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 | 14 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 14 hours ago
0 LEMUR 2 OBA-NI-JESU
1 58902U 24022D 24316.98702285 .00031585 00000-0 13097-2 0 9995
2 58902 97.4629 155.9810 0011734 10.2542 349.8932 15.23755370 43308
Epoch: 2024-11-11T23:41Z
Definitive object data (Epoch: 2024-11-11T23:41:18.774Z)
Latitude | -0.00002° |
Longitude | 109.04837° |
Altitude | 489.678 km |
Speed | 7.625 km/s |
True Right ascension | 10h 23m 55s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -73.86063° |
Longitude | 136.37809° |
Altitude | 520.573 km |
Speed | 7.602 km/s |
Apparent Right ascension | 20h 49m 51s |
Apparent Declination | -72° 04' 55" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 10:00:45 |
Azimuth | 170.191° S |
Elevation | -56.648° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 499.549 km |
Perigee altitude | 483.428 km |
Semi-major axis | 6,869.626 km |
Eccentricity | 0.0011734 |
Inclination | 97.4629° |
RAAN | 155.981° |
Arg. of periapsis | 10.2542° |
True anomaly | 349.86957° |
Mean anomaly | 349.8932° |
Eccentric anomaly | 349.88139° |
Mean motion | 3.81192 °/min |
BSTAR | 0.0013097 |
Orbital period | 94.44 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 | 2024-11-12 13:59:32.381Z | 196.718° SSW | 2024-11-12 14:02:32.381Z | 257.971° W | 29.088° | 2024-11-12 14:05:32.381Z | 325.907° NNW |
4 mins | 2024-11-13 03:03:32.381Z | 323.321° NNW | 2024-11-13 03:04:32.381Z | 299.587° NW | 22.608° | 2024-11-13 03:07:32.381Z | 236.892° WSW |
Authenticating...
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