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). 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.
Focus sentinelFocus sentinel
55037 intel report (Beta)
Loading greatness...
LEMUR 2 EMMACULATE 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 | 8.3 kg wet, 8.1 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| 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 5 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 77692Epoch: 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
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee | 156.04 km |
| Perigee | 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 |
| Period | 87.44 mins |
Loading maneuver chart data...
Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)
LEMUR 2 EMMACULATE Visibility forecast
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. |
|---|