SPRITE-SAT (RISING), 33494
Orbit data source: Space-Track
SPRITE-SAT (RISING), 33494 is a payload satellite owned by Tohoku (JP) in SSO that was launched on Fri, 23 Jan 2009 UTC via an H-IIA 202 launch vehicle from the Tanegashima Space Center (TNSTA). 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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SPRITE-SAT (RISING) details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 10 hours ago |
| Origin | |
| Manufacturer | Tohoku |
| Mission | Civil Technology |
| Bus & Motor | SPRITESAT, Unknown motor |
| Mass | 20 kg wet, 20 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 1 Ant, 0.4 m |
| Radar Cross Section | 0.200 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 10 hours ago
0 SPRITE-SAT (RISING)
1 33494U 09002C 24279.54024812 .00004224 00000-0 65411-3 0 9996
2 33494 98.2028 167.6302 0003664 157.4899 202.6469 14.73752599842488Epoch: 2024-10-05T12:57Z
Definitive object data (Epoch: 2024-10-05T12:57:57.437Z)
| Latitude | -0.00013° |
| Longitude | -41.5542° |
| Altitude | 654.494 km |
| Speed | 7.529 km/s |
| True Right ascension | 11h 10m 31s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | 64.66919° |
| Longitude | 156.51044° |
| Altitude | 658.332 km |
| Speed | 7.535 km/s |
| Apparent Right ascension | 03h 29m 10s |
| Apparent Declination | 19° 20' 50" |
| Sunlit | Object is in full shadow |
Predictive observer data (real-time)
| Local Sidereal Time | 17:15:32 |
| Azimuth | 27.965° NE |
| Elevation | -25.756° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 648.75 km |
| Perigee | 643.603 km |
| Semi-major axis | 7,024.314 km |
| Eccentricity | 0.0003664 |
| Inclination | 98.2028° |
| RAAN | 167.6302° |
| Arg. of periapsis | 157.4899° |
| True anomaly | 202.63074° |
| Mean anomaly | 202.6469° |
| Eccentric anomaly | 202.63882° |
| Mean motion | 3.6867 °/min |
| BSTAR | 0.00065411 |
| Period | 97.65 mins |
No data available
No data available
Other satellites on launch #2 in the year 2009 (2009-01-23 UTC)
SPRITE-SAT (RISING) Visibility forecast
Observer location: 39.9160978°, -105.1181434
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. |
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