KANOPUS-V 6, 43877
Orbit data source: Space-Track
KANOPUS-V 6, 43877 is a payload satellite owned by VNIIEM (CIS) in SSO that was launched on Thu, 27 Dec 2018 UTC via a SOYUZ-2-1A launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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43877 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEM
Mission
Operational Civil Imaging
Bus & Motor
KANOPUS, Unknown motor
Mass
473 kg wet, 473 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
1.665 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 KANOPUS-V 6
1 43877U 18111B 25260.99107554 .00005155 00000-0 16381-3 0 9994
2 43877 97.3729 172.2311 0002174 95.6336 264.5154 15.33074696373713Epoch: 2025-09-17T23:47Z
TLE epoch observation values (Epoch: 2025-09-17T23:47:08.926Z)
Latitude
-0.00006°
Longitude
178.28483°
Altitude
469.897 km
Speed
7.631 km/s
True Right ascension
11h 28m 55s
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
21:59:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.08 km
Perigee altitude
462.105 km
Semi-major axis
6,841.729 km
Eccentricity
0.00022
Inclination
97.3729°
RAAN
172.2311°
Arg. of periapsis
95.6336°
True anomaly
264.4906°
Mean anomaly
264.5154°
Eccentric anomaly
264.503°
Mean motion
3.83526 °/min
Orbital period
93.87 mins
BSTAR
0.00016381
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Other satellites on launch #111 in the year 2018 (2018-12-27 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.KANOPUS-V 6 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 | 2025-09-18 06:37:20.785Z | 35.482° NE | 2025-09-18 06:39:20.785Z | 80.023° E | 30.104° | 2025-09-18 06:42:20.785Z | 162.734° S |
| 5 mins | 2025-09-18 18:43:20.785Z | 208.821° SW | 2025-09-18 18:45:20.785Z | 265.794° W | 28.654° | 2025-09-18 18:48:20.785Z | 327.986° 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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