NORBI, 46494
Orbit data source: Space-Track
NORBI, 46494 is a payload satellite owned by Novosibirsk SU (CIS) in SSO that was launched on Mon, 28 Sep 2020 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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46494 intel report (Beta)
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NORBI radio frequencies
NORBI details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 9 hours ago |
| Origin | |
| Manufacturer | Novosibirsk SU |
| Mission | Operational Amateur Science |
| Bus & Motor | CUBESAT 6U, Unknown motor |
| Mass | ~10 kg wet, ~10 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, Unknown HBR |
| Radar Cross Section | 0.035 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 NORBI
1 46494U 20068J 24361.18750659 .00021162 00000-0 85374-3 0 9992
2 46494 97.8395 329.9274 0012893 19.7503 340.4230 15.24756881233623Epoch: 2024-12-26T04:30Z
Definitive object data (Epoch: 2024-12-26T04:30:00.569Z)
| Latitude | -0.00003° |
| Longitude | 167.25453° |
| Altitude | 486.254 km |
| Speed | 7.627 km/s |
| True Right ascension | 21h 59m 42s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 24.12225° |
| Longitude | -8.85726° |
| Altitude | 501.023 km |
| Speed | 7.612 km/s |
| Apparent Right ascension | 06h 52m 18s |
| Apparent Declination | -20° 36' 38" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 12:24:55 |
| Azimuth | 249.818° W |
| Elevation | -8.065° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 497.347 km |
| Perigee altitude | 479.641 km |
| Semi-major axis | 6,866.631 km |
| Eccentricity | 0.0012893 |
| Inclination | 97.8395° |
| RAAN | 329.9274° |
| Arg. of periapsis | 19.7503° |
| True anomaly | 340.37342° |
| Mean anomaly | 340.423° |
| Eccentric anomaly | 340.39822° |
| Mean motion | 3.81441 °/min |
| BSTAR | 0.00085374 |
| Orbital period | 94.38 mins |
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Other satellites on launch #68 in the year 2020 (2020-09-28 UTC)
NORBI 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 | 2024-12-26 21:57:18.187Z | 152.235° SSE | 2024-12-26 22:00:18.187Z | 66.457° ENE | 40.319° | 2024-12-26 22:03:18.187Z | 356.879° N |
| 5 mins | 2024-12-27 11:00:18.187Z | 18.371° NNE | 2024-12-27 11:02:18.187Z | 144.392° SSE | 44.126° | 2024-12-27 11:05:18.187Z | 189.312° SSW |
Authenticating...
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