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 54065U 26145.57844821 +.00000000 +00000-0 +18685-3 0 00001
2 54065 53.2130 358.8018 0001204 80.3513 279.7615 15.08844157 06
| Epoch (UTC): | 25 May 2026 13:52:57 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 358.8018° |
| argument of perigee: | 80.3513° |
| revolutions per day: | 15.08844157 |
| mean anomaly at epoch: | 279.7615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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