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 51775U 26145.66668980 +.00000000 +00000-0 +26447-2 0 00000
2 51775 53.2183 348.4291 0001499 86.8605 157.2128 15.41814615 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001499 |
| inclination: | 53.2183° |
| perigee height: | 440 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 348.4291° |
| argument of perigee: | 86.8605° |
| revolutions per day: | 15.41814615 |
| mean anomaly at epoch: | 157.2128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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