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 52373U 26145.45472671 +.00000000 +00000-0 +90071-5 0 00009
2 52373 53.2120 204.5078 0001155 85.2942 274.8182 15.08838170 06
| Epoch (UTC): | 25 May 2026 10:54:48 |
| Eccentricity: | 0.0001155 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 204.5078° |
| argument of perigee: | 85.2942° |
| revolutions per day: | 15.08838170 |
| mean anomaly at epoch: | 274.8182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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