TECHEDSAT 13, 51095 (Decayed)
Orbit data source: Space-Track
TECHEDSAT 13, 51095 was an American payload satellite in LEO that was launched on Thu, 13 Jan 2022 UTC via an LAUNCHERONE launch vehicle from the Pegasus Launch, Western Range Air Space (WRAS). 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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51095 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ARC
Mission
Decayed Civil Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Truss + 1 Sail, 0.4 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 TECHEDSAT 13
1 51095U 22003B 24194.23040869 .04907095 10302-4 89464-3 0 9997
2 51095 44.9616 175.9616 0003365 130.6448 229.4767 16.31437883140196Epoch: 2024-07-12T05:31Z
TLE epoch observation values (Epoch: 2024-07-12T05:31:47.31Z)
Latitude
-0.00003°
Longitude
162.40477°
Altitude
190.108 km
Speed
7.793 km/s
True Right ascension
11h 43m 50s
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
09:03:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
192.577 km
Perigee altitude
188.156 km
Semi-major axis
6,568.503 km
Eccentricity
0.00034
Inclination
44.9616°
RAAN
175.9616°
Arg. of periapsis
130.6448°
True anomaly
229.4474°
Mean anomaly
229.4767°
Eccentric anomaly
229.46205°
Mean motion
4.07703 °/min
Orbital period
88.3 mins
BSTAR
0.00089464
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Other satellites on launch #3 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.TECHEDSAT 13 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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