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: 7 hours ago
TLE from 7 hours ago
0 OBJECT A
1 60468U 24149A 26039.46191941 .00010408 00000-0 35541-3 0 9993
2 60468 97.3829 119.9644 0002675 341.7413 18.3732 15.30494794 82359Epoch: 2026-02-08T11:05Z
TLE epoch observation values (Epoch: 2026-02-08T11:05:09.837Z)
Latitude
0.00006°
Longitude
175.10266°
Altitude
475.7 km
Speed
7.629 km/s
True Right ascension
07h 59m 51s
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
19:50:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.118 km
Perigee altitude
469.454 km
Semi-major axis
6,849.423 km
Eccentricity
0.00027
Inclination
97.3829°
RAAN
119.9644°
Arg. of periapsis
341.7413°
True anomaly
18.38287°
Mean anomaly
18.3732°
Eccentric anomaly
18.37803°
Mean motion
3.8288 °/min
Orbital period
94.02 mins
BSTAR
0.00035541
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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 | 2026-02-08 17:55:19.918Z | 21.234° NNE | 2026-02-08 17:58:19.918Z | 96.263° ESE | 40.557° | 2026-02-08 18:01:19.918Z | 179.276° S |
| 4 mins | 2026-02-09 17:29:19.918Z | 59.679° ENE | 2026-02-09 17:30:19.918Z | 83.255° E | 21.981° | 2026-02-09 17:33:19.918Z | 148.833° SSE |
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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