KEPLER-0 (KIPP), 43157 (Decayed)
Orbit data source: Space-Track
KEPLER-0 (KIPP), 43157 was a payload satellite owned by Kepler Comms (CA) in LEO that was launched on Fri, 19 Jan 2018 UTC via a CHANG ZHENG 11 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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43157 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CARelated business
Manufacturer
AAC ClydeSpace
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 KEPLER-0 (KIPP)
1 43157U 18008C 24103.03271106 .18194248 24335-5 16060-2 0 9991
2 43157 97.2162 161.4645 0013704 262.1472 97.8272 16.38947242344805Epoch: 2024-04-12T00:47Z
TLE epoch observation values (Epoch: 2024-04-12T00:47:06.235Z)
Latitude
-0.00002°
Longitude
-51.03238°
Altitude
173.094 km
Speed
7.802 km/s
True Right ascension
10h 45m 51s
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
19:03:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
174.373 km
Perigee altitude
156.438 km
Semi-major axis
6,543.542 km
Eccentricity
0.00137
Inclination
97.2162°
RAAN
161.4645°
Arg. of periapsis
262.1472°
True anomaly
97.98274°
Mean anomaly
97.8272°
Eccentric anomaly
97.90497°
Mean motion
4.10038 °/min
Orbital period
87.8 mins
BSTAR
0.001606
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Other satellites on launch #8 in the year 2018 (2018-01-19 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.KEPLER-0 (KIPP) 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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