Showing default

WNISAT 1R, 42835

Orbit data source: Space-Track

WNISAT 1R, 42835 is a payload satellite owned by WNI (JP) in SSO that was launched on Fri, 14 Jul 2017 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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.

Loading next visibility...
Identifier
42835, 2017-042L
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
AXELSPACE
Mission
Operational Commercial Weather
Bus & Motor
HODOYOSHI, Unknown motor
Mass
40 kg wet, 40 kg dry
Launch date (UTC)
2017-07-14 (8 years ago)
Launch vehicle
SOYUZ-2-1A
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.514 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 WNISAT 1R
1 42835U 17042L   25339.04730170  .00006476  00000-0  52015-3 0  9999
2 42835  97.4161 138.0432 0013292  83.1521 277.1216 15.00293058457386
Epoch: 2025-12-05T01:08Z
TLE epoch observation values (Epoch: 2025-12-05T01:08:06.866Z)
Latitude
0.00003°
Longitude
46.91959°
Altitude
567.923 km
Speed
7.578 km/s
True Right ascension
09h 12m 10s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:25:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.211 km
Perigee altitude
553.758 km
Semi-major axis
6,941.122 km
Eccentricity
0.00133
Inclination
97.4161°
RAAN
138.0432°
Arg. of periapsis
83.1521°
True anomaly
276.97043°
Mean anomaly
277.1216°
Eccentric anomaly
277.04602°
Mean motion
3.75317 °/min
Orbital period
95.92 mins
BSTAR
0.00052015
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|