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 13154U 26159.48952698 +.00000000 +00000-0 +20982-3 0 00005
2 13154 81.1422 111.1372 0029887 24.5188 335.7450 15.10486391 07
| Epoch (UTC): | 08 June 2026 11:44:55 |
| Eccentricity: | 0.0029887 |
| inclination: | 81.1422° |
| perigee height: | 514 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 111.1372° |
| argument of perigee: | 24.5188° |
| revolutions per day: | 15.10486391 |
| mean anomaly at epoch: | 335.7450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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