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, 0.2 m
Radar Cross Section
0.070 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 BESSA
1 68836U 26067CX 26260.09967646 .00008666 00000-0 41065-3 0 9990
2 68836 97.4626 217.3764 0012043 58.9795 301.2621 15.19489245 25695Epoch: 2026-09-17T02:23Z
TLE epoch observation values (Epoch: 2026-09-17T02:23:32.046Z)
Latitude
0.00003°
Longitude
-174.5489°
Altitude
506.174 km
Speed
7.613 km/s
True Right ascension
14h 29m 30s
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
06:19:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.641 km
Perigee altitude
496.064 km
Semi-major axis
6,882.489 km
Eccentricity
0.0012
Inclination
97.4626°
RAAN
217.3764°
Arg. of periapsis
58.9795°
True anomaly
301.14404°
Mean anomaly
301.2621°
Eccentric anomaly
301.20308°
Mean motion
3.80124 °/min
Orbital period
94.71 mins
BSTAR
0.00041065
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-17 21:28:22.293Z | 177.363° S | 2026-09-17 21:32:22.293Z | 299.247° NW | 56.376° | 2026-09-17 21:35:22.293Z | 340.927° N |
| 5 mins | 2026-09-18 10:34:22.293Z | 345.912° N | 2026-09-18 10:36:22.293Z | 292.106° WNW | 39.977° | 2026-09-18 10:39:22.293Z | 220.343° SW |
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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