Showing default

CE-SAT IIB, 46818

Orbit data source: Space-Track

CE-SAT IIB, 46818 is a payload satellite owned by Canon STL (JP) in SSO that was launched on Wed, 28 Oct 2020 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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.

Not visible in the next 10 days
Identifier
46818, 2020-077F
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
Canon STL
Mission
Operational Commercial Imaging
Bus & Motor
CE-SAT, Unknown motor
Mass
35 kg wet, 35 kg dry
Launch date (UTC)
2020-10-28 (6 years ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.575 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 CE-SAT IIB
1 46818U 20077F   26172.91452979  .00286649  38689-4  42754-3 0  9995
2 46818  97.1853 256.1822 0005390 160.0123 200.1370 16.04804600316044
Epoch: 2026-06-21T21:56Z
TLE epoch observation values (Epoch: 2026-06-21T21:56:55.373Z)
Latitude
-0.0001°
Longitude
16.84353°
Altitude
267.706 km
Speed
7.745 km/s
True Right ascension
17h 04m 43s
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
21:42:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
261.555 km
Perigee altitude
254.401 km
Semi-major axis
6,636.115 km
Eccentricity
0.00054
Inclination
97.1853°
RAAN
256.1822°
Arg. of periapsis
160.0123°
True anomaly
200.11575°
Mean anomaly
200.137°
Eccentric anomaly
200.12637°
Mean motion
4.01488 °/min
Orbital period
89.67 mins
BSTAR
0.00042754
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
|