RESURS P2, 40360 (Decayed)
Orbit data source: Space-Track
RESURS P2, 40360 was a payload satellite owned by TsSKB-Progress (CIS) in LEO that was launched on Fri, 26 Dec 2014 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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Identifier
Orbit
Country
CISRelated business
Manufacturer
TSSKBP?
Mission
Decayed Civil Imaging
Bus & Motor
RESURS P, Unknown motor
Mass
6,392 kg wet, ~5,900 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: 1 year ago
TLE from 1 year ago
0 RESURS P2
1 40360U 14087A 25042.79256236 .13998004 24186-5 12028-3 0 9992
2 40360 97.0926 143.0833 0008357 269.3569 218.5177 16.51917227568846Epoch: 2025-02-11T19:01Z
TLE epoch observation values (Epoch: 2025-02-11T19:01:17.387Z)
Latitude
51.73425°
Longitude
-95.30829°
Altitude
147.04 km
Speed
7.82 km/s
True Right ascension
22h 08m 25s
True Declination
51° 33' 04"
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
03:48:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
136.51 km
Perigee altitude
125.631 km
Semi-major axis
6,509.207 km
Eccentricity
0.00084
Inclination
97.0926°
RAAN
143.0833°
Arg. of periapsis
269.3569°
True anomaly
218.45811°
Mean anomaly
218.5177°
Eccentric anomaly
218.4879°
Mean motion
4.13286 °/min
Orbital period
87.11 mins
BSTAR
0.00012028
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Other satellites on launch #87 in the year 2014 (2014-12-26 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 P2 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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