MP42, 52169 (Decayed)
Orbit data source: Space-Track
MP42, 52169 was a Lithuanian payload satellite in LEO that was launched on Fri, 01 Apr 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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52169 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
LT / LTURelated business
Manufacturer
NanoAvionics
Mission
Decayed Commercial Communications
Bus & Motor
MP42, Unknown motor
Mass
~40 kg wet, ~40 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.8 m
Radar Cross Section
0.688 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 MP42
1 52169U 22033N 24294.37605446 .15399449 25241-5 25580-3 0 9995
2 52169 97.2984 28.2979 0013066 270.7453 89.2354 16.47246543143310Epoch: 2024-10-20T09:01Z
TLE epoch observation values (Epoch: 2024-10-20T09:01:31.105Z)
Latitude
0.00005°
Longitude
-136.39968°
Altitude
149.758 km
Speed
7.816 km/s
True Right ascension
01h 53m 11s
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
16:44:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
151.911 km
Perigee altitude
134.869 km
Semi-major axis
6,521.527 km
Eccentricity
0.00131
Inclination
97.2984°
RAAN
28.2979°
Arg. of periapsis
270.7453°
True anomaly
89.38512°
Mean anomaly
89.2354°
Eccentric anomaly
89.31026°
Mean motion
4.12116 °/min
Orbital period
87.35 mins
BSTAR
0.0002558
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Other satellites on launch #33 in the year 2022 (2022-04-01 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.MP42 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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