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 26313U 26100.17393537 +.00000000 +00000-0 +40712-3 0 00002
2 26313 98.4493 166.0794 0071076 333.1119 49.2088 14.57816655 08
| Epoch (UTC): | 10 April 2026 04:10:28 |
| Eccentricity: | 0.0071076 |
| inclination: | 98.4493° |
| perigee height: | 650 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 166.0794° |
| argument of perigee: | 333.1119° |
| revolutions per day: | 14.57816655 |
| mean anomaly at epoch: | 49.2088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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