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LPNTSAT-001

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Mission Photos:
lpntsat001.png satellite
Figure 4.9: Sun tracking with nadir pointing control mode.

LPNTSAT-001 is the first satellite of the Celeste LEO-PNT (Low Earth Orbit – Position, Navigation, & Timing) in-orbit demonstrator mission, which will feature an 11-satellite constellation that will fly close to Earth to test innovative signals across various frequency bands, including L Band and S Band.

One of the objectives of this mission is to assess the PNT (Position, Navigation, & Timing) performance that a future constellation of LEO satellites can achieve, augmenting existing systems like Galileo and Egnos. A key step is to assess the performance of the orbits computed by the IOD system. SLR measurements will be used on a ground system which computes precise the reference orbits of the LEO satellites (in post-processing).

All satellites in the constellation will operate in a quasi polar orbit at an altitude between 500 and 600 km, to demonstrate critical technology, including:

  • Autonomous precise orbit determination independent of ground infrastructure.
  • Assessment of on-board timing stability and synchronization performance without atomic clocks.
  • Verification of radionavigation service provision in the UHF, L , S and C-bands.

For more information: https://www.esa.int/Applications/Satellite_navigation/Celeste

Figure 4.3: External configuration view 2
Figure 4.3: External configuration view 2.

Mission Parameters
Satellite: LPNTSAT-001
Sponsor: ESA
Expected Life: 6 months
Primary Application: Navigation, assessing performance of a future constellation.
COSPAR ID/ILRS ID: 2026-065A/2606501
SIC Code: 8013
Satellite Catalog (NORAD) Number: 68408
Launch Date: 2026-03-28
NP Bin Size: 5 seconds
RRA Shape: Hemispherical/Pyramid
Cube Diameter: 12.7 mm; 10.16 mm height
Reflectors:
Inclination: 97.41 degrees
Eccentricity: 0.00133331
Altitude: 510 km
Orbital Period: 94.84 Minutes
Weight:

Additional Information: