ASNARO-2, 43152
Orbit data source: Space-Track
ASNARO-2, 43152 is a payload satellite owned by J-spacesystems (JP) in SSO that was launched on Wed, 17 Jan 2018 UTC via an EPSILON launch vehicle from the Kagoshima Space Center University Of Tokyo (KSCUT). 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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43152 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
NEC Toshiba/Fuchu
Mission
Operational Commercial Radar Imaging
Bus & Motor
NEXTAR-300L, AOCS?
Mass
570 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan + 1 Dish, 1.8 m
Radar Cross Section
9.327 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ASNARO-2
1 43152U 18007A 25258.31357316 .00016853 00000-0 73072-3 0 9997
2 43152 97.4045 264.4511 0001885 91.0225 269.1227 15.22432492425598Epoch: 2025-09-15T07:31Z
TLE epoch observation values (Epoch: 2025-09-15T07:31:32.721Z)
Latitude
-0.00004°
Longitude
157.04475°
Altitude
501.62 km
Speed
7.614 km/s
True Right ascension
17h 37m 48s
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
11:09:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.764 km
Perigee altitude
494.173 km
Semi-major axis
6,873.606 km
Eccentricity
0.00019
Inclination
97.4045°
RAAN
264.4511°
Arg. of periapsis
91.0225°
True anomaly
269.1011°
Mean anomaly
269.1227°
Eccentric anomaly
269.1119°
Mean motion
3.80861 °/min
Orbital period
94.52 mins
BSTAR
0.00073072
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Other satellites on launch #7 in the year 2018 (2018-01-17 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.ASNARO-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 | 2025-09-16 01:00:51.764Z | 204.61° SW | 2025-09-16 01:02:51.764Z | 257.822° W | 30.788° | 2025-09-16 01:05:51.764Z | 327.308° NNW |
| 4 mins | 2025-09-16 14:04:51.764Z | 317.091° NNW | 2025-09-16 14:05:51.764Z | 290.624° WNW | 23.371° | 2025-09-16 14:08:51.764Z | 232.956° WSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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