OBJECT DF, 58696 (Decayed)
Orbit data source: Space-Track
OBJECT DF, 58696 was a satellite in LEO that was launched on Sat, 11 Nov 2023 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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58696 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Microgravity
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 OBJECT DF
1 58696U 23174DF 25148.35653433 .06249216 23503-5 11407-2 0 9996
2 58696 97.1456 224.2269 0014292 256.8233 103.1468 16.32119036 79902Epoch: 2025-05-28T08:33Z
TLE epoch observation values (Epoch: 2025-05-28T08:33:24.566Z)
Latitude
-0.00005°
Longitude
-150.2666°
Altitude
192.247 km
Speed
7.79 km/s
True Right ascension
14h 56m 54s
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
14:23:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
193.036 km
Perigee altitude
174.28 km
Semi-major axis
6,561.795 km
Eccentricity
0.00143
Inclination
97.1456°
RAAN
224.2269°
Arg. of periapsis
256.8233°
True anomaly
103.30622°
Mean anomaly
103.1468°
Eccentric anomaly
103.22651°
Mean motion
4.08328 °/min
Orbital period
88.16 mins
BSTAR
0.0011407
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Other satellites on launch #174 in the year 2023 (2023-11-11 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 DF 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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