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 00011U 26130.55421596 +.00000000 +00000-0 +52644-3 0 00008
2 00011 32.8696 227.5799 1444663 202.7495 150.2213 11.90416611 00
| Epoch (UTC): | 10 May 2026 13:18:04 |
| Eccentricity: | 0.1444663 |
| inclination: | 32.8696° |
| perigee height: | 554 km |
| apogee height: | 2895 km |
| right ascension of ascending node: | 227.5799° |
| argument of perigee: | 202.7495° |
| revolutions per day: | 11.90416611 |
| mean anomaly at epoch: | 150.2213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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