OBJECT A, 60468
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 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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Edit Public Description
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: 11 hours ago
TLE from 11 hours ago
0 OBJECT A
1 60468U 24149A 25300.15613255 .00010490 00000-0 38830-3 0 9991
2 60468 97.3959 16.3356 0002952 353.2156 6.9043 15.27849735 66415Epoch: 2025-10-27T03:44Z
TLE epoch observation values (Epoch: 2025-10-27T03:44:49.852Z)
Latitude
-0.00001°
Longitude
-75.63414°
Altitude
483.332 km
Speed
7.625 km/s
True Right ascension
01h 05m 20s
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
10:08:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.221 km
Perigee altitude
477.172 km
Semi-major axis
6,857.333 km
Eccentricity
0.0003
Inclination
97.3959°
RAAN
16.3356°
Arg. of periapsis
353.2156°
True anomaly
6.90837°
Mean anomaly
6.9043°
Eccentric anomaly
6.90633°
Mean motion
3.82217 °/min
Orbital period
94.19 mins
BSTAR
0.0003883
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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 | 2025-10-27 18:26:36.392Z | 357.574° N | 2025-10-27 18:29:36.392Z | 301.455° NW | 33.709° | 2025-10-27 18:32:36.392Z | 218.059° SW |
| 5 mins | 2025-10-28 05:02:36.392Z | 145.847° SSE | 2025-10-28 05:04:36.392Z | 64.05° ENE | 39.958° | 2025-10-28 05:07:36.392Z | 357.599° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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