LEMUR 2 NIMBUS2000, 58899
Orbit data source: Space-Track
LEMUR 2 NIMBUS2000, 58899 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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58899 intel report (Beta)
LEMUR 2 NIMBUS2000 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 23 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 23 hours ago
0 LEMUR 2 NIMBUS2000
1 58899U 24022A 24364.80588340 .00021175 00000-0 93796-3 0 9997
2 58899 97.4587 202.6498 0012463 211.2832 148.7663 15.21588265 50527Epoch: 2024-12-29T19:20Z
Definitive object data (Epoch: 2024-12-29T19:20:28.325Z)
| Latitude | -0.00009° |
| Longitude | 173.79485° |
| Altitude | 511.476 km |
| Speed | 7.604 km/s |
| True Right ascension | 13h 30m 35s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 57.38636° |
| Longitude | 6.46978° |
| Altitude | 510.009 km |
| Speed | 7.615 km/s |
| Apparent Right ascension | 04h 13m 06s |
| Apparent Declination | 12° 15' 11" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 17:36:31 |
| Azimuth | 24.922° NE |
| Elevation | -34.349° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 506.585 km |
| Perigee altitude | 489.446 km |
| Semi-major axis | 6,876.152 km |
| Eccentricity | 0.0012463 |
| Inclination | 97.4587° |
| RAAN | 202.6498° |
| Arg. of periapsis | 211.2832° |
| True anomaly | 148.84026° |
| Mean anomaly | 148.7663° |
| Eccentric anomaly | 148.80329° |
| Mean motion | 3.80649 °/min |
| BSTAR | 0.00093796 |
| Orbital period | 94.58 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 NIMBUS2000 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 | 2024-12-31 01:53:20.141Z | 27.692° NE | 2024-12-31 01:56:20.141Z | 81.876° E | 32.208° | 2024-12-31 01:59:20.141Z | 164.512° S |
| 5 mins | 2024-12-31 14:05:20.141Z | 211.921° SW | 2024-12-31 14:07:20.141Z | 256.131° W | 25.608° | 2024-12-31 14:10:20.141Z | 320.687° NNW |
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