Showing default

LUR-1, 60506

Orbit data source: Space-Track

LUR-1, 60506 is a Spanish payload satellite in SSO that was launched on Fri, 16 Aug 2024 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
60506, 2024-149AQ
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
AVS
Mission
Operational Commercial Imaging
Bus & Motor
LUR, Unknown motor
Mass
57 kg wet, 57 kg dry
Launch date (UTC)
2024-08-16 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.275 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 LUR-1
1 60506U 24149AQ  26129.78338338  .00005107  00000-0  18061-3 0  9992
2 60506  97.3737 208.9044 0005681  86.7400 273.4491 15.29601987 96101
Epoch: 2026-05-09T18:48Z
TLE epoch observation values (Epoch: 2026-05-09T18:48:04.324Z)
Latitude
0.00008°
Longitude
59.29051°
Altitude
479.873 km
Speed
7.626 km/s
True Right ascension
13h 55m 37s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
09:43:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.846 km
Perigee altitude
470.06 km
Semi-major axis
6,852.09 km
Eccentricity
0.00057
Inclination
97.3737°
RAAN
208.9044°
Arg. of periapsis
86.74°
True anomaly
273.38412°
Mean anomaly
273.4491°
Eccentric anomaly
273.41661°
Mean motion
3.82656 °/min
Orbital period
94.08 mins
BSTAR
0.00018061
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
|