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 26103.23750527 +.00000000 +00000-0 +15339-3 0 00002
2 13819 81.1026 319.8537 0015047 288.2163 71.7444 15.47487379 07
| Epoch (UTC): | 13 April 2026 05:42:00 |
| Eccentricity: | 0.0015047 |
| inclination: | 81.1026° |
| perigee height: | 414 km |
| apogee height: | 434 km |
| right ascension of ascending node: | 319.8537° |
| argument of perigee: | 288.2163° |
| revolutions per day: | 15.47487379 |
| mean anomaly at epoch: | 71.7444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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