Showing default

R2, 46913

Orbit data source: Space-Track

R2, 46913 is a payload satellite owned by NanoAvionics (LT) in LEO that was launched on Sat, 07 Nov 2020 UTC via a PSLV-DL launch vehicle from the Sirharikota (SRI). 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
46913, 2020-081J
Orbit
LEO
Country
Flag of LTLT / LTU
Related business
Manufacturer
NanoAvionics US
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
6.8 kg wet, 6.8 kg dry
Launch date (UTC)
2020-11-07 (5 years ago)
Launch vehicle
PSLV-DL
Launch site
Sirharikota (SRI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 R2
1 46913U 20081J   26080.76551364  .00012220  00000-0  49513-3 0  9999
2 46913  36.8980 239.3798 0006917 261.2652  98.7313 15.24045318298639
Epoch: 2026-03-21T18:22Z
TLE epoch observation values (Epoch: 2026-03-21T18:22:20.378Z)
Latitude
-0.00002°
Longitude
144.51333°
Altitude
493.486 km
Speed
7.62 km/s
True Right ascension
15h 57m 31s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
07:15:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.358 km
Perigee altitude
491.847 km
Semi-major axis
6,874.739 km
Eccentricity
0.00069
Inclination
36.898°
RAAN
239.3798°
Arg. of periapsis
261.2652°
True anomaly
98.80963°
Mean anomaly
98.7313°
Eccentric anomaly
98.77047°
Mean motion
3.80767 °/min
Orbital period
94.55 mins
BSTAR
0.00049513
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|