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 48410U 26145.44055850 +.00000000 +00000-0 +46839-4 0 00003
2 48410 53.1596 299.6004 0000946 88.2464 271.8646 15.31698277 02
| Epoch (UTC): | 25 May 2026 10:34:24 |
| Eccentricity: | 0.0000946 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 299.6004° |
| argument of perigee: | 88.2464° |
| revolutions per day: | 15.31698277 |
| mean anomaly at epoch: | 271.8646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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