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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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: 11 hours ago
TLE from 11 hours ago
0 NORBI
1 46494U 20068J 26071.99935824 .00027563 00000-0 60064-3 0 9990
2 46494 97.8697 79.7786 0005289 232.4886 127.5881 15.44224666301349Epoch: 2026-03-12T23:59Z
TLE epoch observation values (Epoch: 2026-03-12T23:59:04.551Z)
Latitude
-0.00001°
Longitude
-90.63155°
Altitude
438.966 km
Speed
7.647 km/s
True Right ascension
05h 19m 06s
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
15:23:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.213 km
Perigee altitude
427.01 km
Semi-major axis
6,808.748 km
Eccentricity
0.00053
Inclination
97.8697°
RAAN
79.7786°
Arg. of periapsis
232.4886°
True anomaly
127.63611°
Mean anomaly
127.5881°
Eccentric anomaly
127.61211°
Mean motion
3.86316 °/min
Orbital period
93.19 mins
BSTAR
0.00060064
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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 | 2026-03-13 12:59:38.297Z | 33.698° NE | 2026-03-13 13:01:38.297Z | 82.955° E | 32.206° | 2026-03-13 13:04:38.297Z | 168.635° S |
| 4 mins | 2026-03-14 01:00:38.297Z | 216.352° SW | 2026-03-14 01:02:38.297Z | 278.723° WNW | 25.433° | 2026-03-14 01:04:38.297Z | 320.64° NNW |
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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