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 26382U 26106.94148111 +.00000000 +00000-0 +00000-0 0 00008
2 26382 13.2128 17.3583 0003135 308.4215 227.8106 1.00099120 00
| Epoch (UTC): | 16 April 2026 22:35:43 |
| Eccentricity: | 0.0003135 |
| inclination: | 13.2128° |
| perigee height: | 35822 km |
| apogee height: | 35848 km |
| right ascension of ascending node: | 17.3583° |
| argument of perigee: | 308.4215° |
| revolutions per day: | 1.00099120 |
| mean anomaly at epoch: | 227.8106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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