OBJECT Q, 43772 (Decayed)
Orbit data source: Space-Track
OBJECT Q, 43772 was a satellite in LEO that was launched on Mon, 03 Dec 2018 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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43772 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Manufacturer
GaTech
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 1.5U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.025 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 Q
1 43772U 18099Q 26182.81231119 .08872736 25300-5 91617-3 0 9998
2 43772 97.3932 266.0295 0016550 265.7852 94.1554 16.37399568417018Epoch: 2026-07-01T19:29Z
TLE epoch observation values (Epoch: 2026-07-01T19:29:43.686Z)
Latitude
-0.00012°
Longitude
53.73381°
Altitude
176.781 km
Speed
7.8 km/s
True Right ascension
17h 44m 07s
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
02:28:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
180.376 km
Perigee altitude
158.703 km
Semi-major axis
6,547.677 km
Eccentricity
0.00166
Inclination
97.3932°
RAAN
266.0295°
Arg. of periapsis
265.7852°
True anomaly
94.34452°
Mean anomaly
94.1554°
Eccentric anomaly
94.24996°
Mean motion
4.09649 °/min
Orbital period
87.88 mins
BSTAR
0.00091617
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Other satellites on launch #99 in the year 2018 (2018-12-03 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 Q 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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