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 40298U 26145.63836426 +.00000000 +00000-0 +43698-3 0 00005
2 40298 97.3449 222.3593 0003063 198.5187 161.5937 15.19719816 08
| Epoch (UTC): | 25 May 2026 15:19:14 |
| Eccentricity: | 0.0003063 |
| inclination: | 97.3449° |
| perigee height: | 505 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 222.3593° |
| argument of perigee: | 198.5187° |
| revolutions per day: | 15.19719816 |
| mean anomaly at epoch: | 161.5937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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