OBJECT P, 59111 (Decayed)
Orbit data source: Space-Track
OBJECT P, 59111 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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59111 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 P
1 59111U 24043P 25362.11879174 .14029753 26033-5 24723-3 0 9997
2 59111 97.4892 149.6618 0008805 285.7146 74.3186 16.47369876102073Epoch: 2025-12-28T02:51Z
TLE epoch observation values (Epoch: 2025-12-28T02:51:03.606Z)
Latitude
0.00004°
Longitude
10.06141°
Altitude
147.981 km
Speed
7.818 km/s
True Right ascension
09h 58m 38s
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
02:14:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
148.815 km
Perigee altitude
137.331 km
Semi-major axis
6,521.21 km
Eccentricity
0.00088
Inclination
97.4892°
RAAN
149.6618°
Arg. of periapsis
285.7146°
True anomaly
74.41577°
Mean anomaly
74.3186°
Eccentric anomaly
74.36718°
Mean motion
4.12146 °/min
Orbital period
87.35 mins
BSTAR
0.00024723
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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 P 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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