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 52095U 26145.30567296 +.00000000 +00000-0 +95158-3 0 00001
2 52095 53.2147 105.1772 0001928 78.3659 281.7549 15.08898773 08
| Epoch (UTC): | 25 May 2026 07:20:10 |
| Eccentricity: | 0.0001928 |
| inclination: | 53.2147° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.1772° |
| argument of perigee: | 78.3659° |
| revolutions per day: | 15.08898773 |
| mean anomaly at epoch: | 281.7549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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