LEMUR 2 VALHALLA, 58900
Orbit data source: Space-Track
LEMUR 2 VALHALLA, 58900 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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58900 intel report (Beta)
LEMUR 2 VALHALLA details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 1 day 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 1 day ago
0 LEMUR 2 VALHALLA
1 58900U 24022B 24347.54670966 .00013203 00000-0 59573-3 0 9996
2 58900 97.4606 185.6041 0012638 275.2104 84.7689 15.21058298 47905Epoch: 2024-12-12T13:07Z
Definitive object data (Epoch: 2024-12-12T13:07:15.714Z)
| Latitude | -0.00006° |
| Longitude | -92.93685° |
| Altitude | 504.955 km |
| Speed | 7.612 km/s |
| True Right ascension | 12h 22m 24s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 45.07924° |
| Longitude | -99.32487° |
| Altitude | 515.513 km |
| Speed | 7.607 km/s |
| Apparent Right ascension | 07h 17m 12s |
| Apparent Declination | 12° 59' 14" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 14:40:29 |
| Azimuth | 293.425° NW |
| Elevation | -6.975° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 508.306 km |
| Perigee altitude | 490.922 km |
| Semi-major axis | 6,877.751 km |
| Eccentricity | 0.0012638 |
| Inclination | 97.4606° |
| RAAN | 185.6041° |
| Arg. of periapsis | 275.2104° |
| True anomaly | 84.91314° |
| Mean anomaly | 84.7689° |
| Eccentric anomaly | 84.84102° |
| Mean motion | 3.80517 °/min |
| BSTAR | 0.00059573 |
| Orbital period | 94.61 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 VALHALLA 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 | 2024-12-14 01:59:37.434Z | 23.71° NE | 2024-12-14 02:02:37.434Z | 75.806° E | 36.451° | 2024-12-14 02:05:37.434Z | 171.237° S |
| 4 mins | 2024-12-14 14:12:37.434Z | 229.081° WSW | 2024-12-14 14:14:37.434Z | 277.403° WNW | 21.523° | 2024-12-14 14:16:37.434Z | 314.138° NW |
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