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 51807U 26145.27901080 +.00000000 +00000-0 +27465-4 0 00007
2 51807 53.2119 355.2944 0001063 86.4812 273.6301 15.08832316 04
| Epoch (UTC): | 25 May 2026 06:41:46 |
| Eccentricity: | 0.0001063 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 355.2944° |
| argument of perigee: | 86.4812° |
| revolutions per day: | 15.08832316 |
| mean anomaly at epoch: | 273.6301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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