OBJECT AT, 68457
Orbit data source: Space-Track
OBJECT AT, 68457 is a satellite in SSO that was launched on Mon, 30 Mar 2026 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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68457 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Ant, 1.1 m
Radar Cross Section
0.006 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 OBJECT AT
1 68457U 26067AT 26217.41555272 .00006878 00000-0 31943-3 0 9992
2 68457 97.4577 175.3884 0002967 123.9686 236.1831 15.20324334 19423Epoch: 2026-08-05T09:58Z
TLE epoch observation values (Epoch: 2026-08-05T09:58:23.755Z)
Latitude
-0.00004°
Longitude
71.81915°
Altitude
509.088 km
Speed
7.609 km/s
True Right ascension
11h 41m 33s
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
19:46:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.87 km
Perigee altitude
499.788 km
Semi-major axis
6,879.966 km
Eccentricity
0.0003
Inclination
97.4577°
RAAN
175.3884°
Arg. of periapsis
123.9686°
True anomaly
236.15486°
Mean anomaly
236.1831°
Eccentric anomaly
236.16898°
Mean motion
3.80333 °/min
Orbital period
94.65 mins
BSTAR
0.00031943
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Other satellites on launch #67 in the year 2026 (2026-03-30 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 AT 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 | 2026-08-06 10:13:21.662Z | 8.332° NNE | 2026-08-06 10:16:21.662Z | 336.009° NNW | 42.796° | 2026-08-06 10:19:21.662Z | 199.563° SSW |
| 5 mins | 2026-08-06 20:52:21.662Z | 130.568° SE | 2026-08-06 20:54:21.662Z | 75.116° E | 31.928° | 2026-08-06 20:57:21.662Z | 7.127° NNE |
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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