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 52790U 26145.47782000 +.00000000 +00000-0 +22565-3 0 00005
2 52790 50.0061 307.7409 0033846 60.2109 300.2187 14.81274947 07
| Epoch (UTC): | 25 May 2026 11:28:03 |
| Eccentricity: | 0.0033846 |
| inclination: | 50.0061° |
| perigee height: | 602 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 307.7409° |
| argument of perigee: | 60.2109° |
| revolutions per day: | 14.81274947 |
| mean anomaly at epoch: | 300.2187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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