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 26110.17034191 +.00000000 +00000-0 -48903-2 0 00009
2 26113 94.1831 314.6019 7475869 294.4117 7.7410 1.68665638 07
| Epoch (UTC): | 20 April 2026 04:05:17 |
| Eccentricity: | 0.7475869 |
| inclination: | 94.1831° |
| perigee height: | 1147 km |
| apogee height: | 45720 km |
| right ascension of ascending node: | 314.6019° |
| argument of perigee: | 294.4117° |
| revolutions per day: | 1.68665638 |
| mean anomaly at epoch: | 7.7410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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