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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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
NEC Toshiba/Fuchu
Mission
Operational Commercial 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, 2.2 m
Radar Cross Section
9.327 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ASNARO
1 40298U 14070A 26258.63606568 .00004995 00000-0 23707-3 0 9997
2 40298 97.3379 332.2820 0004288 182.0233 178.0985 15.19694207657745Epoch: 2026-09-15T15:15Z
TLE epoch observation values (Epoch: 2026-09-15T15:15:56.074Z)
Latitude
-0.0001°
Longitude
108.6992°
Altitude
512.807 km
Speed
7.606 km/s
True Right ascension
22h 09m 07s
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
17:26:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.678 km
Perigee altitude
500.776 km
Semi-major axis
6,881.864 km
Eccentricity
0.00043
Inclination
97.3379°
RAAN
332.282°
Arg. of periapsis
182.0233°
True anomaly
178.10013°
Mean anomaly
178.0985°
Eccentric anomaly
178.09931°
Mean motion
3.80175 °/min
Orbital period
94.69 mins
BSTAR
0.00023707
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-16 04:03:42.078Z | 105.329° ESE | 2026-09-16 04:05:42.078Z | 72.537° E | 15.769° | 2026-09-16 04:07:42.078Z | 36.7° NE |
| 5 mins | 2026-09-16 05:37:42.078Z | 213.792° SW | 2026-09-16 05:39:42.078Z | 267.478° W | 31.951° | 2026-09-16 05:42:42.078Z | 325.938° NNW |
| 4 mins | 2026-09-16 17:08:42.078Z | 62.648° ENE | 2026-09-16 17:09:42.078Z | 84.267° E | 21.94° | 2026-09-16 17:12:42.078Z | 144.276° SSE |
| 4 mins | 2026-09-16 18:42:42.078Z | 317.728° NNW | 2026-09-16 18:43:42.078Z | 295.506° NW | 21.476° | 2026-09-16 18:46:42.078Z | 240.143° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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