RESURS P1 DEB, 60215 (Decayed)
Orbit data source: Space-Track
RESURS P1 DEB, 60215 was space debris in LEO originally from a Commonwealth of Independent States-origin launch on Tue, 25 Jun 2013 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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60215 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
TSSKBP?
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 RESURS P1 DEB
1 60215U 13030D 24201.02269827 .22006651 22682-5 23266-2 0 9994
2 60215 96.9439 251.2101 0017045 281.4061 78.5323 16.37163983 3498Epoch: 2024-07-19T00:32Z
TLE epoch observation values (Epoch: 2024-07-19T00:32:41.13Z)
Latitude
-0.00007°
Longitude
-54.26574°
Altitude
174.416 km
Speed
7.803 km/s
True Right ascension
16h 44m 50s
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
00:01:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
181.311 km
Perigee altitude
158.987 km
Semi-major axis
6,548.286 km
Eccentricity
0.0017
Inclination
96.9439°
RAAN
251.2101°
Arg. of periapsis
281.4061°
True anomaly
78.7238°
Mean anomaly
78.5323°
Eccentric anomaly
78.62804°
Mean motion
4.09592 °/min
Orbital period
87.89 mins
BSTAR
0.0023266
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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 DEB 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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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 ascending order |
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