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, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 NORBI
1 46494U 20068J 26305.16515359 .00016112 00000-0 24909-3 0 9992
2 46494 97.8533 333.7549 0007065 109.4047 250.7969 15.54160649337441Epoch: 2026-11-01T03:57Z
TLE epoch observation values (Epoch: 2026-11-01T03:57:49.270Z)
Latitude
-0.00004°
Longitude
-126.16083°
Altitude
409.296 km
Speed
7.664 km/s
True Right ascension
22h 15m 01s
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
04:41:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
406.324 km
Perigee altitude
396.744 km
Semi-major axis
6,779.671 km
Eccentricity
0.00071
Inclination
97.8533°
RAAN
333.7549°
Arg. of periapsis
109.4047°
True anomaly
250.72047°
Mean anomaly
250.7969°
Eccentric anomaly
250.75868°
Mean motion
3.88804 °/min
Orbital period
92.59 mins
BSTAR
0.00024909
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-01 15:20:23.383Z | 349.259° N | 2026-11-01 15:22:23.383Z | 290.457° WNW | 38.072° | 2026-11-01 15:24:23.383Z | 225.543° WSW |
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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