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 51859U 26144.96440536 +.00000000 +00000-0 -57043-4 0 00009
2 51859 53.2137 26.7174 0001713 89.0165 271.1023 15.08841874 01
| Epoch (UTC): | 24 May 2026 23:08:44 |
| Eccentricity: | 0.0001713 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 26.7174° |
| argument of perigee: | 89.0165° |
| revolutions per day: | 15.08841874 |
| mean anomaly at epoch: | 271.1023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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