HIMAWARI 5 (GMS 5), 23522
Orbit data source: Space-Track
HIMAWARI 5 (GMS 5), 23522 is a payload satellite owned by NASDA (JP) in GEO that was launched on Sat, 18 Mar 1995 UTC via an H-II 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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23522 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
NEC/HSES
Mission
Non-operational Civil Weather
Bus & Motor
HS-378, STAR 27
Mass
746 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 1.8 m
Radar Cross Section
7.793 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 HIMAWARI 5 (GMS 5)
1 23522U 95011B 25346.04274807 -.00000035 00000-0 00000-0 0 9991
2 23522 14.2232 5.7932 0007049 174.3282 177.0966 0.99401623111736Epoch: 2025-12-12T01:01Z
TLE epoch observation values (Epoch: 2025-12-12T01:01:33.433Z)
Latitude
-2.09974°
Longitude
-98.90232°
Altitude
36,061.906 km
Speed
3.064 km/s
True Right ascension
23h 49m 54s
True Declination
-2° 05' 51"
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
05:23:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,063.177 km
Perigee altitude
36,003.385 km
Semi-major axis
42,411.418 km
Eccentricity
0.0007
Inclination
14.2232°
RAAN
5.7932°
Arg. of periapsis
174.3282°
True anomaly
177.10069°
Mean anomaly
177.0966°
Eccentric anomaly
177.09864°
Mean motion
0.2485 °/min
Orbital period
1,448.72 mins
BSTAR
0
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Other satellites on launch #11 in the year 1995 (1995-03-18 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.HIMAWARI 5 (GMS 5) 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-12-13 06:54:37.811Z | 176.526° S | 2025-12-13 07:48:37.811Z | 175.831° S | 40.882° | 2025-12-14 06:54:37.811Z | 183.574° SSW |
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23522 neighbors
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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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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