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 26094U 26105.98414623 +.00000000 +00000-0 +13568-3 0 00001
2 26094 100.2191 110.2564 0031795 4.9924 355.1573 14.47211672 03
| Epoch (UTC): | 15 April 2026 23:37:10 |
| Eccentricity: | 0.0031795 |
| inclination: | 100.2191° |
| perigee height: | 712 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 110.2564° |
| argument of perigee: | 4.9924° |
| revolutions per day: | 14.47211672 |
| mean anomaly at epoch: | 355.1573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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