GOSAT 2, 43672
Orbit data source: Space-Track
GOSAT 2, 43672 is a payload satellite owned by JAXA (JP) in SSO that was launched on Mon, 29 Oct 2018 UTC via an H-IIA 202 launch vehicle from the Tanegashima Space Center (TNSTA). 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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43672 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
MELCO
Mission
Operational Civil Science
Bus & Motor
GOSAT, AOCS
Mass
1,750 kg wet, ~1,700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 8.4 m
Radar Cross Section
20.392 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GOSAT 2
1 43672U 18084B 25309.20364097 .00003019 00000-0 36677-3 0 9998
2 43672 97.8674 58.6693 0001473 90.2822 269.8562 14.84247406380335Epoch: 2025-11-05T04:53Z
TLE epoch observation values (Epoch: 2025-11-05T04:53:14.579Z)
Latitude
0.00004°
Longitude
-59.32113°
Altitude
618.98 km
Speed
7.549 km/s
True Right ascension
03h 54m 40s
True Declination
0° 00' 00"
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
05:27:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.013 km
Perigee altitude
611.953 km
Semi-major axis
6,991.12 km
Eccentricity
0.00015
Inclination
97.8674°
RAAN
58.6693°
Arg. of periapsis
90.2822°
True anomaly
269.83932°
Mean anomaly
269.8562°
Eccentric anomaly
269.84776°
Mean motion
3.71298 °/min
Orbital period
96.96 mins
BSTAR
0.00036677
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Other satellites on launch #84 in the year 2018 (2018-10-29 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.GOSAT 2 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-06 20:16:33.734Z | 13.538° NNE | 2025-11-06 20:20:33.734Z | 43.119° NE | 44.632° | 2025-11-06 20:24:33.734Z | 191.751° SSW |
| 7 mins | 2025-11-07 07:10:33.734Z | 149.549° SSE | 2025-11-07 07:13:33.734Z | 85.088° E | 40.287° | 2025-11-07 07:17:33.734Z | 356.613° N |
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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