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 26133.57330774 +.00000000 +00000-0 +44453-3 0 00009
2 00011 32.8713 216.1546 1444923 219.9299 128.5746 11.90422032 08
| Epoch (UTC): | 13 May 2026 13:45:33 |
| Eccentricity: | 0.1444923 |
| inclination: | 32.8713° |
| perigee height: | 553 km |
| apogee height: | 2895 km |
| right ascension of ascending node: | 216.1546° |
| argument of perigee: | 219.9299° |
| revolutions per day: | 11.90422032 |
| mean anomaly at epoch: | 128.5746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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