LEMUR 2 SAM-AMELIA, 42781 (Decayed)
Orbit data source: Space-Track
LEMUR 2 SAM-AMELIA, 42781 was a payload satellite owned by Spire (US) in LEO that was launched on Fri, 23 Jun 2017 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). 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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42781 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Decayed Commercial Com/MetRO
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, 0.3 m
Radar Cross Section
0.093 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 LEMUR 2 SAM-AMELIA
1 42781U 17036S 24091.96942353 .15355412 23980-5 48873-3 0 9992
2 42781 97.0755 138.1159 0010178 255.0250 104.9926 16.44056844378080Epoch: 2024-03-31T23:15Z
TLE epoch observation values (Epoch: 2024-03-31T23:15:58.193Z)
Latitude
0°
Longitude
-40.69297°
Altitude
160.026 km
Speed
7.809 km/s
True Right ascension
09h 12m 27s
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
07:54:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
158.467 km
Perigee altitude
145.175 km
Semi-major axis
6,529.958 km
Eccentricity
0.00102
Inclination
97.0755°
RAAN
138.1159°
Arg. of periapsis
255.025°
True anomaly
105.10522°
Mean anomaly
104.9926°
Eccentric anomaly
105.04892°
Mean motion
4.11318 °/min
Orbital period
87.52 mins
BSTAR
0.00048873
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Other satellites on launch #36 in the year 2017 (2017-06-23 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.LEMUR 2 SAM-AMELIA 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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