LEMUR 2 RAMONAMAE, 51021 (Decayed)
Orbit data source: Space-Track
LEMUR 2 RAMONAMAE, 51021 was an American payload satellite in LEO that was launched on Thu, 13 Jan 2022 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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51021 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, 0.4 m
Radar Cross Section
0.077 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 LEMUR 2 RAMONAMAE
1 51021U 22002AP 24150.09260637 .09842555 25473-5 37929-3 0 9997
2 51021 97.3749 233.9668 0015372 267.9703 91.9837 16.42409109132581Epoch: 2024-05-29T02:13Z
TLE epoch observation values (Epoch: 2024-05-29T02:13:21.19Z)
Latitude
-0.00005°
Longitude
-46.47685°
Altitude
163.02 km
Speed
7.808 km/s
True Right ascension
15h 35m 52s
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
10:53:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
166.25 km
Perigee altitude
146.161 km
Semi-major axis
6,534.342 km
Eccentricity
0.00154
Inclination
97.3749°
RAAN
233.9668°
Arg. of periapsis
267.9703°
True anomaly
92.15973°
Mean anomaly
91.9837°
Eccentric anomaly
92.07172°
Mean motion
4.10904 °/min
Orbital period
87.61 mins
BSTAR
0.00037929
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Other satellites on launch #2 in the year 2022 (2022-01-13 UTC)
LEMUR 2 RAMONAMAE 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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