LEMUR 2 OBA-NI-JESU, 58902
Orbit data source: Space-Track
LEMUR 2 OBA-NI-JESU, 58902 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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58902 intel report (Beta)
LEMUR 2 OBA-NI-JESU details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 15 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 15 hours ago
0 LEMUR 2 OBA-NI-JESU
1 58902U 24022D 24356.09705406 .00025550 00000-0 99242-3 0 9991
2 58902 97.4585 194.9531 0009091 224.4576 135.5933 15.26018743 49262Epoch: 2024-12-21T02:19Z
Definitive object data (Epoch: 2024-12-21T02:19:45.47Z)
| Latitude | -0.00008° |
| Longitude | 69.86054° |
| Altitude | 495.288 km |
| Speed | 7.615 km/s |
| True Right ascension | 12h 59m 48s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -22.50826° |
| Longitude | -112.60648° |
| Altitude | 490.351 km |
| Speed | 7.622 km/s |
| Apparent Right ascension | 02h 22m 38s |
| Apparent Declination | -33° 37' 53" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 16:25:16 |
| Azimuth | 85.316° E |
| Elevation | -64.786° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 490.927 km |
| Perigee altitude | 478.449 km |
| Semi-major axis | 6,862.825 km |
| Eccentricity | 0.0009091 |
| Inclination | 97.4585° |
| RAAN | 194.9531° |
| Arg. of periapsis | 224.4576° |
| True anomaly | 135.66614° |
| Mean anomaly | 135.5933° |
| Eccentric anomaly | 135.62972° |
| Mean motion | 3.81759 °/min |
| BSTAR | 0.00099242 |
| Orbital period | 94.3 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 OBA-NI-JESU 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 02:29:39.737Z | 6.052° NNE | 2024-12-22 02:32:39.737Z | 281.739° WNW | 43.205° | 2024-12-22 02:35:39.737Z | 201.401° SSW |
| 5 mins | 2024-12-22 13:05:39.737Z | 133.247° SE | 2024-12-22 13:07:39.737Z | 84.984° E | 31.197° | 2024-12-22 13:10:39.737Z | 8.852° NNE |
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