RESURS P1 DEB, 60225 (Decayed)
Orbit data source: Space-Track
RESURS P1 DEB, 60225 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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60225 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 60225U 13030P 24209.39050849 .11687150 22258-5 21757-2 0 9994
2 60225 96.9385 259.7880 0018364 269.5974 90.3218 16.31687613 4582Epoch: 2024-07-27T09:22Z
TLE epoch observation values (Epoch: 2024-07-27T09:22:19.933Z)
Latitude
-0.00003°
Longitude
173.65276°
Altitude
191.352 km
Speed
7.791 km/s
True Right ascension
17h 19m 09s
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
00:03:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
196.859 km
Perigee altitude
172.755 km
Semi-major axis
6,562.944 km
Eccentricity
0.00184
Inclination
96.9385°
RAAN
259.788°
Arg. of periapsis
269.5974°
True anomaly
90.53223°
Mean anomaly
90.3218°
Eccentric anomaly
90.42702°
Mean motion
4.08221 °/min
Orbital period
88.19 mins
BSTAR
0.0021757
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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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