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 26107U 26145.24806566 +.00000000 +00000-0 +00000-0 0 00004
2 26107 9.0799 58.4005 0005016 3.6646 15.0808 1.00274170 05
| Epoch (UTC): | 25 May 2026 05:57:12 |
| Eccentricity: | 0.0005016 |
| inclination: | 9.0799° |
| perigee height: | 35765 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 58.4005° |
| argument of perigee: | 3.6646° |
| revolutions per day: | 1.00274170 |
| mean anomaly at epoch: | 15.0808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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