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.
Focus sentinelFocus sentinel
58903 intel report (Beta)
LEMUR 2 CAEL details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 6 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 6 hours ago
0 LEMUR 2 CAEL
1 58903U 24022E 24356.49632156 .00015792 00000-0 69312-3 0 9999
2 58903 97.4595 194.7387 0010570 221.7272 138.3159 15.21985769 49287Epoch: 2024-12-21T11:54Z
Definitive object data (Epoch: 2024-12-21T11:54:42.182Z)
| Latitude | -0.00002° |
| Longitude | -74.4837° |
| Altitude | 508.377 km |
| Speed | 7.607 km/s |
| True Right ascension | 12h 58m 57s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 4.66395° |
| Longitude | 106.35229° |
| Altitude | 497.356 km |
| Speed | 7.619 km/s |
| Apparent Right ascension | 02h 26m 36s |
| Apparent Declination | -18° 18' 07" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 16:27:25 |
| Azimuth | 59.119° ENE |
| Elevation | -56.183° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 504.084 km |
| Perigee altitude | 489.55 km |
| Semi-major axis | 6,874.954 km |
| Eccentricity | 0.001057 |
| Inclination | 97.4595° |
| RAAN | 194.7387° |
| Arg. of periapsis | 221.7272° |
| True anomaly | 138.39637° |
| Mean anomaly | 138.3159° |
| Eccentric anomaly | 138.35614° |
| Mean motion | 3.80749 °/min |
| BSTAR | 0.00069312 |
| Orbital period | 94.55 mins |
Loading maneuver chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
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 | 2024-12-22 02:39:48.620Z | 359.071° N | 2024-12-22 02:42:48.620Z | 309.344° NW | 34.329° | 2024-12-22 02:45:48.620Z | 217.851° SW |
| 6 mins | 2024-12-22 13:17:48.620Z | 151.468° SSE | 2024-12-22 13:19:48.620Z | 109.178° ESE | 39.957° | 2024-12-22 13:23:48.620Z | 355.244° N |
Authenticating...
Click to sort rows by NORAD ID header in ascending order | Click to sort rows by Common name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
|---|