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 52845U 26145.43036376 +.00000000 +00000-0 +24331-4 0 00004
2 52845 53.2140 49.6839 0001008 77.6882 282.4223 15.08829869 06
| Epoch (UTC): | 25 May 2026 10:19:43 |
| Eccentricity: | 0.0001008 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 49.6839° |
| argument of perigee: | 77.6882° |
| revolutions per day: | 15.08829869 |
| mean anomaly at epoch: | 282.4223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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