ASNARO, 40298
Orbit data source: Space-Track
ASNARO, 40298 is a payload satellite owned by J-spacesystems (JP) in SSO that was launched on Thu, 06 Nov 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40298 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
NEC Toshiba/Fuchu
Mission
Operational Civil Imaging
Bus & Motor
NEXTAR-300L, AOCS?
Mass
495 kg wet, 450 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 1.8 m
Radar Cross Section
9.327 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ASNARO
1 40298U 14070A 25285.69576253 -.00000068 00000-0 -70312-7 0 9996
2 40298 97.3705 3.1128 0002155 251.6151 108.4850 15.19565870606426Epoch: 2025-10-12T16:41Z
TLE epoch observation values (Epoch: 2025-10-12T16:41:53.882Z)
Latitude
-0.00001°
Longitude
91.12909°
Altitude
510.713 km
Speed
7.608 km/s
True Right ascension
00h 12m 27s
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
16:14:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.6 km
Perigee altitude
502.633 km
Semi-major axis
6,882.254 km
Eccentricity
0.00022
Inclination
97.3705°
RAAN
3.1128°
Arg. of periapsis
251.6151°
True anomaly
108.50842°
Mean anomaly
108.485°
Eccentric anomaly
108.49671°
Mean motion
3.80143 °/min
Orbital period
94.7 mins
BSTAR
-7.0312e-8
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Other satellites on launch #70 in the year 2014 (2014-11-06 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 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 | 2025-10-14 05:10:25.537Z | 158.227° S | 2025-10-14 05:13:25.537Z | 92.701° ESE | 42.907° | 2025-10-14 05:16:25.537Z | 354.864° N |
| 5 mins | 2025-10-14 18:16:25.537Z | 2.68° NNE | 2025-10-14 18:18:25.537Z | 243.743° WSW | 43.04° | 2025-10-14 18:21:25.537Z | 199.525° SSW |
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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