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 52940U 26145.60736612 +.00000000 +00000-0 +00000-0 0 00002
2 52940 3.6554 78.8101 0002302 246.7157 255.5509 1.00274483 09
| Epoch (UTC): | 25 May 2026 14:34:36 |
| Eccentricity: | 0.0002302 |
| inclination: | 3.6554° |
| perigee height: | 35776 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 78.8101° |
| argument of perigee: | 246.7157° |
| revolutions per day: | 1.00274483 |
| mean anomaly at epoch: | 255.5509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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