KANOPUS-V 1, 38707 (Decayed)
Orbit data source: Space-Track
KANOPUS-V 1, 38707 was a payload satellite owned by VNIIEM (CIS) in LEO that was launched on Sun, 22 Jul 2012 UTC via a SOYUZ-FG 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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38707 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEM
Mission
Decayed Civil Imaging
Bus & Motor
KANOPUS, Unknown motor
Mass
400 kg wet, 400 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: 10 months ago
TLE from 10 months ago
0 KANOPUS-V 1
1 38707U 12039A 24323.81578493 .08695980 26821-5 76758-3 0 9994
2 38707 97.4797 272.4019 0006631 150.5746 270.1213 16.39248839685412Epoch: 2024-11-18T19:34Z
TLE epoch observation values (Epoch: 2024-11-18T19:34:43.817Z)
Latitude
59.8711°
Longitude
-92.61445°
Altitude
178.042 km
Speed
7.805 km/s
True Right ascension
17h 17m 36s
True Declination
59° 42' 30"
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
23:32:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
168.952 km
Perigee altitude
160.275 km
Semi-major axis
6,542.751 km
Eccentricity
0.00066
Inclination
97.4797°
RAAN
272.4019°
Arg. of periapsis
150.5746°
True anomaly
270.04531°
Mean anomaly
270.1213°
Eccentric anomaly
270.08331°
Mean motion
4.10112 °/min
Orbital period
87.78 mins
BSTAR
0.00076758
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Other satellites on launch #39 in the year 2012 (2012-07-22 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 1 Visibility
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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. |
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| This satellite is decayed. |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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