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). Payload-class satellites include a variety of spacecraft 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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Edit Public Description
Identifier
Orbit
Country
CISRelated business
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
Shape & HBR
Box + 2 Pan, Unknown HBR
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 NORBI
1 46494U 20068J 25288.91614664 .00026151 00000-0 74923-3 0 9998
2 46494 97.8665 280.6433 0011400 65.1780 295.0647 15.35836806278554Epoch: 2025-10-15T21:59Z
TLE epoch observation values (Epoch: 2025-10-15T21:59:15.069Z)
Latitude
-0.00001°
Longitude
-73.85285°
Altitude
458.239 km
Speed
7.64 km/s
True Right ascension
18h 42m 34s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
22:25:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.191 km
Perigee altitude
447.611 km
Semi-major axis
6,833.538 km
Eccentricity
0.00114
Inclination
97.8665°
RAAN
280.6433°
Arg. of periapsis
65.178°
True anomaly
294.9463°
Mean anomaly
295.0647°
Eccentric anomaly
295.00551°
Mean motion
3.84215 °/min
Orbital period
93.7 mins
BSTAR
0.00074923
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Other satellites on launch #68 in the year 2020 (2020-09-28 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NORBI Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-16 12:37:24.418Z | 4.051° NNE | 2025-10-16 12:39:24.418Z | 327.707° NNW | 40.588° | 2025-10-16 12:42:24.418Z | 204.107° SW |
| 4 mins | 2025-10-16 23:09:24.418Z | 126.114° SE | 2025-10-16 23:11:24.418Z | 62.222° ENE | 29.668° | 2025-10-16 23:13:24.418Z | 12.873° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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