KANOPUS-V-IK, 42825
Orbit data source: Space-Track
KANOPUS-V-IK, 42825 is a payload satellite owned by VNIIEM (CIS) in SSO that was launched on Fri, 14 Jul 2017 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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42825 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
550 kg wet, 550 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: 16 hours ago
TLE from 16 hours ago
0 KANOPUS-V-IK
1 42825U 17042A 25349.00328497 .00002984 00000-0 12777-3 0 9991
2 42825 97.3686 253.0931 0002000 83.4138 276.7327 15.23564128467338Epoch: 2025-12-15T00:04Z
TLE epoch observation values (Epoch: 2025-12-15T00:04:43.821Z)
Latitude
0°
Longitude
168.00242°
Altitude
498.036 km
Speed
7.616 km/s
True Right ascension
16h 52m 22s
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
15:11:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.434 km
Perigee altitude
490.686 km
Semi-major axis
6,870.197 km
Eccentricity
0.0002
Inclination
97.3686°
RAAN
253.0931°
Arg. of periapsis
83.4138°
True anomaly
276.70994°
Mean anomaly
276.7327°
Eccentric anomaly
276.72132°
Mean motion
3.81144 °/min
Orbital period
94.45 mins
BSTAR
0.00012777
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Other satellites on launch #42 in the year 2017 (2017-07-14 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-IK 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-15 17:32:41.521Z | 150.104° SSE | 2025-12-15 17:35:41.521Z | 83.807° E | 38.21° | 2025-12-15 17:38:41.521Z | 0.995° NNE |
| 5 mins | 2025-12-16 06:36:41.521Z | 17.673° NNE | 2025-12-16 06:38:41.521Z | 163.756° S | 43.317° | 2025-12-16 06:41:41.521Z | 189.339° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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