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 53795U 26145.41558972 +.00000000 +00000-0 -29679-4 0 00009
2 53795 53.2138 289.3661 0001236 81.9549 278.1584 15.08838236 05
| Epoch (UTC): | 25 May 2026 09:58:26 |
| Eccentricity: | 0.0001236 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.3661° |
| argument of perigee: | 81.9549° |
| revolutions per day: | 15.08838236 |
| mean anomaly at epoch: | 278.1584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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