LEMUR 2 PAPPY, 44861 (Decayed)
Orbit data source: Space-Track
LEMUR 2 PAPPY, 44861 was a payload satellite owned by Spire (US) in LEO that was launched on Wed, 11 Dec 2019 UTC via a PSLV-QL 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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44861 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 LEMUR 2 PAPPY
1 44861U 19089K 24281.31938788 .03913180 32013-1 43153-2 0 9997
2 44861 36.9369 359.8453 0011361 60.3040 299.8868 16.12538234266181
Epoch: 2024-10-07T07:39Z
TLE epoch observation values (Epoch: 2024-10-07T07:39:55.112Z)
Latitude
-0°
Longitude
-131.58303°
Altitude
235.228 km
Speed
7.77 km/s
True Right ascension
23h 59m 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
08:30:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
250.467 km
Perigee altitude
235.422 km
Semi-major axis
6,621.081 km
Eccentricity
0.00114
Inclination
36.9369°
RAAN
359.8453°
Arg. of periapsis
60.304°
True anomaly
299.77385°
Mean anomaly
299.8868°
Eccentric anomaly
299.83033°
Mean motion
4.02856 °/min
Orbital period
89.36 mins
BSTAR
0.0043153
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Other satellites on launch #89 in the year 2019 (2019-12-11 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 PAPPY 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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