OBJECT A, 60468
Orbit data source: Space-Track
OBJECT A, 60468 is a satellite in SSO that was launched on Fri, 16 Aug 2024 UTC launched 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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60468 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.072 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 OBJECT A
1 60468U 24149A 26084.56020336 .00010144 00000-0 33622-3 0 9998
2 60468 97.3757 164.8299 0004433 142.7710 217.3839 15.31462722 89259Epoch: 2026-03-25T13:26Z
TLE epoch observation values (Epoch: 2026-03-25T13:26:41.570Z)
Latitude
-0.00006°
Longitude
140.13495°
Altitude
476.968 km
Speed
7.626 km/s
True Right ascension
10h 59m 19s
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
04:00:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.432 km
Perigee altitude
465.362 km
Semi-major axis
6,846.534 km
Eccentricity
0.00044
Inclination
97.3757°
RAAN
164.8299°
Arg. of periapsis
142.771°
True anomaly
217.35307°
Mean anomaly
217.3839°
Eccentric anomaly
217.36848°
Mean motion
3.83122 °/min
Orbital period
93.96 mins
BSTAR
0.00033622
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Other satellites on launch #149 in the year 2024 (2024-08-16 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 A 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-26 05:15:26.617Z | 161.491° S | 2026-03-26 05:18:26.617Z | 24.172° NE | 43.079° | 2026-03-26 05:21:26.617Z | 351.363° N |
| 5 mins | 2026-03-26 18:14:26.617Z | 7.611° NNE | 2026-03-26 18:16:26.617Z | 334.032° NNW | 43.627° | 2026-03-26 18:19:26.617Z | 197.652° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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