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: 11 hours ago
TLE from 11 hours ago
0 GOSAT 2
1 43672U 18084B 25339.94527930 .00004686 00000-0 56598-3 0 9994
2 43672 97.8692 88.9914 0001535 92.7369 267.4021 14.84225095384898Epoch: 2025-12-05T22:41Z
TLE epoch observation values (Epoch: 2025-12-05T22:41:12.131Z)
Latitude
-0.00003°
Longitude
33.71077°
Altitude
619.096 km
Speed
7.549 km/s
True Right ascension
05h 55m 57s
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
08:00:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.126 km
Perigee altitude
611.98 km
Semi-major axis
6,991.19 km
Eccentricity
0.00015
Inclination
97.8692°
RAAN
88.9914°
Arg. of periapsis
92.7369°
True anomaly
267.38453°
Mean anomaly
267.4021°
Eccentric anomaly
267.39331°
Mean motion
3.71293 °/min
Orbital period
96.96 mins
BSTAR
0.00056598
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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 | 2025-12-06 20:16:59.605Z | 13.706° NNE | 2025-12-06 20:20:59.605Z | 151.284° SSE | 44.791° | 2025-12-06 20:24:59.605Z | 191.944° SSW |
| 7 mins | 2025-12-07 07:10:59.605Z | 148.183° SSE | 2025-12-07 07:13:59.605Z | 64.223° ENE | 40.336° | 2025-12-07 07:17:59.605Z | 355.784° 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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