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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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Identifier
68507, 2026-067CV
Orbit
SSO
Country
Flag of PTPT / POR
Related business
Manufacturer
LUSO
Mission
Operational spacecraft
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
~15 kg wet, ~15 kg dry
Launch date (UTC)
2026-03-30 (3 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 CAMOES
1 68507U 26067CV  26194.11739700  .00005327  00000-0  26041-3 0  9990
2 68507  97.4651 152.2623 0003084  27.7292 332.4106 15.18650627 15854
Epoch: 2026-07-13T02:49Z
TLE epoch observation values (Epoch: 2026-07-13T02:49:03.100Z)
Latitude
-0.00006°
Longitude
178.99288°
Altitude
511.122 km
Speed
7.609 km/s
True Right ascension
10h 09m 02s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:25:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.011 km
Perigee altitude
504.765 km
Semi-major axis
6,885.025 km
Eccentricity
0.00031
Inclination
97.4651°
RAAN
152.2623°
Arg. of periapsis
27.7292°
True anomaly
332.39423°
Mean anomaly
332.4106°
Eccentric anomaly
332.40241°
Mean motion
3.79914 °/min
Orbital period
94.76 mins
BSTAR
0.00026041
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