LEMUR 2 MMOLO, 55038 (Decayed)
Orbit data source: Space-Track
LEMUR 2 MMOLO, 55038 was a payload satellite owned by Spire/Lux (US) 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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55038 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
4.6 kg wet, 4.6 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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 LEMUR 2 MMOLO
1 55038U 23001AF 24293.80668559 .07326636 24760-5 19423-2 0 9992
2 55038 97.3876 6.5032 0009280 264.8961 95.1273 16.28341207100523Epoch: 2024-10-19T19:21Z
TLE epoch observation values (Epoch: 2024-10-19T19:21:37.634Z)
Latitude
-0.00007°
Longitude
47.33963°
Altitude
200.789 km
Speed
7.786 km/s
True Right ascension
00h 26m 00s
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
199.922 km
Perigee altitude
187.725 km
Semi-major axis
6,571.961 km
Eccentricity
0.00093
Inclination
97.3876°
RAAN
6.5032°
Arg. of periapsis
264.8961°
True anomaly
95.2332°
Mean anomaly
95.1273°
Eccentric anomaly
95.18025°
Mean motion
4.07381 °/min
Orbital period
88.37 mins
BSTAR
0.0019423
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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)
LEMUR 2 MMOLO 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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