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 50180U 26145.58264654 +.00000000 +00000-0 +30127-4 0 00002
2 50180 53.2119 263.9416 0001142 87.1406 272.9717 15.08837707 03
| Epoch (UTC): | 25 May 2026 13:59:00 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 263.9416° |
| argument of perigee: | 87.1406° |
| revolutions per day: | 15.08837707 |
| mean anomaly at epoch: | 272.9717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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