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 35493U 26145.42406005 +.00000000 +00000-0 +00000-0 0 00006
2 35493 0.0123 288.7843 0000655 3.5620 17.1770 1.00272520 06
| Epoch (UTC): | 25 May 2026 10:10:38 |
| Eccentricity: | 0.0000655 |
| inclination: | 0.0123° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 288.7843° |
| argument of perigee: | 3.5620° |
| revolutions per day: | 1.00272520 |
| mean anomaly at epoch: | 17.1770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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