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 51881U 26145.34709203 +.00000000 +00000-0 +31431-4 0 00008
2 51881 53.2140 14.9915 0001340 91.9969 268.1176 15.08833930 01
| Epoch (UTC): | 25 May 2026 08:19:48 |
| Eccentricity: | 0.0001340 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 14.9915° |
| argument of perigee: | 91.9969° |
| revolutions per day: | 15.08833930 |
| mean anomaly at epoch: | 268.1176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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