Showing default

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.

Loading next visibility...
Identifier
68507, 2026-067CV
Orbit
SSO
Country
Flag of PTPT / POR
Related business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
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: 10 hours ago

TLE from 10 hours ago
0 CAMOES
1 68507U 26067CV  26171.44871885  .00007134  00000-0  35111-3 0  9998
2 68507  97.4642 129.8810 0005017  75.5825 284.5965 15.18288241 12411
Epoch: 2026-06-20T10:46Z
TLE epoch observation values (Epoch: 2026-06-20T10:46:09.308Z)
Latitude
-0.00009°
Longitude
59.67904°
Altitude
513.231 km
Speed
7.608 km/s
True Right ascension
08h 39m 31s
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
07:17:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.439 km
Perigee altitude
504.53 km
Semi-major axis
6,886.121 km
Eccentricity
0.0005
Inclination
97.4642°
RAAN
129.881°
Arg. of periapsis
75.5825°
True anomaly
284.54086°
Mean anomaly
284.5965°
Eccentric anomaly
284.56868°
Mean motion
3.79823 °/min
Orbital period
94.78 mins
BSTAR
0.00035111
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|