OBJECT R, 59113 (Decayed)
Orbit data source: Space-Track
OBJECT R, 59113 was a satellite in LEO that was launched on Mon, 04 Mar 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.
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59113 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.0 m
Radar Cross Section
0.004 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 OBJECT R
1 59113U 24043R 25355.90708954 .02204764 24632-5 13185-2 0 9991
2 59113 97.4933 142.9432 0005613 319.0070 41.0795 16.18437974101105Epoch: 2025-12-21T21:46Z
TLE epoch observation values (Epoch: 2025-12-21T21:46:12.536Z)
Latitude
-0.00002°
Longitude
85.67816°
Altitude
224.223 km
Speed
7.774 km/s
True Right ascension
09h 31m 46s
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
08:12:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
224.34 km
Perigee altitude
216.932 km
Semi-major axis
6,598.773 km
Eccentricity
0.00056
Inclination
97.4933°
RAAN
142.9432°
Arg. of periapsis
319.007°
True anomaly
41.12179°
Mean anomaly
41.0795°
Eccentric anomaly
41.10064°
Mean motion
4.04901 °/min
Orbital period
88.91 mins
BSTAR
0.0013185
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.OBJECT R 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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