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 51980U 26145.17412553 +.00000000 +00000-0 -17678-3 0 00005
2 51980 53.2138 55.7673 0001506 90.7722 269.3442 15.08854697 02
| Epoch (UTC): | 25 May 2026 04:10:44 |
| Eccentricity: | 0.0001506 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 55.7673° |
| argument of perigee: | 90.7722° |
| revolutions per day: | 15.08854697 |
| mean anomaly at epoch: | 269.3442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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