▸Orbital parameters

Orbit class	GEO
Inclination	0.0530°
Eccentricity	0.0002443
Period	1436.1 min
Apogee	35,797 km
Perigee	35,777 km
Mean motion	1.00270945 rev/day
RAAN	225.4860°
Arg of perigee	316.5972°
Mean anomaly	80.5648°
B*	0.0000e+0
Rev at epoch	5,229

▸Two-line element set (TLE)

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

1 37207U 10056B 26187.63387416 -.00000335 00000-0 00000-0 0 9995

2 37207 0.0530 225.4860 0002443 316.5972 80.5648 1.00270945 52299

▸ source OMM (JSON)

{
  "OBJECT_NAME": "BSAT-3B",
  "OBJECT_ID": "2010-056B",
  "EPOCH": "2026-07-06T15:12:46.727+00:00",
  "MEAN_MOTION": 1.00270945,
  "ECCENTRICITY": 0.0002443,
  "INCLINATION": 0.053,
  "RA_OF_ASC_NODE": 225.486,
  "ARG_OF_PERICENTER": 316.5972,
  "MEAN_ANOMALY": 80.5648,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 37207,
  "REV_AT_EPOCH": 5229,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000335,
  "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	BSAT-3B
Operator	Broadcasting Satellite System Corp.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	JapanMEDIUMvia Wikidata
Launch date	Oct 28, 2010HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2060HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—

▸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/37207

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