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: 4 hours ago
TLE from 4 hours ago
0 ASNARO
1 40298U 14070A 25256.32655994 .00000737 00000-0 38037-4 0 9990
2 40298 97.3733 334.4368 0002774 94.3864 265.7688 15.19336943601960Epoch: 2025-09-13T07:50Z
TLE epoch observation values (Epoch: 2025-09-13T07:50:14.778Z)
Latitude
-0.00003°
Longitude
-135.68629°
Altitude
511.075 km
Speed
7.608 km/s
True Right ascension
22h 17m 44s
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
04:36:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.718 km
Perigee altitude
502.899 km
Semi-major axis
6,882.946 km
Eccentricity
0.00028
Inclination
97.3733°
RAAN
334.4368°
Arg. of periapsis
94.3864°
True anomaly
265.7371°
Mean anomaly
265.7688°
Eccentric anomaly
265.75295°
Mean motion
3.80086 °/min
Orbital period
94.72 mins
BSTAR
0.000038037
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-13 17:52:39.960Z | 22.118° NNE | 2025-09-13 17:56:39.960Z | 129.867° SE | 36.853° | 2025-09-13 17:59:39.960Z | 177.259° S |
| 4 mins | 2025-09-14 04:32:39.960Z | 106.459° ESE | 2025-09-14 04:34:39.960Z | 63.932° ENE | 19.764° | 2025-09-14 04:36:39.960Z | 26.14° NE |
| 4 mins | 2025-09-14 06:06:39.960Z | 229.631° WSW | 2025-09-14 06:08:39.960Z | 275.906° WNW | 20.66° | 2025-09-14 06:10:39.960Z | 312.682° 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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