LEMUR 2 CAEL, 58903
Orbit data source: Space-Track
LEMUR 2 CAEL, 58903 is an American payload satellite in SSO that was launched on Wed, 31 Jan 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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58903 intel report (Beta)
LEMUR 2 CAEL details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 12 hours ago |
| Origin | |
| Manufacturer | Spire/Glasgow |
| Mission | Operational Commercial Early Warn |
| Bus & Motor | CUBESAT 3U, Unknown motor |
| Mass | ~25 kg wet, ~25 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 1 m |
| Radar Cross Section | 0.146 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 12 hours ago
0 LEMUR 2 CAEL
1 58903U 24022E 25037.54087199 .00016921 00000-0 70271-3 0 9994
2 58903 97.4586 241.4652 0012479 61.7922 298.4574 15.23827835 56442Epoch: 2025-02-06T12:58Z
Definitive object data (Epoch: 2025-02-06T12:58:51.339Z)
| Latitude | -0.00001° |
| Longitude | -90.16469° |
| Altitude | 493.322 km |
| Speed | 7.62 km/s |
| True Right ascension | 16h 05m 51s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -63.39818° |
| Longitude | -74.58514° |
| Altitude | 523.361 km |
| Speed | 7.598 km/s |
| Apparent Right ascension | 16h 06m 25s |
| Apparent Declination | -52° 35' 32" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 03:27:38 |
| Azimuth | 204.445° SW |
| Elevation | -75.69° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 499.843 km |
| Perigee altitude | 482.698 km |
| Semi-major axis | 6,869.407 km |
| Eccentricity | 0.0012479 |
| Inclination | 97.4586° |
| RAAN | 241.4652° |
| Arg. of periapsis | 61.7922° |
| True anomaly | 298.33159° |
| Mean anomaly | 298.4574° |
| Eccentric anomaly | 298.3945° |
| Mean motion | 3.8121 °/min |
| BSTAR | 0.00070271 |
| Orbital period | 94.44 mins |
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Other satellites on launch #22 in the year 2024 (2024-01-31 UTC)
| LEMUR 2 NIMBUS2000, 58899 |
| LEMUR 2 VALHALLA, 58900 |
| ELECTRON KICK STAGE R/B, 58901 |
| LEMUR 2 OBA-NI-JESU, 58902 |
| LEMUR 2 CAEL, 58903 |
| ELECTRON R/B, 58904 (Decayed) |
LEMUR 2 CAEL 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-02-07 02:09:25.981Z | 22.727° NE | 2025-02-07 02:12:25.981Z | 135.515° SSE | 39.735° | 2025-02-07 02:15:25.981Z | 181.677° SSW |
| 4 mins | 2025-02-07 14:20:25.981Z | 232.335° WSW | 2025-02-07 14:22:25.981Z | 276.407° WNW | 18.368° | 2025-02-07 14:24:25.981Z | 311.648° NW |
Authenticating...
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