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.
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60506 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
AVS
Mission
Operational Commercial Imaging
Bus & Motor
LUR, Unknown motor
Mass
57 kg wet, 57 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.275 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 LUR-1
1 60506U 24149AQ 25289.19532117 .00008964 00000-0 35396-3 0 9998
2 60506 97.3996 5.1807 0005893 91.0990 269.0923 15.25735925 64719Epoch: 2025-10-16T04:41Z
TLE epoch observation values (Epoch: 2025-10-16T04:41:15.749Z)
Latitude
-0.00004°
Longitude
-90.09344°
Altitude
491.741 km
Speed
7.619 km/s
True Right ascension
00h 20m 43s
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
12:35:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.579 km
Perigee altitude
481.49 km
Semi-major axis
6,863.671 km
Eccentricity
0.00059
Inclination
97.3996°
RAAN
5.1807°
Arg. of periapsis
91.099°
True anomaly
269.02478°
Mean anomaly
269.0923°
Eccentric anomaly
269.05854°
Mean motion
3.81688 °/min
Orbital period
94.32 mins
BSTAR
0.00035396
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.LUR-1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-17 06:01:11.041Z | 234.611° WSW | 2025-10-17 06:02:11.041Z | 256.924° W | 19.682° | 2025-10-17 06:05:11.041Z | 315.145° NNW |
| 5 mins | 2025-10-17 17:28:11.041Z | 46.756° ENE | 2025-10-17 17:30:11.041Z | 93.83° ESE | 25.201° | 2025-10-17 17:33:11.041Z | 156.019° SSE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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