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 48479U 26145.40969716 +.00000000 +00000-0 +35691-3 0 00002
2 48479 53.1598 194.5590 0001017 88.8213 271.2905 15.31717049 01
| Epoch (UTC): | 25 May 2026 09:49:57 |
| Eccentricity: | 0.0001017 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 194.5590° |
| argument of perigee: | 88.8213° |
| revolutions per day: | 15.31717049 |
| mean anomaly at epoch: | 271.2905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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