BSAT-3A, 32019
Orbit data source: Space-Track
BSAT-3A, 32019 is a payload satellite owned by BSAT (JP) in GEO that was launched on Tue, 14 Aug 2007 UTC via an ARIANE 5ECA launch vehicle from the French Guiana (FRGUI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
LMCSS
Mission
Non-operational Commercial Communications
Bus & Motor
A2100A, LEROS?
Mass
1,967 kg wet, 930 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 7.3 m
Radar Cross Section
15.563 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 BSAT-3A
1 32019U 07036B 25259.56440527 -.00000016 00000-0 00000-0 0 9995
2 32019 0.9414 95.8234 0005801 98.9254 266.8722 0.99137861 47768Epoch: 2025-09-16T13:32Z
TLE epoch observation values (Epoch: 2025-09-16T13:32:44.615Z)
Latitude
0.07641°
Longitude
-97.38591°
Altitude
36,108.261 km
Speed
3.063 km/s
True Right ascension
06h 46m 12s
True Declination
0° 04' 35"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:05:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,133.21 km
Perigee altitude
36,083.917 km
Semi-major axis
42,486.7 km
Eccentricity
0.00058
Inclination
0.9414°
RAAN
95.8234°
Arg. of periapsis
98.9254°
True anomaly
266.80583°
Mean anomaly
266.8722°
Eccentric anomaly
266.83901°
Mean motion
0.24784 °/min
Orbital period
1,452.58 mins
BSTAR
0
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Other satellites on launch #36 in the year 2007 (2007-08-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.BSAT-3A Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-09-17 04:20:57.484Z | 171.835° S | 2025-09-17 19:40:57.484Z | 175.758° S | 35.201° | 2025-09-18 04:20:57.484Z | 178.074° S |
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32019 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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