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: 1 day ago
TLE from 1 day ago
0 GOSAT 2
1 43672U 18084B 26106.74335247 .00000842 00000-0 10689-3 0 9994
2 43672 97.8722 219.0146 0001448 93.3490 266.7890 14.84239736404448Epoch: 2026-04-16T17:50Z
TLE epoch observation values (Epoch: 2026-04-16T17:50:25.653Z)
Latitude
-0.00002°
Longitude
106.5212°
Altitude
619.058 km
Speed
7.549 km/s
True Right ascension
14h 36m 03s
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
00:48:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.019 km
Perigee altitude
611.995 km
Semi-major axis
6,991.144 km
Eccentricity
0.00014
Inclination
97.8722°
RAAN
219.0146°
Arg. of periapsis
93.349°
True anomaly
266.77243°
Mean anomaly
266.789°
Eccentric anomaly
266.78072°
Mean motion
3.71296 °/min
Orbital period
96.96 mins
BSTAR
0.00010689
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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 | 2026-04-17 20:17:08.764Z | 13.549° NNE | 2026-04-17 20:21:08.764Z | 44.493° NE | 44.66° | 2026-04-17 20:25:08.764Z | 191.765° SSW |
| 7 mins | 2026-04-18 07:11:08.764Z | 149.571° SSE | 2026-04-18 07:14:08.764Z | 84.914° E | 40.315° | 2026-04-18 07:18:08.764Z | 356.577° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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