DB-BECON-2-VU, 68468
Orbit data source: Space-Track
DB-BECON-2-VU, 68468 is a payload 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). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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68468 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
Shape & HBR
Box + 2 Pan, 1.1 m
Radar Cross Section
0.017 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 DB-BECON-2-VU
1 68468U 26067BE 26236.14287731 .00007338 00000-0 35699-3 0 9991
2 68468 97.4594 193.5420 0006827 161.7299 198.4182 15.18670034 22242Epoch: 2026-08-24T03:25Z
TLE epoch observation values (Epoch: 2026-08-24T03:25:44.599Z)
Latitude
-0.00001°
Longitude
169.67735°
Altitude
517.409 km
Speed
7.602 km/s
True Right ascension
12h 54m 10s
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
10:29:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.529 km
Perigee altitude
502.129 km
Semi-major axis
6,884.966 km
Eccentricity
0.00068
Inclination
97.4594°
RAAN
193.542°
Arg. of periapsis
161.7299°
True anomaly
198.3935°
Mean anomaly
198.4182°
Eccentric anomaly
198.40585°
Mean motion
3.79919 °/min
Orbital period
94.76 mins
BSTAR
0.00035699
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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.DB-BECON-2-VU 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 | 2026-08-24 20:57:37.421Z | 144.194° SSE | 2026-08-24 21:00:37.421Z | 54.167° ENE | 35.959° | 2026-08-24 21:03:37.421Z | 0.591° NNE |
| 6 mins | 2026-08-25 10:02:37.421Z | 16.328° NNE | 2026-08-25 10:05:37.421Z | 157.074° SSE | 43.116° | 2026-08-25 10:08:37.421Z | 188.354° 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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