0077°
Eccentricity	0.0001943
Period	101.1 min
Apogee	812 km
Perigee	809 km
Mean motion	14.24432203 rev/day
RAAN	181.2008°
Arg of perigee	128.2186°
Mean anomaly	231.9167°
B*	3.7960e-5
Rev at epoch	45,414

▸Two-line element set (TLE)

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

1 25397U 98043D 26187.94313303 .00000041 00000-0 37960-4 0 9994

2 25397 99.0077 181.2008 0001943 128.2186 231.9167 14.24432203454147

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TECHSAT 1B (GO-32)",
  "OBJECT_ID": "1998-043D",
  "EPOCH": "2026-07-06T22:38:06.694+00:00",
  "MEAN_MOTION": 14.24432203,
  "ECCENTRICITY": 0.0001943,
  "INCLINATION": 99.0077,
  "RA_OF_ASC_NODE": 181.2008,
  "ARG_OF_PERICENTER": 128.2186,
  "MEAN_ANOMALY": 231.9167,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 25397,
  "REV_AT_EPOCH": 45414,
  "BSTAR": 0.00003796,
  "MEAN_MOTION_DOT": 4.1e-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	TECHSAT 1B (GO-32)
Operator	TechnionHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Technion – Israel Institute of TechnologyMEDIUMvia Wikidata
Country	Israel
Launch date	Jul 10, 1998HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	50HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/25397

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