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 50835U 26145.40116148 +.00000000 +00000-0 +77875-3 0 00004
2 50835 53.2143 194.7568 0001262 55.8656 304.2456 15.09786619 03
| Epoch (UTC): | 25 May 2026 09:37:40 |
| Eccentricity: | 0.0001262 |
| inclination: | 53.2143° |
| perigee height: | 536 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 194.7568° |
| argument of perigee: | 55.8656° |
| revolutions per day: | 15.09786619 |
| mean anomaly at epoch: | 304.2456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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