OBJECT AW, 59142
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT AW, 59142 is a satellite in SSO 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.
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59142 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational 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: 14 hours ago
TLE from 14 hours ago
0 OBJECT AW
1 59142U 24043AW 25297.36070793 .00054546 00000-0 94736-3 0 9990
2 59142 97.5282 75.5197 0006246 311.3165 48.7548 15.50642992 91591Epoch: 2025-10-24T08:39Z
TLE epoch observation values (Epoch: 2025-10-24T08:39:25.165Z)
Latitude
-0.00002°
Longitude
-87.34187°
Altitude
415.179 km
Speed
7.663 km/s
True Right ascension
05h 02m 04s
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
17:27:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
416.019 km
Perigee altitude
407.537 km
Semi-major axis
6,789.915 km
Eccentricity
0.00062
Inclination
97.5282°
RAAN
75.5197°
Arg. of periapsis
311.3165°
True anomaly
48.80864°
Mean anomaly
48.7548°
Eccentric anomaly
48.78172°
Mean motion
3.87924 °/min
Orbital period
92.8 mins
BSTAR
0.00094736
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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 AW Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-25 09:34:43.186Z | 186.068° SSW | 2025-10-25 09:36:43.186Z | 287.185° WNW | 39.559° | 2025-10-25 09:38:43.186Z | 336.475° NNW |
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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