KEPLER-19, 51051 (Decayed)
Orbit data source: Space-Track
KEPLER-19, 51051 was a payload satellite owned by Kepler Comms (CA) in LEO that was launched on Thu, 13 Jan 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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51051 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CARelated business
Manufacturer
KEPLER/UTIAS
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
15 kg wet, 15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.196 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 KEPLER-19
1 51051U 22002BV 25089.69813844 .17884277 25226-5 34267-3 0 9996
2 51051 97.3016 165.0953 0015232 274.0257 85.9304 16.46148553178557Epoch: 2025-03-30T16:45Z
TLE epoch observation values (Epoch: 2025-03-30T16:45:19.161Z)
Latitude
-0.00008°
Longitude
85.44082°
Altitude
152.069 km
Speed
7.815 km/s
True Right ascension
11h 00m 22s
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
06:48:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
156.231 km
Perigee altitude
136.355 km
Semi-major axis
6,524.43 km
Eccentricity
0.00152
Inclination
97.3016°
RAAN
165.0953°
Arg. of periapsis
274.0257°
True anomaly
86.10453°
Mean anomaly
85.9304°
Eccentric anomaly
86.01746°
Mean motion
4.11841 °/min
Orbital period
87.41 mins
BSTAR
0.00034267
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Other satellites on launch #2 in the year 2022 (2022-01-13 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-19 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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