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 51861U 26145.35353116 +.00000000 +00000-0 +23189-4 0 00006
2 51861 53.2123 24.9628 0001189 83.7797 276.3330 15.08832711 00
| Epoch (UTC): | 25 May 2026 08:29:05 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 24.9628° |
| argument of perigee: | 83.7797° |
| revolutions per day: | 15.08832711 |
| mean anomaly at epoch: | 276.3330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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