DECAYED
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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.

Not visible in the next 10 days
Identifier
55037, 2023-001AE
Orbit
Decayed
Last TLE update
11 months ago
Origin
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)
2023-01-03 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.7 m
Radar Cross Section
0.054 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 11 months 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 77692
Epoch: 2024-05-23T20:05Z
Definitive object data (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
Object was in full shadow at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
156.04 km
Perigee altitude
139.432 km
Semi-major axis
6,525.873 km
Eccentricity
0.0012725
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
BSTAR
0.0004101
Orbital period
87.44 mins
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LEMUR 2 EMMACULATE Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed
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