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 13819U 26160.30799976 +.00000000 +00000-0 +25004-3 0 00004
2 13819 81.1020 249.6668 0015885 88.8444 271.4622 15.49027917 09
| Epoch (UTC): | 09 June 2026 07:23:31 |
| Eccentricity: | 0.0015885 |
| inclination: | 81.1020° |
| perigee height: | 409 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 249.6668° |
| argument of perigee: | 88.8444° |
| revolutions per day: | 15.49027917 |
| mean anomaly at epoch: | 271.4622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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