RESURS P1 DEB, 60220 (Decayed)
Orbit data source: Space-Track
RESURS P1 DEB, 60220 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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60220 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 RESURS P1 DEB
1 60220U 13030J 24209.57598156 .16467769 22127-5 22649-2 0 9990
2 60220 96.8745 259.3178 0020829 274.9624 84.9296 16.34480138 4809
Epoch: 2024-07-27T13:49Z
TLE epoch observation values (Epoch: 2024-07-27T13:49:24.806Z)
Latitude
-0.00005°
Longitude
106.22945°
Altitude
182.607 km
Speed
7.797 km/s
True Right ascension
17h 17m 16s
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
00:07:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
190.974 km
Perigee altitude
163.665 km
Semi-major axis
6,555.456 km
Eccentricity
0.00208
Inclination
96.8745°
RAAN
259.3178°
Arg. of periapsis
274.9624°
True anomaly
85.1674°
Mean anomaly
84.9296°
Eccentric anomaly
85.0485°
Mean motion
4.0892 °/min
Orbital period
88.04 mins
BSTAR
0.0022649
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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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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