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 50319U 26145.45777353 +.00000000 +00000-0 +00000-0 0 00000
2 50319 0.0163 294.4606 0000067 246.6135 310.5328 1.00272593 02
| Epoch (UTC): | 25 May 2026 10:59:11 |
| Eccentricity: | 0.0000067 |
| inclination: | 0.0163° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 294.4606° |
| argument of perigee: | 246.6135° |
| revolutions per day: | 1.00272593 |
| mean anomaly at epoch: | 310.5328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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