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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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: 13 hours ago
TLE from 13 hours ago
0 GOSAT 2
1 43672U 18084B 26082.87810473 .00002180 00000-0 26677-3 0 9991
2 43672 97.8688 195.4640 0001523 98.5489 261.5898 14.84225286400907Epoch: 2026-03-23T21:04Z
TLE epoch observation values (Epoch: 2026-03-23T21:04:28.248Z)
Latitude
-0.00003°
Longitude
57.98251°
Altitude
619.203 km
Speed
7.549 km/s
True Right ascension
13h 01m 51s
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
14:41:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.117 km
Perigee altitude
611.988 km
Semi-major axis
6,991.189 km
Eccentricity
0.00015
Inclination
97.8688°
RAAN
195.464°
Arg. of periapsis
98.5489°
True anomaly
261.57254°
Mean anomaly
261.5898°
Eccentric anomaly
261.58117°
Mean motion
3.71293 °/min
Orbital period
96.96 mins
BSTAR
0.00026677
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-24 20:17:49.698Z | 14.032° NNE | 2026-03-24 20:20:49.698Z | 28.159° NE | 43.733° | 2026-03-24 20:24:49.698Z | 191.655° SSW |
| 6 mins | 2026-03-25 07:11:49.698Z | 145.207° SSE | 2026-03-25 07:13:49.698Z | 99.006° ESE | 39.632° | 2026-03-25 07:17:49.698Z | 357.254° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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