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 65410U 26145.39666462 +.00000000 +00000-0 +66619-1 0 00008
2 65410 53.1578 235.6865 0015153 225.0613 134.9161 15.34274356 01
| Epoch (UTC): | 25 May 2026 09:31:11 |
| Eccentricity: | 0.0015153 |
| inclination: | 53.1578° |
| perigee height: | 453 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 235.6865° |
| argument of perigee: | 225.0613° |
| revolutions per day: | 15.34274356 |
| mean anomaly at epoch: | 134.9161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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