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 26113U 26140.40834432 +.00000000 +00000-0 +33926-1 0 00001
2 26113 94.2067 315.0050 7452478 290.9630 8.3365 1.68665746 07
| Epoch (UTC): | 20 May 2026 09:48:00 |
| Eccentricity: | 0.7452478 |
| inclination: | 94.2067° |
| perigee height: | 1216 km |
| apogee height: | 45650 km |
| right ascension of ascending node: | 315.0050° |
| argument of perigee: | 290.9630° |
| revolutions per day: | 1.68665746 |
| mean anomaly at epoch: | 8.3365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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