CAMOES, 68507
Orbit data source: Space-Track
CAMOES, 68507 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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68507 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: 1 day ago
TLE from 1 day ago
0 CAMOES
1 68507U 26067CV 26307.45604989 .00005599 00000-0 26124-3 0 9996
2 68507 97.4830 264.4433 0001927 359.2897 0.8335 15.20249762 33066Epoch: 2026-11-03T10:56Z
TLE epoch observation values (Epoch: 2026-11-03T10:56:42.710Z)
Latitude
-0.00002°
Longitude
57.54689°
Altitude
506.849 km
Speed
7.611 km/s
True Right ascension
17h 37m 46s
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
11:13:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.381 km
Perigee altitude
500.73 km
Semi-major axis
6,880.192 km
Eccentricity
0.00019
Inclination
97.483°
RAAN
264.4433°
Arg. of periapsis
359.2897°
True anomaly
0.83382°
Mean anomaly
0.8335°
Eccentric anomaly
0.83366°
Mean motion
3.80314 °/min
Orbital period
94.66 mins
BSTAR
0.00026124
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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.CAMOES 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 | 2026-11-04 21:50:01.043Z | 206.024° SW | 2026-11-04 21:52:01.043Z | 255.576° W | 34.64° | 2026-11-04 21:55:01.043Z | 325.14° NNW |
| 4 mins | 2026-11-05 09:21:01.043Z | 63.619° ENE | 2026-11-05 09:22:01.043Z | 83.581° E | 19.512° | 2026-11-05 09:25:01.043Z | 140.544° SSE |
| 4 mins | 2026-11-05 10:55:01.043Z | 320.559° NNW | 2026-11-05 10:56:01.043Z | 296.959° NW | 24.061° | 2026-11-05 10:59:01.043Z | 237.563° WSW |
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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