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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.

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<iframe src="https://www.satcat.com/sats-embedded/46818?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/46818?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

46818, 2020-077F

Orbit

SSO

Country

JP / JPN

Related business

Canon Electronics Inc. (JP)

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 (5 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: 2 days ago

TLE from 2 days ago

0 CE-SAT IIB
1 46818U 20077F   26087.24842021  .00083010  00000-0  41809-3 0  9996
2 46818  97.2097 165.2106 0004140 115.9283 244.2413 15.81419616302425

Epoch: 2026-03-28T05:57Z

TLE epoch observation values (Epoch: 2026-03-28T05:57:43.506Z)

Latitude

0.00002°

Longitude

-109.89206°

Altitude

330.812 km

Speed

7.709 km/s

True Right ascension

11h 00m 50s

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

02:25:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

326.076 km

Perigee altitude

320.527 km

Semi-major axis

6,701.438 km

Eccentricity

0.00041

Inclination

97.2097°

RAAN

165.2106°

Arg. of periapsis

115.9283°

True anomaly

244.19858°

Mean anomaly

244.2413°

Eccentric anomaly

244.21994°

Mean motion

3.95632 °/min

Orbital period

90.99 mins

BSTAR

0.00041809

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Other satellites on launch #77 in the year 2020 (2020-10-28 UTC)

FLOCK 4EP 2, 46820 (Decayed)

FLOCK 4EP 7, 46814 (Decayed)

FLOCK 4EP 4, 46821 (Decayed)

ELECTRON KICK STAGE R/B, 46824 (Decayed)

FLOCK 4EP 3, 46819 (Decayed)

FLOCK 4EP 8, 46816 (Decayed)

FLOCK 4EP 9, 46815 (Decayed)

ELECTRON R/B, 46823 (Decayed)

FLOCK 4EP 5, 46817 (Decayed)

FLOCK 4EP 1, 46813 (Decayed)

FLOCK 4EP 6, 46822 (Decayed)

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CE-SAT IIB 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.
5 mins	2026-03-30 05:09:46.024Z	164.384° S	2026-03-30 05:12:46.024Z	2.732° NNE	39.693°	2026-03-30 05:14:46.024Z	350.699° N

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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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Check out CE-SAT IIB, 46818 on other resources

View CE-SAT IIB, 46818 on NASA - NSSDCA Website

View CE-SAT IIB, 46818 on Heavens-Above

View CE-SAT IIB, 46818 on Keep Track

View CE-SAT IIB, 46818 on Celestrak

View CE-SAT IIB, 46818 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

CE-SAT IIB, 46818

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-03-28T05:57:43.506Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #77 in the year 2020 (2020-10-28 UTC)

CE-SAT IIB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CE-SAT IIB, 46818 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago