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: 7 hours ago
TLE from 7 hours ago
0 GOSAT 2
1 43672U 18084B 26230.92383990 -.00000601 00000-0 -65540-4 0 9992
2 43672 97.8837 341.6698 0001571 91.4254 268.7141 14.84225519422864Epoch: 2026-08-18T22:10Z
TLE epoch observation values (Epoch: 2026-08-18T22:10:19.767Z)
Latitude
0.00006°
Longitude
41.80274°
Altitude
619.07 km
Speed
7.549 km/s
True Right ascension
22h 46m 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
19:44:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.151 km
Perigee altitude
611.954 km
Semi-major axis
6,991.189 km
Eccentricity
0.00016
Inclination
97.8837°
RAAN
341.6698°
Arg. of periapsis
91.4254°
True anomaly
268.6961°
Mean anomaly
268.7141°
Eccentric anomaly
268.7051°
Mean motion
3.71293 °/min
Orbital period
96.96 mins
BSTAR
-0.00006554
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-19 06:25:24.621Z | 101.706° ESE | 2026-08-19 06:27:24.621Z | 70.222° E | 17.25° | 2026-08-19 06:30:24.621Z | 24.493° NE |
| 6 mins | 2026-08-19 08:00:24.621Z | 199.937° SSW | 2026-08-19 08:03:24.621Z | 263.808° W | 31.604° | 2026-08-19 08:06:24.621Z | 324.696° NNW |
| 6 mins | 2026-08-19 19:47:24.621Z | 38.127° NE | 2026-08-19 19:50:24.621Z | 101.426° ESE | 30.237° | 2026-08-19 19:53:24.621Z | 159.319° S |
| 4 mins | 2026-08-19 21:24:24.621Z | 322.044° NNW | 2026-08-19 21:26:24.621Z | 286.704° WNW | 18.013° | 2026-08-19 21:28:24.621Z | 255.283° W |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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