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 51959U 26145.40024486 +.00000000 +00000-0 +95898-4 0 00001
2 51959 53.1613 40.6560 0001165 100.4718 259.6415 15.31696062 06
| Epoch (UTC): | 25 May 2026 09:36:21 |
| Eccentricity: | 0.0001165 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 40.6560° |
| argument of perigee: | 100.4718° |
| revolutions per day: | 15.31696062 |
| mean anomaly at epoch: | 259.6415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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