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 | 5 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 5 hours ago
0 LEMUR 2 VALHALLA
1 58900U 24022B 24356.49274338 .00015811 00000-0 70669-3 0 9999
2 58900 97.4599 194.4689 0012535 240.6336 119.3648 15.21343166 49263Epoch: 2024-12-21T11:49Z
Definitive object data (Epoch: 2024-12-21T11:49:33.028Z)
| Latitude | -0.00003° |
| Longitude | -73.46183° |
| Altitude | 509.117 km |
| Speed | 7.607 km/s |
| True Right ascension | 12h 57m 52s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 2.4968° |
| Longitude | -73.59122° |
| Altitude | 509.22 km |
| Speed | 7.607 km/s |
| Apparent Right ascension | 09h 56m 39s |
| Apparent Declination | -40° 26' 07" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 15:36:49 |
| Azimuth | 234.562° WSW |
| Elevation | -21.453° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 507.375 km |
| Perigee altitude | 490.134 km |
| Semi-major axis | 6,876.892 km |
| Eccentricity | 0.0012535 |
| Inclination | 97.4599° |
| RAAN | 194.4689° |
| Arg. of periapsis | 240.6336° |
| True anomaly | 119.48989° |
| Mean anomaly | 119.3648° |
| Eccentric anomaly | 119.42735° |
| Mean motion | 3.80588 °/min |
| BSTAR | 0.00070669 |
| Orbital period | 94.59 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 | 2024-12-22 02:35:21.019Z | 0.155° NNE | 2024-12-22 02:38:21.019Z | 298.164° NW | 37.816° | 2024-12-22 02:41:21.019Z | 212.302° SW |
| 6 mins | 2024-12-22 13:13:21.019Z | 147.223° SSE | 2024-12-22 13:15:21.019Z | 102.085° ESE | 38.225° | 2024-12-22 13:19:21.019Z | 357.186° N |
Authenticating...
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