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 26073.22561870 +.00000000 +00000-0 +38300-3 0 00001
2 13819 81.1059 356.6865 0017666 36.1797 324.0639 15.46531792 06
| Epoch (UTC): | 14 March 2026 05:24:53 |
| Eccentricity: | 0.0017666 |
| inclination: | 81.1059° |
| perigee height: | 415 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 356.6865° |
| argument of perigee: | 36.1797° |
| revolutions per day: | 15.46531792 |
| mean anomaly at epoch: | 324.0639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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