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 51799U 26144.99840821 +.00000000 +00000-0 +41381-4 0 00003
2 51799 53.2151 6.5544 0001764 89.8137 270.3058 15.08840595 08
| Epoch (UTC): | 24 May 2026 23:57:42 |
| Eccentricity: | 0.0001764 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 6.5544° |
| argument of perigee: | 89.8137° |
| revolutions per day: | 15.08840595 |
| mean anomaly at epoch: | 270.3058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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