CARBONITE 2, 43115 (Decayed)
Orbit data source: Space-Track
CARBONITE 2, 43115 was a UK payload satellite in LEO that was launched on Fri, 12 Jan 2018 UTC via a PSLV-XL 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.
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43115 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UKRelated business
Manufacturer
SSTL (Astrium)
Mission
Decayed Commercial Imaging
Bus & Motor
CBNT, Unknown motor
Mass
100 kg wet, 100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + Cyl, 0.5 m
Radar Cross Section
1.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 CARBONITE 2
1 43115U 18004E 25137.20304171 .04606220 23996-5 59053-3 0 9992
2 43115 97.1894 221.7544 0010900 254.1267 105.8829 16.35734082410069Epoch: 2025-05-17T04:52Z
TLE epoch observation values (Epoch: 2025-05-17T04:52:22.803Z)
Latitude
-0.0001°
Longitude
-86.48834°
Altitude
182.39 km
Speed
7.796 km/s
True Right ascension
14h 47m 01s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:05:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
181.121 km
Perigee altitude
166.837 km
Semi-major axis
6,552.116 km
Eccentricity
0.00109
Inclination
97.1894°
RAAN
221.7544°
Arg. of periapsis
254.1267°
True anomaly
106.00299°
Mean anomaly
105.8829°
Eccentric anomaly
105.94295°
Mean motion
4.09233 °/min
Orbital period
87.97 mins
BSTAR
0.00059053
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Other satellites on launch #4 in the year 2018 (2018-01-12 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CARBONITE 2 Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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