MYRADAR1, 52419 (Decayed)
Orbit data source: Space-Track
MYRADAR1, 52419 was a payload satellite owned by ACME AtronOmatic (US) in LEO that was launched on Mon, 02 May 2022 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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52419 intel report (Beta)
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MYRADAR1 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ACME AtronOmatic
Mission
Decayed Commercial Imaging
Bus & Motor
POCKETQUBE 1P, Unknown motor
Mass
0.25 kg wet, 0.25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.0 m
Radar Cross Section
0.004 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 MYRADAR1
1 52419U 22047AB 24233.98531526 .15245793 25412-5 43352-3 0 9994
2 52419 97.3504 328.5188 0014320 268.5058 91.4604 16.44088942130048Epoch: 2024-08-20T23:38Z
TLE epoch observation values (Epoch: 2024-08-20T23:38:51.238Z)
Latitude
0.00004°
Longitude
4.01131°
Altitude
158.458 km
Speed
7.811 km/s
True Right ascension
21h 54m 04s
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
13:24:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.099 km
Perigee altitude
142.397 km
Semi-major axis
6,529.885 km
Eccentricity
0.00143
Inclination
97.3504°
RAAN
328.5188°
Arg. of periapsis
268.5058°
True anomaly
91.62443°
Mean anomaly
91.4604°
Eccentric anomaly
91.54242°
Mean motion
4.11325 °/min
Orbital period
87.52 mins
BSTAR
0.00043352
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Other satellites on launch #47 in the year 2022 (2022-05-02 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.MYRADAR1 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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