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 | 16 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 16 hours ago
0 LEMUR 2 NIMBUS2000
1 58899U 24022A 24348.03279676 .00013835 00000-0 62547-3 0 9997
2 58899 97.4606 186.0283 0012442 276.2611 83.7207 15.20983405 47970Epoch: 2024-12-13T00:47Z
Definitive object data (Epoch: 2024-12-13T00:47:13.64Z)
| Latitude | -0.00001° |
| Longitude | 92.01687° |
| Altitude | 505.037 km |
| Speed | 7.612 km/s |
| True Right ascension | 12h 24m 06s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -29.51773° |
| Longitude | 96.89156° |
| Altitude | 509.235 km |
| Speed | 7.611 km/s |
| Apparent Right ascension | 09h 04m 43s |
| Apparent Declination | -66° 00' 23" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 14:57:42 |
| Azimuth | 209.834° SW |
| Elevation | -35.216° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 508.397 km |
| Perigee altitude | 491.282 km |
| Semi-major axis | 6,877.977 km |
| Eccentricity | 0.0012442 |
| Inclination | 97.4606° |
| RAAN | 186.0283° |
| Arg. of periapsis | 276.2611° |
| True anomaly | 83.86244° |
| Mean anomaly | 83.7207° |
| Eccentric anomaly | 83.79157° |
| Mean motion | 3.80498 °/min |
| BSTAR | 0.00062547 |
| 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 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 | 2024-12-14 02:36:47.139Z | 356.957° N | 2024-12-14 02:39:47.139Z | 271.057° WNW | 36.904° | 2024-12-14 02:42:47.139Z | 211.567° SW |
| 5 mins | 2024-12-14 13:14:47.139Z | 147.072° SSE | 2024-12-14 13:16:47.139Z | 83.117° E | 40.24° | 2024-12-14 13:19:47.139Z | 358.716° N |
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