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, 8.3 m
Radar Cross Section
20.392 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 GOSAT 2
1 43672U 18084B 25258.03506773 .00001704 00000-0 20979-3 0 9998
2 43672 97.8623 8.2225 0001440 91.8925 268.2455 14.84248615372749Epoch: 2025-09-15T00:50Z
TLE epoch observation values (Epoch: 2025-09-15T00:50:29.851Z)
Latitude
0.00002°
Longitude
1.35261°
Altitude
619.005 km
Speed
7.549 km/s
True Right ascension
00h 32m 53s
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
16:26:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
613.986 km
Perigee altitude
611.972 km
Semi-major axis
6,991.116 km
Eccentricity
0.00014
Inclination
97.8623°
RAAN
8.2225°
Arg. of periapsis
91.8925°
True anomaly
268.22901°
Mean anomaly
268.2455°
Eccentric anomaly
268.23725°
Mean motion
3.71299 °/min
Orbital period
96.96 mins
BSTAR
0.00020979
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-16 07:43:04.708Z | 185.949° SSW | 2025-09-16 07:46:04.708Z | 286.807° WNW | 39.595° | 2025-09-16 07:49:04.708Z | 336.963° NNW |
| 4 mins | 2025-09-16 19:31:04.708Z | 65.018° ENE | 2025-09-16 19:32:04.708Z | 84.651° E | 21.738° | 2025-09-16 19:35:04.708Z | 140.441° SSE |
| 6 mins | 2025-09-16 21:06:04.708Z | 337.903° N | 2025-09-16 21:08:04.708Z | 301.871° NW | 24.388° | 2025-09-16 21:12:04.708Z | 232.98° WSW |
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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