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 52609U 26145.40596073 +.00000000 +00000-0 +24514-4 0 00007
2 52609 53.2123 294.6793 0001289 87.0902 273.0237 15.08845582 06
| Epoch (UTC): | 25 May 2026 09:44:35 |
| Eccentricity: | 0.0001289 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.6793° |
| argument of perigee: | 87.0902° |
| revolutions per day: | 15.08845582 |
| mean anomaly at epoch: | 273.0237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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