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 13811U 26107.92348389 +.00000000 +00000-0 +75565-3 0 00000
2 13811 82.9319 275.4359 0010279 294.1357 219.8201 14.15959654 05
| Epoch (UTC): | 17 April 2026 22:09:49 |
| Eccentricity: | 0.0010279 |
| inclination: | 82.9319° |
| perigee height: | 832 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 275.4359° |
| argument of perigee: | 294.1357° |
| revolutions per day: | 14.15959654 |
| mean anomaly at epoch: | 219.8201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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