OBJECT F, 62614 (Decayed)
Orbit data source: Space-Track
OBJECT F, 62614 was a satellite in LEO that was launched on Tue, 14 Jan 2025 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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62614 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Amateur Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 OBJECT F
1 62614U 25009F 26095.97728757 .16455444 25422-5 51905-3 0 9995
2 62614 97.3587 188.5500 0016550 268.6986 91.2419 16.43244871 68571Epoch: 2026-04-05T23:27Z
TLE epoch observation values (Epoch: 2026-04-05T23:27:17.646Z)
Latitude
-0.00002°
Longitude
2.45151°
Altitude
160.694 km
Speed
7.81 km/s
True Right ascension
12h 34m 12s
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
10:18:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
164.797 km
Perigee altitude
143.176 km
Semi-major axis
6,532.123 km
Eccentricity
0.00166
Inclination
97.3587°
RAAN
188.55°
Arg. of periapsis
268.6986°
True anomaly
91.4315°
Mean anomaly
91.2419°
Eccentric anomaly
91.3367°
Mean motion
4.11113 °/min
Orbital period
87.57 mins
BSTAR
0.00051905
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Other satellites on launch #9 in the year 2025 (2025-01-14 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 F 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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