CARBONITE 1, 40718
Orbit data source: Space-Track
CARBONITE 1, 40718 is a payload satellite owned by SSTL (Astrium) (UK) in SSO that was launched on Fri, 10 Jul 2015 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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40718 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
SSTL (Astrium)
Mission
Operational Commercial Imaging
Bus & Motor
CBNT, Unknown motor
Mass
91 kg wet, 91 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + Cyl, 0.5 m
Radar Cross Section
0.780 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 CARBONITE 1
1 40718U 15032D 26155.30024012 .00001231 00000-0 15546-3 0 9993
2 40718 97.6500 333.9067 0014121 343.0606 17.0135 14.83543822587435Epoch: 2026-06-04T07:12Z
TLE epoch observation values (Epoch: 2026-06-04T07:12:20.746Z)
Latitude
-0.00004°
Longitude
-26.92622°
Altitude
611.746 km
Speed
7.558 km/s
True Right ascension
22h 15m 37s
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
14:01:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.061 km
Perigee altitude
605.31 km
Semi-major axis
6,993.322 km
Eccentricity
0.00141
Inclination
97.65°
RAAN
333.9067°
Arg. of periapsis
343.0606°
True anomaly
17.06093°
Mean anomaly
17.0135°
Eccentric anomaly
17.03721°
Mean motion
3.71123 °/min
Orbital period
97 mins
BSTAR
0.00015546
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Other satellites on launch #32 in the year 2015 (2015-07-10 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 1 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-10 12:15:52.287Z | 191.391° SSW | 2026-06-10 12:18:52.287Z | 286.356° WNW | 37.329° | 2026-06-10 12:21:52.287Z | 335.079° NNW |
| 5 mins | 2026-06-11 00:03:52.287Z | 57.342° ENE | 2026-06-11 00:05:52.287Z | 101.267° ESE | 25.151° | 2026-06-11 00:08:52.287Z | 151.47° SSE |
| 5 mins | 2026-06-11 01:39:52.287Z | 325.709° NNW | 2026-06-11 01:41:52.287Z | 285.661° WNW | 22.412° | 2026-06-11 01:44:52.287Z | 239.31° WSW |
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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