CHUBUSAT 2, 41338
Orbit data source: Space-Track
CHUBUSAT 2, 41338 is a payload satellite owned by Nagoya (JP) in LEO that was launched on Wed, 17 Feb 2016 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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41338 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
Nagoya
Mission
Non-operational Amateur Science
Bus & Motor
Unknown
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.5 m
Radar Cross Section
0.480 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 CHUBUSAT 2
1 41338U 16012B 26284.66132239 .00007127 00000-0 29992-3 0 9994
2 41338 30.9972 276.4185 0008642 192.6943 167.3481 15.21888825586173Epoch: 2026-10-11T15:52Z
TLE epoch observation values (Epoch: 2026-10-11T15:52:18.254Z)
Latitude
-0.00004°
Longitude
18.09148°
Altitude
504.443 km
Speed
7.611 km/s
True Right ascension
18h 25m 40s
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
22:08:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.953 km
Perigee altitude
498.058 km
Semi-major axis
6,882.142 km
Eccentricity
0.00086
Inclination
30.9972°
RAAN
276.4185°
Arg. of periapsis
192.6943°
True anomaly
167.36977°
Mean anomaly
167.3481°
Eccentric anomaly
167.35894°
Mean motion
3.80152 °/min
Orbital period
94.7 mins
BSTAR
0.00029992
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Other satellites on launch #12 in the year 2016 (2016-02-17 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.CHUBUSAT 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-12 04:45:48.658Z | 216.336° SW | 2026-10-12 04:48:48.658Z | 163.145° S | 19.327° | 2026-10-12 04:50:48.658Z | 129.454° SE |
| 4 mins | 2026-10-12 06:26:48.658Z | 210.811° SW | 2026-10-12 06:27:48.658Z | 189.88° SSW | 20.693° | 2026-10-12 06:30:48.658Z | 137.491° SSE |
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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