RESURS P1, 39186 (Decayed)
Orbit data source: Space-Track
RESURS P1, 39186 was a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Tue, 25 Jun 2013 UTC via a SOYUZ-2-1B 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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39186 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
TSSKBP?
Mission
Decayed Civil Imaging
Bus & Motor
RESURS P, Unknown motor
Mass
5,691 kg wet, ~5,600 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 6.5 m
Radar Cross Section
27.080 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 RESURS P1
1 39186U 13030A 24322.87932346 .19438957 23624-5 15676-3 0 9995
2 39186 96.9560 16.4419 0007950 262.9077 216.9341 16.52387254639808Epoch: 2024-11-17T21:06Z
TLE epoch observation values (Epoch: 2024-11-17T21:06:13.546Z)
Latitude
59.59066°
Longitude
-165.59906°
Altitude
147.405 km
Speed
7.821 km/s
True Right ascension
13h 53m 28s
True Declination
59° 25' 34"
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
13:12:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
135.003 km
Perigee altitude
124.655 km
Semi-major axis
6,507.966 km
Eccentricity
0.0008
Inclination
96.956°
RAAN
16.4419°
Arg. of periapsis
262.9077°
True anomaly
216.8794°
Mean anomaly
216.9341°
Eccentric anomaly
216.90675°
Mean motion
4.13405 °/min
Orbital period
87.08 mins
BSTAR
0.00015676
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Other satellites on launch #30 in the year 2013 (2013-06-25 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.RESURS P1 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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