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). Payloads include a variety of satellites, spacecraft, and rockets 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)
No 3D visualization available: RSO Decayed
LEMUR 2 RAMONAMAE details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 5 months ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 0.8 m |
| Radar Cross Section | 0.077 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 5 months 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
Definitive object data (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 | Object was in full shadow at TLE epoch |
Predictive object data (real-time)
| Latitude | Unknown |
| Longitude | Unknown |
| Altitude | Unknown |
| Speed | Unknown |
| Apparent Right ascension | Unknown |
| Apparent Declination | Unknown |
| Sunlit | Unknown |
Predictive observer data (real-time)
| Local Sidereal Time | 02:49:54 |
| Azimuth | Unknown |
| Elevation | Unknown |
| Doppler factor | Unknown |
Orbital elements
| Apogee | 166.25 km |
| Perigee | 146.161 km |
| Semi-major axis | 6,534.342 km |
| Eccentricity | 0.0015372 |
| 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 |
| BSTAR | 0.00037929 |
| Period | 87.61 mins |
No data available
No data available
Other satellites on launch #2 in the year 2022 (2022-01-13 UTC)
LEMUR 2 RAMONAMAE Visibility forecast
Observer location: 39.9160978°, -105.1181434
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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