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 48395U 26145.55692671 +.00000000 +00000-0 +39004-4 0 00001
2 48395 53.1609 337.3968 0001374 83.9545 276.1613 15.31696759 01
| Epoch (UTC): | 25 May 2026 13:21:58 |
| Eccentricity: | 0.0001374 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 337.3968° |
| argument of perigee: | 83.9545° |
| revolutions per day: | 15.31696759 |
| mean anomaly at epoch: | 276.1613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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