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 51808U 26144.99932507 +.00000000 +00000-0 +24364-4 0 00009
2 51808 53.2161 356.5525 0001385 94.7311 265.3839 15.08841580 01
| Epoch (UTC): | 24 May 2026 23:59:01 |
| Eccentricity: | 0.0001385 |
| inclination: | 53.2161° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 356.5525° |
| argument of perigee: | 94.7311° |
| revolutions per day: | 15.08841580 |
| mean anomaly at epoch: | 265.3839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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