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 26034.27126212 .00002770 00000-0 33712-3 0 9996
2 43672 97.8680 147.5168 0001822 106.7387 253.4028 14.84248452393695Epoch: 2026-02-03T06:30Z
TLE epoch observation values (Epoch: 2026-02-03T06:30:37.047Z)
Latitude
0.00006°
Longitude
-83.59216°
Altitude
619.338 km
Speed
7.549 km/s
True Right ascension
09h 50m 04s
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
18:58:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.253 km
Perigee altitude
611.706 km
Semi-major axis
6,991.117 km
Eccentricity
0.00018
Inclination
97.868°
RAAN
147.5168°
Arg. of periapsis
106.7387°
True anomaly
253.38279°
Mean anomaly
253.4028°
Eccentric anomaly
253.3928°
Mean motion
3.71299 °/min
Orbital period
96.96 mins
BSTAR
0.00033712
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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 | 2026-02-03 20:00:55.609Z | 21.897° NNE | 2026-02-03 20:04:55.609Z | 93.005° ESE | 39.285° | 2026-02-03 20:08:55.609Z | 177.783° S |
| 6 mins | 2026-02-04 06:55:55.609Z | 125.148° SE | 2026-02-04 06:57:55.609Z | 77.551° E | 31.672° | 2026-02-04 07:01:55.609Z | 4.492° NNE |
| 4 mins | 2026-02-04 08:32:55.609Z | 244.62° WSW | 2026-02-04 08:33:55.609Z | 261.24° W | 16.337° | 2026-02-04 08:36:55.609Z | 306.978° NW |
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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