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 46916U 26145.60849279 +.00000000 +00000-0 +00000-0 0 00002
2 46916 0.8199 324.4684 0001658 91.3096 171.4181 1.00269472 08
| Epoch (UTC): | 25 May 2026 14:36:13 |
| Eccentricity: | 0.0001658 |
| inclination: | 0.8199° |
| perigee height: | 35780 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 324.4684° |
| argument of perigee: | 91.3096° |
| revolutions per day: | 1.00269472 |
| mean anomaly at epoch: | 171.4181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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