KANOPUS-V 4, 43181
Orbit data source: Space-Track
KANOPUS-V 4, 43181 is a payload satellite owned by VNIIEM (CIS) in SSO that was launched on Thu, 01 Feb 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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43181 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
490 kg wet, 490 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: 13 hours ago
TLE from 13 hours ago
0 KANOPUS-V 4
1 43181U 18014B 25256.78525894 -.00000113 00000-0 -19292-5 0 9994
2 43181 97.3693 162.7030 0001644 87.6474 272.4951 15.22804419422662Epoch: 2025-09-13T18:50Z
TLE epoch observation values (Epoch: 2025-09-13T18:50:46.372Z)
Latitude
-0.00001°
Longitude
-113.00385°
Altitude
500.432 km
Speed
7.614 km/s
True Right ascension
10h 50m 48s
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
00:45:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.477 km
Perigee altitude
493.217 km
Semi-major axis
6,872.484 km
Eccentricity
0.00016
Inclination
97.3693°
RAAN
162.703°
Arg. of periapsis
87.6474°
True anomaly
272.47628°
Mean anomaly
272.4951°
Eccentric anomaly
272.48569°
Mean motion
3.80954 °/min
Orbital period
94.5 mins
BSTAR
-0.0000019292
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Other satellites on launch #14 in the year 2018 (2018-02-01 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 4 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 | 2025-09-14 17:04:09.477Z | 118.021° SE | 2025-09-14 17:07:09.477Z | 59.351° ENE | 19.61° | 2025-09-14 17:09:09.477Z | 23.333° NE |
| 4 mins | 2025-09-14 18:39:09.477Z | 237.505° WSW | 2025-09-14 18:40:09.477Z | 260.593° W | 20.264° | 2025-09-14 18:43:09.477Z | 316.7° NNW |
| 4 mins | 2025-09-15 06:08:09.477Z | 59.814° ENE | 2025-09-15 06:09:09.477Z | 87.369° E | 26.183° | 2025-09-15 06:12:09.477Z | 155.341° SSE |
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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