BESSA, 68836
Orbit data source: Space-Track
BESSA, 68836 is a Portuguese 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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68836 intel report (Beta)
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Identifier
Orbit
Country
PT / PORRelated business
Manufacturer
LUSO
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
~15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 14.5 m
Radar Cross Section
0.070 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 BESSA
1 68836U 26067CX 26220.11942111 .00003962 00000-0 19250-3 0 9994
2 68836 97.4555 177.8895 0010202 180.3598 179.7631 15.18982226 19628Epoch: 2026-08-08T02:51Z
TLE epoch observation values (Epoch: 2026-08-08T02:51:57.983Z)
Latitude
-0.00004°
Longitude
178.26257°
Altitude
519.03 km
Speed
7.6 km/s
True Right ascension
11h 51m 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
00:14:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.908 km
Perigee altitude
498.862 km
Semi-major axis
6,884.022 km
Eccentricity
0.00102
Inclination
97.4555°
RAAN
177.8895°
Arg. of periapsis
180.3598°
True anomaly
179.76358°
Mean anomaly
179.7631°
Eccentric anomaly
179.76334°
Mean motion
3.79997 °/min
Orbital period
94.74 mins
BSTAR
0.0001925
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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.BESSA 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-08 21:58:43.432Z | 220.628° SW | 2026-08-08 22:00:43.432Z | 268.043° W | 23.827° | 2026-08-08 22:03:43.432Z | 322.167° NNW |
| 4 mins | 2026-08-09 09:29:43.432Z | 54.759° ENE | 2026-08-09 09:31:43.432Z | 104.956° ESE | 23.818° | 2026-08-09 09:33:43.432Z | 146.604° SSE |
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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