LEMUR 2 EMMACULATE, 55037 (Decayed)
Orbit data source: Space-Track
LEMUR 2 EMMACULATE, 55037 was an American payload satellite in LEO that was launched on Tue, 03 Jan 2023 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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55037 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
8.3 kg wet, 8.1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.054 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 LEMUR 2 EMMACULATE
1 55037U 23001AE 24144.83707817 .18410834 25877-5 41010-3 0 9994
2 55037 97.4040 216.6886 0012725 265.0585 94.9264 16.45604697 77692Epoch: 2024-05-23T20:05Z
TLE epoch observation values (Epoch: 2024-05-23T20:05:23.553Z)
Latitude
-0.00012°
Longitude
33.41521°
Altitude
154.918 km
Speed
7.813 km/s
True Right ascension
14h 26m 45s
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
03:12:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
156.04 km
Perigee altitude
139.432 km
Semi-major axis
6,525.873 km
Eccentricity
0.00127
Inclination
97.404°
RAAN
216.6886°
Arg. of periapsis
265.0585°
True anomaly
95.07166°
Mean anomaly
94.9264°
Eccentric anomaly
94.99903°
Mean motion
4.11704 °/min
Orbital period
87.44 mins
BSTAR
0.0004101
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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)
LEMUR 2 EMMACULATE Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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