View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 48452U 26145.32735374 +.00000000 +00000-0 +38073-4 0 00003
2 48452 53.1587 181.6810 0001166 79.8662 280.2471 15.31702045 03
| Epoch (UTC): | 25 May 2026 07:51:23 |
| Eccentricity: | 0.0001166 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.6810° |
| argument of perigee: | 79.8662° |
| revolutions per day: | 15.31702045 |
| mean anomaly at epoch: | 280.2471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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