DECAYED
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CP11 (ISX), 43856 (Decayed)

Orbit data source: Space-Track

CP11 (ISX), 43856 was a payload satellite owned by Cal Poly (US) in LEO that was launched on Sun, 16 Dec 2018 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
43856, 2018-104H
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
Cal Poly
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3.5 kg wet, 3.5 kg dry
Launch date (UTC)
2018-12-16 (7 years ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

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

TLE from 1 year ago
0 CP11 (ISX)
1 43856U 18104H   24137.54898874  .09084474 -14778-5  12966-2 0  9995
2 43856  84.9711 295.3142 0013845 258.8411 101.1335 16.34609461302249
Epoch: 2024-05-16T13:10Z
TLE epoch observation values (Epoch: 2024-05-16T13:10:32.627Z)
Latitude
-0.00001°
Longitude
-137.06353°
Altitude
185.251 km
Speed
7.794 km/s
True Right ascension
19h 41m 15s
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
16:06:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
185.982 km
Perigee altitude
167.831 km
Semi-major axis
6,555.043 km
Eccentricity
0.00138
Inclination
84.9711°
RAAN
295.3142°
Arg. of periapsis
258.8411°
True anomaly
101.28911°
Mean anomaly
101.1335°
Eccentric anomaly
101.21131°
Mean motion
4.08959 °/min
Orbital period
88.03 mins
BSTAR
0.0012966
Loading maneuver chart data...
Computing Atmospheric mass density...

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